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CAR-66

of 187 Issue II, dated 4th April 2016

CAR – 66 (Issue II)

LICENSING OF AIRCRAFT

MAINTENANCE ENGINEERS

DIRECTORATE GENERAL OF CIVIL AVIATION TECHNICALCENTRE,OPPSAFDURJUNGAIRPORT,NEWDELHI

CAR-66


SalientFeaturesoftheCAR-66

TheCAR-66

hasbeendraftedin linewiththecurrentRule61and toharmonise the aircraft

maintenancepersonnellicensingsystemwithEASAPart66(General).

details,requirementsforqualifyinganindividualtoobtainanAircraftMaintenance

Engineer’sLicenceandextensionofsuchlicence[CAR-66]

eliminatesthesystemofobtainingAirframe,Engine,Electrical,InstrumentandRa-

dioSystemLicencesseparately[66.A.03]

redefines the syllabus for basic knowledge examination in modular pattern

[66.A.25]

provides for endorsement ofan AME licence aftersuccessful completion of type

trainingandthetypetrainingexamination/typeexaminationwhichshallconsistof

boththeoreticalandpracticalexaminations[66.A.45(c)]

liststhedetailsofpracticaltaskstoqualifyanindividualtoobtainatyperating[Ap-

pendixIItoAMC]

provides for acquiring group type rating of aircraft and certification privileges

66.A.45(a)

hasaprovisiontoconverttheexistingAMElicencetoCAR66licence[66.A.70]with

orwithoutlimitation.

CAR-66


GENERAL

InordertoharmonizeIndianrequirementsfor licensingofaircraftmaintenanceengi-

neerswith internationalrequirements;CAR-66Rev.0dated11thNovember2011,was

introduced.

ThisCAR is issued on the basis ofamended Rule 61(6th amendment)of the AircraftRules,1937asnotifiedvideGSR1001(E)dated22ndDecember2010.ThisCARiseffectivefrom01.01.2012.HowevertheexistingrequirementsofCARSection-2SeriesLwillalsocontinuetillthedatenotifiedbytheDirectorGeneralforfacilitatingsmoothtransitionofaircraftmaintenanceengineerlicensingsystemintoCAR66pattern.TheCAR-66isapplicabletoallpersonnel/Organizationsengagedinmaintenanceand/orcertificationofaircraftregisteredinIndia.TheSectionAofCAR-66establishestherequirementsfortheissueandextensionofan

aircraftmaintenanceengineer’s license,conditionsof itsvalidityanduse. Italsohasa

provisionforconvertingtheaircraftmaintenanceengineer’s(AME)licenseissuedprior

totheCAR-66comingintoforce.TherequirementsarefollowedbyAcceptablemeansof

compliance(AMC)andGuidanceMaterial(GM)

TheAMElicensesinCAR66patternwillbeavailableintwodifferentways:

a)AfterconversionofexistingAMElicenseswithapplicablelimitation.

b)IssueoffreshlicenseafterpassingofapplicablemodulesofBasicKnowledgeExamto

beconductedbyCEO.

CAR-66


Record of Revisions

Initial Issue (Revision 0) 11th November 2011 ThisCAR66providesrequirementsfortheissueofanaircraftmaintenanceengineer’slicenceandconditionsofitsvalidityanduseforaeroplanesandhelicopters.Revision 1, 23rd April 2015 TheRevision-01toCAR66wasissuedtoreviseconversionof licencesissuedpriortoCAR-66andexaminationcredits.TherevisionalsorevisestheLicenseformat.CAR 66 Issue II------------------TheCAR66IssueIIisbeingissuedtoamendthetraining,examination,knowledgeandexperiencerequirementsfortheissuanceofaircraftmaintenancelicences

SalientfeaturesoftheCAR66IssueIIare:1.Thetraining,examination,knowledgeandexperiencerequirementsfortheissuanceof

aircraftmaintenancelicencesandtoadapttheserequirementstothecomplexityof

thedifferentcategoriesofaircraftamended

2.TheAMCsandGMsrelatedtoapointhavebeenbroughttogetherforeasyreferencepurposes.

3.Provisionforaircraftgroupingadded(66.A.5)4. Requirements for completing all the module for basic knowledge within 10 year

(66.A.25(b)added

5.Headingof(66.A.45)ischangedfromtype/tasktrainingtoEndorsementwithair-craftrating.RelatedAMCandGMamended.

6.Point66.A.50andrelatedAMCaddedtomakeaprovisionforintroducingorremoval

oflimitationfromthelicense7.ExistingAMCsandGMsaresuitableamended.8. Appendix -1- Basic knowledge requirements amended to revise the syllabus for

knowledgeexamination9.Appendix-2-Basicexaminationstandardhavebeenrevised

10. Appendix-3-Type examinationstandardhavebeenamended, minimumstandardanddurationfortypetraining,coursecurriculumhavebeenintroduced,practicalelementsrequirementstobecoveredduringtypetrainingadded,typetrainingexam-inationsand assessmentstandardhavebeenrevised,relevantAMC andGMhavebeenalsoamended/added

CAR-66


11.Appendix-IIItoAMCofCAR66forcompetencyassessmentofassessorsadded.12.ProceduresforCAR-66(Section–B)isremovedfromthisCARandshallbepartof

AirworthinessProceduresManual(Chapter-17)

CAR-66


CONTENTS

Paragraph Description PageNo

General 3

RecordofRevisions 4

SECTION A TECHNICAL REQUIREMENTS

SUBPART A AIRCRAFT MAINTENANCE ENGINEER’S LICENCE AEROPLANES AND HEL-

COPTERS

66.A.01

66.A.03

66.A.5

Scope

LicenceCategories

AircraftGroups

9

9

9

66.A.10 Application 10

66.A.15 Eligibility 10

66.A.20 Privileges 10

66.A.25 Basicknowledgerequirements 11

66.A.30 BasicExperienceRequirements 12

66.A.33

66.A.35

TypeTrainingandexamination

SkillTestRequirement

13

13

66.A.40 Continuedvalidityoftheaircraftmaintenanceengineer’slicence

13

66.A.45

66.A.50

EndorsementwithAircraftratings

Limitations

14

15

66.A.55 Evidenceofqualification 15

66.A.70 Conversionprovisions 16

Appendices

AppendixI BasicKnowledgeRequirements18

AppendixII BasicExaminationandStandard66

CAR-66


AppendixIII AircraftTypetrainingandExaminationStandard-70

Onthejobtraining

AppendixIV ExperiencerequirementsforextendingaCAR-66Aircraft90MaintenanceEngineer’sLicence

AppendixVApplicationsandFormats91

AppendixVI AircraftMaintenanceEngineer’sLicencereferredtoin

Rule61oftheAircraftRules,1937(CAR-66)-CAForm26125

Acceptable Means of Compliance (AMC) and Guidance Material

to SECTION A of – CAR 66

GM66.A.3 Licencecategories 129

AMC66.A.10Application 129

AMC.A.15(a)Eligibility129

GM66.A.20(a) Privileges 130

AMC66.A.20(b)2 Privilege 132

GM66.A.20(b)2 Privileges 134

AMC66.A.20(b)3

GM66.A.20(b)4

GM66.A.25(a)

Privileges134

Privileges136

Basicknowledgerequirements 136

AMC66.A.30(a) Experiencerequirements136

AMC66.A.30(d) Experiencerequirements137

AMC66.A.30(e)Experiencerequirements137

GM66.A.35SkillTestRequirement137

GM66.A.40ContinuedValidityofAMELicence138

GM66.A.45(b) Endorsementwithaircraftratings 138

AMC66.A.45(e)

AMC66.A.45(d),

(e)3,(f)1and(g)1

GM66.A.45

Endorsementwithaircraftratings138



CAR-66


AMC66.A.50(b)

GM66.A.70

GM66.A.70(c)

Limitations141

ConversionProvisions142

Conversionprovisions 143

GM66.A.70(d)AMCtoSection1ofAppendixIIItoCAR-66AMCtoParagraph3.1(d)ofAppendixIIItoCAR-66AMCtoParagraphs1(b)3.2and4.2ofAppendixIIItoCAR-66AMCtoParagraph1(c)ofAppendixIIItoCAR-66AMCtoSection5ofAppendixIIItoCAR-66AMCtoSection6ofAppendixIIItoCAR-66AMCtoAppendixIIItoCAR-66AppendixItoAMCofCAR66AppendixIItoAMCofCAR66

Conversionprovisions 143

AircraftTypeTrainingandExaminationStandard144On- the- JobTraining

“AircraftTypeTrainingandExaminationStandard146On-the-JobTraining“AircraftTypeTrainingandExaminationStandard150On- the- JobTraining“AircraftTypeTrainingandExaminationStandard150On-the-JobTraining“AircraftTypeTrainingandExaminationStandard151On-the-JobTraining“AircraftTypeTrainingandExaminationstandard151On-the-JobTraining

AircraftTypeTrainingandExaminationStandard153On-the-JobTrainingAircrafttyperatings154

Aircrafttypepracticalexperienceand On-the-Job 170

Traininglistoftask

AppendixIIItoAMCofCAR66

Evaluationofthecompetence:assessmentand177assessors

AppendixIVtoAMC FuelTankSafetytraining181

ApplicationsForm184

HighlightsofCAR66IssueII185

CAR-66


SECTION A

Technical Requirements

SUBPART A

AIRCRAFT MAINTENANCE ENGINEER’S LICENCE AEROPLANES AND HELICOPTERS

66. A.01 Scope

Thissectiondefinestheaircraftmaintenanceengineer’slicenceandestablishesthere-

quirementsforapplication,issueandconditionsofitsvalidity

66.A.3 Licence categories

(a)Aircraftmaintenancelicencesincludethefollowingcategories:

-CategoryA

-CategoryB1

-CategoryB2

-CategoryC

(b) CategoriesAandB1aresubdividedintosubcategoriesrelativetocombinationsof

aeroplanes,helicopters,turbineandpistonengines.Thesubcategoriesare:

-A1andB1.1AeroplanesTurbine

-A2andB1.2AeroplanesPiston

-A3andB1.3HelicoptersTurbine

-A4andB1.4HelicoptersPiston

(c)RESERVED

66.A.05 Aircraft groups

Forthepurposeofratingsonaircraftmaintenanceengineerslicences,aircraftshallbe

classifiedinthefollowinggroups:

1.Group1:complexmotor-poweredaircraftaswellasmultipleenginehelicopters,aer-

oplanes with maximum certified operating altitude exceeding FL290, aircraft

equippedwithfly-by-wiresystemsandotheraircraftrequiringanaircrafttyperating

whendefinedsobytheDGCA

CAR-66


2.Group2:aircraftotherthanthoseinGroup1belongingtothefollowingsubgroups:

—sub-group2a:singleturbo-propellerengineaeroplanes

—sub-group2b:singleturbineenginehelicopters

—sub-group2c:singlepistonenginehelicopters.

3.Group3:pistonengineaeroplanesotherthanthoseinGroup1.

66. A.10. Application

a)Anapplication foran aircraft maintenanceengineer’s licence orchange to such li-

cenceshallbemadeonCAForm19-01/02(ReferAppendix-V)withnecessarydoc-

umentsandfeestoDGCA.

b)Reserved.

c) Inadditiontothedocumentsrequiredinpoints66.A.10(a)asappropriate,theappli-

cantforadditionalcategoriesorsub-categoriestoanaircraftmaintenanceengineer’s

licenceshallsubmithis/hercurrentoriginalaircraftmaintenanceengineer’slicence

totheDGCAtogetherwithCAForm19-02.

d)Reserved

e)Reserved

(f)Eachapplicationshallbesupportedbydocumentationtodemonstratecompliance

withtheapplicabletheoreticalknowledge,practicaltraining,experienceandskilltest

requirementsatthetimeofapplication.

66. A.15.Eligibility

a) The applicant must have passed 10+2 examination in Physics, Chemistry andMathematicsfromarecognizedboardoruniversityoritsequivalent

b)Anapplicantforanaircraftmaintenanceengineer’slicenceshallbeatleast18years

ofage.

66. A.20 Privileges

a)Subjecttothecompliancewithparagraph(b),thefollowingprivilegesshallapply:

1. AcategoryA aircraftmaintenanceengineer’slicencepermitstheholdertoissuecertificatesofreleasetoservicefollowingminorscheduledlinemaintenanceandsimpledefectrectificationwithinthelimitsof tasksspecificallyendorsedontheauthorizationissuedbyanorganizationapprovedunderrule133Bforthetypeofaircraftendorsedonthelicence.Thecertificationprivilegesshallberestrictedtoworkthatthelicenceholderhaspersonallyperformedinamaintenanceorganiza-tionapprovedbytheDGCA.

CAR-66


2. AcategoryB1 aircraftmaintenanceengineer’slicenceshallpermittheholderto

issue certificates of release to service following maintenance including aircraft

structure,powerplantandmechanicalandelectricalsystemsinrespectofanair-

crafttypeendorsedonlicense.Replacementofavioniclinereplaceableunits,re-

quiringsimpleteststoprovetheirserviceabilityshallalsobeincludedinthepriv-

ileges.CategoryB1shallautomaticallyincludetheappropriateAsubcate-

gory.

3. A category B2 aircraft maintenance engineer’s licence shall permit the holder

toissuecertificatesofreleasetoservicefollowingmaintenanceonavionicand

electricalsystemsofanaircrafttypeendorsedonthelicence.

4.RESERVED

5.Acategory Caircraftmaintenanceengineer’slicenceshallpermittheholdertoissue

certificatesofreleasetoservicefollowingbasemaintenanceonaircrafttypeen-

dorsedonthelicence.TheprivilegesapplytotheaircraftinitsentiretyinCAR145

organization.

b)TheholderofAircraftMaintenanceEngineerlicensemaynotexercisecertification

privilegesunless:

1.in compliance with the applicable requirements of CAR M and/or CAR 145;and

2.intheprecedingtwoyearperiodhe/shehaseitheracquiredsixmonthsofmainte-

nanceexperienceinaccordancewiththeprivilegesgrantedbytheAircraftMainte-

nanceEngineer’sLicenceormettheprovisionfortheissueofappropriateprivi-

leges;and

3.he/shehastheadequatecompetencetocertifymaintenanceonthecorresponding

aircraft;and

4.he/sheisabletoread,writeandcommunicatetoanunderstandablelevelinthe

language(s) in which the technical documentation and procedures necessary to

supporttheissueofthecertificateofreleasetoservicearewritten.

66. A.25 Basic Knowledge requirements:

a)Anapplicantforanaircraftmaintenanceengineer’slicenceortheadditionofacate-

goryorsubcategorytosuchanaircraftmaintenanceengineer’slicenceshalldemon-

stratebyexamination,alevelofknowledgeintheappropriatesubjectmodulesinac-

cordancewithAppendixItothisCAR.Thebasicknowledgeexaminationshallbecon-

ductedbyCentralExaminationOrganizationofDGCA.

b)Thetrainingcoursesandexaminationsshallbepassedwithin10yearspriortothe

applicationforanaircraftmaintenancelicenceortheadditionofacategoryorsub-

categorytosuchaircraftmaintenancelicence.Shouldthisnotbethecase,examina-

tioncreditsmayhoweverbeobtainedinaccordancewithpoint(c).

CAR-66


(c)TheapplicantmayapplytotheDGCAforfullorpartialexaminationcredittothe

basicknowledgerequirementsfor

1.basicknowledgeexaminationsthatdonotmeettherequirementdescribedinpoint

(b)above;and

2.anyothertechnicalqualificationconsideredbytheDGCAtobeequivalenttothe

knowledgestandardofCAR-66

CreditsshallbegrantedinaccordancewithAPMChapter17.

d)Creditsexpire10yearsaftertheyweregrantedtotheapplicantbytheDGCA.The

applicantmayapplyfornewcreditsafterexpiration.

66. A.30 Basic Experience requirements:

a)Anapplicantforanaircraftmaintenanceengineer’slicenceshallhaveacquired:

1. for category A and sub categories B1.2 and B1.4 four years of practical aircraft

maintenanceexperience.

2. forcategoryB2andsub-categoriesB1.1andB1.3 fiveyearsofpractical aircraft

maintenanceexperience.

3.forCategoryCwithrespecttolargeaircraft:

i. threeyearsofexperienceexercisingcategoryB1.1orB1.3orB2privilegeson

largeaircraftorasCAR145B1.1,B1.3orB2supportstaff,or,acombinationof

both;or

ii.fiveyearsofexperienceexercisingcategoryB1.2orB1.4privilegesonlargeair-

craftorasCAR145B1.2orB1.4supportstaff,oracombinationofboth;or

4. forcategoryCwithrespecttononlargeaircraft:

Three years of experience exercising category B1 or B2 privileges on non large aircraft

or as CAR 145 B1 or B2 support staff, or a combination of both.

b)Anapplicantforanextensiontoanaircraftmaintenanceengineer’slicenceshallhave

aminimumcivilaircraftmaintenanceexperiencerequirementappropriatetothead-

ditionalcategoryorsub-categoryoflicenceappliedforasdefinedinAppendixIVto

thisCAR.

c) Theexperienceshallbepracticalandinvolvewitharepresentativecrosssectionof

maintenancetasksonaircraft.

d)Atleastoneyearoftherequiredexperienceshallberecentmaintenanceexperience

onaircraftofthecategory/subcategoryforwhichtheinitialaircraftmaintenanceen-

gineer’slicenceissought.Forsubsequentcategory/subcategoryadditionstoanex-

istingaircraftmaintenanceengineer’slicence,theadditionalrecentmaintenanceex-

periencerequiredmaybelessthanoneyear,butshallbeatleastthreemonths.The

CAR-66


requiredexperienceshallbedependentuponthedifferencebetweenthelicencecat-

egory/subcategoryheldandappliedfor.Suchadditionalexperiencemustbetypical

ofthenewlicencecategory/subcategorysought.

e)Twelveyearsofpracticalaircraftmaintenanceexperience,gainedoutsideacivilair-

craftmaintenanceenvironmentshallbeacceptedasequivalenttotherequirements

laid down in (1) and (2) of Paragraph (a) above, in the relevant category supple-

mentedbyatleastoneyearofrecentexperienceinthecivilaircraftmaintenanceen-

vironment;

(f)Experienceshallhavebeenacquiredwithinthe10yearsprecedingtheapplication

foranaircraftmaintenance licenceortheadditionofacategoryorsubcategoryto

suchalicence.

66.A. 33 Type Training and Examination Requirement

AnapplicantforgrantorextensionofAircraftMaintenanceEngineer’slicencewith

type rating shall meet the aircraft type training and examination requirement as

specifiedinCARA.45

.6.A. 35 Skill Test Requirement

AnapplicantforgrantorextensionofAircraftMaintenanceEngineer’slicenceshall

demonstratehisaircraftmaintenanceskillinrespectofeachcategoryorsub-category

oflicenseorspecifictypeofaircrafttotheDirectorGeneral

.66. A.40 Continued validity of the aircraft maintenance engineer’s licence

(a) Theaircraftmaintenanceengineer’slicencebecomesinvalidafterfiveyearsofits

lastissueorrenewal,unlesstheholdersubmitshis/heraircraftmaintenanceen-

gineer’s licencetotheDGCA,inordertoverifytheinformationcontainedinthe

licenceisthesameasthatcontainedintheDGCArecords,pursuanttopoint66.B.

120.

(b) The holder of an aircraft maintenance engineer’s licence shall complete the CA

Form19-03(ReferAppendix-V)andsubmititwiththe holder’scopyofthelicence

totheDGCA,unlesstheholderworksinamaintenanceorganizationapprovedin

accordancewithCAR145thathasaprocedureinitsexpositionwherebysuchor-

ganisation may submit the necessary documentation on behalf of the aircraft

maintenanceengineer’slicenceholder.

(c) Anycertificationprivilegesbaseduponanaircraftmaintenanceengineer’slicence

becomesinvalidassoonastheaircraftmaintenanceengineer’slicenceisinvalid.

(d) The aircraft maintenance engineer’s licence is only valid when issued and/or

changedbyDGCAandwhentheholderhassignedthedocument.

CAR-66


66. A.45 Endorsement with aircraft ratings

a)Inordertobeentitledtoexercisecertificationprivilegesonaspecificaircrafttype,theholderofanaircraftmaintenanceengineerlicenceneedtohavehis/herlicenceendorsedwiththerelevantaircraftratings.

—ForcategoryA,B1,B2orCtherelevantaircraftratingsarethefollowing:

1.Forgroup1aircraft,theappropriateaircrafttyperating.2.Forgroup2aircraft,theappropriateaircrafttyperating,manufacturersub-group

ratingorfullsubgrouprating.3.Forgroup3aircraft,theappropriateaircrafttyperatingorfullgrouprating.

—Reserved

b)TheendorsementofaircrafttyperatingsrequiresthesatisfactorycompletionoftherelevantcategoryA,B1,B2orCaircrafttypetraining.

(c)Inadditiontotherequirementofpoint(b),theendorsementofthefirstaircrafttype

ratingwithinagivencategory/sub-categoryrequiressatisfactorycompletionofthecorrespondingOntheJobTraining,asdescribedinAppendixIIItoCAR-66

(d)Byderogationfrompoints(b)and(c),forgroup2and3aircraft,aircrafttyperat-

ingsmayalsobegrantedafter:

—satisfactorycompletionoftherelevantcategoryA,B1,B2orCaircrafttypeexam-inationdescribedinAppendixIIItothisAnnex(CAR-66),and

—inthecaseofA,B1andB2category,demonstrationofpracticalexperienceonthe

aircrafttype.Inthatcase,thepracticalexperienceshallincludearepresentativecrosssectionofmaintenanceactivitiesrelevanttothelicencecategory.

(e)Forgroup2aircraft:

1.theendorsementofmanufacturersub-groupratingsforcategoryB1andClicenceholdersrequirescomplyingwiththeaircrafttyperatingrequirementsofatleasttwoaircrafttypesfromthesamemanufacturerwhichcombinedarerepresentativeoftheapplicablemanufacturersub-group;

2. theendorsementof fullsub-groupratingsforcategoryB1andC licenceholders

requirescomplyingwiththeaircrafttyperatingrequirementsofatleastthreeair-crafttypesfromdifferentmanufacturerswhichcombinedarerepresentativeoftheapplicablesub-group;

3.theendorsementofmanufacturersub-groupsandfullsub-groupratingsforcate-

goryB2licenceholdersrequiresdemonstrationofpracticalexperiencewhichshall

CAR-66


includearepresentativecrosssectionofmaintenanceactivitiesrelevanttotheli-cencecategoryandtotheapplicableaircraftsub-group.

(f)Forgroup3aircraft:

1.theendorsementofthefullgroup3ratingforcategoryA,B1,B2andClicencehold-ersrequiresdemonstrationofpracticalexperience,whichshall includearepre-sentativecrosssectionofmaintenanceactivitiesrelevanttothelicencecategoryandtothegroup3.

2.forcategoryB1,unlesstheapplicantprovidesevidenceofappropriateexperience,

thegroup3ratingshallbesubjecttothefollowinglimitations,whichshallbeen-dorsedonthelicence:

—pressurisedaeroplanes—metalstructureaeroplanes

—compositestructureaeroplanes—woodenstructureaeroplanes—aeroplaneswithmetaltubingstructurecoveredwithfabric.

(g)Reserved66.A.50 Limitations (a)Limitationsintroducedonanaircraftmaintenancelicenceareexclusionsfromthe

certificationprivilegesandaffecttheaircraftinitsentirety.(b)Forlimitationsreferredtoinpoint66.A.45,limitationsshallberemovedupon:

1.demonstrationofappropriateexperience;or2.afterasatisfactorypracticalassessmentperformedbytheDGCA.

c)Forlimitationsreferredtoinpoint66.A.70,limitationsshallberemoveduponsatis-factorycompletionofexaminationonthosemodules/subjectsdefinedintheapplica-bleconversionreportreferredtoinAPMChapter17

66. A.55 Evidence of qualification

Personnel exercising certification privileges as well as support staff must produce

theirlicenceasevidenceofqualification,ifrequiredbyanauthorizedpersonofDGCA,

within24hours.

CAR-66


66. A.70 Conversion provisions-

a)TheholderofavalidAircraftMaintenanceEngineer’sLicenceonthedateofcoming

intoforceofthisCARmaycontinuetoexercisetheprivilegesofhislicenceandshall

be issued, with or without limitation andwithout furtherexamination, an Aircraft

MaintenanceEngineer’sLicence in theappropriatecategorysubject tosuchcondi-

tionsspecifiedin AirworthinessProceduresManualChapter17

b)A person undergoing a qualification process, prior to the GSR No. 1001(E) dated

22.12.2010regardingtheRule61oftheAircraftRules,1937shallcontinuetobequal-

ifiedtilldateasspecifiedbytheDirectorGeneral.Theholderofaqualificationgained

followingsuchqualificationprocessmaybeissuedanaircraftmaintenanceengineer’s

licence subject to the conditions specified in . Airworthiness Procedures Manual

Chapter17

c)Wherenecessary,theaircraftmaintenanceengineer’slicenceshallcontainlimitations inaccordancewithpoint66.A.50toreflectthedifferencesbetween(i)thescopeofthecertifyingstaffqualification(ii)thebasicknowledgerequirementsand thebasicexaminationstandardslaiddowninAppendixIandIItothisCAR66.

d)AircraftMaintenanceEngineer’sLicencesissuedpriortothisCARcomingintoforce

incategory“A”tocoverGliders,Balloonsand incategory“B”, “D”and“X” tocover

Aircraft,Engine,propelleranditemsofequipmenttocarryoutmaintenanceandissue

‘CertificateofReleasetoService’thatcouldnotbetransferredtoCAR-66licence‘Type

Rating’shallbetransferredtotheCAR-66licencesectionXIV(a)withoutalteringthe

privilegeshithertoexercisedbytheholder.

Sd-

(MSathiyavathy)

DirectorGeneralofCivilAviation

CAR-66


SUBPART B

AIRCRAFT OTHER THAN AEROPLANES AND HELICOPTERS

66. A.100 General

UntilsuchtimeasthisCARspecifiesarequirementforcertifyingstaffofaircraftother

thanaeroplanesandhelicopters,theexistingregulationshallapply.

SUBPART C

COMPONENTS

66. A. 200 General

UntilsuchtimeasthisCARspecifiesarequirementforcertifyingcomponents,theex-

istingregulationshallapply.

CAR-66


AppendixI-BasicKnowledgeRequirements

1. KNOWLEDGE LEVELS - CATEGORY A, B1, B2 AND C AIRCRAFT MAINTENANCE

ENGINEER’s LICENCE

BasicknowledgeforcategoriesA,B1andB2areindicatedbytheknowledgelevels(1,2or3)againsteachapplicablesubject.CategoryCapplicant shall meeteithercategoryB1orB2basicknowledgelevel.Theknowledgelevelindicatorsaredefinedondefinedon3levelsasfollows:

LEVEL 1

Familiarizationwiththeprincipalelementsofthesubject.

Objectives:

(a)Theapplicantshouldbefamiliarwiththebasicelementsofthesubject.

(b)Theapplicantshouldbeabletogiveasimpledescriptionofthewholesubject,

usingcommonwordsandexamples.

(c)Theapplicantshouldbeabletousetypicalterms.

LEVEL 2

Ageneralknowledgeofthetheoreticalandpracticalaspectsofthesubjectand anabilitytoapplythatknowledge.

Objectives:

(a ) Theapplicantshouldbe able to understand theoretical fundamentals of thesubject.

(b) The applicant should be able to give a general description of the subject

usingasappropriate,typicalexamples.

(c)Theapplicantshouldbeabletousemathematicalformulaeinconjunction withphysicallawsdescribingthesubject.

(d) Theapplicantshouldbeabletoreadandunderstandsketches,drawingsand

schematicsdescribingthesubject.(e)Theapplicantshouldbeabletoapplyhisknowledgeinapracticalmanner

usingdetailedprocedures.

CAR-66


LEVEL 3

Adetailedknowledgeofthetheoreticalandpracticalaspectsofthesubjectanda capacity tocombineandapply theseparateelementsofknowledge ina logicaland

comprehensivemanner. Objectives:

(a) The applicant should know the theory of the subject and interrelation shipwithothersubjects.

(b)Theapplicantshouldbeabletogiveadetaileddescriptionofthesubjectus

ingtheoreticalfundamentalsandspecificexamples.(c)Theapplicantshouldunderstandandbeabletousemathematicalformulae

relatedtothesubject.(d)Theapplicantshouldbeabletoread,understandandpreparesketches,simpledrawingsandschematicsdescribingthesubject.(e) Theapplicantshouldbeabletoapplyhisknowledgeinapracticalmanner

usingmanufacturer'sinstructions.(f)Theapplicantshouldbeabletointerpretresultsfromvarioussourcesand

measurementsandapplycorrectiveactionwhereappropriate.

CAR-66


2. MODULARISATION

QualificationonbasicsubjectsforeachCAR66aircraftmaintenanceengineer’slicence

categoryorsubcategoryshouldbeinaccordancewiththefollowingmatrix.Applicable

subjectsareindicatedbyan‘X’:

SubjectModules

AorB1aeroplanewith AorB1helicopterwith B2

Turbineen-gine(s)

Pistonengine(s)

Turbineen-gine(s)

Pistonengine(s)

Avionics

A1 B1.1 A2 B1.2 A3 B1.3 A4 B1.4

1 NotApplicable

2 NotApplicable

3 X X X X X X X X X

4 X X X X X

5 X X X X X X X X X

6 X X X X X X X X X

7 X X X X X X X X X

8 X X X X X X X X X

9 X X X X X X X X X

10 X X X X X X X X X

11A X X

11B X X

12 X X X X

13 X

14 X

15 X X X X

16 X X X X

17 X X X X

CAR-66


MODULES & SYLLABUS LEVEL

A B1 B2

MODULE 1. Reserved - - -

MODULE 2. Reserved - - -

MODULE 3. ELECTRICAL FUNDAMENTALS LEVEL

A B1 B2

3.1 Electron Theory 1 1 1

Structure and distribution of electrical charges within: atoms, molecules,ions,compounds;

Molecularstructureofconductors,semiconductorsandinsulators.

3.2 Static Electricity and Conduction 1 2 2

Staticelectricityanddistributionofelectrostaticcharges;

Electrostaticlawsofattractionandrepulsion;

Unitsofcharge,Coulomb'sLaw;

Conductionofelectricityinsolids,liquids,gasesandavacuum.

3.3 Electrical Terminology 1 2 2

Thefollowingterms,theirunitsandfactorsaffectingthem:potentialdiffer-ence,electromotiveforce,voltage,current,resistance,conductance,charge,conventionalcurrentflow,electronflow.

3.4 Generation of Electricity 1 1 1

Productionofelectricitybythefollowingmethods:light,heat,friction,pres-sure,chemicalaction,magnetismandmotion.

3.5 DC Sources of Electricity 1 2 2 Constructionandbasicchemicalactionof:primarycells,secondarycells,leadacidcells,nickelcadmiumcells,otheralkalinecells; Cellsconnectedinseriesandparallel;Internalresistanceanditseffectonabattery;

Construction,materialsandoperationofthermocouples;

Operationofphoto-cells.

3.6 DC Circuits - 2 2

OhmsLaw,Kirchoff'sVoltageandCurrentLaws;

Calculationsusingtheabovelawstofindresistance,voltageandcurrent;

Significanceoftheinternalresistanceofasupply.

3.7 Resistance/Resistor

(a) - 2 2

Resistanceandaffectingfactors;

Specificresistance; Resistorcolour code, values and tolerances, preferred values, wattage rat-ings;

Resistorsinseriesandparallel;

CAR-66



A B1 B2

Calculationoftotalresistanceusingseries,parallelandseriesparallelcombi-nations;

Operationanduseofpotentiometersandrheostats;

OperationofWheatstoneBridge.

(b) - 1 1

Positiveandnegativetemperaturecoefficientconductance;

Fixedresistors,stability,toleranceandlimitations,methodsofconstruction;

Variableresistors,thermistors,voltagedependentresistors;

Constructionofpotentiometersandrheostats;

ConstructionofWheatstoneBridge;

3.8 Power - 2 2

Power,workandenergy(kineticandpotential);

Dissipationofpowerbyaresistor;

Powerformula;

Calculationsinvolvingpower,workandenergy.

3.9 Capacitance/Capacitor - 2 2

Operationandfunctionofacapacitor;

Factorsaffectingcapacitanceareaofplates,distancebetweenplates,numberofplates,dielectricanddielectricconstant,workingvoltage,voltagerating;

Capacitortypes,constructionandfunction;

Capacitorcolourcoding;

Calculationsofcapacitanceandvoltageinseriesandparallelcircuits;

Exponentialchargeanddischargeofacapacitor,timeconstants;

Testingofcapacitors.

3.10 Magnetism

(a) - 2 2

Theoryofmagnetism;

Propertiesofamagnet

ActionofamagnetsuspendedintheEarth'smagneticfield;

Magnetisationanddemagnetisation;

Magneticshielding;

Varioustypesofmagneticmaterial;

Electromagnetsconstructionandprinciplesofoperation; Handclasprulestodetermine:magneticfieldaroundcurrentcarryingcon-ductor.

(b) - 2 2Magnetomotiveforce,fieldstrength,magneticfluxdensity,permeability,hys-teresisloop,retentivity,coerciveforcereluctance,saturationpoint,eddycur-rents;

Precautionsforcareandstorageofmagnets.

3.11 Inductance/Inductor - 2 2

CAR-66



A B1 B2

Faraday'sLaw;

Actionofinducingavoltageinaconductormovinginamagneticfield;

Inductionprinciples;

Effects of the following on the magnitude of an induced voltage:magneticfieldstrength,rateofchangeofflux,numberofconductorturns;

Mutualinduction;

Theeffecttherateofchangeofprimarycurrentandmutualinductancehasoninducedvoltage;

Factorsaffectingmutualinductance:numberofturnsincoil,physicalsizeofcoil,permeabilityofcoil,positionofcoilswithrespecttoeachother;

Lenz'sLawandpolaritydeterminingrules;

Backemf,selfinduction;

Saturationpoint;

Principleusesofinductors;

3.12 DC Motor/Generator Theory - 2 2

Basicmotorandgeneratortheory;

ConstructionandpurposeofcomponentsinDCgenerator;

Operationof,andfactorsaffectingoutputanddirectionofcurrentflowinDCgenerators;

Operationof,andfactorsaffectingoutputpower,torque,speedanddirectionofrotationofDCmotors;

Serieswound,shuntwoundandcompoundmotors;

StarterGeneratorconstruction.

3.13 AC Theory 1 2 2

Sinusoidalwaveform:phase,period,frequency,cycle;

Instantaneous,average,rootmeansquare,peak,peaktopeakcurrentvaluesandcalculationsofthesevalues,inrelationtovoltage,currentandpower

Triangular/Squarewaves;

Single/3phaseprinciples.

3.14 Resistive (R), Capacitive (C) and Inductive (L) Circuits - 2 2

PhaserelationshipofvoltageandcurrentinL,CandRcircuits,parallel,seriesandseriesparallel;

PowerdissipationinL,CandRcircuits;

Impedance,phaseangle,powerfactorandcurrentcalculations;

Truepower,apparentpowerandreactivepowercalculations.

3.15 Transformers - 2 2

Transformerconstructionprinciplesandoperation;

Transformerlossesandmethodsforovercomingthem;

Transformeractionunderloadandno-loadconditions; Powertransfer,efficiency,polaritymarkings;

Calculationoflineandphasevoltagesandcurrents;

CAR-66



A B1 B2

Calculationofpowerinathreephasesystem;

PrimaryandSecondarycurrent,voltage,turnsratio,power,efficiency;

Autotransformers.

3.16 Filters - 1 1

Operation,applicationandusesofthefollowingfilters:lowpass,highpass,bandpass,bandstop.

3.17 AC Generators - 2 2

Rotationofloopinamagneticfieldandwaveformproduced;

OperationandconstructionofrevolvingarmatureandrevolvingfieldtypeACgenerators;

Singlephase,twophaseandthreephasealternators;

Threephasestaranddeltaconnectionsadvantagesanduses;

PermanentMagnetGenerators.

3.18 AC Motors - 2 2

Construction,principlesofoperationandcharacteristicsof:ACsynchronousandinductionmotorsbothsingleandpolyphase;

Methodsofspeedcontrolanddirectionofrotation; Methods of producing a rotating field: capacitor, inductor, shaded or splitpole.

MODULE 4. ELECTRONIC FUNDAMENTALS LEVEL

A B1 B2

4.1 Semiconductors

4.1.1 Diodes

(a) - 2 2

Diode symbols;

Diode characteristics and properties;

Diodes in series and parallel;

Main characteristics and use of silicon controlled rectifiers (thyristors), light emitting diode, photo conductive diode, varistor, rectifier diodes;

Functional testing of diodes.

(b) - - 2

Materials, electron configuration, electrical properties;

P and N type materials: effects of impurities on conduction, majority and mi-nority characters;

PN junction in a semiconductor, development of a potential across a PN junc-tion in unbiased, forward biased and reverse biased conditions;

Operation and function of diodes in the following circuits: clippers, clampers, full and half wave rectifiers, bridge rectifiers, voltage doublers and triplers;

Detailed operation and characteristics of the following devices: silicon con-trolled rectifier (thyristor), light emitting diode, Shottky diode, photo conduc-tive diode, varactor diode, varistor, rectifier diodes, Zener diode.

CAR-66



A B1 B2

4.1.2 Transistors

(a) - 1 2

Transistor symbols;

Component description and orientation;

Transistor characteristics and properties.

(b) - - 2

Construction and operation of PNP and NPN transistors;

Base, collector and emitter configurations;

Testing of transistors.

Basic appreciation of other transistor types and their uses.

Application of transistors: classes of amplifier (A, B, C);

Simple circuits including: bias, decoupling, feedback and stabilisation;

Multistage circuit principles: cascades, push-pull, oscillators, multivibrators, flip-flop circuits.

4.1.3 Integrated Circuits

(a) - 1 -

Description and operation of logic circuits and linear circuits/operational am-plifiers.

(b) - - 2

Description and operation of logic circuits and linear circuits;

Introduction to operation and function of an operational amplifier used as: in-tegrator, differentiator, voltage follower, comparator;

Operation and amplifier stages connecting methods: resistive capacitive, induc-tive (transformer), inductive resistive (IR), direct;

Advantages and disadvantages of positive and negative feedback.

4.2 Printed Circuit Boards - 1 2

Description and use of printed circuit boards.

4.3 Servomechanisms

(a) - 1 -

Understanding of the following terms: Open and closed loop systems, feedback, follow up, analogue transducers;

Principles of operation and use of the following synchro system compo-nents/features: resolvers, differential, control and torque, transformers, in-ductance and capacitance transmitters. (b)

-

-

2

Understanding of the following terms: Open and closed loop, follow up, servo-mechanism, analogue, transducer, null, damping, feedback, deadband;

CAR-66



A B1 B2

Construction operation and use of the following synchro system components: resolvers, differential, control and torque, E and I transformers, inductance transmitters, capacitance transmitters, synchronous transmitters;

Servomechanism defects, reversal of synchro leads, hunting.

MODULE 5. DIGITAL TECHNIQUES ELECTRONIC INSTRUMENT SYSTEMS

LEVEL

A B1.1 B1.3

B1.2 B1.4 B2

5.1 Electronic Instrument Systems 1 2 2 3

Typicalsystemsarrangementsandcockpitlayoutofelectronicinstru-mentsystems.

5.2 Numbering Systems - 1 - 2

Numberingsystems:binary,octalandhexadecimal;

Demonstrationofconversionsbetweenthedecimalandbinary,octalandhexadecimalsystemsandviceversa.

5.3 Data Conversion - 1 - 2

AnalogueData,DigitalData; Operation and application of analogue to digital, and digital to ana-logueconverters,inputsandoutputs,limitationsofvarioustypes.

5.4 Data Buses - 2 - 2

Operation of data buses in aircraft systems, including knowledge ofARINCandotherspecifications.

5.5 Logic Circuits

(a) - 2 - 2

Identificationofcommonlogicgatesymbols,tablesandequivalentcir-cuits;

Applicationsusedforaircraftsystems,schematicdiagrams.

(b)Interpretationoflogicdiagrams. - - - 2

5.6 Basic Computer Structure

(a) 1 2 - - Computerterminology(includingbit,byte,software,hardware,CPU,IC,andvariousmemorydevicessuchasRAM,ROM,PROM);

Computertechnology(asappliedinaircraftsystems).

(b) - - - 2

Computerrelatedterminology;

Operation, layoutand interfaceof themajorcomponents in amicrocomputerincludingtheirassociatedbussystems; Informationcontainedinsingleandmultiaddressinstructionwords;

Memoryassociatedterms;

Operationoftypicalmemorydevices;

CAR-66



LEVEL

A B1.1 B1.3

B1.2 B1.4 B2

Operation,advantagesanddisadvantagesofthevariousdatastoragesystems.

5.7 Microprocessors - - - 2 Functionsperformedandoveralloperationofamicroprocessor; Basicoperationofeachofthefollowingmicroprocessorelements:controlandprocessingunit,clock,register,arithmeticlogicunit.

5.8 Integrated Circuits - - - 2

Operationanduseofencodersanddecoders

Functionofencodertypes

Usesofmedium,largeandverylargescaleintegration.

5.9 Multiplexing - - - 2

Operation, application and identification in logic diagrams of multi-plexersanddemultiplexers.

5.10 Fibre Optics - 1 1 2

Advantagesand disadvantages of fibreoptic data transmission overelectricalwirepropagation;

Fibreopticdatabus;

Fibreopticrelatedterms;

Terminations;

Couplers,controlterminals,remoteterminals;

Applicationoffibreopticsinaircraftsystems.

5.11 Electronic Displays - 2 1 2

Principlesofoperationofcommontypesofdisplaysusedinmodernaircraft,including

CathodeRayTubes,LightEmittingDiodesandLiquid

CrystalDisplay.

5.12 Electrostatic Sensitive Devices 1 2 2 2 Specialhandlingofcomponentssensitivetoelectrostaticdischarges; Awarenessof risks and possible damage, component and personnelanti-staticprotectiondevices.

5.13 Software Management Control - 2 1 2 Awarenessofrestrictions,airworthinessrequirementsandpossiblecatastrophiceffectsofunapprovedchangestosoftwareprogrammes.

5.14 Electromagnetic Environment - 2 2 2

CAR-66



LEVEL

A B1.1 B1.3

B1.2 B1.4 B2

Influence of the following phenomena on maintenance practices forelectronicsystem:

EMC-ElectromagneticCompatibility

EMI-ElectromagneticInterference

HIRF-HighIntensityRadiatedField

Lightning/lightningprotection

5.15 Typical Electronic/Digital Aircraft Systems - 2 2 2 Generalarrangementoftypicalelectronic/digitalaircraftsystemsandassociatedBITE

(BuiltInTestEquipment)testingsuchas:

ACARS-ARINCCommunicationandAddressingand

ReportingSystem

ECAM-ElectronicCentralisedAircraftMonitoring

EFIS-ElectronicFlightInstrumentSystem

EICAS-EngineIndicationandCrewAlertingSystem

FBW-FlybyWire

FMS-FlightManagementSystem GPS-GlobalPositioningSystemIRS-InertialreferencesystemTCAS-TrafficCollissionAvoidancesystemIntegratedmodularAvionicaCabinSystemInformationsystem

MODULE 6. MATERIALS AND HARDWARE LEVEL

A B1 B2

6.1 Aircraft Materials — Ferrous

(a) 1 2 1

Characteristics, properties and identificationof commonalloy steels used inaircraft;

Heattreatmentandapplicationofalloysteels;

(b) - 1 1

Testingofferrousmaterialsforhardness,tensilestrength,fatiguestrengthandimpactresistance.

6.2 Aircraft Materials — Non-Ferrous

(a) 1 2 1

Characteristics,propertiesandidentificationofcommonnon-ferrousmaterialsusedinaircraft;

Heattreatmentandapplicationofnon-ferrousmaterials;

(b) - 1 1

Testingofnon-ferrousmaterialforhardness,tensilestrength,fatiguestrengthandimpactresistance.

6.3 Aircraft Materials - Composite and Non- Metallic

CAR-66



A B1 B2

6.3.1 Composite and non-metallic other than wood and fabric

(a)Characteristics,propertiesandidentificationofcommoncompositeandnon-metallicmaterials,otherthanwood,usedinaircraft;

1 2 2

Sealantandbondingagents.

(b) 1 2 -

Thedetectionofdefects/deteriorationincompositeandnon-metallicmaterial.

Repairofcompositeandnon-metallicmaterial.

6.3.2 Wooden structures 1 2 -

Constructionmethodsofwoodenairframestructures;

Characteristics,propertiesandtypesofwoodandglueusedinaeroplanes;

Preservationandmaintenanceofwoodenstructure;

Typesofdefectsinwoodmaterialandwoodenstructures;

Thedetectionofdefectsinwoodenstructure;

Repairofwoodenstructure.

6.3.3 Fabric covering 1 2 -

Characteristics,propertiesandtypesoffabricsusedinaeroplanes;

Inspectionsmethodsforfabric;

Typesofdefectsinfabric;

Repairoffabriccovering.

6.4 Corrosion

(a) 1 1 1

Chemicalfundamentals;

Formationby,galvanicactionprocess,microbiological,stress;

(b) 2 3 2

Typesofcorrosionandtheiridentification;

Causesofcorrosion;

Materialtypes,susceptibilitytocorrosion.

6.5 Fasteners

6.5.1 Screw threads 2 2 2

Screwnomenclature;

Threadforms,dimensionsandtolerancesforstandardthreadsusedinaircraft;

Measuringscrewthreads;

6.5.2 Bolts, studs and screws 2 2 2

CAR-66



A B1 B2

Bolttypes:specification, identificationandmarkingofaircraftbolts, interna-tionalstandards;

Nuts:selflocking,anchor,standardtypes;

Machinescrews:aircraftspecifications;

Studs:typesanduses,insertionandremoval;

Selftappingscrews,dowels.

6.5.3 Locking devices 2 2 2

Tabandspringwashers,lockingplates,splitpins,palnuts,wirelocking,quickreleasefasteners,keys,circlips,cotterpins.

6.5.4 Aircraft rivets 1 2 1

Typesofsolidandblindrivets:specificationsandidentification,heattreatment.

6.6 Pipes and Unions

(a) 2 2 2

Identificationof,andtypesofrigidandflexiblepipesandtheirconnectorsusedinaircraft;

(b) 2 2 1

Standardunionsforaircrafthydraulic,fuel,oil,pneumaticandairsystempipes.

6.7 Springs - 2 1

Typesofsprings,materials,characteristicsandapplications.

6.8 Bearings 1 2 2

Purposeofbearings,loads,material,construction;

Typesofbearingsandtheirapplication.

6.9 Transmissions 1 2 2

Geartypesandtheirapplication;

Gear ratios, reduction and multiplication gear systems, driven and drivinggears,idlergears,meshpatterns;

Beltsandpulleys,chainsandsprockets.

6.10 Control Cables 1 2 1

Typesofcables;

Endfittings,turnbucklesandcompensationdevices;

Pulleysandcablesystemcomponents;

Bowdencables;

Aircraftflexiblecontrolsystems.

6.11 Electrical Cables and Connectors 1 2 2

Cabletypes,constructionandcharacteristics;

Hightensionandco-axialcables;

Crimping;

CAR-66



A B1 B2

Connector types, pins, plugs, sockets, insulators, current and voltage rating,coupling,identificationcodes.

MODULE 7. MAINTENANCE PRACTICES LEVEL

A B1 B2

7.1 Safety Precautions-Aircraft and Workshop 3 3 3

Aspectsofsafeworkingpracticesincludingprecautionstotakewhenworkingwithelectricity,gasesespeciallyoxygen,oilsandchemicals.

Also,instructionintheremedialactiontobetakenintheeventofafireoran-otheraccidentwithoneormoreofthesehazardsincludingknowledgeonex-tinguishingagents.

7.2 Workshop Practices 3 3 3

Careoftools,controloftools,useofworkshopmaterials;

Dimensions,allowancesandtolerances,standardsofworkmanship;

Calibrationoftoolsandequipment,calibrationstandards.

7.3 Tools 3 3 3

Commonhandtooltypes;

Commonpowertooltypes;

Operationanduseofprecisionmeasuringtools;

Lubricationequipmentandmethods.

Operation,functionanduseofelectricalgeneraltestequipment;

7.4 Avionic General Test Equipment - 2 3

Operation,functionanduseofavionicgeneraltestequipment.

7.5 Engineering Drawings, Diagrams and Standards 1 2 2

Drawingtypesanddiagrams,theirsymbols,dimensions,tolerancesandpro-jections;

Identifyingtitleblockinformation

Microfilm,microficheandcomputerisedpresentations;

Specification100oftheAirTransportAssociation(ATA)ofAmerica;

Aeronauticalandotherapplicablestandardsincluding

ISO,AN,MS,NASandMIL;

Wiringdiagramsandschematicdiagrams.

7.6 Fits and Clearances 1 2 1

Drillsizesforboltholes,classesoffits;

Commonsystemoffitsandclearances;

Scheduleoffitsandclearancesforaircraftandengines;

Limitsforbow,twistandwear;

CAR-66



A B1 B2

Standardmethodsforcheckingshafts,bearingsandotherparts.

7.7 Electrical Wiring Interconnection System (EWIS) 1 3 3

Continuity,insulationandbondingtechniquesandtesting;

Useofcrimptools:handandhydraulicoperated;

Testingofcrimpjoints;

Connectorpinremovalandinsertion;

Co-axialcables:testingandinstallationprecautions;

Identificationofwiretypes,theirinspectioncriteriaand

damagetolerance.

Wiringprotectiontechniques:Cableloomingandloom

support,cableclamps,protectivesleevingtechniques

includingheatshrinkwrapping,shielding.

EWISinstallations,inspection,repair,maintenanceand

cleanlinessstandards.

7.8 Riveting 1 2 -

Rivetedjoints,rivetspacingandpitch;

Toolsusedforrivetinganddimpling;

Inspectionofrivetedjoints.

7.9 Pipes and Hoses 1 2 -

Bendingandbelling/flaringaircraftpipes;

Inspectionandtestingofaircraftpipesandhoses;

Installationandclampingofpipes.

7.10 Springs 1 2 -

Inspectionandtestingofsprings.

7.11 Bearings 1 2 -

Testing,cleaningandinspectionofbearings;

Lubricationrequirementsofbearings;

Defectsinbearingsandtheircauses.

7.12 Transmissions 1 2 -

Inspectionofgears,backlash;

Inspectionofbeltsandpulleys,chainsandsprockets;

Inspectionofscrewjacks,leverdevices,push-pullrodsystems.

7.13 Control Cables 1 2 -

Swagingofendfittings;

Inspectionandtestingofcontrolcables;

Bowdencables;aircraftflexiblecontrolsystems.

7.14 Material handling

7.14.1 Sheet Metal - 2 -

Markingoutandcalculationofbendallowance;

CAR-66



A B1 B2

Sheetmetalworking,includingbendingandforming;

Inspectionofsheetmetalwork.

7.14.2 Composite and non-metallic - 2 -

Bondingpractices;

Environmentalconditions

Inspectionmethods

7.15 Welding, Brazing, Soldering and Bonding

(a) - 2 2

Solderingmethods;inspectionofsolderedjoints.

(b) - 2 -

Weldingandbrazingmethods;

Inspectionofweldedandbrazedjoints;

Bondingmethodsandinspectionofbondedjoints.

7.16 Aircraft Weight and Balance

(a) - 2 2

CentreofGravity/Balancelimitscalculation:useofrelevantdocuments;

(b) - 2 -

Preparationofaircraftforweighing;

Aircraftweighing;

7.17 Aircraft Handling and Storage 2 2 2

Aircrafttaxiing/towingandassociatedsafetyprecautions;

Aircraftjacking,chocking,securingandassociatedsafetyprecautions;

Aircraftstoragemethods;

Refuelling/defuellingprocedures;

De-icing/anti-icingprocedures;

Electrical,hydraulicandpneumaticgroundsupplies.

Effectsofenvironmentalconditionsonaircrafthandlingandoperation.

7.18 Disassembly, Inspection, Repair and Assembly Techniques

(a) 2 3 3

Typesofdefectsandvisualinspectiontechniques.

Corrosionremoval,assessmentandreprotection.

(b) - 2 -

Generalrepairmethods,StructuralRepairManual;

Ageing,fatigueandcorrosioncontrolprogrammes;

(c) - 2 1

Non destructive inspection techniques including, penetrant, radiographic,eddycurrent,ultrasonicandboroscopemethods.

(d)

2

2

2

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A B1 B2

Disassemblyandre-assemblytechniques.

(e) - 2 2

Troubleshootingtechniques

7.19 Abnormal Events

(a) 2 2 2

InspectionsfollowinglightningstrikesandHIRFpenetration.

(b) 2 2 -

Inspectionsfollowingabnormaleventssuchasheavy

landingsandflightthroughturbulence.

7.20 Maintenance Procedures 1 2 2

Maintenanceplanning;

Modificationprocedures;

Storesprocedures;

Certification/releaseprocedures;

Interfacewithaircraftoperation;

MaintenanceInspection/QualityControl/QualityAssurance;

Additionalmaintenanceprocedures.

Controloflifelimitedcomponents

MODULE 8. BASIC AERODYNAMICS LEVEL

A B1 B2

8.1 Physics of the Atmosphere 1 2 2

InternationalStandardAtmosphere(ISA),applicationtoaerodynamics.

8.2 Aerodynamics 1 2 2

Airflowaroundabody;

Boundarylayer,laminarandturbulentflow,freestreamflow,relativeairflow,upwashanddownwash,vortices,stagnation;

Theterms:camber,chord,meanaerodynamicchord,profile(parasite)drag,induceddrag,centreofpressure,angleofattack,washinandwashout,fine-nessratio,wingshapeandaspectratio;

Thrust,Weight,AerodynamicResultant;

GenerationofLiftandDrag:AngleofAttack,Liftcoefficient,

Dragcoefficient,polarcurve,stall;

Aerofoilcontaminationincludingice,snow,frost.

8.3 Theory of Flight 1 2 2

Relationshipbetweenlift,weight,thrustanddrag;

Glideratio;

Steadystateflights,performance;

Theoryoftheturn;

Influenceofloadfactor:stall,flightenvelopeandstructurallimitations;

Liftaugmentation.

CAR-66


8.4 Flight Stability and Dynamics 1 2 2

Longitudinal,lateralanddirectionalstability(activeandpassive).

MODULE 9. HUMAN FACTORS LEVEL

A B1 B2

9.1 General 1 2 2

Theneedtotakehumanfactorsintoaccount;

Incidentsattributabletohumanfactors/humanerror;

‘Murphy's’law.

9.2 Human Performance and Limitations 1 2 2

Vision;

Hearing;

Informationprocessing;

Attentionandperception;

Memory;

Claustrophobiaandphysicalaccess.

9.3 Social Psychology 1 1 1

Responsibility:individualandgroup;

Motivationandde-motivation;

Peerpressure;

‘Culture’issues;

Teamworking;

Management,supervisionandleadership

9.4 Factors Affecting Performance 2 2 2

Fitness/health;

Stress:domesticandworkrelated;

Timepressureanddeadlines;

Workload:overloadandunderload;

Sleepandfatigue,shiftwork;

Alcohol,medication,drugabuse.

9.5 Physical Environment 1 1 1

Noiseandfumes;

Illumination;

Climateandtemperature;

Motionandvibration;

Workingenvironment.

9.6 Tasks 1 1 1

Physicalwork;

Repetitivetasks;

Visualinspection;

CAR-66


MODULE 9. HUMAN FACTORS LEVEL

A B1 B2

Complexsystems.

9.7 Communication 2 2 2

Withinandbetweenteams;

Workloggingandrecording;

Keepinguptodate,currency;

Disseminationofinformation.

9.8 Human Error 1 2 2

Errormodelsandtheories;

Typesoferrorinmaintenancetasks;

Implicationsoferrors(i.eaccidents)

Avoidingandmanagingerrors.

9.9 Hazards in the Workplace 1 2 2

Recognisingandavoidinghazards;

Dealingwithemergencies.

MODULE 10. AVIATION LEGISLATION LEVEL

A B1 B2

10.1 Regulatory Framework 1 1 1

RoleofInternationalCivilAviationOrganisation;

TheAircraftActandRulesmadethereunder

RoleoftheDGCA;

RelationshipbetweenCAR-21,CAR-M,CAR-145,CAR-66,CAR147

TheAircraftRules(ApplicabletoAircraftMaintenanceandRelease)

Aeronautical InformationCirculars(ApplicabletoAircraftMaintenanceandRelease)

CARSections1and2

10.2 CAR-66 Certifying Staff - Maintenance 2 2 2

DetailedunderstandingofCAR-66.

10.3 CAR-145 — Approved Maintenance Organisations 2 2 2

DetailedunderstandingofCAR-145andCARMSubpartF

10.4 Aircraft Operations 1 1 1

CommercialAirTransport/CommercialOperations

AirOperatorsCertificates;

Operators Responsibilities, in particular regarding continuing airworthinessandmaintenance;

Documentstobecarriedonboard;

AircraftPlacarding(Markings);

CAR-66



A B1 B2

10.5 Aircraft Certification

(a)General - 1 1

Certificationrules:suchasFAA&EACS23/25/27/29;

TypeCertification;

SupplementalTypeCertification;

CAR-21Design/ProductionOrganisationApprovals.

AircraftModificationsandrepairsapprovalandcertification

Permittoflyrequirements

(b)Documents - 2 2

CertificateofAirworthiness;

CertificateofRegistration;

NoiseCertificate;

WeightSchedule;

RadioStationLicenceandApproval.

10.6 CAR-M DetailunderstandingofCARMprovisionsrelatedtoContinuingAirworthiness

2 2 2

DetailedunderstandingofCAR-M.

10.7 Applicable National and International Requirements

(a) 1 2 2

MaintenanceProgramme,Maintenancechecksandinspections;

MasterMinimumEquipmentLists,MinimumEquipment

List,DispatchDeviationLists;

AirworthinessDirectives;

ServiceBulletins,manufacturersserviceinformation;

Modificationsandrepairs;

Maintenancedocumentation:maintenancemanuals,structuralrepairmanual,illustratedpartscatalogue,etc.;

(b) - 1 1

Continuingairworthiness;

Testflights;

ETOPS/EDTO,maintenanceanddispatchrequirements;

RVSM,maintenanceanddispatchrequirements

RNP,MNPSOperations

AllWeatherOperations,

Category2/3operationsandminimumequipmentrequirements.

10.8 Safety Management System 2 2 2

StateSafetyProgramme

BasicSafetyConcepts

Hazards&SafetyRisks

SMSOperation

SMSSafetyperformance

SafetyAssurance

CAR-66



A B1 B2

10.9 Fuel Tank Safety 2 2 2

SpecialFederalAviationRegulations(SFARs)from14CFRSFAR88oftheFAAandofJAATGL47

ConceptofCDCCL,

AirworthinessLimitationsItems(ALI)

MODULE 11A. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYS-TEMS

LEVEL

A1 B1.1

11.1 Theory of Flight

11.1.1 Aeroplane Aerodynamics and Flight Controls 1 2

Operationandeffectof:

—rollcontrol:aileronsandspoilers;

—pitchcontrol:elevators,stabilators,variableincidencestabilisersandcanards;

—yawcontrol,rudderlimiters;

Controlusingelevons,ruddervators;

Highliftdevices,slots,slats,flaps,flaperons;

Draginducingdevices,spoilers,liftdumpers,speedbrakes;

Effectsofwingfences,sawtoothleadingedges; Boundary layercontrolusing, vortexgenerators, stall wedgesor leadingedgede-vices; Operationandeffectoftrimtabs,balanceandantibalance(leading)tabs,servotabs,springtabs,massbalance,controlsurfacebias,aerodynamicbalancepanels;

11.1.2 High Speed Flight 1 2

Speedofsound,subsonicflight,transonicflight,supersonicflight,

Mach number, critical Mach number, compressibility buffet, shock wave, aerody-namicheating,arearule;

Factorsaffectingairflowinengineintakesofhighspeedaircraft;

EffectsofsweepbackoncriticalMachnumber.

11.2 Airframe Structures — General Concepts

(a) 2 2

Airworthinessrequirementsforstructuralstrength;

Structuralclassification,primary,secondaryandtertiary;

Failsafe,safelife,damagetoleranceconcepts;

Zonalandstationidentificationsystems; Stress,strain,bending,compression,shear,torsion,tension,hoopstress,fatigue;

Drainsandventilationprovisions;

Systeminstallationprovisions;

Lightningstrikeprotectionprovision.

Aircraftbonding

(b) 1 2

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LEVEL

A1 B1.1

Constructionmethodsof:stressedskinfuselage,formers,stringers,longerons,bulk-heads,frames,doublers,struts,ties,beams,floorstructures,reinforcement,methodsofskinning,anti-corrosiveprotection,wing,empennageandengineattachments;

Structureassemblytechniques:riveting,bolting,bonding

Methodsofsurfaceprotection,suchaschromating,anodising,painting;

Surfacecleaning.

Airframesymmetry:methodsofalignmentandsymmetrychecks.

11.3 Airframe Structures — Aeroplanes

11.3.1 Fuselage (ATA 52/53/56) 1 2

Constructionandpressurisationsealing;

Wing,stabiliser,pylonandundercarriageattachments;

Seatinstallationandcargoloadingsystem;

Doorsandemergencyexits:construction,mechanisms,operationandsafetydevices;

Windowsandwindscreenconstructionandmechanisms.

11.3.2 Wings (ATA 57) 1 2

Construction;

Fuelstorage;

Landinggear,pylon,controlsurfaceandhighlift/dragattachments.

11.3.3 Stabilisers (ATA 55) 1 2

Construction;

Controlsurfaceattachment.

11.3.4 Flight Control Surfaces (ATA 55/57) 1 2

Constructionandattachment;

Balancing—massandaerodynamic.

11.3.5 Nacelles/Pylons (ATA 54) 1 2

Construction;

Firewalls;

Enginemounts.

11.4 Air Conditioning and Cabin Pressurisation (ATA 21)

11.4.1 Air supply 1 2

Sourcesofairsupplyincludingenginebleed,APUandgroundcart;

11.4.2 Air Conditioning 1 3 Airconditioningsystems;

Aircycleandvapourcyclemachines

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LEVEL

A1 B1.1

Distributionsystems;

Flow,temperatureandhumiditycontrolsystem.

11.4.3 Pressurisation 1 3

Pressurisationsystems;

Controlandindicationincludingcontrolandsafetyvalves;

Cabinpressurecontrollers.

11.4.4 Safety and warning devices 1 3

Protectionandwarningdevices.

11.5 Instruments/Avionic Systems

11.5.1 Instrument Systems (ATA 31) 1 2

Pitotstatic:altimeter,airspeedindicator,verticalspeedindicator; Gyroscopic:artificialhorizon,attitudedirector,directionindicator,horizontalsitua-tionindicator,turnandslipindicator,turncoordinator;

Compasses:directreading,remotereading; Angleofattackindication,stallwarningsystems;GlassCockpit

Otheraircraftsystemindication.

11.5.2 Avionic Systems 1 1

Fundamentalsofsystemlay-outsandoperationof;

AutoFlight(ATA22);

Communications(ATA23);

NavigationSystems(ATA34).

11.6 Electrical Power (ATA 24) 1 3

BatteriesInstallationandOperation;

DCpowergeneration;

ACpowergeneration;

Emergencypowergeneration;

Voltageregulation;

Powerdistribution;

Inverters,transformers,rectifiers;

Circuitprotection.

External/Groundpower;

11.7 Equipment and Furnishings (ATA 25)

(a) 2 2

Emergencyequipmentrequirements;

Seats,harnessesandbelts. (b)

1

1

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LEVEL

A1 B1.1

Cabinlay-out;

Equipmentlay-out;

CabinFurnishingInstallation;

Cabinentertainmentequipment;

Galleyinstallation;

Cargohandlingandretentionequipment;

Airstairs.

11.8 Fire Protection (ATA 26)

(a) 1 3

Fireandsmokedetectionandwarningsystems;

Fireextinguishingsystems;

Systemtests.

(b) 1 1 Portablefireextinguisher

11.9 Flight Controls (ATA 27) 1 3

Primarycontrols:aileron,elevator,rudder,spoiler;

Trimcontrol;

Activeloadcontrol;

Highliftdevices;

Liftdump,speedbrakes;

Systemoperation:manual,hydraulic,pneumatic,electrical,fly-by-wire;

Artificialfeel,Yawdamper,Machtrim,rudderlimiter,gustlockssystems;

Balancingandrigging;

Stallprotection/warningsystem.

11.10 Fuel Systems (ATA 28) 1 3

Systemlay-out;

Fueltanks;

Supplysystems;

Dumping,ventinganddraining;

Cross-feedandtransfer;

Indicationsandwarnings;

Refuellinganddefuelling;

Longitudinalbalancefuelsystems.

11.11 Hydraulic Power (ATA 29) 1 3

Systemlay-out;

Hydraulicfluids;

Hydraulicreservoirsandaccumulators;

Pressuregeneration:electric,mechanical,pneumatic; Emergencypressuregeneration;Filters

PressureControl;

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LEVEL

A1 B1.1

Powerdistribution;

Indicationandwarningsystems;

Interfacewithothersystems.

11.12 Ice and Rain Protection (ATA 30) 1 3

Iceformation,classificationanddetection;

Anti-icingsystems:electrical,hotairandchemical;

De-icingsystems:electrical,hotair,pneumaticandchemical;

Rainrepellant;

Probeanddrainheating.

Wipersystems

11.13 Landing Gear (ATA 32) 2 3

Construction,shockabsorbing;

Extensionandretractionsystems:normalandemergency;

Indicationsandwarning;

Wheels,brakes,antiskidandautobraking;

Tyres; Steering.Air-groundsensing

11.14 Lights (ATA 33) 2 3

External:navigation,anti-collision,landing,taxiing,ice;

Internal:cabin,cockpit,cargo;

Emergency.

11.15 Oxygen (ATA 35) 1 3

Systemlay-out:cockpit,cabin;

Sources,storage,charginganddistribution;

Supplyregulation;


11.16 Pneumatic/Vacuum (ATA 36) 1 3

Systemlay-out;

Sources:engine/APU,compressors,reservoirs,groundsupply;

Pressurecontrol;

Distribution;


Interfaceswithothersystems.

11.17 Water/Waste (ATA 38) 2 3

Watersystemlay-out,supply,distribution,servicinganddraining;

Toiletsystemlay-out,flushingandservicing;

Corrosionaspects.

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LEVEL

A1 B1.1

11.18 On Board Maintenance Systems (ATA 45) 1 2

Centralmaintenancecomputers;

Dataloadingsystem;

Electroniclibrarysystem;

Printing; Structuremonitoring(damagetolerancemonitoring).

11.19 Integrated Modular Avionics (ATA42 ) FunctionsthatmaybetypicallyintegratedintheIntegratedModularAvionic(IMA)modulesare,amongothers:BleedManagement,AirPressureControl,AirVentilationandControl,AvionicsandCockpitVentilationControl,TemperatureControl,AirTraf-fic Communication, Avionics Communication Router, Electrical LoadManagement,CircuitBreakerMonitoring,ElectricalSystemBITE,FuelManagement,BrakingCon-trol,SteeringControl,LandingGearExtensionandRetraction,TyrePressureIndica-tion,OleoPressureIndication,BrakeTemperatureMonitoring,etc.

1

2

11.20 Cabin Systems (ATA44) Theunitsandcomponentswhichfurnishameansofentertainingthepassengersandprovidingcommunicationwithintheaircraft(CabinIntercommunicationDataSys-tem)andbetweentheaircraftcabinandgroundstations(CabinNetworkService).Includesvoice,data,musicandvideotransmissions.The Cabin Intercommunication Data System provides an interface between cock-pit/cabincrewandcabinsystems.Thesesystemssupportdataexchangeofthedif-ferentrelatedLRU'sandtheyaretypicallyoperatedviaFlightAttendantPanels.TheCabinNetworkServicetypicallyconsistsonaserver,typicallyinterfacingwith,amongothers,thefollowingsystems:—Data/RadioCommunication,In-FlightEntertainmentSystem.TheCabinNetworkServicemayhostfunctionssuchas:—Accesstopre-departure/departurereports,—E-mail/intranet/Internetaccess,—Passengerdatabase;CabinCoreSystem;In-flightEntertainmentSystem;ExternalCommunicationSystem;CabinMassMemorySystem;CabinMonitoringSystem;MiscellaneousCabinSystem.11.21 Information Systems (ATA46)

Theunitsandcomponentswhichfurnishameansofstoring,updatingandretrievingdigitalinformationtraditionallyprovidedonpaper,microfilmormicrofiche.Includesunitsthatarededicatedtotheinformationstorageandretrievalfunction

1

1

2

2

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LEVEL

A1 B1.1 suchastheelectroniclibrarymassstorageandcontroller.Doesnotincludeunitsorcomponents installedforotherusesandsharedwithothersystems,suchasflightdeckprinterorgeneralusedisplay.TypicalexamplesincludeAirTrafficandInformationManagementSystemsandNet-workServerSystemsAircraftGeneralInformationSystem;FlightDeckInformationSystem;MaintenanceInformationSystem;PassengerCabinInformationSystem;MiscellaneousInformationSystem.

MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYS-TEMS

LEVELL

A2 B1.2

Note:ThescopeofthisModuleshouldreflectthetechnologyofaeroplanespertinenttotheA2andB1.2subcategory.


11.1.1 Aeroplane Aerodynamics and Flight Controls 1 2






Highliftdevices,slots,slats,flaps,flaperons;

Draginducingdevices,spoilers,liftdumpers,speedbrakes;

Effectsofwingfences,sawtoothleadingedges;

Boundary layercontrolusing,vortexgenerators, stallwedgesor leadingedgede-vices;

Operationandeffectoftrimtabs,balanceandantibalance(leading)tabs,servotabs,springtabs,massbalance,controlsurfacebias,aerodynamicbalancepanels;

11.1.2 High Speed Flight — N/A — - -

11.2 Airframe Structures — General Concepts

(a) 2 2




Zonalandstationidentificationsystems;

Stress,strain,bending,compression,shear,torsion,tension,hoopstress,fatigue;

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LEVELL

A2 B1.2


Systeminstallationprovisions;


Aircraftbonding

(b) 1 2

Constructionmethodsof:stressedskinfuselage,formers,stringers,longerons,bulk-heads,frames,doublers,struts,ties,beams,floorstructures,reinforcement,methodsofskinning,anti-corrosiveprotection,wing,empennageandengineattachments;

Structureassemblytechniques:riveting,bolting,bonding;

Methodsofsurfaceprotection,suchaschromating,

anodising,painting;

Surfacecleaning;


11.3 Airframe Structures — Aeroplanes

11.3.1 Fuselage (ATA 52/53/56) 1 2

Constructionandpressurisationsealing;

Wing,tail-planepylonandundercarriageattachments;

Seatinstallation;

Doorsandemergencyexits:constructionandoperation;

Windowandwindscreenattachment.

11.3.2 Wings (ATA 57) 1 2

Construction;

Fuelstorage;

Landinggear,pylon,controlsurfaceandhighlift/dragattachments.

11.3.3 Stabilisers (ATA 55) 1 2

Construction;

Controlsurfaceattachment.

11.3.4 Flight Control Surfaces (ATA 55/57) 1 2

Constructionandattachment;

Balancing—massandaerodynamic.

11.3.5 Nacelles/Pylons (ATA 54)

1 2

Nacelles/Pylons:

—Construction;

—Firewalls;

—Enginemounts.

11.4 Air Conditioning and Cabin Pressurisation (ATA 21) 1 3

Pressurisationandairconditioningsystems;

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LEVELL

A2 B1.2

Cabinpressurecontrollers,protectionandwarningdevices

HeatingSystems




Compasses:directreading,remotereading; Angleofattackindication,stallwarningsystems.Glasscockpit;



Fundamentalsofsystemlay-outsandoperationof:

—AutoFlight(ATA22);

—Communications(ATA23);

—NavigationSystems(ATA34).

11.6 Electrical Power (ATA 24) 1 3


DCpowergeneration;

Voltageregulation;

Powerdistribution;

Circuitprotection;

Inverters,transformers.


(a) 2 2


Seats,harnessesandbelts.

(b) 1 1

Cabinlay-out;

Equipmentlay-out;

CabinFurnishingInstallation(level2);

Cabinentertainmentequipment;

Galleyinstallation;

Cargohandlingandretentionequipment;

Airstairs.

11.8 Fire Protection (ATA 26) 1 3

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LEVELL

A2 B1.2

(a)



Systemtests.

(b) 1 3 Portablefireextinguisher.

11.9 Flight Controls (ATA 27) 1 3

Primarycontrols:aileron,elevator,rudder;

Trimtabs;

Highliftdevices;

Systemoperation:manual;

Gustlocks;

Balancingandrigging;

Stallwarningsystem.


Systemlay-out;

Fueltanks;

Supplysystems;



Refuellinganddefuelling.


Systemlay-out;

Hydraulicfluids;

Hydraulicreservoirsandaccumulators; Pressuregeneration:electric,mechanical;Filters

PressureControl;

Powerdistribution;

Indicationandwarningsystems.



De-icingsystems:electrical,hotair,pneumaticandchemical;

Probeanddrainheating;

Wipersystems.





Wheels,brakes,antiskidandautobraking;

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LEVELL

A2 B1.2

Tyres; Steering.Air-groundsensing

11.14 Lights (ATA 33) 2 3

External:navigation,anticollision,landing,taxiing,ice;


Emergency.

11.15 Oxygen (ATA 35) 1 3

Systemlay-out:cockpit,cabin;

Sources,storage,charginganddistribution;

Supplyregulation;



Systemlay-out;

Sources:engine/APU,compressors,reservoirs,groundsupply;

Pressurecontrol;

Distribution;


Interfaceswithothersystems.

11.17 Water/Waste (ATA 38) 2 3

Watersystemlay-out,supply,distribution,servicinganddraining;

Toiletsystemlay-out,flushingandservicing;

Corrosionaspects.

MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS LEVEL

A3 A4 B1.3 B1.4

12.1 Theory of Flight — Rotary Wing Aerodynamics 1 2

Terminology;

Effectsofgyroscopicprecession;

Torquereactionanddirectionalcontrol;

Dissymmetryoflift,Bladetipstall;

Translatingtendencyanditscorrection;

Corioliseffectandcompensation;

Vortexringstate,powersettling,overpitching;

Auto-rotation;

Groundeffect.

12.2 Flight Control Systems 2 3

Cycliccontrol;

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A3 A4 B1.3 B1.4

Collectivecontrol;

Swashplate;

Yawcontrol:Anti-TorqueControl,Tailrotor,bleedair;

MainRotorHead:DesignandOperationfeatures;

BladeDampers:Functionandconstruction; RotorBlades:Mainandtailrotorbladeconstructionandattachment;

Trimcontrol,fixedandadjustablestabilisers;

Systemoperation:manual,hydraulic,electricalandflyby-wire;

Artificialfeel;

BalancingandRigging.

12.3 Blade Tracking and Vibration Analysis 1 3

Rotoralignment;

Mainandtailrotortracking;

Staticanddynamicbalancing;

Vibrationtypes,vibrationreductionmethods;

Groundresonance.

12.4 Transmissions 1 3

Gearboxes,mainandtailrotors;

Clutches,freewheelunitsandrotorbrake.

Tailrotordriveshafts,flexiblecouplings,bearings,

vibrationdampersandbearinghangers

12.5 Airframe Structures

(a) 2 2





Stress,strain,bending,compression,shear,torsion,tension,hoopstress,fatigue;


Systeminstallationprovisions; Lightningstrikeprotectionprovision.

(b) 1 2 Constructionmethodsof:stressedskinfuselage,formers,stringers,longerons,bulk-heads,frames,doublers,struts,ties,beams,floorstructures,reinforcement,meth-odsofskinningandanti-corrosiveprotection.

Pylon,stabiliserandundercarriageattachments;

Seatinstallation;

Doors:construction,mechanisms,operationandsafetydevices;

Windowsandwindscreenconstruction;

Fuelstorage;

Firewalls;

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A3 A4 B1.3 B1.4

Enginemounts;

Structureassemblytechniques:riveting,bolting,bonding; Methodsofsurfaceprotection,suchaschromating,anodising,painting;

Surfacecleaning.


12.6 Air Conditioning (ATA 21)

12.6.1 Air supply 1 2

Sourcesofairsupplyincludingenginebleedandgroundcart;

12.6.2 Air Conditioning 1 3

Airconditioningsystems;

Distributionsystems;

Flowandtemperaturecontrolsystems;

Protectionandwarningdevices.




Compasses:directreading,remotereading; Vibrationindicatingsystems—HUMS;GlassCockpit



Fundamentalsofsystemlayoutsandoperationof:

AutoFlight(ATA22);

Communications(ATA23);

NavigationSystems(ATA34). 12.8 Electrical Power (ATA 24) 1 3


DCpowergeneration,ACpowergeneration;


Voltageregulation,Circuitprotection.

Powerdistribution;


External/Groundpower.


(a) 2 2


Seats,harnessesandbelts;

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A3 A4 B1.3 B1.4

Liftingsystems.

(b) 1 1

Emergencyflotationsystems;

Cabinlay-out,cargoretention;

Equipmentlay-out;

CabinFurnishingInstallation.

12.10 Fire Protection (ATA 26) 1 3



Systemtests.


Systemlay-out;

Fueltanks;

Supplysystems;

Dumping,ventinganddraining;



Refuellinganddefuelling.


Systemlay-out;

Hydraulicfluids;

Hydraulicreservoirsandaccumulators;

Pressuregeneration:electric,mechanical,pneumatic; Emergencypressuregeneration;Filters

PressureControl;

Powerdistribution;

Indicationandwarningsystems;

Interfacewithothersystems.



Anti-icingandde-icingsystems:electrical,hotairandchemical;

Rainrepellantandremoval;

Probeanddrainheating.

Wipersystem




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A3 A4 B1.3 B1.4


Wheels,tyres,brakes; Steering;Air-groundsensing

Skids,floats.

12.15 Lights (ATA 33) 2 3

External:navigation,landing,taxiing,ice;


Emergency.


Systemlay-out;

Sources:engine,compressors,reservoirs,groundsupply.;

Pressurecontrol;

Distribution;

Indicationsandwarnings; Interfaceswithothersystems.12.17 Integrated Modular Avionics (ATA42) FunctionsthatmaybetypicallyintegratedintheIntegratedModularAvionic(IMA)modulesare,amongothers:BleedManagement,AirPressureControl,AirVentilationandControl,AvionicsandCockpitVentilationControl,TemperatureControl,AirTrafficCommunication,Avion-icsCommunicationRouter,ElectricalLoadManagement,CircuitBreakerMonitoring,ElectricalSystemBITE,FuelManagement,BrakingControl,SteeringControl,LandingGearExtensionandRetraction,TyrePressureIndication,OleoPressureIndication,BrakeTemperatureMonitoring,etc.CoreSystem;NetworkComponents.12.18 On Board Maintenance Systems (ATA45) Centralmaintenancecomputers;Dataloadingsystem;Electroniclibrarysystem;Printing;Structuremonitoring(damagetolerancemonitoring).12.19 Information Systems (ATA46) Theunitsandcomponentswhichfurnishameansofstoring,updatingandretrievingdigitalinformationtraditionallyprovidedonpaper,microfilmormicrofiche.Includesunitsthatarededicatedtotheinformationstorageandretrievalfunctionsuchastheelectroniclibrarymassstorageandcontroller.Doesnotincludeunitsorcomponentsinstalledforotherusesandsharedwithothersystems,suchasflightdeckprinterorgeneralusedisplay.TypicalexamplesincludeAirTrafficandInformationManagementSystemsandNet-workServerSystems.

1

1

1

2 2 2

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A3 A4 B1.3 B1.4

AircraftGeneralInformationSystem;FlightDeckInformationSystem;MaintenanceInformationSystem;PassengerCabinInformationSystem;MiscellaneousInformationSystem.

MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

LEVEL

B2


(a)AeroplaneAerodynamicsandFlightControls 1






Highliftdevices:slots,slats,flaps;

Draginducingdevices:spoilers,liftdumpers,speedbrakes;

Operationandeffectoftrimtabs,servotabs,controlsurfacebias.

(b)HighSpeedFlight 1

Speedofsound,subsonicflight,transonicflight,supersonicflight,

Machnumber,criticalMachnumber.

(c)RotaryWingAerodynamics 1

Terminology;

Operationandeffectofcyclic,collectiveandanti-torquecontrols.

13.2 Structures — General Concepts

(a) 1

Fundamentalsofstructuralsystems.

(b) 2


Electricalbonding;


13.3 Autoflight (ATA 22) 3

Fundamentalsofautomaticflightcontrolincluding

workingprinciplesandcurrentterminology;

Commandsignalprocessing;

Modesofoperation:roll,pitchandyawchannels; Yawdampers;Autothrottlesystems.AutomaticLandingSystems:principlesandcategories,modesofoperation,approach,glideslope,land,goaround,systemmonitorsandfailureconditions.

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LEVEL

B2

13.4 Communication/Navigation (ATA 23/34) 3

Fundamentalsofradiowavepropagation,antennas,transmissionlines,communication,receiverandtransmitter;

Workingprinciplesoffollowingsystems:

—VeryHighFrequency(VHF)communication;

—HighFrequency(HF)communication;

—Audio;

—EmergencyLocatorTransmitters;

—CockpitVoiceRecorder;

—VeryHighFrequencyomnidirectionalrange(VOR);

—AutomaticDirectionFinding(ADF);

—InstrumentLandingSystem(ILS);

—MicrowaveLandingSystem(MLS);

—FlightDirectorsystems;DistanceMeasuringEquipment(DME);

—VeryLowFrequencyandhyperbolicnavigation(VLF/Omega);

—Dopplernavigation;

—Areanavigation,RNAVsystems;

—FlightManagementSystems;

—GlobalPositioningSystem(GPS),GlobalNavigationSatelliteSystems(GNSS);

—InertialNavigationSystem;

—AirTrafficControltransponder,secondarysurveillanceradar;

—TrafficAlertandCollisionAvoidanceSystem(TCAS);

—Weatheravoidanceradar;

—Radioaltimeter;

—ARINCcommunicationandreporting;

13.5 Electrical Power (ATA 24) 3


DCpowergeneration;

ACpowergeneration;


Voltageregulation;

Powerdistribution;


Circuitprotection;

External/Groundpower.

13.6 Equipment and Furnishings (ATA 25) 3

CAR-66


Electronicemergencyequipmentrequirements; Cabinentertainmentequipment.


LEVEL

B2

13.7 Flight Controls (ATA 27) (a) 2

Primarycontrols:aileron,elevator,rudder,spoiler;

Trimcontrol;

Activeloadcontrol;

Highliftdevices;

Liftdump,speedbrakes;

Systemoperation:manual,hydraulic,pneumatic;

Artificialfeel,Yawdamper,Machtrim,rudderlimiter,gustlocks.

Stallprotectionsystems.

(b) 3

Systemoperation:electrical,flybywire.

13.8 Instrument Systems (ATA 31) 3

Classification;

Atmosphere;

Terminology;

Pressuremeasuringdevicesandsystems;

Pitotstaticsystems;

Altimeters;

Verticalspeedindicators;

Airspeedindicators;

Machmeters;

Altitudereporting/alertingsystems;

Airdatacomputers;

Instrumentpneumaticsystems;

Directreadingpressureandtemperaturegauges;

Temperatureindicatingsystems;

Fuelquantityindicatingsystems;

Gyroscopicprinciples;

Artificialhorizons;

Slipindicators;

Directionalgyros;

GroundProximityWarningSystems;

Compasssystems;

FlightDataRecordingsystems;

ElectronicFlightInstrumentSystems; Instrumentwarningsystemsincludingmasterwarningsystemsandcentralisedwarningpanels;

Stallwarningsystemsandangleofattackindicatingsystems; Vibrationmeasurementandindication.GlassCockpit

13.9 Lights (ATA 33) 3

CAR-66


External:navigation,landing,taxiing,ice;

Internal:cabin,cockpit,cargo;Emergency


LEVEL

B2

13.10 On board Maintenance Systems (ATA 45) 3

Centralmaintenancecomputers;

Dataloadingsystem;

Electroniclibrarysystem;

Printing; Structuremonitoring(damagetolerancemonitoring).13.11 Air Conditioning and Cabin Pressurisation (ATA21) 13.11.1.AirsupplySourcesofairsupplyincludingenginebleed,APUandgroundcart13.11.2.AirConditioningAirconditioningsystems;Aircycleandvapourcyclemachines;Distributionsystems;Flow,temperatureandhumiditycontrolsystem.13.11.3. Pressurisation Pressurisationsystems;Controlandindicationincludingcontrolandsafetyvalves;Cabinpressurecontrollers13.11.4.SafetyandwarningdevicesProtectionandwarningdevices13.12 Fire Protection (ATA 26) (a)Fireandsmokedetectionandwarningsystems;Fireextinguishingsystems;Systemtests;(b)Portablefireextinguisher.13.13 Fuel Systems (ATA 28) Systemlay-out;Fueltanks;Supplysystems;Dumping,ventinganddraining;Cross-feedandtransfer;Indicationsandwarnings;Refuellinganddefuelling;Longitudinalbalancefuelsystems

2

3

3

1

2 3 2 3

1 1 1 1

2 3 1 3

3

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13.14 Hydraulic Power (ATA 29 ) Systemlay-out;Hydraulicfluids;Hydraulicreservoirsandaccumulators;Pressuregeneration:electrical,mechanical,pneumatic;Emergencypressuregeneration;Filters;Pressurecontrol;Powerdistribution;Indicationandwarningsystems;Interfacewithothersystems.13.15 Ice and Rain Protection (ATA 30) Iceformation,classificationanddetection;Anti-icingsystems:electrical,hotairandchemical;De-icingsystems:electrical,hotair,pneumatic,chemical;Rainrepellent;Probeanddrainheating;WiperSystems.13.16 Landing Gear (ATA 32) Construction,shockabsorbing;Extensionandretractionsystems:normalandemergency;Indicationsandwarnings;Wheels,brakes,antiskidandautobraking;Tyres;Steering;Air-groundsensing.13.17 Oxygen (ATA 35) Systemlay-out:cockpit,cabin;Sources,storage,charginganddistribution;Supplyregulation;Indicationsandwarnings. 13.18 Pneumatic/Vacuum (ATA 36) Systemlay-out;Sources:engine/APU,compressors,reservoirs,groundsupply;Pressurecontrol;Distribution;Indicationsandwarnings;Interfaceswithothersystems.13.19 Water/Waste (ATA 38)

1 1 1 3 3 1 3 1 3 3

2 2 3 1 3 1

1 3 3 3 1 3 3 3 3 3 3

2 2 3 1 3 3 2

LEVEL

B2

CAR-66


Watersystemlay-out,supply,distribution,servicinganddraining;Toiletsystemlay-out,flushingandservicing.


13.20 Integrated Modular Avionics (ATA42) FunctionsthatmaybetypicallyintegratedintheIntegratedModularAvionic(IMA)modulesare,amongothers:BleedManagement,AirPressureControl,AirVentilationandControl,AvionicsandCockpitVentilationControl,TemperatureControl,AirTrafficCommunication,AvionicsCommunicationRouter,ElectricalLoadManagement,CircuitBreakerMonitoring,ElectricalSystemBITE,FuelManagement,BrakingControl,SteeringControl,LandingGearExtensionandRetraction,TyrePressureIndication,OleoPressureIndication,BrakeTemperatureMonitoring,etc.;CoreSystem;NetworkComponents. 13.21 Cabin Systems (ATA44)Theunitsandcomponentswhichfurnishameansofentertainingthepassengersandprovidingcommunicationwithintheaircraft(CabinIntercommunicationDataSystem)andbetweentheaircraftcabinandgroundstations(CabinNetworkService).In-cludesvoice,data,musicandvideotransmissions.TheCabinIntercommunicationDataSystemprovidesaninterfacebetweencockpit/cabincrewandcabinsystems.ThesesystemssupportdataexchangeofthedifferentrelatedLRU'sandtheyaretypicallyoperatedviaFlightAttendantPanels.TheCabinNetworkServicetypicallyconsistsonaserver,typicallyinterfacingwith,amongothers,thefollowingsystems:—Data/RadioCommunication,In-FlightEntertainmentSystem.TheCabinNetworkServicemayhostfunctionssuchas:—Accesstopre-departure/departurereports,—E-mail/intranet/Internetaccess,—Passengerdatabase;CabinCoreSystem;In-flightEntertainmentSystem;ExternalCommunicationSystem;CabinMassMemorySystem;CabinMonitoringSystem;MiscellaneousCabinSystem.13.22 Information Systems (ATA46) Theunitsandcomponentswhichfurnishameansofstoring,updatingandretrievingdigitalinformationtraditionallyprovidedonpaper,microfilmormicrofiche.Includesunitsthatarededicatedtotheinformationstorageandretrievalfunctionsuchastheelectroniclibrarymassstorageandcontroller.Doesnotincludeunitsorcomponentsinstalledforotherusesandsharedwithothersystems,suchasflightdeckprinterorgeneralusedisplay.

3

3

LEVEL

B2

3

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MODULE 14. PROPULSION

LEVEL

B2

14.1 Turbine Engines

(a) 1

Constructionalarrangementandoperationofturbojet,turbofan,turboshaftandturbopro-pellerengines;

(b) 2 ElectronicEnginecontrolandfuelmeteringsystems(FADEC).

14.2 Engine Indicating Systems 2

Exhaustgastemperature/Interstageturbinetemperaturesystems;

Enginespeed;

EngineThrustIndication:EnginePressureRatio,engineturbinedischargepressureorjetpipepressuresystems;

Oilpressureandtemperature;

Fuelpressure,temperatureandflow;

Manifoldpressure;

Enginetorque; Propellerspeed.14.3 Starting and Ignition Systems Operationofenginestartsystemsandcomponents;Ignitionsystemsandcomponents;Maintenancesafetyrequirements

MODULE 15. GAS TURBINE ENGINE

LEVEL

A1 A3

B1.1 B1.3

15.1 Fundamentals 1 2 Potentialenergy,kineticenergy,Newton'slawsofmotion,Braytoncycle; Therelationshipbetweenforce,work,power,energy,velocity,acceleration;

Constructionalarrangementandoperationofturbojet,turbofan,turboshaft,turboprop.

15.2 Engine Performance - 2 Gross thrust, net thrust, choked nozzle thrust, thrust distribution, resultant thrust,thrusthorsepower,equivalentshafthorsepower,specificfuelconsumption;

Engineefficiencies;

TypicalexamplesincludeAirTrafficandInformationManagementSystemsandNetworkServerSystems.AircraftGeneralInformationSystem;FlightDeckInformationSystem;MaintenanceInformationSystem;PassengerCabinInformationSystem;MiscellaneousInformationSystem.

2

MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS LEVEL

B2

CAR-66



LEVEL

A1 A3

B1.1 B1.3

By-passratioandenginepressureratio;

Pressure,temperatureandvelocityofthegasflow; Engineratings,staticthrust,influenceofspeed,altitudeandhotclimate,flatrating,limitations.

15.3 Inlet 2 2

Compressorinletducts

Effectsofvariousinletconfigurations; Iceprotection.

15.4 Compressors 1 2

Axialandcentrifugaltypes;

Constructionalfeaturesandoperatingprinciplesandapplications;

Fanbalancing;

Operation:

Causesandeffectsofcompressorstallandsurge;

Methods of air flow control: bleed valves, variable inlet guide vanes, variable statorvanes,rotatingstatorblades;

Compressorratio.

15.5 Combustion Section 1 2

Constructionalfeaturesandprinciplesofoperation.

15.6 Turbine Section 2 2

Operationandcharacteristicsofdifferentturbinebladetypes;

Bladetodiskattachment;

Nozzleguidevanes;

Causesandeffectsofturbinebladestressandcreep. 15.7 Exhaust 1 2

Constructionalfeaturesandprinciplesofoperation;

Convergent,divergentandvariableareanozzles;

Enginenoisereduction;

Thrustreversers.

15.8 Bearings and Seals - 2 Constructionalfeaturesandprinciplesofoperation.

15.9 Lubricants and Fuels 1 2

Propertiesandspecifications;

Fueladditives;

Safetyprecautions.

CAR-66



LEVEL

A1 A3

B1.1 B1.3

15.10 Lubrication Systems 1 2

Systemoperation/lay-outandcomponents.

15.11 Fuel Systems 1 2

Operationofenginecontrolandfuelmeteringsystems

includingelectronicenginecontrol(FADEC);

Systemslay-outandcomponents.

15.12 Air Systems 1 2 Operation of engine air distribution and anti-ice control systems, including internalcooling,sealingandexternalairservices.

15.13 Starting and Ignition Systems 1 2

Operationofenginestartsystemsandcomponents;

Ignitionsystemsandcomponents; Maintenancesafetyrequirements.

15.14 Engine Indication Systems 1 2

ExhaustGasTemperature/InterstageTurbine

Temperature; EngineThrustIndication:EnginePressureRatio,engineturbinedischargepressureorjetpipepressuresystems;


Fuelpressureandflow;

Enginespeed;

Vibrationmeasurementandindication;

Torque;

Power.

15.15 Power Augmentation Systems - 1

Operationandapplications;

Waterinjection,watermethanol;

Afterburnersystems.

15.16 Turbo-prop Engines 1 2

Gascoupled/freeturbineandgearcoupledturbines;

Reductiongears;

Integratedengineandpropellercontrols;

Overspeedsafetydevices.

15.17 Turbo-shaft engines 1 2

Arrangements,drivesystems,reductiongearing,

couplings,controlsystems.

15.18 Auxiliary Power Units (APUs) 1 2

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LEVEL

A1 A3

B1.1 B1.3

Purpose,operation,protectivesystems.

15.19 Powerplant Installation 1 2

Configuration of firewalls, cowlings, acoustic panels, engine mounts, anti-vibrationmounts,hoses,pipes,feeders,connectors,wiringlooms,controlcablesandrods,liftingpointsanddrains.

15.20 Fire Protection Systems 1 2

Operationofdetectionandextinguishingsystems.

15.21 Engine Monitoring and Ground Operation 1 3

Proceduresforstartingandgroundrun-up;

Interpretationofenginepoweroutputandparameters;

Trend(includingoilanalysis,vibrationandboroscope)monitoring;

Inspectionofengineandcomponentstocriteria,tolerancesanddataspecifiedbyenginemanufacturer;

Compressorwashing/cleaning;

ForeignObjectDamage.

15.22 Engine Storage and Preservation - 2

Preservationanddepreservationfortheengineandaccessories/systems.

MODULE 16. PISTON ENGINE

LEVEL

A2 A4

B1.2 B1.4

16.1 Fundamentals 1 2

Mechanical,thermalandvolumetricefficiencies;

Operatingprinciples—2stroke,4stroke,OttoandDiesel;

Pistondisplacementandcompressionratio;

Engineconfigurationandfiringorder.

16.2 Engine Performance 1 2

Powercalculationandmeasurement;

Factorsaffectingenginepower;

Mixtures/leaning,pre-ignition.

16.3 Engine Construction 1 2

Crankcase,crankshaft,camshafts,sumps;

Accessorygearbox;

Cylinderandpistonassemblies;

Connectingrods,inletandexhaustmanifolds;

Valvemechanisms;

Propellerreductiongearboxes.

16.4 Engine Fuel Systems

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LEVEL

A2 A4

B1.2 B1.4

16.4.1 Carburetors 1 2

Types,constructionandprinciplesofoperation;

Icingandheating.

16.4.2 Fuel injection systems 1 2

Types,constructionandprinciplesofoperation.

16.4.3 Electronic engine control 1 2

Operationofenginecontrolandfuelmeteringsystems

includingelectronicenginecontrol(FADEC);

Systemslay-outandcomponents.

16.5 Starting and Ignition Systems 1 2

Startingsystems,pre-heatsystems;

Magnetotypes,constructionandprinciplesofoperation;

Ignitionharnesses,sparkplugs;

Lowandhightensionsystems.

16.6 Induction, Exhaust and Cooling Systems 1 2

Constructionandoperationof:inductionsystems

includingalternateairsystems;

Exhaustsystems,enginecoolingsystems—airandliquid.

16.7 Supercharging/Turbocharging 1 2

Principlesandpurposeofsupercharginganditseffectsonengineparameters;

Constructionandoperationofsupercharging/turbochargingsystems;

Systemterminology;

Controlsystems;

Systemprotection.

16.8 Lubricants and Fuels 1 2

Propertiesandspecifications;

Fueladditives;

Safetyprecautions.

16.9 Lubrication Systems 1 2

Systemoperation/lay-outandcomponents.

16.10 Engine Indication Systems 1 2

Enginespeed;

Cylinderheadtemperature;

Coolanttemperature;


ExhaustGasTemperature;

Fuelpressureandflow;

CAR-66



LEVEL

A2 A4

B1.2 B1.4

Manifoldpressure.

16.11 Powerplant Installation 1 2 Configuration of firewalls, cowlings, acoustic panels, engine mounts, anti-vibrationmounts,hoses,pipes,feeders,connectors,wiringlooms,controlcablesandrods,liftingpointsanddrains.

16.12 Engine Monitoring and Ground Operation 1 3 Proceduresforstartingandgroundrun-up;

Interpretationofenginepoweroutputandparameters;

Inspectionofengineandcomponents:criteria,tolerances,anddataspecifiedbyenginemanufacturer.

16.13 Engine Storage and Preservation - 2

Preservationanddepreservationfortheengineandaccessories/systems

MODULE 17. PROPELLER

LEVEL

A1 A2

B1.1 B1.2

17.1 Fundamentals 1 2

Bladeelementtheory;

High/lowbladeangle,reverseangle,angleofattack,rotationalspeed;

Propellerslip;

Aerodynamic,centrifugal,andthrustforces;

Torque;

Relativeairflowonbladeangleofattack;

Vibrationandresonance.

17.2 Propeller Construction 1 2 Constructionmethodsandmaterialsusedinwooden,compositeandmetalpropellers;

Bladestation,bladeface,bladeshank,bladebackandhubassembly;

Fixedpitch,controllablepitch,constantspeedingpropeller;

Propeller/spinnerinstallation.

17.3 Propeller Pitch Control 1 2

Speedcontrolandpitchchangemethods,mechanicalandelectrical/electronic;

Featheringandreversepitch;

Overspeedprotection.

17.4 Propeller Synchronising - 2 Synchronisingandsynchrophasingequipment.

17.5 Propeller Ice Protection 1 2

CAR-66


Fluidandelectricalde-icingequipment.

17.6 Propeller Maintenance 1 3

Staticanddynamicbalancing;

Bladetracking;

Assessmentofbladedamage,erosion,corrosion,impactdamage,delamination;

Propellertreatment/repairschemes;

Propellerenginerunning.

17.7 Propeller Storage and Preservation 1 2

Propellerpreservationanddepreservation

CAR-66


Appendix II –Basic Examination Standard

1. General

1.1 Allbasicexaminationsmustbecarriedoutusingthemultiplechoicequestion.

1.2 Eachmultiplechoicequestionsmusthavemorethantwoalternativeanswers

ofwhichonlyonemustbethecorrectanswerandthecandidateshallbeallowed

atimepermodulewhichisbaseduponanominalaverageof75secondsper

question.

1.3 ThepassmarkforCAR-66moduleandsub-modulemultiplechoicepartofthe

examinationis75%.

1.4 Penalty marking systems is not used to determine whether a candidate has

passed.

1.5 Afailedmodulemaynotberetakenforatleast90daysfollowingthedateofthefailed module examination. except in the case of an approved maintenancetrainingorganisationwhichconductsacourseofretrainingtailoredtothefailedsubjectsintheparticularmodule.Insuchcase,thefailedmodulemayberetakenafter30days.

1.6 Thetimeperiodsrequiredbypoint66.A.25applytoeachindividualmoduleex-

amination,withtheexceptionofthosemoduleexaminationswhichwerepassed

aspartofanothercategorylicence,wherethelicencehasalreadybeenissued

1.7 Themaximumnumberofconsecutiveattemptsforeachmoduleisthree.Fur-

thersetsofthreeattemptsareallowedwitha1yearwaitingperiodbetween

sets.

1.8 TheapplicantshallconfirminwritingtotheDGCAforanexamination,thenum-

beranddatesofattemptsduringthelastyearwheretheseattemptstookplace.

CAR-66


2. Question Numbers and Examination Duration for the CAR-66 Appendix I

Modules

ModuleCategory

MultiplechoiceQues-

tions

Timeallowed(Minutes)No. Subject

1 Mathematics AllCategories NotApplicable

2 Physics AllCategories NotApplicable

3 ElectricalFundamentals

A 20 25

B1 52 65

B2 52 65

4 ElectronicFundamentals

A NotApplicable

B1 20 25

B2 40 50

5DigitalTechniques/ElectronicInstrumentSystems

A 16 20

B1.1,B1.3 40 50

B1.2,B1.4 20 25

B2 72 90

6 MaterialsandHardware

A 52 65

B1 72 90

B2 60 75

7 MaintenancePractices

A 72 90

B1 80 100

B2 60 75

8 BasicAerodynamics

A 20 25

B1 20 25

B2 20 25

9 Humanfactors

A 20 25

B1 20 25

B2 20 25

10 AviationLegislation

A 32 40

B1 40 50

B2 40 50

CAR-66


ModuleCategory

MultiplechoiceQues-

tions

Timeallowed(Minutes)No. Subject

11ATurbineAeroplaneAerody-namics,StructuresandSys-tems

A1 108 135

B1.1 140 175

B2 0 0

11BPistonAeroplaneAerodynam-ics,StructuresandSystems

A2 72 90

B1.2 100 125

B2 0 0

12HelicopterAerodynamics,StructuresandSystems

A3/A4 100 125

B1.3/B1.4 128 160

B2 0 0

13

AircraftAerodynamics,Struc-turesandSystems

A 0 0

B1 0 0

B2 180 225

14 Propulsion

A 0 0

B1 0 0

B2 24 30

15 GasTurbineEngine

A 60 75

B1 92 115

B2 0 0

16 PistonEngine

A 52 65

B1 72 90

B2 0 0

17 Propeller

A 20 25

B1 32 40

B2 0 0

CAR-66


3. ISSUANCE OF CERTIFICATE Applicantswhohavepassedallbasicknowledgeexaminationmodulesinrespectofa

particularcategory/sub-categoryofAMElicencemayapplytoCEO,DGCAonFormCA

19-11fortheissuanceofBasicKnowledgeExaminationCertificate.

CAR-66


Appendix III -TypetrainingandExaminationStandard

On the job training

1. General

Aircrafttypetrainingshallconsistoftheoreticaltrainingandexamination,and,except

forthecategoryCratings,practicaltrainingandassessment.

(a)Theoreticaltrainingandexaminationshallcomplywiththefollowingrequirements:

(i) Shall be conducted by a maintenance training organisation appropriately ap-

provedinaccordancewithCAR-147or,whenconductedbyotherorganisations,as

directlyapprovedbytheDGCA.

(ii)Shallcomply,exceptaspermittedbythedifferencestrainingdescribedinpoint

(c),with:

- therelevantelementsdefinedinthemandatorypartoftheoperationalsuita-

bilitydataestablishedinaccordancewithCAR66orthestandarddescribed

inpoint3.1ofthisAppendix,and

- thetypetrainingexaminationstandarddescribedinpoint4.1ofthisAppendix.

(iii)Reserved

(iv)Shallhavebeenstartedandcompletedwithinthe3yearsprecedingtheapplica-

tionforatyperatingendorsement.

(b)Practicaltrainingandassessmentshallcomplywiththefollowingrequirements:

(i) Shall be conducted by a maintenance training organisation appropriately ap-

provedinaccordancewithCAR-147or,whenconductedbyotherorganisations,

asdirectlyapprovedbytheDGCA.

(ii)Shallcomply,exceptaspermittedbythedifferencestrainingdescribedinpoint

(c),with:

- therelevantelementsdefinedinthemandatorypartoftheoperationalsuita-

bilitydataestablishedor,thestandarddescribedinpoint3.2ofthisAppendix,

and

- thetypetrainingassessmentstandarddescribedinpoint4.2ofthisAppendix.

(iii)Shallincludearepresentativecrosssectionofmaintenanceactivitiesrelevantto

theaircrafttype.

CAR-66


(iv) Shall include demonstrations using equipment, components, simulators, other

trainingdevicesoraircraft.

(v)Shallhavebeenstartedandcompletedwithinthe3yearsprecedingtheapplica-

tionforatyperatingendorsement.

(c)Differencestraining

(i)Differencestrainingisthetrainingrequiredinordertocoverthedifferencesbe-

tweentwodifferentaircrafttyperatingsofthesamemanufacturerasdetermined

bytheDGCA.

(ii)Differencestraininghastobedefinedonacase-to-casebasistakingintoaccount

therequirements containedinthisAppendixIIIinrespectofboththeoreticaland

practicalelementsoftyperatingtraining

(iii)Atyperatingshallonlybeendorsedonalicenceafterdifferencestrainingwhen

theapplicantalsocomplieswithoneofthefollowingconditions:

—havingalreadyendorsedonthelicencetheaircrafttyperatingfromwhichthe

differencesarebeingidentified,or

—havingcompletedthetypetrainingrequirementsfortheaircraftfromwhich

thedifferencesarebeingidentified.

2. Aircraft Type training levels

The three levels listed below define the objectives, the depth of training and level of

knowledgethattrainingisintendedtoachieve.

Level 1

Abriefoverviewoftheairframe,systemsandpowerplantsasoutlinedintheSystems

DescriptionSectionoftheAircraftMaintenanceManual/InstructionsforContinuedAir-

worthiness.

Course objectives:Uponcompletionofthecourse,thestudentwillbeableto:

a) provideasimpledescriptionofthewholesubject,usingcommonwordsandex-

amples, using typical terms and identify safety precautions related to the air-

frame,itssystemsandpowerplant;

b) identifyaircraftmanuals,maintenancepractices important to the airframe, its

systemsandpowerplant;

c) definethegenerallayoutoftheaircraft'smajorsystems;

d) definethegenerallayoutandcharacteristicsofthepowerplant;

e) identifyspecialtoolingandtestequipmentusedwiththeaircraft

Level 2

CAR-66


Basicsystemoverviewofcontrols,indicators,principalcomponentsincludingtheirlo-

cationandpurpose,servicingandminortroubleshooting. Generalknowledgeofthethe-

oretical andpracticalaspectsofthesubject

Course objectives:InadditiontotheinformationcontainedintheLevel1,training,at

thecompletionofthisLevel2,trainingthestudentwillbeableto:

(a)understandthetheoreticalfundamentals;applyknowledgeinapracticalmannerus-

ingdetailedprocedures;

(b)recallthesafetyprecautionstobeobservedwhenworkingonorneartheaircraft,

powerplantandsystems;

(c) describe systems andaircraft handling particularly access, power availability and

sources;

(d)identifythelocationsoftheprincipalcomponents;

(e)explainthenormalfunctioningofeachmajorsystem,includingterminologyandno-

menclature;

(f)performtheproceduresforservicingassociatedwiththeaircraftforthefollowing

systems:Fuel,PowerPlants,Hydraulics,LandingGear,Water/Waste,andOxygen;

(g)demonstrateproficiencyinuseofcrewreportsandon-boardreportingsystems(mi-

nortroubleshooting)anddetermineaircraftairworthinesspertheMEL/CDL;

(h)demonstratetheuse,interpretationandapplicationofappropriatedocumentation

includinginstructionsforcontinuedairworthiness,maintenancemanual,illustrated

partscatalogue,etc.

Level 3

Detailed description,operation,component location,removal/installationandbiteand

troubleshootingprocedurestomaintenancemanuallevel.

Course objectives:InadditiontotheinformationcontainedinLevel1andLevel2train-

ing,atthecompletionofLevelIII,thestudentwillbeableto:

(a) demonstrateatheoreticalknowledgeofaircraftsystemsandstructuresandinterre-lationshipswithothersystems,provideadetaileddescriptionofthesubjectusingthe-oretical fundamentals and specific examples and to interpret results from varioussourcesandmeasurementsandapplycorrectiveactionwhereappropriate;

(b) Performsystem,powerplant,componentandfunctionalchecksasspecifiedinthe

maintenancemanual.

CAR-66


(c) demonstrate the use, interpret and apply appropriate documentation includingstructuralrepairmanual,troubleshootingmanual,etc.;

(d) Correlateinformationforthepurposeofmakingdecisionsinrespectoffaultdiag-nosisandrectificationtomaintenancemanuallevel.

(e) Describeproceduresforreplacementofcomponentsuniquetoaircrafttype

3. Aircraft Type training standard Althoughaircrafttypetrainingincludesboththeoreticalandpracticalelements,courses

canbeapprovedforthetheoreticalelement,thepracticalelementorforacombinationof

both.

3.1 Theoretical element

(a) Objective

Oncompletionofatheoreticaltrainingcoursethestudentshallbeabletodemonstrate,to

thelevelsidentifiedintheAppendixIIIsyllabus,thedetailedtheoreticalknowledgeofthe

aircraft's applicable systems, structure, operations, maintenance, repair, and trouble-

shootingaccordingtoapprovedmaintenancedata.Thestudentshallbeabletodemon-

stratetheuseofmanualsandapprovedprocedures,includingtheknowledgeofrelevant

inspectionsandlimitations.

(b) Level of training:

Traininglevelsarethoselevelsdefinedinpoint2above.Afterthefirsttypecoursefor

categoryCcertifyingstaffallsubsequentcoursesneedonlybetolevel1.Duringalevel3

theoreticaltraining,level1and2trainingmaterialmaybeusedtoteachthefullscopeof

thechapterifrequired.However,duringthetrainingthemajorityofthecoursematerial

andtrainingtimeshallbeatthehigherlevel

( c ) Duration:

CAR-66


Thetheoreticaltrainingminimumtuitionhoursarecontainedinthefollowingtable:

Category Hours

Aeroplanes with a maximum take-off mass above 30 000 kg:

B1.1 150

B1.2 120

B2 100

C 30Aeroplanes with a maximum take-off mass equal or less than 30 000 kg and above 5 700

kg:

B1.1 120

B1.2 100

B2 100

C 25Aeroplanes with a maximum take-off mass of 5 700 kg and below(

B1.1 80

B1.2 60

B2 60

C 15Helicopters(2)

B1.3 120

B1.4 100

B2 100

C 25

(1)Fornon-pressurisedpistonengineaeroplanesbelow2000kgMTOMthemin-

imumdurationcanbereducedby50%.

(2)Forhelicoptersingroup2(asdefinedinpoint66.A.42)theminimumduration

canbereducedby30%.

Forthepurposeofthetableabove,atuitionhourmeans60minutesofteachingandex-

cludeanybreaks,examination,revision,preparationandaircraftvisit.Thesehoursapply

onlytotheoreticalcoursesforcompleteaircraft/enginecombinationsaccordingtothe

typeratingasdefinedbytheDGCA.

(d) Justification of course duration:

Trainingcoursescarriedoutinamaintenancetrainingorganisationapprovedinaccord-

ancewithCAR-147andcoursesdirectlyapprovedbytheDGCAshalljustifytheirhourdu-

rationandthecoverageofthefullsyllabusbyatrainingneedsanalysisbasedon:

—thedesignoftheaircrafttype,itsmaintenanceneedsandthetypesofoperation,

—detailedanalysisofapplicablechapters

—seecontentstableinpoint3.1(e)below,

CAR-66


— detailed competency analysis showing that the objectives as stated in point 3.1(a)

abovearefullymet.

Wherethetrainingneedsanalysisshowsthatmorehoursareneeded,courselengthsshall

belongerthantheminimumspecifiedinthetable.

Similarly,tuitionhoursofdifferencescoursesorothertrainingcoursecombinations(such

ascombinedB1/B2courses),andincasesoftheoreticaltypetrainingcoursesbelowthe

figuresgiveninpoint3.1(c)above,theseshallbejustifiedtotheDGCAbythetraining

needsanalysisasdescribedabove.

Inaddition,thecoursemustdescribeandjustifythefollowing:

—Theminimumattendancerequiredtothetrainee,inordertomeettheobjectivesofthe

course.

—Themaximumnumberofhoursoftrainingperday,takingintoaccountpedagogical

andhumanfactorsprinciples.

Iftheminimumattendancerequiredisnotmet,thecertificateofrecognitionshallnotbe

issued.Additionaltrainingmaybeprovidedbythetrainingorganisationinordertomeet

theminimumattendancetime.

( e ) Content:

Asaminimum,theelementsintheSyllabusbelowthatarespecifictotheaircrafttypeshall

becovered.Additionalelementsintroducedduetotypevariations,technologicalchanges,

etc.shallalsobeincluded.Thetrainingsyllabusshallbefocusedonmechanicalandelec-

tricalaspectsforB1personnel,andelectricalandavionicaspectsforB2.

Level Chapters

Aeroplanes Turbine

Aeroplane Piston

Helicopter turbine

Helicopter Piston

Avi-on-ics

B1 C B1 C B1 C B1 C B2

Introduction module:

05 Time limits/maintenance checks

1 1 1 1 1 1 1 1 1

06 Dimensions/Areas (MTOM, etc.)

1 1 1 1 1 1 1 1 1

07 Lifting and Shoring 1 1 1 1 1 1 1 1 1

08 Levelling and weighing 1 1 1 1 1 1 1 1 1

09 Towing and taxiing 1 1 1 1 1 1 1 1 1

10 Parking/mooring, Storing and Return to Service

1 1 1 1 1 1 1 1 1

CAR-66


Level Chapters

Aeroplanes Turbine

Aeroplane Piston

Helicopter turbine

Helicopter Piston

Avi-on-ics


11 Placards and Markings 1 1 1 1 1 1 1 1 1

12 Servicing 1 1 1 1 1 1 1 1 1

20 Standard practices — only type particular

1 1 1 1 1 1 1 1 1

Helicopters

18. Vibration and Noise Anal-ysis( Blade tracking )

– -- – – 3 1 3 1 –

60 Standard Practices Rotor - - - - 3 1 3 1 -

62 Rotors – – – – 3 1 3 1 1

62A Rotors — Monitoring and indicating

_ _ _ _ 3 1 3 1 3

63 Rotor Drives -- -- -- -- 3 1 3 1 1

63A Rotor Drives — Monitor-ing and indicating

-- -- -- -- 3 1 3 1 3

64 Tail Rotor – – – – 3 1 3 1 1

64A Tail rotor — Monitoring and indicating

-- -- -- -- 3 1 3 1 3

65 Tail Rotor Drive -- – – – 3 1 3 1 1

65A Tail Rotor Drive — Mon-

itoring and indicating -- -- -- -- 3 1 3 1 3

66 Folding Blades/Pylon – – – – 3 1 3 1 –

67 Rotors Flight Control -- -- -- -- 3 1 3 1 --

53 Airframe Structure (Heli-

copter) -- -- -- -- 3 1 3 1 --

25 Emergency Flotation

Equipment -- -- -- -- 3 1 3 1 1

Airframe Structure

51 Standard practices and

structures (damage classifica-

tion, assessment and repair)

3 1 3 1 – – – – 1

53 Fuselage 3 1 3 1 – – – – 1

54 Nacelles/Pylons 3 1 3 1 – – – – 1

55 Stabilizers 3 1 3 1 – – – – 1

56 Windows 3 1 3 1 – – – – 1

57 Wings 3 1 3 1 – – – – 1

27A Flight Control Surfaces ( All )

3 1 3 1 – – – – 1

CAR-66


Level Chapters

Aeroplanes Turbine

Aeroplane Piston

Helicopter turbine

Helicopter Piston

Avi-on-ics


52 Doors 3 1 3 1 – – – – 1

Zonal & Station Identification Systems

1 1 1 1 1 1 1 1 1

Airframe Systems

21 Air Conditioning 3 1 3 1 3 1 3 1 3

21A Air Supply 3 1 3 1 1 3 3 1 2

21B Pressurization 3 1 3 1 3 1 3 1 3

21C Safety & Warning Devices 3 1 3 1 3 1 3 1 3

22 Autoflights 2 1 2 1 2 1 2 1 3

23 Communication 2 1 2 1 2 1 2 1 3

24 Electrical Power 3 1 3 1 3 1 3 1 3

25 Equipment & Furnishings 3 1 3 1 3 1 3 1 1

25A Electronic Emergency Equip. & Cabin Entertainment Equipment

1 1 1 1 1 1 1 1 3

26 Fire Protection 3 1 3 1 3 1 3 1 3

27 Flight Controls 3 1 3 1 3 1 3 1 2

27A Sys. Operation: Electri-cal/Fly-by-Wire

3 1 – – – – – – 3

28 Fuel Systems 3 1 3 1 3 1 3 1 2

28A Fuel Systems — Monitor-ing and indication

3 1 3 1 3 1 3 1 3

29 Hydraulic Power 3 1 3 1 3 1 3 1 2

29A Hydraulic Power — Mon-itoring and indicating

3 1 3 1 3 1 3 1 3

30 Ice & Rain Protection 3 1 3 1 3 1 3 1 3

31 Indicating/Recording Sys-tems

3 1 3 1 3 1 3 1 3

31A Instrument Systems 3 1 3 1 3 1 3 1 3

32 Landing Gear 3 1 3 1 3 1 3 1 2

32A Landing Gear — Monitor-ing and indicating

3 1 3 1 3 1 3 1 3

33 Lights 3 1 3 1 3 1 3 1 3

34 Navigation 2 1 2 1 2 1 2 1 3

35 Oxygen 3 1 3 1 – – – – 2

36 Pneumatic 3 1 3 1 3 1 3 1 2

36A Pneumatic — Monitoring and indicating

3 1 3 1 3 1 3 1 3

CAR-66


Level Chapters

Aeroplanes Turbine

Aeroplane Piston

Helicopter turbine

Helicopter Piston

Avi-on-ics


37 Vacuum 3 1 3 1 3 1 3 1 2

38 Water/Waste 3 1 3 1 -- -- -- -- 2

41 Water Ballast 3 1 3 1 -- -- -- -- 1

42 Integrated modular avion-ics

2 1 2 1 2 1 2 1 3

44 Cabin Systems 2 1 2 1 2 1 2 1 3

45 On-board Maintenance Systems

3 1 3 1 3 1 – – 3

46 Information Systems 2 1 2 1 2 1 2 1 3

50 Cargo and Accessory Com-partments

3 1 3 1 3 1 3 1 1

Turbine Engines:

70 Standard Practices — En-gines,

3 1 – – 3 1 – – 1

70A constructional arrange-ment and operation (Installa-tion Inlet, Compressors, Com-bustion Section, Turbine Sec-tion, Bearings and Seals, Lu-brication Systems).

3 1 -- -- 3 1 -- -- 1

70B Engine Performance 3 1 – – 3 1 – – 1

71 Powerplant 3 1 – – 3 1 – – 1

72 Engine Turbine/Turbo Prop/Ducted Fan/Unducted fan

3 1 -- -- 3 1 -- -- 1

73 Engine Fuel and Control 3 1 – – 3 1 – – 1

75 Air 3 1 – – 3 1 – – 1

76 Engine controls 3 1 – – 3 1 – – 1

78 Exhaust 3 1 – – 3 1 – – 1

79 Oil 3 1 – – 3 1 – – 1

80 Starting 3 1 – – 3 1 – – 1

82 water injection 3 1 – – 3 1 – – 1

83 Accessory Gear Boxes 3 1 – – 3 1 – – 1

84 Propulsion Augmentation 3 1 – – 3 1 – – 1

73A FADEC 2 1 – – 2 1 – – 3

74 Ignition 3 1 – – 3 1 – – 3

77 Engine Indicating Systems 3 1 – – 3 1 – – 3

CAR-66


Level Chapters

Aeroplanes Turbine

Aeroplane Piston

Helicopter turbine

Helicopter Piston

Avi-on-ics


49 Auxiliary Power Units (APUs)

3 1 – – -- -- – – 2

Piston Engines:

70 Standard Practices — En-gines

-- -- 3 1 – – 3 1 1

70A Constructional arrangement and operation (Installation, Car-burettors, Fuel injection sys-tems, Induction, Exhaust and Cooling Systems, Supercharging/ Turbocharging, Lubrication Sys-tems).

– – 3 1 -- -- 3 1 1

70B Engine Performance _ _ 3 1 -- -- 3 1 1

71 Powerplant – – 3 1 – – 3 1 1

73 Engine Fuel and Control – – 3 1 – – 3 1 1

76 Engine Control – – 3 1 – – 3 1 1

79 Oil – – 3 1 – – 3 1 1

80 Starting – – 3 1 – – 3 1 1

81 Turbine -- -- 3 1 -- -- 3 1 1

82 Water Injections – – 3 1 – – 3 1 1

83 Accessory Gear Boxes – – 3 1 – – 3 1 1

84 Propulsion Augmentation – – 3 1 – – 3 1 1

73A FADEC – – 3 1 – – 3 1 3

74 Ignition – – 3 1 – – 3 1 3

77 Engine Indication Systems – – 3 1 – – 3 1 3

Propellers:

60A Standard Practices — Propeller

3 1 3 1 – – – – 1

61 Propellers/Propulsion 3 1 3 1 – – – – 1

61APropeller Construction 3 1 3 1 -- -- -- -- 1

61B Propeller Pitch Control 3 1 3 1 – – – – –

61C Propeller Synchronizing 3 1 3 1 – – – – 1

61D Propeller Electronic con-trol

2 1 2 1 – – – – 3

61E Propeller Ice Protection 3 1 3 1 – – – – –

61 F Propeller Maintenance 3 1 3 1 – – – – 1

CAR-66


(f)MultimediaBasedTraining(MBT)methodsmaybeusedtosatisfythetheoreticaltrain-

ingelementeitherintheclassroomorinavirtualcontrolledenvironmentsubjecttothe

acceptanceoftheDGCAapprovingthetrainingcourse.

3. 2Practical element

a) Objective:

Theobjectiveofpracticaltrainingistogaintherequiredcompetenceinperformingsafe

maintenance, inspections and routine work according to the maintenance manual and

otherrelevantinstructionsandtasksasappropriateforthetypeofaircraft,forexample

troubleshooting,repairs,adjustments,replacements,riggingandfunctionalchecks.Itin-

cludestheawarenessoftheuseofalltechnicalliteratureanddocumentationfortheair-

craft,theuseofspecialist/specialtoolingandtestequipmentforperformingremovaland

replacementofcomponentsandmodulesuniquetotype,includinganyon-wingmainte-

nanceactivity.

b) Content:

Atleast50%ofthecrosseditemsinthetablebelow,whicharerelevanttotheparticular

aircrafttype,shallbecompletedaspartofthepracticaltraining.

Taskscrossedrepresentsubjectsthatareimportantforpracticaltrainingpurposestoen-

surethattheoperation,function,installationandsafetysignificanceofkeymaintenance

tasksisadequatelyaddressed;particularlywherethesecannotbefullyexplainedbythe-

oreticaltrainingalone.Althoughthelistdetailstheminimumpracticaltrainingsubjects,

otheritemsmaybeaddedwhereapplicabletotheparticularaircrafttype.

Taskstobecompletedshallberepresentativeoftheaircraftandsystemsbothincomplex-

ityandinthetechnicalinputrequiredtocompletethattask.Whilerelativelysimpletasks

maybeincluded,othermorecomplextasksshallalsobeincorporatedandundertakenas

appropriatetotheaircrafttype.

Glossary of table : LOC: Location; FOT: Functional / Operation Test; SGH : Service and Ground; Han-dling; R/I : Removal / Installation; MEL: Minimum Equipment List; TS: Trouble Shooting

Chapters B1/B2 B1 B2

LOC FOT S

GH R/I MEL TS FOT

SGH

R/I MEL

TS

Introduction module:

05 Time limits/maintenance checks X/X -- -- -- -- -- -- -- -- -- -

06 Dimensions/Areas (MTOM, etc.) X/X -- -- -- -- -- -- -- -- -- -

07 Lifting and Shoring X/X -- -- -- -- -- -- -- -- -- -

CAR-66



LOC FOT S

GH R/I MEL TS FOT

SGH

R/I MEL

TS

08 Levelling and weighing X/X -- X -- -- -- -- X -- -- -

09 Towing and Taxing X/X -- X -- -- -- -- X -- -- -

10 Parking/Mooring storing and return to service

X/X -- X -- -- -- -- X -- -- -

11 Playcard and marking X/X -- -- -- -- -- -- -- -- -- -

12 Servicing X/X -- X -- -- -- -- X -- -- -

20 Standard practices –only type partic-ular

X/X -- X -- -- -- -- X -- -- -

Helicopters:

18 Vibration and Noise Analysis (Blade tracking)

X/-- -- -- -- -- X -- -- -- -- -

60 Standard Practices Rotor — only type specific

X/X -- X -- -- -- -- X -- -- -

62 Rotors X/-- -- X X -- X -- -- -- -- -

62A Rotors — Monitoring and indicating X/X X X X X X -- -- X -- x

63 Rotor Drives X/-- X -- -- -- X -- -- -- -- -

63A Rotor Drives — Monitoring and indi-cating

X/X X -- X X X -- -- X -- X

64 Tail Rotor X/-- -- X -- -- X -- -- -- -- -

64A Tail rotor -Monitoring and indicating X/X X -- X X X -- -- X -- X

65 Tail Rotor Drive X/-- X -- -- -- X -- -- -- -- -

65A Tail Rotor Drive — Monitoring and indicating

X/X X -- X X X -- -- X -- X

66 Folding Blades/Pylon X/-- X X -- -- X -- -- -- -- -

67 Rotors Flight Control X/-- X X -- X X -- -- -- -- -

53 Airframe Structure (Helicopter) Note: covered under Airframe structures

25 Emergency Flotation Equipment X/X X X X X X X X -- -- -

Airframe structures:

51 Standard Practices and Structures (damage classification, assessment and repair

53 Fuselage X/-- -- -- -- -- X -- -- -- -- -

54 Nacelles/Pylons X/-- -- -- -- -- -- -- -- -- -- -

CAR-66



LOC FOT S

GH R/I MEL TS FOT

SGH

R/I MEL

TS

55 Stabilisers X/-- -- -- -- -- -- -- -- -- -- -

56 Windows X/-- -- -- -- -- X -- -- -- -- -

57 Wings X/-- -- -- -- -- -- -- -- -- -- -

27A Flight Control Surfaces X/-- -- -- -- -- X -- -- -- -- -

52 Doors X/X X X -- -- -- -- X -- -- -

Airframe systems:

21 Air Conditioning X/X X X -- X X X X -- X X

21A Air Supply X/X X -- -- -- -- X -- -- -- -

21B Pressurisation X/X X -- -- X X X -- -- X X

21C Safety and warning Devices X/X -- X -- -- -- -- X -- -- -

22 Autoflight X/X -- -- -- X -- X X X X X

23 Communications X/X -- X -- X -- X X X X X

24 Electrical Power X/X X X X X X X X X X X

25 Equipment and Furnishings X/X X X X -- -- X X X -- -

25A Electronic Equipment including emergency equipment

X/X X X X -- -- X X X -- -

26 Fire Protection X/X X X X X X X X X X X

27 Flight Controls X/X X X X X X X -- -- -- -

27A Sys. Operation: Electrical/Fly-by- Wire

X/X X X X X -- X -- X -- X

28 Fuel Systems X/X X X X X X X X -- X -

28A Fuel Systems — Monitoring and in-dicating

X/X X -- -- -- -- X -- X -- X

29 Hydraulic Power X/X X X X X X X X -- X -

29A Hydraulic Power — Monitoring and indicating

X/X X -- X X X X -- X X X

30 Ice and Rain Protection X/X X X -- X X X X -- X X

31 Indicating/Recording Systems X X/X X X X X X X X X X X

CAR-66



LOC FOT S

GH R/I MEL TS FOT

SGH

R/I MEL

TS

31A Instrument Systems X/X X X X X X X X X X X

32 Landing Gear X/X X X X X X X X X X -

32A Landing Gear — Monitoring and in-dicating

X/X X -- X X X X -- X X X

33 Lights X/X X X -- X -- X X X X -

34 Navigation X/X -- X -- X -- X X X X X

35 Oxygen X/-- X X X -- -- X X -- -- -

36 Pneumatic X/-- X -- X X X X -- X X X

36A Pneumatic — Monitoring and indi-cating

X/X X X X X X X X X X X

37 Vacuum X/-- X -- X X X -- -- -- -- -

38 Water/Waste X/-- X X -- -- -- X X -- -- -

41 Water Ballast X/-- -- -- -- -- -- -- -- -- -- -

42 Integrated modular avionics X/X -- -- -- -- -- X X X X X

44 Cabin Systems X/X -- -- -- -- -- X X X X X

45 On-Board Maintenance System (or covered in 31)

X/X X X X X X X X X X X

46 Information Systems X/X -- -- -- -- -- X -- X X X

50 Cargo and Accessory Compartments X/X -- X -- -- -- -- -- -- -- -

Turbine/Piston Engine Module:

70 Standard Practices — Engines — only type particular

--- -- X -- -- -- -- X -- -- -

70A Constructional arrangement and op-eration (Installation Inlet, Compressors, Combustion Section, Turbine Section, Bearings and Seals, Lubrication Systems)

X/X -- -- -- -- -- -- -- -- - -

Turbine engines:

70B Engine Performance -- -- -- -- -- X -- -- -- -- -

71 Power Plant X/-- X X -- -- -- -- X -- -- -

72 Engine Turbine/Turbo Prop/Ducted Fan/ Unducted fan

X/-- -- -- -- -- -- -- -- -- -- -

73 Engine Fuel and Control X/X X -- -- -- -- -- -- -- -- -

CAR-66



LOC FOT S

GH R/I MEL TS FOT

SGH

R/I MEL

TS

73A FADEC Systems X/X X -- X X X X -- X X X

74 Ignition X/X X -- -- -- -- X -- -- -- -

75 Air X/-- -- -- X -- X -- -- -- -- -

76 Engine Controls X/-- X -- -- -- X -- -- -- -- -

77 Engine Indicating X/X X -- -- X X X -- -- X X

78 Exhaust X/-- X -- -- X -- -- -- -- -- -

79 Oil X/-- -- X X -- -- -- -- -- -- -

80 Starting X/-- X -- -- X X -- -- -- -- -

82 Water Injection X/-- X -- -- -- -- -- -- -- -- -

83 Accessory Gearboxes X/-- -- X -- -- -- -- -- -- -- -

84 Propulsion Augmentation X/-- X -- -- -- -- -- -- -- -- -

Auxiliary Power Units (APUs):

49 Auxiliary Power Units (APUs) X/-- X X -- -- X -- -- -- -- -

Piston Engines:

70 Standard Practices — Engines — only type particular

-- -- X -- -- -- -- X -- -- -

70A Constructional arrangement and op-eration (Installation Inlet, Compressors, Combustion Section, Turbine Section, Bearings and Seals, Lubrication Systems)

X/X -- -- -- -- -- -- -- -- - -

70B Engine Performance -- -- -- -- -- X -- -- -- -- -

71 Power Plant X/-- X X -- -- -- -- X -- -- -

73 Engine Fuel and Control X/X X -- -- -- -- -- -- -- -- -

73A FADEC Systems X/X X -- X X X X X X X X

74 Ignition X/X X -- -- -- -- X -- -- -- -

76 Engine Controls X/-- X -- -- -- X -- -- -- -- -

77 Engine Indicating X/X X -- -- X X X -- -- X X

78 Exhaust X/-- X -- -- X X -- -- -- -- -

79 Oil X/-- -- X X -- -- -- -- -- -- -

80 Starting X/-- X -- -- X X -- -- -- -- -

CAR-66



LOC FOT S

GH R/I MEL TS FOT

SGH

R/I MEL

TS

81 Turbines X/-- X X X -- X -- -- -- -- -

82 Water Injection X/-- X -- -- -- -- -- -- -- -- -

83 Accessory Gearboxes X/-- -- X X -- -- -- -- -- -- -

84 Propulsion Augmentation X/-- X -- -- -- -- -- -- -- -- -

Propellers:

60A Standard Practices — Propeller -- -- -- X -- -- -- -- -- -- -

61 Propellers/Propulsion X/X X X -- X X -- -- -- -- -

61A Propeller Construction X/-- -- X -- -- -- -- -- -- -- -

61B Propeller Pitch Control X/-- X -- X X X -- -- -- -- -

61C Propeller Synchronising X/-- X -- -- -- X -- -- -- X -

61D Propeller Electronic control X/X X X X X X X X X X X

61E Propeller Ice Protection X/-- X -- X X X -- -- -- -- -

61F Propeller Maintenance X/X X X X X X X X X X X

4. Type training examination and assessment standard

4.1.Theoreticalelementexaminationstandard

Afterthetheoreticalportionoftheaircrafttypetraininghasbeencompleted,awritten

examinationshallbeperformed,whichshallcomplywiththefollowing:

(a)Formatoftheexaminationisofthemulti-choicetype.Eachmulti-choicequestionshall

have3alternativeanswersofwhichonlyoneshallbethecorrectanswer.Thetotal

timeisbasedonthetotalnumberofquestionsandthetimeforansweringisbased

uponanominalaverageof90secondsperquestion.

(b)Theincorrectalternativesshallseemequallyplausibletoanyoneignorantofthesub-

ject.Allthealternativesshallbeclearlyrelatedtothequestionandofsimilarvocabu-

lary,grammaticalconstructionandlength.

(c)Innumericalquestions,theincorrectanswersshallcorrespondtoproceduralerrors

CAR-66


suchastheuseofincorrectsense(+versus-)orincorrectmeasurementunits.They

shallnotbemererandomnumbers.

(d)Thelevelofexaminationforeachchapter(1)shallbetheonedefinedinpoint2‘Air-

crafttypetraininglevels’.However,theuseofalimitednumberofquestionsatalower

levelisacceptable.

(e)Theexaminationshallbeoftheclosedbooktype.Noreferencematerialispermitted.

AnexceptionwillbemadeforthecaseofexaminingaB1orB2candidate'sabilityto

interprettechnicaldocuments.

(f) Thenumberofquestionsshallbeatleast1questionperhourofinstruction.Thenum-

berofquestionsforeachchapterandlevelshallbeproportionateto:

—theeffectivetraininghoursspentteachingatthatchapterandlevel,

—thelearningobjectivesasgivenbythetrainingneedsanalysis.

DGCAwillassessthenumberandthelevelofthequestionswhenapprovingthecourse.

(g)Theminimumexaminationpassmarkis75%.Whenthetypetrainingexaminationis

splitinseveralexaminations,eachexaminationshallbepassedwithatleasta75%

mark.Inordertobepossibletoachieveexactlya75%passmark,thenumberofques-

tionsintheexaminationshallbeamultipleof4.

(h)Penaltymarking(negativepointsforfailedquestions)isnottobeused.

(i)Endofmodulephaseexaminationscannotbeusedaspartofthefinalexamination

unlesstheycontainthecorrectnumberandlevelofquestionsrequired.

4.2.Practicalelementassessmentstandard.

Afterthepracticalelementoftheaircrafttypetraininghasbeencompleted,anassess-

mentmustbeperformed,whichmustcomplywiththefollowing:

(a)Theassessmentshallbeperformedbydesignatedassessorsappropriatelyqualified.

(b)Theassessmentshallevaluatetheknowledgeandskillsofthetrainee.

5. Type examination standard

Typeexaminationshallbeconductedbytrainingorganisationsappropriatelyapproved

underCAR-147orbytheDGCA

CAR-66


Theexaminationshallbeoral,writtenandorpracticalassessmentbased,oracombina-

tionthereofanditshallcomplywiththefollowingrequirements:

(a)Oralexaminationquestionsshallbeopen.

(b)Writtenexaminationquestionsshallbeessaytypeormulti-choicequestions.

(c)Practicalassessmentshalldetermineaperson'scompetencetoperformatask.

(d)Examinationsshall be on a sample of chapters (1) drawn from point 3 type train-

ing/examinationsyllabus,attheindicatedlevel.

(e)Theincorrectalternativesshallseemequallyplausibletoanyoneignorantofthesub-

ject.Allofthealternativesshallbeclearlyrelatedtothequestionandofsimilarvocab-

ulary,grammaticalconstructionandlength.

(f)Innumericalquestions,theincorrectanswersshallcorrespondtoproceduralerrors

suchascorrectionsappliedinthewrongsenseorincorrectunitconversions:theyshall

notbemererandomnumbers.

(g)Theexaminationshallensurethatthefollowingobjectivesaremet:

1.Properlydiscusswithconfidencetheaircraftanditssystems.

2.Ensuresafeperformanceofmaintenance,inspectionsandroutineworkaccording

tothemaintenancemanualandotherrelevantinstructionsandtasksasappropriate

forthetypeofaircraft,forexampletroubleshooting,repairs,adjustments,replace-

ments,riggingandfunctionalcheckssuchasenginerun,etc.,ifrequired.

3.Correctlyusealltechnicalliteratureanddocumentationfortheaircraft.

4.Correctlyusespecialist/specialtoolingandtestequipment,performremovalandre-

placement of components and modules unique to type, including any on-wing

maintenanceactivity

(h)Thefollowingconditionsapplytotheexamination:

1. Themaximumnumberofconsecutiveattemptsisthree.Furthersetsofthreeattempts

areallowedwitha1yearwaitingperiodbetweensets.Awaitingperiodof30daysis

requiredafterthefirstfailedattemptwithinoneset,andawaitingperiodof60daysis

requiredafterthesecondfailedattempt.

TheapplicantshallconfirminwritingtotheDGCAthenumberanddatesofattempts

CAR-66


duringthelastyear..DGCAisresponsibleforcheckingthenumberofattemptswithin

theapplicabletimeframes.

2.Thetypeexaminationshallbepassedandtherequiredpracticalexperienceshallbe

completedwithinthe3yearsprecedingtheapplicationfortheratingendorsementon

theaircraftmaintenancelicence.

3.Typeexaminationshallbeperformedwithatleastoneexaminerpresent.Theexam-

iner(s)shallnothavebeeninvolvedintheapplicant'straining.

(i)Awrittenandsignedreportshallbemadebytheexaminer(s)toexplainwhythecan-

didatehaspassedorfailed.

6. On the Job Training

OntheJobTraining(OJT)shallbeapprovedbytheDGCA.

Itshallbeconductedatandunderthecontrolofamaintenanceorganisationappropri-

atelyapprovedforthemaintenanceoftheparticularaircrafttypeandshallbeassessedby

designatedassessorsappropriatelyqualified.

Itshallhavebeenstartedandcompletedwithinthe3yearsprecedingtheapplicationfor

atyperatingendorsement.

(a) Objective:

TheobjectiveofOJTistogaintherequiredcompetenceandexperienceinperformingsafe

maintenance.

Content:

OJTshallcoveracrosssectionoftasksacceptabletotheDGCA.TheOJTtaskstobecom-

pletedshallberepresentativeoftheaircraftandsystemsbothincomplexityandinthe

technicalinputrequiredtocompletethattask.Whilerelativelysimpletasksmaybein-

cluded,othermorecomplexmaintenancetasksshallalsobeincorporatedandundertaken

asappropriatetotheaircrafttype.

Eachtaskshallbesignedoffbythestudentandcountersignedbyadesignatedsupervisor.

Thetaskslistedshallrefertoanactualjobcard/worksheet,etc.

ThefinalassessmentofthecompletedOJTismandatoryandshallbeperformedbyades-

ignatedassessorappropriatelyqualified.

ThefollowingdatashallbeaddressedontheOJTworksheets/logbook:

CAR-66


1.NameofTrainee;

2.DateofBirth;

3.ApprovedMaintenanceOrganisation;

4.Location;

5.Nameofsupervisor(s)andassessor,(includinglicencenumberifapplicable);

6.Dateoftaskcompletion;

7.Descriptionoftaskandjobcard/workorder/techlog,etc.;

8.Aircrafttypeandaircraftregistration;

9.Aircraftratingappliedfor.

InordertofacilitatetheverificationbytheDGCA,demonstrationoftheOJTshallconsist

of i)detailedworksheets/logbookand(ii)acompliancereportdemonstratinghowthe

OJTmeetstherequirementofthisPart.

CAR-66


Appendix IV - Experience requirements for extending a CAR-66

AircraftMaintenanceEngineer’sLicence

Thetablebelowshowstheexperiencerequirementsforaddinganewcategoryorsub-

categorytoanexistingCAR-66licence.

Theexperiencemustbepracticalmaintenanceexperienceonanoperatingaircraftinthe

subcategoryrelevanttotheapplication.

Theexperienceistobesignedbythepostholderonlyandthisprocedureistobere-

flectedinMOE

Theexperiencerequirementwillbereducedby50%iftheapplicanthascompletedan

approvedCAR-147courserelevanttothesubcategory

To: A1 A2 A3 A4 B1.1 B1.2 B1.3 B1.4 B2

From - - - - - - - - -

A1 X6

months6

months6

months2years

6months

2years 1year 2years

A2 6

months X6

months6

months2years

6months

2years 1year 2years

A3 6

months6

months

X6

months2years 1year 2years

6months

2years

A4 6

months6

months6

months

X2years 1years 2years

6months

2years

B1.1 NONE6

months6

months6

months

X6

months6

months6

months1year

B1.2 6

monthsNONE

6months

6months

2years

X2years

6months

2years

B1.3 6

months6

monthsNONE

6months

6months

6months

X

6months

1year

B1.4 6

months6

months6

monthsNONE 2years

6months

2years X 2years

B2 6

months6

months6

months6

months1year 1year 1year 1year X

CAR-66


AppendixV–ApplicationsandFormats

APPLICATION FOR INITIAL ISSUE OF CAR- 66

AIRCRAFT MAINTENANCE ENGINEER’S LICENCE

DGCA INDIA

CA Form 19-01

Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Fields

marked with an asterisk * are mandatory and must be completed in all cases. Use Date Format – DD-MM-YYYY

1. PERSONAL DETAILS

Affix recent pass-port size photo graph duly at-tested on the

front side

CEO Computer No.

*Name in full

*Date of birth

* Nationality

*Educational Qualification

* Details of Fees Paid …………………………………………….............................

*Permanent address…………………………………………….................................……………………………………………………………

…………………………………………………………………………………………………………………………PIN Code................................

*Address for Communication (if different from above)……………………….....................................................

………………………………………………………………………………………………………….……………….PIN Code................................

Applicant Contact Phone Number ………………………….................. E-mail…….………………………………………………….

Name of the Current Employer………………………………………………………………………………………………………………………

Contact Phone Number of Employer ……………………….................. E-mail…….…………………………………………………

2. *APPLICATION

I wish to apply for initial CAR-66 Aircraft Maintenance Engineer’s License as indicated and confirm that the in-

formation contained in this form was correct at the time of application (Specify the category A1,A2,A3,A4..

B1.1,B1.2,1.B1.3, B1.4, B2, C and required type ratings as per Appendix I to AMC of CAR – 66)

Category/Sub-category of License applied for A B

Mechanical

Avionic

3. *DETAILS OF CREDIT SOUGHT

I wish to claim the following credits (if applicable) Please enclose all relevant certificates:

Experience credit by virtue of passing approved aircraft maintenance training/Engineering degree examination/

defence experience..……………………………………………………………………………………………………………………

Examination credit due equivalent exam certificates......................................................................................

CAR-66


4. *SUMMARY OF EXPERIENCE - ( Attach additional sheet indicating detail of practical experience obtained in cross representation section of maintenance task as per Appendix-II to AMC of CAR 66 )

Date Aircraft Engine(s) and

/or Equipment Organisation Description of Work

From To

5.* Details of basic knowledge certificate if any issued by CEO/DGCA

Category Sub-category Modules Passed

5a.* Details of Type Rating courses certificates

Aircraft Type / Series Engine Type course approval details

5b. *Details of skill test passed

Aircraft Type / Series Date of Exam Name of DGCA office that con-

ducted the test

*Relevant certificates/documents required to be submitted as enclosures in Section 7

6. PHYSICAL DISABILITY / DISORDER

Known Physical disability or disor-

der

7.*DECLARATION

I hereby confirm that: i) I apply for initial issue of CAR-66 Aircraft Maintenance Engineer’s Licence as indicated and confirm that the information contained in this form was correct at the time of application. ii) I never had a CAR 66 AME Licence issued which was revoked or suspended by DGCA iii) I am not in possession of any other AME Licence issued by DGCA. iv) I did not apply earlier to the office of DGCA for issue of my AME Licence and the request was not turned down.

PLACE SIGNATURE

DATE NAME

CAR-66


Instruction and Checklist

CHECKLIST 8.DETAILS OF ENCLOSURES

Enclo-sure No.

Enclosure Page No.

DGCA Re-

marks

Sat/Unsat

Certified true copy proof of Date of Birth certificate I

Certified true copy of 10+2 with Physics, Chemistry, Mathematics or equivalent II

Certified true copy of Passport or any photo identity card issued by the Govern-ment

III

Certified true copy of Course completion from approved aircraft maintenance training organization / Degree in Engineering certificate if applicable / Defence experience certificate and organisation approval certificate

IV

Certified true copies of basic knowledge examination result sheet / certificate if any issued by CEO

V

Module No. Session No. passed

Roll No. - - -

3. Electrical Fundamentals V (3)

4. Electronic Fundamental V (4)

5.Digital Techniques/ Electronic instrument Sys-tems

V (5)

6. Materials & Hardwares V (6)

7. Maintenance Practices V (7)

8. Basic Aerodynamics V (8)

9. Human Factors V (9)

10. Aviation Legislation V (10)

11A. Turbine Engine Aeroplane Aerodynamics, Structures and Systems

V (11A)

11B. Piston Engine Aeroplane Aerodynamics, Structures and Systems

V (11B)

12. Helicopter Aerodynamics, Structures and Sys-tems

V (12)

13. Aircraft Aerodynamics, Structures and Sys-tems

V (13)

14. Propulsion V (14)

15. Gas Turbine Engine V (14)

16. Piston Engine V (16)

17. Propeller V (17)

Type course examination result sheet, course completion certificate and organi-sation approval certificate.

VI

Certified true copy of skill test result VII

Certified true copies of Logbook / Work records on CA form 19-10 VIII

Medical fitness certificate issued by MBBS doctor on CA form 19-06 IX

Three copies of the recent photographs ( Stamp Size ) with the name of the ap-plicant on the back side

Fees as specified in Rule 62

CAR-66


INSTRUCTION TO CA FORM 19-01 It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant,

issue, renewal or extension of any certificate, licence, approval, permission or other document. Persons doing so render

themselves liable, to administrative/legal action as per Aircraft Rule 1937. Further the licence is liable for revocation /

cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Li-

cence.

Please refer to current notification for details of fees required. All original documents if required to be submitted,

will be returned through the self addressed cover affixed with necessary postal stamp (Speed post) provided by the ap-

plicant.

Completed application with the checklist should be posted along with the required documentation to: The Direc-

torate General of Civil Aviation, Opposite Safdarjung Airport, New Delhi 110003

Notes: Having clear concise supporting data will enable DGCA to issue licences more effectively and with less risk

of errors or rejections. DGCA will not contact you for clarification of details on applications and therefore it is most im-

portant that you have the correct information before applying.

In order that DGCA can process the licence application as quickly as possible, it is important that all sections marked

with an asterisk on the application form are completed and the required supporting documentats enclosed. Please note

failure to submit a correctly completed application form and the required documentation will lead to the rejection of the

application and the fees submitted will be utilized towards processing the application

Section 2: Indicate what type of licence you are applying for indicating Airframe or Engine as per Appendix- I to AMC of

CAR-66

Section 3: Credit claimed for exemptions from passing module or experience.

Section 4: This section is required for DGCA record purposes and should provide a brief summary of experience applicable

to your application. You will still need to submit detailed maintenance experience records in addition to this information,

please refer to CAR-66.A.25 and CAR-66.A.30. The detail of experience should indicate practical experience obtained in

cross representation section of Maintenance task as per Appendix- II to AMC of CAR-66.

Section 5: Indicate the subject modules passed or basic knowledge certificate issued by CEO (DGCA)

Section 5a: Indicate details of type rating courses completed for covering aeroplane/engine/helicopter.

Section 5b: Indicate details of name of the DGCA office conducted the skill test.

Section 6: State the details of existing known physical disability or disorder

Section 7: By signing the declaration you are confirming that all of the information is correct and true.

Section 8: Assign annexure number as indicated and continuous page numbers to the enclosures and indicate it under

column 3 against each item

CAR-66


APPLICATION FOR EXTENSION OF CAR- 66

AIRCRAFT MAINTENANCE ENGINEER’S LICENCE

DGCA INDIA

CA Form 19-02

Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance

notes. Fields marked with an asterisk * are mandatory and must be completed in all cases. Use Date Format –

DD-MM-YYYY

1. PERSONAL DETAILS

*Name in full Computer No.

*AME LICENCE No.

*Fees Paid

Permanent address…………………………. …………………………………………………..…………………….................................……

…………………………………………………………………………………………………………………………PIN Code................................

Address for Communication (if different from above)……………………….....................................................

………………………………………………………………………………………………………….……………….PIN Code................................

Applicant Contact Phone Number ……………………….................. E-mail…….………………………………………………………

Name of the Current Employer………………………………………………………………………………………………………………………..

Contact Phone Number of Employer……………………….................. E-mail…….………………………………………………….

2. *APPLICATION

I wish to apply for extension of CAR-66 Aircraft Maintenance Engineer’s License as indicated and confirm that

the information contained in this form was correct at the time of application ( Specify the category

A1,A2,A3,A4.. B1.1,B1.2,1.B1.3, B1.4, B2, C and required type ratings as per Appendix- I to AMC of CAR – 66)


Mechanical

Avionic

3. *DETAILS OF CREDIT SOUGHT

I wish to claim the following credits (if applicable) Please enclose all relevant certificates:

Experience credit by virtue of passing approved aircraft maintenance training/defence experi-

ence..………………………………………………………………………………………………………………………………………………….

Examination credit due equivalent exam certificates...............................................................................

4. *SUMMARY OF EXPERIENCE - ( Attach additional sheet indicating detail of practical experience obtained in cross representation section of maintenance task as per Appendix-II to AMC of CAR 66 )

Date Aircraft Engine(s) and

/or Equipment Organisation Description of Work

From To

CAR-66


5.* Details of basic knowledge certificate if any issued by CEO/DGCA

Category Sub-category Modules Passed

5a.* Details of Type Rating courses certificates

Aircraft Type / Series Engine Type course approval details

5b. *Details of skill test passed

Aircraft Type / Series Date of Exam Name of DGCA office that con-

ducted the test


6. PHYSICAL DISABILITY / DISORDER

Known Physical disability or disorder

7.*DECLARATION

I hereby confirm that: i) I apply for extension of CAR-66 Aircraft Maintenance Engineer’s Licence as indicated and confirm that the information contained in this form was correct at the time of application. ii) I never had a CAR 66 AME Licence issued which was revoked or suspended by DGCA iii) I am not in possession of any other AME Licence issued by DGCA. iv) I did not apply earlier to the office of DGCA for extension of my AME Licence and the request was not turned down.

PLACE SIGNATURE

DATE NAME

CAR-66


INSTRUCTION AND CHECKLIST

8. CHECKLIST TO CA FORM 19-02

DETAILS OF ENCLOSURES

Enclo-sure No.

Enclo-sure Page No.

DGCA Re-

marks

Sat/Unsat

Original CAR-66 Aircraft Maintenance Engineer’s licence I

Certified true copies of basic knowledge examination result sheet / certifi-cate issued by CEO

II

Certified true copy of Passport or any photo identity card issued by the Government

III

Module No Session No. passed Roll No.

IV(a)

IV(b)

IV(c)

Type course examination result sheet, course completion certificate and organisation approval certificate

V

Certified true copy of skill test and oral cum practical examination VI

Certified true copies of Logbook / Work records on CA form 19-10

Fees

INSRUCTION TO CA FORM 19-02

It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, issue, renewal

or extension of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable to adminis-

trative/legal actions as per Aircraft Rules 1937. Further the licence is liable for revocation / cancellation / suspension or permanently

makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence.

Please refer to current notification for details of fees required. All original documents if required to be submitted, will be returned

through the self addressed cover affixed with necessary postal stamp (Speed post) provided by the applicant.

Completed application with the checklist should be posted along with the required documentation to the respective Regional /

Sub-Regional Airworthiness Office

Notes: Having clear concise supporting data will enable Regional / sub-regional offices of DGCA to extend the licences more ef-

fectively and with less risk of errors or rejections. DGCA office will not contact you for clarification of details on applications and therefore

it is most important that you have the correct information before applying.

In order that DGCA can process the licence application as quickly as possible, it is important that all sections marked with an asterisk on

the application form are completed and the required supporting documentation enclosed. Please note failure to submit a correctly

completed application form and the required documentation will lead to the rejection of the application and the fees submitted will be

utilized towards processing the application.

Section 2: Indicate what type of licence you are applying for and indicate Airframe -Engine combination as per Appendix- I to AMC of

CAR 66

Section 3: credit claimed for exemptions from passing module or experience.

Section 4: This section is required for DGCA record purposes and should provide a brief summary of experience applicable to your ap-

plication. You will still need to submit detailed maintenance experience records in addition to this information, please refer to CAR-

66.A.25 and CAR-66.A.30. The detail of experience should indicate practical experience obtained in cross representation section of

Maintenance task as per Appendix- II to AMC of CAR 66.

Section 5:Indicate the subject modules passed or basic knowledge certificate issued by CEO (DGCA)

Section 5a: Indicate details of type rating courses completed covering aeroplane/engine/helicopter.

Section 5b: Indicate details of Name of the DGCA office conducted the skill test.

Section 6: State the details of existing known physical disability or disorder

Section 7: By signing the declaration you are confirming that all the information is correct and true.

Section 8: Assign annexure number as indicated and continuous page numbers to the enclosures and indicate it under column 3

against each item

CAR-66


APPLICATION FOR RENEWAL OF

CAR- 66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE

DGCA INDIA

CA Form 19-03

Please complete the form in BLOCK CAPITALS using black or dark blue ink after reading the attached guidance notes. Fields marked with an asterisk * are mandatory and must be completed in all cases. Use Date Format – DD-MM-YYYY

1. PERSONAL DETAILS

AME Licence No. Expiry Date

*Name in full

Details of Fees

*Permanent address (in case of any change) ……………………………………………………………………………………………………………………...

……………………………………………………………………………………………………………………………………………. PIN Code ………………………………

*Address for Communication …………………………………………………………………………………………………………….............................. …………………………………………………………………………………………………………………................ PIN Code ……………………………

Applicant Contact Phone Number ………………………........................ E-mail………………..….……………………………………………..…….

Name of the Current Employer ….…………………………………………………………………………………………….…………….……………….…..

Contact Phone Number of Employer ……………………….................. E-mail…….……………………………..………………………..……………….

2. *APPLICATION

I wish to apply for Renewal of CAR-66 Aircraft Maintenance License as indicated and confirm that the information contained

in this form was correct at the time of application

3. *SUMMARY OF AERONAUTICAL EXPERIENCE PRECEEDING TWENTY FOUR MONTHS

Date Organisation Aircraft Description of Work

From To


4. DETAILS OF REFRESHER COURSE ATTENDED

4.*DECLARATION

I hereby confirm that: i) I apply for renewal of CAR-66 Aircraft Maintenance Engineer’s Licence as indicated and confirm

that the information contained in this form was correct at the time of application. ii) I never had a CAR 66 AME Licence

issued which was revoked or suspended by DGCA iii) I did not apply earlier to the any other office of DGCA for renewal of

my AME Licence and the request was not turned down.

PLACE SIGNATURE

DATE NAME

CAR-66


INSTRUCTION AND CHECKLIST

CHECKLIST TO CA FORM 19-03

DETAILS OF ENCLOSURES

Enclo-sure No.

Enclo-sure Page No.

DGCA Re-

marks

Sat/Unsat

1. Original CAR 66 Aircraft Maintenance Engineer’s licence I

2. Certified true copies of Logbook / Work records for the corresponding pe-riod

II

3. Medical fitness certificate III

4. Copies of refresher training corresponding to the previous five years IV

4. Fee paid

It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant,


themselves liable to administrative/Legal action n as per Aircraft Rule 1937. Further the licence is liable for revocation /

cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence.


will be returned through the self addressed cover affixed with necessary postal stamp (Speed post) provided by the appli-

cant.

Completed application with the checklist should be posted along with the required documentation to the respective

Regional / Sub-Regional Airworthiness Office

Notes: Having clear concise supporting data will enable DGCA office to renew the licenses more effectively and with

less risk of errors or rejections. DGCA office will not contact you for clarification of details on applications and therefore it

is most important that you have the correct information before applying.

In order that DGCA can process the licence application as quickly as possible, it is important that all sections marked

with an asterisk on the application form are completed and the required supporting documentation enclosed. Please note

failure to submit a correctly completed application form and the required documentation will lead to the rejection of the

application and the fees submitted will be utilized towards processing the application

Section 1: Indicate personal details as required. Section 3: Indicate aircraft maintenance and certification work done during the period.

CAR-66


APPLICATION FOR CONVERSION/REMOVAL OF LIMITATIONS OF CAR- 66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE

DGCA INDIA

CA Form 19-04


*1. PERSONAL DETAILS

AME Licence No. Expiry Date

Name Nationality

Date of birth Computer No.

Permanent Address .........................................……………………………………………………………

…………………………………………………………………………………………………………………………PIN Code................................

Address for Communication (if different from above)……………………….....................................................

………………………………………………………………………………………………………….……………….PIN Code................................

Applicant Contact Phone Number ……………………..................E-mail…….……………………………………………………….

Name of the Current Employer ………………………………………………………………………………………………………………..

Contact Phone Number of Employer………………………..................E-mail…….…………………………………………………….

*2(a) AME LICENCE HELD 2(b) DETAILS OF CAR-66 AME LICENCE APPLIED FOR

Category Type Rating Category A/c Type Rating Limitation Code

CAR-66


*2(a) AME LICENCE HELD 2(b) DETAILS OF CAR-66 AME LICENCE APPLIED FOR

Category Type Rating Category A/c Type Rating Limitation Code

*3. DETAILS OF LIMITATION CODE TO BE REVOKED

License Held Limitation Code En-dorsed

Examination Module Completed

Category Type Rating

*4. SUMMARY OF AERONAUTICAL EXPERIENCE GAINED WITH RESPECT TO THE LIMITATION OF AME

Licence

Date Organisation Aircraft Description of Work

From To

5.DECLARATION

I hereby confirm that: i) I apply for Conversion/Removal of limitation as indicated and confirm that the infor-

mation contained in this form was correct at the time of application.

PLACE SIGNATURE

DATE NAME

CAR-66


6.INSTRUCTION AND CHECKLIST

CHECKLIST TO CA FORM 19-04 DOCUMENTS ENCLOSED

Enclosure No.

Enclo-sure Page No.

DGCA Re-

marks

Sat/Unsat

Original Pre - CAR 66 AME licence. I

Three copies of stamp size photograph duly attested on its back side. (for conversion)

II

Certified true copies of Knowledge Examination modules (where appli-cable) result sheets/ certificates.

III

Certified true copies of documentary evidence of experience, skill test (where applicable).

IV

Type course completion certificate, where applicable. V

Copy of skill test result relating to the limitation of the licence VI

Certified true copies of Logbook / Work records as applicable. VII

Instruction to complete CA Form 19-04 It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant,


themselves liable to administrative/legal actions as per Aircraft Rules 1937. Further the licence is liable for revocation /


All original documents if required to be submitted, will be returned through the self addressed cover affixed with

necessary postal stamp (Speed post) provided by the applicant.

Completed application with the checklist should be posted along with the required documentation to: The Directorate

General of Civil Aviation, Opposite Safdarjung Airport, New Delhi 110003

Notes: Having clear concise supporting data will enable DGCA to issue licences more effectively and with less risk

of errors or rejections. DGCA will not contact you for clarification of details on applications and therefore it is most im-

portant that you have the correct information before applying.

In order that DGCA can process the licence application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation enclosed. Please note failure to submit a correctly completed application form and the required documentation will lead to the rejection of the application and the fees submitted will be utilized towards processing the application

Section 2: Indicate category & type rating of licence held/and the category and typerating applied for with or without limitation. Section 3: This section should be used if applying for the removal of limitation(s) from type rating(s), and should detail aircraft types by airframe/engine combination. Please enter the limitation (s) in the appropriate column. Enter only one airframe/engine per line. Section 4: Provide details of experience gained corresponding to the limitation code & aircraft type.

APPLICATION FOR ISSUE OF DUPLICATE

CAR- 66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE DGCA INDIA

CAR-66


CA Form 19-05


1. PERSONAL DETAILS

*Name in full

AME Licence No.

*Permanent address ................................……………………………………………………………

…………………………………………………………………………………………………………………………PIN Code................................

*Address for Communication (if different from above)……………………….....................................................

………………………………………………………………………………………………………….……………….PIN Code................................

Applicant Contact Phone Number …………………..................E-mail…….……………………………………………………..

Name of the Current Employer …………………………………………………………………………………………………………..

Contact Phone Number of Employer ………………………..................E-mail…….…………………………………………………

2. *APPLICATION

I wish to apply for issue of Duplicate CAR-66 Aircraft Maintenance License as indicated and the information

contained in this form was correct at the time of application.

3. *Reason for issue of duplicate AME Licence( Mark √ as ap-

plicable) LOST

MUTI-

LATED

If the licence was lost provide a brief account of circumstances under which the licence was lost:

4.*DECLARATION

I hereby confirm that: i) I apply for issue of duplicate CAR-66 Aircraft Maintenance Engineer’s Licence as indi-

cated and confirm that the information contained in this form is correct at the time of application. ii) My CAR

66 AME Licence not suspended / cancelled by DGCA and no disciplinary case is pending against me iii) I did not

apply earlier to the office of DGCA for issue of my duplicate AME Licence and the request was not turned down.

PLACE SIGNATURE

DATE NAME

CAR-66


5.DETAILS OF DOCUMENTS, PHOTOGRAPH AND FEE ENCLOSURES Enclosure No.

Tick Mark

DGCA

Remarks

1.Original Mutilated AME Licence or Affidavit duly notarized by Authorized notary in case of loss of AME Licence

I

2. Copy of FIR lodged with the police station in case of loss of AME Licence II

3. Copy of AME Licence if available in case of loss III

4. Two copy of recent photograph IV

5. Details of fee paid as per Rule 62 V

Please refer to current notification for details of fees required. All original documents submitted will be returned through the self addressed cover affixed with necessary postal stamp (for speed post). Completed application should be posted along with the required documentation to: Licensing & Training Stand-ards, Directorate General of Civil Aviation, Opposite Safdarjung Airport, New Delhi 110003,

Notes: Having clear concise supporting data will enable DGCA to issue licences more effectively and with less risk of errors or rejections. Licensing & Training Standards will not contact you for clarification of details on applications and therefore it is most important that you have the correct information before applying.

Instruction on how to complete CAR-66 Licence issue of duplicate Application Form (CA Form 19-05). In order that DGCA can process your licence application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation submitted. Please note failure to submit a correctly completed application form and the required documenta-tion will lead to the rejection of your application and the fees submitted will be utilized towards processing the application.

Section 2: Indicate what type of licence you are applying for. Section 3: Tick whether the AME Licence is lost or mutilated Section 4: By signing the declaration you are confirming that all of the information is correct and true.

CAR-66


MEDICAL CERTIFICATE

(To be provided by a Registered Medical Practitioner holding at least MBBS)

DGCA INDIA

CA Form 19-06

Mr. / Ms _________________________ whose signature is appended below, has been medically examined for

any known disability or disorder which may become an hindrance to perform the normal functions of an Aircraft

Maintenance Engineer.

He/She has …………………………………………………………………………………………………………………………………………..…………

physical disabilities or disorder / no physical disabilities or disorder.

He/She has been assessed medically fit / unfit to function as an Aircraft Maintenance Engineer.

( Strikeout whichever is not applicable)

Signature of the Doctor……………………………….

Registration No.

Designation

Signature of the Applicant with date Date

MEDICAL CERTIFICATE FOR COLOUR VISION

I, Dr. _______________________ hereby certify that I have examined Mr. /Ms ___________________ whose

signature is appended below, and certify that his colour vision is Normal/Defective safe/Defective unsafe.

The colour vision has been tested with,

Pseudo – Isochromatic plates

Approved Lantern test

Any other test applicable

( Strikeout whichever is not applicable)

Signature of the Doctor……………………………….

Registration No.

Designation

Signature of the Applicant with date Date

CAR-66


APPLICATION FOR ALLOTMENT OF COMPUTER NUMBER FOR APPEARING IN AME LICENCE EXAMINATIONS

DGCA INDIA

CA Form 19-07

Paste recent passport size photograph *

(attested partly cover-ing photograph & Page

of this application)


Paste recent passport size photograph

(WITHOUT ATTESTA-

TION)

………………………………….....

SIGNATURE

FOR OFFICE USE - Computer Number Allotted (Allotment of Computer Number does not indicate the ac-ceptance of the applicant’s candidature in Basic Knowledge Examination)

E-

1.*PERSONAL DETAILS

*Name in full

FIRST NAME MIDDLE NAME SURNAME Fathers Name

*Date of

Birth

* Nationality SEX (Male/ Female)

*Permanent address ……………………………………………………………………………………………………………………..…………….

……………………………………………………………………………………………………………..………PIN Code...................................

*Address for Communication (if different from above address) ……………………………………………………………..…… ………………………………………………………………………………………………………………………PIN Code...................................

*Applicant Contact Phone Number…….......……………............... E-mail…….……..……………….………………………………

Employer/ Training School Contact Phone Number …………........................ E-mail…….…………….……..………………

*Subject studied and passed in 10+2 or

equivalent Year of Passing

Name of the Edu-cation Board

Details of the School

Physics, Chemistry & Mathematics

2. * AIRCRAFT MAINTENANCE EXPERIENCE / DURATION OF STUDY IN AN APPROVED TRAINING ESTAB-LISHMENT

Maintenance Organization/ Approved Institute

Type of air-craft/ engine/

system

Duration

From To Period in months

CAR-66


3. *DECLARATION

I hereby declare that the information provided in this form is correct in every respect to the best of my knowledge and belief and

that nothing has been concealed or withheld by me. I understand that if any of my particulars/ entries are found false or incorrect

before or after the examination, my candidature shall be rejected and further action can be taken against me by DGCA as deemed

fit. Further, I declare that I have read and understood the INSTRUCTIONS.

PLACE SIGNATURE

DATE NAME

It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, issue,

renewal or variation of any certificate, licence, approval, permission or other document. Persons doing so render them-

selves liable, on summary conviction, to a fine of one Lakh Rupees and/or imprisonment for a term not exceeding three

months. Further, it renders the person permanently ineligible to have an Aircraft Maintenance Engineer’s Licence.

*CERTIFICATE [To be certified by QM/ CI/ Chief Engg. Officer(in case of serving defence candidates)]

It is certified that the particulars claimed by Mr. / Ms ___________________________ has been verified by

me and found correct.

DATE:

PLACE: (SEAL OF ORGANISATION)

SIGNATURE…………………………………………………………………

NAME ………………………………………………………………….

Designation…………………………………………………………………

4.*DETAILS OF DOCUMENTS, PHOTOGRAPH AND FEE ENCLOSURES Enclosure

No. Tick

Mark DGCA Re-

marks

1. Certified true copy proof of Date of Birth certificate I

2. Certified true copy of 10+2 with Physics, Chemistry, Mathematics or equivalent

II

3. Certified true copy of Passport or any photo identity card issued by the Government

III

4. Certified true copy of Course completion from AME institute/ Degree in Engineering certificate is applicable

IV

Completed application should be posted along with the required documentation to the Central Examination Organisation, O/o the Directorate General of Civil Aviation, East block II, R K Puram, New Delhi 110066. Failure to submit a correctly completed application form and the required documentation will lead to the rejection of your application.

Instruction to complete application for allotment of computer No. for appearing in CAR-66 basic knowledge exami-nation (CA Form 19-07). In order that CEO can process your licence application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documents submitted.

CAR-66


APPLICATION FOR APPEARING IN WRITTEN PAPER(S) OF

CAR 66 BASIC KNOWLEDGE EXAMINATION

DGCA INDIA

CA Form 19-08 A


1.* FEE DEAILS:

Amount (in Rs.) Demand Draft/ Banker’s Cheque No.

Name of Bank Date of Issue

2.*PERSONAL DETAILS

COMPUTER NO: EXAMINATION SESSION & CENTRE

E- MONTH YEAR CENTRE

NAME:

FIRST NAME MIDDLE NAME SURNAME

*CATEGORY/ SUB-CATEGORY OF EXAMINATION (Tick appropriate box(s)

Category A B

Aeroplane Turbine A1 B1.1

Aeroplane Piston A2 B1.2

Helicopter Turbine A3 B1.3

Helicopter Piston A4 B1.4

Avionic B2

3. *EXAMINATION PAPERS (Please tick box(es) against the module(s) you wish to take at this examination)

Module Module

3. Electrical Fundamentals 11A. Turbine Engine Aeroplane Aerodynamics, Structures and Systems

4. Electronic Fundamental 11B. Piston Engine Aeroplane Aerodynamics, Structures and Systems

5.Digital Techniques/ Electronic instrument Systems

12. Helicopter Aerodynamics, Structures and Systems

6. Materials & Hardwares

13. Aircraft Aerodynamics, Structures and Systems .(Please tick (√)the appropriate box)

Ex-

clud-

ing

13.5,1

3.9

Ex-

clud-

ing

13.8

Ex-

clud-

ing

13.4

Ex-

clud-

ing

13.5,1

3.6,13.

8&13.

9

Ex-

clud-

ing

13.4,1

3.5&1

3.9

Ex-clud-ing13.4&,13.8

7. Maintenance Practices 14. Propulsion

8. Basic Aerodynamics 15. Gas Turbine Engine

CAR-66


9. Human Factors

16. Piston Engine

10. Aviation Legislation

17. Propeller

4. * DETAILS OF AERONAUTICAL ENGINEERING EXPERIENCE:

Type of aircraft/ engine/ system

Organization/ Approved Insti-

tute Area or Work

Duration


5.* DECLARATION (delete as appropriate)

I hereby declare that the information provided in this form is correct in every respect to the best of my knowledge and belief and that nothing has been concealed or withheld by me. I understand that if any of my particulars/ entries are found false or incorrect before or after the examination, my candidature shall be rejected and further action can be taken against me by DGCA as deemed fit. Further, I declare that I have read and understood the INSTRUCTIONS.

PLACE SIGNATURE

DATE NAME

It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, issue, renewal or variation of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable, on summary conviction, to a fine of one Lakh Rupees and/or imprisonment for a term not exceeding three months. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence.


It is certified that the particulars claimed by Mr. / Ms ___________________________ has been verified by me

and found correct.

DATE: (SEAL OF ORGANISATION)

SIGNATURE

NAME

Designation

Instruction to complete application form for CAR-66 AME Licence Knowledge (written) examination (CA Form 19-08 A). In order that DGCA (CEO) can process your application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation submitted. Please note failure to submit a correctly completed application form and the required documentation will lead to the rejection of your applica-tion and the fees submitted will be utilized towards processing the application.

CAR-66


APPLICATION FOR APPEARING IN CAR 66 TYPE EXAMINATION

*To be Submitted to the respective DGCA RAO’s

DGCA INDIA

CA Form 19-08 B


1.* FEE DEAILS:

Amount (in Rs.) Demand Draft/ Banker’s Cheque No.

Name of Bank Date of Issue

2.*PERSONAL DETAILS

COMPUTER NO: EXAMINATION SESSION & CENTRE

E- MONTH YEAR CENTRE

FIRST NAME MIDDLE NAME SURNAME

*CATEGORY/ SUB-CATEGORY OF EXAMINATION (Please tick (√) the appropriate Category/Categories)

Category A B

Aeroplane Turbine A1 B1.1

Aeroplane Piston A2 B1.2

Helicopter Turbine A3 B1.3

Helicopter Piston A4 B1.4

Avionic B2

3. *DETAILS OF BASIC KNOWLEDGE EXAMINATION PAPERS PASSED PERTAINING TO THE CATEGORY (Please tick (√)against the module(s) , enclose a�ested true copies of result cards)

Module Module

3. Electrical Fundamentals 11A. Turbine Engine, Aeroplane Aerodynamics, Struc-tures and Systems

4. Electronic Fundamental 11B. Piston Engine, Aeroplane Aerodynamics, Struc-tures and Systems

5.Digital Techniques/ Electronic in-strument Systems

12. Helicopter Aerodynamics, Structures and Systems

6. Materials & Hardwares

13. Aircraft Aerodynamics, Structures and Systems (Please tick (√)the appropriate box(es))

Exclud-

ing

13.5 &

13.9

Exclud-

ing

13.8

Exclud-

ing

13.4

Exclud-

ing

13.5,

13.6,

13.8 &

13.9

Exclud-

ing

13.4,

13.5 &

13.9

Exclud-ing 13.4 & 13.8

7. Maintenance Practices 14. Propulsion

8. Basic Aerodynamics 15. Gas Turbine Engine

9. Human Factors 16. Piston Engine

CAR-66


10. Aviation Legislation 17. Propeller

4. *Type of Applicant (Please tick (√) the ap-propriate type)

AME TRG DEF AEG GEN

5.*Type of Aircraft, Engine for Type Exami-nation (As per the Appendix I to AMC of CAR-66)

6. * DETAILS OF TOTAL AERONAUTICAL ENGINEERING EXPERIENCE:

Type of air-craft/ engine/

system

Organization/ Approved Insti-

tute Area or Work

Duration


7.*DETAILS OF TYPE RATED EXPERIENCE

Type of Aircraft, Engines, Sys-tems

Organisation/ Approved Insti-tute

Area of Work Duration Periods

in Months

Brief Details of Experi-ence From To

8.* Name of the Approved Institute/Sponsoring Or-ganization/Employer

9.* DECLARATION (delete as appropriate)

I hereby declare that the information provided in this form is correct in every respect to the best of my knowledge and belief and that nothing has been concealed or withheld by me. I understand that if any of my particulars/ entries are found false or incorrect before or after the examination, my candidature shall be rejected and further action can be taken against me by DGCA as deemed fit. Further, I declare that I have read and understood the INSTRUCTIONS.

PLACE SIGNATURE

DATE NAME

It is an offence to make, with intent to deceive, any false representations for the purpose of procuring the grant, issue, renewal or variation of any certificate, licence, approval, permission or other document. Persons doing so render themselves liable to administrative/ Legal action as per Aircraft rule 1937. Further the licence is liable for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence.


It is certified that the particulars claimed by Mr. / Ms ___________________________ has been verified by me

and found correct.

DATE: (SEAL OF ORGANISATION)

SIGNATURE

NAME

Designation

FOR OFFICIAL USE ONLY

CAR-66


CATEGORIES ACCEPTED ROLL NO ALLOTED

A B REASONS FOR REJECTION, IF ANY:

A1 B1.1

A2 B1.2

A3 B1.3

A4 B1.4

B2

NAME OF THE DGCA OFFICER

SIGNATURE OF THE DGCA OFFICER

Instruction to complete application form for CAR-66 AME Licence Type examination (CA Form 19-08 B). In order that DGCA (RAO) can process your application as quickly as possible, it is important that all sections marked with an asterisk on the application form are completed and the required supporting documentation submitted. Please note failure to submit a correctly completed application form and the required documentation will lead to the rejection of your application and the fees submitted will be utilized towards processing the application. *AEG-Aeronautical Engineering Graduate & Graduates of other allied field of Engineering.

CAR-66


APPLICATION FOR APPEARING IN SKILL TEST OF

CAR-66 AME LICENCE

DGCA INDIA

CA Form 19-09


Roll Number Allot-ted

COMPUTER No. E

1.*PERSONAL DETAILS Licence No. ( If held)

FIRST NAME MIDDLE NAME SURNAME AME Licence

RTR

2. DETAILS OF LICENCE HELD ( If held)

CAT/ SUB-CAT AIRCRAFT TYPE CAT/ SUB-CAT AIRCRAFT TYPE

3.*DETAILS OF SKILL TEST APPLIED FOR:

CAT/ SUB-CAT AIRCRAFT TYPE EXAMINATION CENTRE

*DETAILS OF PREVIOUS SKILL TEST (For the same Airframe and Engine combination):

CAT/ SUB-CAT AIRCRAFT TYPE DATE of EXAMINATION CENTRE

4.*EXAMINATION MODULE(S) passed relevant to Cat/ Sub-Cat applied for )

Module Session Module Session Module Session

CAR-66


5.*DETAILS OF SPECIFIC PAPER / OF TYPE COURSE PASSED:

CAT/ SUB-CAT AIRCRAFT TYPE SESSION / Name of

the Approved Organ-isation

Level of the Course

MARKS secured

RESULT

6. * DETAILS OF AIRCRAFT TYPE MAINTENANCE EXPERIENCE

Type of aircraft/ engine/ system

Organization Area or Work

Duration

From To Period in

months

7. *FEE DEAILS: ROLL NUMNER ALLOTED

Fees Demand Draft/ Banker’s Cheque No.

Date of Issue Name of Bank

8. *DECLARATION (delete as appropriate)

I hereby declare that the information provided in this form is correct in every respect to the best of my knowledge and belief and that nothing has been concealed or withheld by me. I understand that if any of my particulars/ entries are found false or incorrect before or after the examination, my candidature shall be re-jected and further action can be taken against me by DGCA as deemed fit. Further, I declare that I have read and understood the INSTRUCTIONS.

PLACE SIGNATURE

DATE NAME

9.*DETAILS OF ENCLOSURES Enclosure No

Tick Mark

DGCA Re-marks

1. Details of DGCA Examinations passed. I

Module No. and Paper Session

No. passed

Roll No.

3. Electrical Fundamentals I(1)

4. Electronic Fundamental I(2)

5.Digital Techniques/ Electronic instrument Systems I(3)

6. Materials & Hardwares I(4)

CAR-66


7. Maintenance Practices I(5)

8. Basic Aerodynamics I(6)

9. Human Factors I(7)

10. Aviation Legislation I(8)

11A. Turbine Engine Aeroplane Aerodynamics, Struc-

tures and Systems

I(9)

11B. Piston Engine Aeroplane Aerodynamics, Struc-

tures and Systems

I(10)

12. Helicopter Aerodynamics, Structures and Systems I(11)

13. Aircraft Aerodynamics, Structures and Systems I(12)

14. Propulsion I(13)

15. Gas Turbine Engine I(14)

16. Piston Engine I(15)

17. Propeller I(16)

2. Type course completion certificate with examination result sheet

II

3. Certified true copy of previous skill test result, if any III

4. Certified true copies of Logbook / Work records on CA Form 19-10

IV


will be returned through the self addressed cover affixed with necessary postal stamp (for speed post). Completed appli-

cation should be posted along with the required documentation to the respective regional / sub-regional office.


issue, renewal or variation of any certificate, licence, approval, permission or other document. Persons doing so render

themselves liable to administrative/legal actions as per Aircraft Rules 1937. Further the licence is liable for revocation /


Notes: Having clear concise supporting data will enable regional office to process the application more effectively

and with less risk of errors or rejections. Regional office will not contact you for clarification of details on applications and

therefore it is most important that you have the correct information before applying.

Failure to submit a correctly completed application form and the required documentation will lead to the rejection

of your application and fee submitted would be utilized for processing the application.

FOR OFFICIAL USE

CAR-66


NAME OF CANDIDATE ROLL NUMBER

CAT/ SUB-CAT AIRCRAFT TYPE

Candidate was examined on the following topics:

Candidate was found weak in the following topics:

Percentage marks awarded in the Skill Test and Results:

Date of Skill Test Cat/ Sub-Cat Aircraft Type % Marks Pass/ Fail

Issue/ Extension/ of AME licence in respect of Sh. ___________________________ is recommended only in

Cat/ Sub-Cat_____ to cover _____________________ (Aircraft).

(Signature) Member of Examina-

tion Board

(Signature) Member of Examina-

tion Board

(Signature) Member of Exami-

nation Board

Name: Name: Name:

Date: Date: Date:

FORMAT OF AIRCRAFT MAINTENACE ENGINEER

WORK RECORD / LOG BOOK

DGCA INDIA

CA Form 19-10

CAR-66


1. PERSONAL DETAILS Affix recent pass-port size photo graph duly at-tested on the

front side

CEO Computer No.

*Name in full

*Date of birth * National-

ity

*Educational Qualification

GENDER M / F AME Licence No.

*Permanent Address……………………………………………................………………………………………………………………………

……………………………………………………………………………………………………..……………PIN Code....................................

Changed Permanent Address

*Address for Communication (if different from above)………………………...........................................................

………………………………………………………………………………………………………………..….PIN Code...................................

Changed Address for Communication:

Applicant Contact Phone Number ………………………….............. E-mail…….………………………………..……………….

Name of the Current Employer……………………………………………………………………………………………………………….

Contact Phone Number of Employer ………………….................... E-mail…….…………………………………………………

Log Book Owners Name…………………………………………………………….... Signature ………………………………………..

CAR-66


2. Record of Training:

Training Completed Training Establish-

ment and Location From To Result

CAR-66


3. (i) Details of Employer / Organisation at which engaged in Aircraft Maintenance

Employer / Organisation:

FROM To Position Nature of Work

Types of Aircraft or other products

Confirmation of the Organisation

NAME SIGNATURE POSITION & STAMP DATE

3 (ii). Details of Employer / Organisation at which engaged in Aircraft Maintenance






3 (iii) . Details of Employer / Organisation at which engaged in Aircraft Maintenance






CAR-66


4.BASIC SKILL

*Typical Maintenance Tasks (1)

CATE-GORY

Aircraft Reg. No & Type

(2)

Date on which performed (3)

Organization (4)

Supervisor Name and

AME Licence No.

Time limit/ Maintenance

#

#

LV .Accessory Gear Box

c. *Check Chip detector

All the applicable aircraft maintenance tasks listed under Appendix II to AMC of CAR-66 should be reproduced

under column (1).

Details of tasks performed should be furnished under column 2, 3, 4 and 5

Maintenance tasks not performed should be indicated as “ NOT PERFORMED”

5.*DECLARATION

I hereby confirm that the information contained in this form was correct at the time of application.

PLACE SIGNATURE

DATE NAME


issue, renewal or variation of any certificate, licence, approval, permission or other document. Persons doing so

render themselves liable to administrative/legal actions as per Aircraft Rules 1937. Further the licence is liable

for revocation / cancellation / suspension or permanently makes the person ineligible to have an Aircraft Mainte-

nance Engineer’s Licence.

CAR-66


APPLICATION FOR ISSUE OF BASIC KNOWLEDGE

EXAMINATION CERTIFICATE DGCA INDIA

CA Form 19-11


1. *PERSONAL DETAILS

CEO Computer No.

*Name in full

*Permanent address

……………………..…………………………………………………………………………………………………..

……………………………………………………………………………………………………………..

PIN Code................................

*Address for Communication (if different from above) ……………………..…………

……………………..………………………………………………………………………………………

PIN Code................................

Applicant Contact Phone Number ………………………..................E-

mail…….………………………………………..

Name of the Current Employer…………………………………………………………………………..

Contact Phone Number of Employer ……………………..................

E-mail…….…………………………………………

2. *APPLICATION

I hereby request DGCA to issue of basic knowledge examination certificate as indicated and con-

firm that the information contained in this form was correct at the time of application ( Specify

the required category / sub-category of basic knowledge certificate)


Mechanical

Avionic

CAR-66


3. *Details of basic modules/papers relevant to modules passed

Cate-

gory/sub-cat-

egory

Module No.

Exam Session

in which

Passed

Category/sub-

category Module No.

Exam Session

in which

Passed

4 *FEE DEAILS:

Fees Demand Draft/ Banker’s Cheque No.

Date of Issue Name of Bank

5.*DECLARATION

I hereby confirm that: i) I apply for issue of basic knowledge certificate as indicated and confirm

that the information contained in this form was correct at the time of application ii) I did not apply

earlier to the office of DGCA for issue of basic knowledge certificate and the request was not

turned down.

PLACE SIGNA-

TURE

DATE NAME

It is an offence to make, with intent to deceive, any false representations for the purpose of pro-

curing the grant, issue, renewal or variation of any certificate, licence, approval, permission or

other document. Persons doing so render themselves liable to administrative/legal actions as per

Aircraft Rules 1937. Further the licence is liable for revocation / cancellation / suspension or per-

manently makes the person ineligible to have an Aircraft Maintenance Engineer’s Licence.

CAR-66


5.*DETAILS OF DOCUMENTS, PHOTOGRAPH AND FEE ENCLO-SURES

Enclosure No.

Tick Mark

DGCA Re-

marks

Details of DGCA Examinations passed : I

Module No. and Paper Session

No. passed

Roll No.

3. Electrical Fundamentals I (a)

4. Electronic Fundamental I (b)

5.Digital Techniques/ Electronic instrument Systems

I (c)

6. Materials & Hardwares I (d)

7. Maintenance Practices I (e)

8. Basic Aerodynamics I (f)

9. Human Factors I (g)

10. Aviation Legislation I (h)

11A.Turbine Engine Aeroplane Aerody-

namics, Structures and System I (i)

11B. Piston Engine Aeroplane Aerodynam-

ics, Structures and Systems I (j)

12. Helicopter Aerodynamics, Structures

and Systems I (k)

13. Aircraft Aerodynamics, Structures and

Systems I (l)

14. Propulsion I (m)

15. Gas Turbine Engine I (n)

16. Piston Engine I (o)

17. Propeller I (p)

Please refer to current notification for details of fees required. All original documents submitted will be returned through the self addressed cover affixed with necessary postal stamp (for speed post). Completed application should be posted along with the required documentation to the Central Examination Organisation, O/o the Directorate General of Civil Aviation, East block II, R K Puram, New Delhi 110066.

Notes: Having clear concise supporting data will CEO to issue licences more effectively and with less risk of errors or rejections. CEO will not contact you for clarification of details on applications and therefore it is most important that you have the correct information before applying. Failure to submit a correctly completed application form and the required documentation will lead to the rejection of your application and the fee will be utilized for processing the application.

CAR-66


DGCA INDIA

CA Form 19-12

DIRECTORATE GENERAL OF CIVIL AVIATION

CENTRAL EXAMINATION ORGANIZATION

East Block III, RK Puram, New Delhi 110066

Aircraft Maintenance Engineer’s

Basic Knowledge Examination Certificate

This is to certify that Mr./Ms __________________________________________________

Computer Number. ________________________ has passed the following subjects/module/

papers examinations conducted by this office in partial fulfillment of requirements for grant of

Aircraft Maintenance Engineer’s License.

Stream/Category/Papers/ Module names: _ __________________ Session ____________in

which

Passed.

Seal

Signatures

(Head, Central Examination Organization)

For the Director General of Civil Aviation

CAR-66


AppendixVI-AircraftMaintenanceEngineer’sLicencereferredtoinRule61oftheAircraftRules,1937-CAForm26

CA26

GOVERNMENTOFINDIA

DIRECTORATEGENERALOFCIVILAVIA-

TION

CAR-66

AIRCRAFTMAINTENANCEENGINEER’sLI-

CENCE

I INDIA IX. CONDITIONS

II. Aircraft Maintenance Engineer’s Licence a. Certified that holder is authorized to exercise the privi-

legesofthelicenceasgiveninRule61oftheAircraftRules,

1937.

b.EndorsementofaircrafttypesatsectionXII(b)titledAIR-

CRAFTTYPERATINGmeanstheholderisqualifiedtoissue

acertificateofreleasetoserviceforsuchaircraftfromthe

dateofendorsementwithavalidauthorizationissuedby

approvedmaintenanceorganization.

c.Holderofthislicenceshallnotexercisetheprivilegesof

thelicenceandrelatedratingsatanytimewhenhe/sheis

awareofanydecreaseinmedicalfitnesswhichmightren-

derhim/herunable tosafelyandproperlyexercise these

privileges.

d.Thislicenceisnotvalidunlessitbearsthesignatureoftheholder.

e.ThislicenceremainscurrentuntiltheexpirydatespecifiedatsectionXIVwhilstincompliancewiththeAircraftRule61andCAR66unlesspreviouslysuspendedorrevoked.

f. This licence when endorsed with an aircraft type ratingmeetstheintentofICAOAnnex1.

III. Licencenumber

STAMPSIZE

PHOTOIV.

Nameofholder

infull

IVa Dateofbirth

V. Addressof

holder

VI. Nationality

VII. SignatureofHolder

VIII.

IssuedinaccordancewiththeprovisionsoftheAircraftAct

1934,andAircraftRules1937.

X SignatureofIssu-

ingAuthority

………………………………………………..……

(fortheDirectorGeneralofCivilAviation)

DaDateofIssue:

CAR-66


XI. StampoftheIs-

suingAuthority

g. Entry, endorsement or alteration in the licence shall bemadebypersonauthorizedforthispurposebytheDirectorGeneral.

1 III. LIC No. 2

XII (a). LICENCE (SUB) CATEGORIES XII (b). AIRCARFT TYPE RATING

CATEGORIES A B1 B2 C DATE AIRCRAFTTYPEORGROUPCATE-

GORYSTAMP&DATE

AEROPLANESTURBINE n/

a

n/

a

AEROPLANESPISTON n/

a

n/

a

HELICOPTERSTURBINE n/

a

n/

a

HELICOPTERSPISTON n/

a

n/

a

AVIONICSn/

a

n/

a

n/

a

AIRCRAFTn/

a

n/

a

n/

a

III. LIC No. 3 III. LIC No. 4

XIII. LIMITATIONS XIV. LICENCE VALIDITY

AIRCRAFT

TYPEOR

GROUP

CATEGORY

LIMITA-

TION

CODE

SIGNATUREWITH

DATE(REMOVALOF

LIMITATION)

DATEOFEXPIRYSIGNATUREWITH

DATESEAL

III. LIC No. 5 III. LIC No 6

CAR-66


XIV a). LICENCE ENDORSEMENTS INHERITED FROM THE AME

LICENCE HELD PRIOR TO CAR-66 LICENCE XIV (b). REMARKS

RATING CATEGORYSIGNATUREWITH

DATE

III. LIC No. 7 III. LIC No. 8

CAR-66


1. Theaircraftmaintenanceengineer’slicenceonceissuedisrequiredtobekeptbytheperson

towhomitappliesingoodconditionandwhoshallremainaccountableforensuringthatno

unauthorizedentriesaremade.

2. Failuretocomplywithparagraph1mayinvalidatethedocumentandcouldleadtotheholder

notbeingpermittedtoholdanyCAR-145certificationauthorization

3. Failuretocomplywithparagraph1mayalsoresultinprosecutionunderrelevantIndianPe-

nalCode.

4. Eachpageissuedshallbeinthisformatandcontainthespecifiedinformationforthatpage.

5. Iftherearenolimitationsapplicable,theLIMITATIONSpagewillbeissuedstating‘Nolimi-

tations’.

CAR-66


Acceptable Means of Compliance (AMC) / Guidance Material

(GM) to SECTION A of CAR-66

ThischaptercontainsAcceptableMeansofCompliance(AMC)andGuidanceMaterial(GM)toCAR-66SectionA–TechnicalRequirements.AcceptableMeansofCompliance(AMC)illustrateameans,orseveralalternativemeans,butnotnecessarilytheonlypos-siblemeansbywhicharequirementcanbemet.

SECTION A

TECHNICAL REQUIREMENTS

GM 66.A.3 Licence categories

Individualaircraftmaintenancelicenceholdersneednotberestrictedtoasinglecate-gory.Providedthateachqualificationrequirementissatisfied,anycombinationofcate-goriesmaybegranted.

AMC 66.A.10 Application

1.Maintenanceexperienceshouldbewritteninamannerthatthereaderhasareason-

able understanding of where, when and what maintenance constitutes the experi-

ence.Ataskbytaskaccountisnotnecessarybutatthesametimeablankstatement

“Xyear’smaintenanceexperiencecompleted”isnotacceptable.Alogbookofmainte-

nanceexperience isdesirableandbekept. It is acceptable tocrossrefer in theCA

Form19-01tootherdocumentscontaininginformationonmaintenance.

2. Applicants claimingthemaximumreduction in 66.A.30(a) total experience based

uponhavingsuccessfullycompletedapprovedbasictrainingshouldincludethecer-

tificateofapprovalwithitsvalidityscheduleofthetrainingestablishment.

3.Applicantsclaimingreductionin66.A.30(a)totalexperiencebaseduponhavingsuc-

cessfullycompletedtechnicaltraininginanorganizationorinstituterecognizedby

DGCAasacompetentorganizationorinstituteshouldincludetherelevantcertificate

ofsuccessfulcompletionoftraining.

AMC 66.A.15 (a) Eligibility

DiplomainAeronautical,Mechanical,ElectricalandElectronicsengineeringrecognized

bystatetechnicaleducationboardshallbeconsideredasequivalentqualification.

Toprovetheequivalenceto10+2,theapplicantisrequiredtosubmitacertificatefrom

acompetentauthoritysuchasAssociationofIndianUniversities(AIU).

CAR-66


GM 66.A.20(a) Privileges

1. Thefollowingdefinitionsapply:

Electrical systemmeanstheaircraftelectricalpowersupplysource,plusthedistri-butionsystemtothedifferentcomponentscontainedintheaircraftandrelevantcon-nectors.Lightingsystemsarealsoincludedinthisdefinition.Whenworkingoncablesandconnectorswhicharepartoftheseelectricalsystems,thefollowingtypicalprac-ticesareincludedintheprivileges:

Continuity,insulationandbondingtechniquesandtesting; Crimpingandtestingofcrimpedjoints; Connectorpinremovalandinsertion; Wiringprotectiontechniques.

Avionics system means an aircraft system that transfers, processes, displays orstoresanalogueordigitaldatausingdatalines,databuses,coaxialcables,wirelessorotherdatatransmissionmedium,andincludesthesystem’scomponentsandconnect-ors.Examplesofavionicssystemsincludethefollowing:

Autoflight; Communication,RadarandNavigation; Instruments(seeNOTEbelow); In-FlightEntertainmentSystems; IntegratedModularAvionics(IMA); On-BoardMaintenanceSystems; InformationSystems; Fly-by-WireSystems(relatedtoATA27“FlightControls”); FibreOpticControlSystems.

NOTE: Instruments are formally included in the privileges of the B2 licence holders. How-ever, maintenance on electromechanical and pitot-static components may also be released by a B1 license holder.

Simple testmeansatestdescribedinapprovedmaintenancedataandmeetingallthefollowingcriteria:

Theserviceabilityofthesystemcanbeverifiedusingaircraftcontrols,switches,Built-inTestEquipment(BITE),CentralMaintenanceComputer(CMC)orexternal

testequipmentnotinvolvingspecialtraining. Theoutcomeofthetestisauniquego–nogoindicationorparameter,whichcan

beasinglevalueoravaluewithinanintervaltolerance.Nointerpretationofthetestresultorinterdependenceofdifferentvaluesisallowed.

The test does not involve more than 10 actions as described in the approved

maintenancedata(notincludingthoserequiredtoconfiguretheaircraftpriortothetest,i.e.jacking,flapsdown,etc.,ortoreturntheaircrafttoitsinitialconfigu-

CAR-66


ration).Pushingacontrol,switchorbutton,andreadingthecorrespondingout-comemaybeconsideredasasinglestepevenifthemaintenancedatashowsthemseparated.

Troubleshooting means the procedures and actions necessary to identify the rootcauseofadefectormalfunctionusingapprovedmaintenancedata.ItmayincludetheuseofBITEorexternaltestequipment.

Line maintenance meansanymaintenancethatiscarriedoutbeforeflighttoensurethattheaircraftisfitfortheintendedflight.Itmayinclude:

troubleshooting;

defectrectification;

componentreplacementwiththeuseofexternaltestequipment,ifrequired.Com-ponentreplacementmayincludecomponentssuchasenginesandpropellers;

scheduledmaintenanceand/orchecksincludingvisualinspectionsthatwilldetectobviousunsatisfactoryconditions/discrepanciesbutdonotrequireextensivein-depthinspection.Itmayalsoincludeinternalstructure,systemsandpowerplantitemswhicharevisiblethroughquickopeningaccesspanels/doors;

minorrepairsandmodificationswhichdonotrequireextensivedisassemblyand

canbeaccomplishedbysimplemeans; fortemporaryoroccasionalcases(AirworthinessDirectives,hereinafterAD;ser-

vicebulletins,hereinafterSB)thequalitymanagermayacceptbasemaintenancetasks to be performedby a line maintenanceorganisation providedall require-mentsarefulfilled.TheDGCAwillprescribetheconditionsunderwhichthesetasksmaybeperformed.

Base MaintenancemeansanytaskfallingoutsidethecriteriaaregivenaboveforLineMaintenance.

NOTE:

Aircraftmaintainedinaccordancewith“progressive”typeprogrammesneedtobeindi-viduallyassessedinrelationtothisparagraph.Inprinciple,thedecisiontoallowsome“progressive”checkstobecarriedout isdeterminedbytheassessmentthatall taskswithin theparticularcheckcanbecarriedoutsafelyto therequiredstandardsat thedesignatedlinemaintenancestation.2.Reserved3.ThecategoryClicencepermitscertificationofscheduledbasemaintenancebytheis-

sueofasinglecertificateofreleasetoserviceforthecompleteaircraftafterthecom-pletionofallsuchmaintenance.ThebasisforthiscertificationisthatthemaintenancehasbeencarriedoutbycompetentmechanicsandcategoryB1,B2supportstaff,asappropriate,havesignedforthemaintenancetasksundertheirrespectivespeciali-sation. Theprincipal functionof thecategoryCcertifyingstaff is toensure thatall

CAR-66


requiredmaintenancehasbeencalledupandsignedoffbythecategoryB1,B2sup-portstaff,asappropriate,beforeissueofthecertificateofreleasetoservice.Onlycat-egoryCpersonnel whoalsoholdcategoryB1,B2qualificationsmayperformbothrolesinbasemaintenance.

AMC 66.A.20 (b) (2) Privileges

The6monthsmaintenanceexperiencein2yearsshouldbeunderstoodasconsistingof

twoelements,durationandnatureoftheexperience.Theminimumtomeettherequire-

mentsfortheseelementsmayvarydependingonthesizeandcomplexityoftheaircraft

andtypeofoperationandmaintenance.

1.Duration:

Withinanapprovedmaintenanceorganization:

6monthscontinuousemploymentwithinthesameorganisation;or

6monthssplitupintodifferentblocks,employedwithinthesameorindifferent

organisations.

The6monthsperiodcanbereplacedby100daysofmaintenanceexperienceinac-

cordancewiththeprivileges,whetherthesehavebeenperformedwithinanapproved

organisationorasindependentcertifyingstaffaccordingtoM.A.801(b)2orasacom-

binationthereof.

WhencertifyingstaffmaintainsandreleasesaircraftinaccordancewithM.A.801(b)

2,incertaincircumstancesthisnumberofdaysmayevenbereducedby50%when

agreedinadvancebytheDGCA.Thesecircumstancesconsiderthecaseswherethe

holderof aCAR-66 licencehappens to be theownerofan aircraft and carriesout

maintenanceonhisownaircraft,orwherealicenceholdermaintainsanaircraftop-

eratedfor lowutilization, thatdoesnotallowthelicenceholdertoaccumulatethe

requiredexperience.Thisreductionshouldnotbecombinedwiththe20%reduction

permittedwhencarryingouttechnicalsupport,ormaintenanceplanning,continuing

airworthinessmanagementorengineeringactivities.Toavoidatoolongperiodwith-

outexperience,theworkingdaysshouldbespreadovertheintended6monthspe-

riod.

2.Natureoftheexperience:

Dependingonthecategoryoftheaircraftmaintenanceengineer’slicence,thefollowing

activitiesareconsideredrelevantformaintenanceexperience:

-Servicing;

-Inspection;

-Operationalandfunctionaltesting;

-Trouble-shooting;

CAR-66


-Repairing;

-Modifying;

-Changingcomponent;

-Supervisingtheseactivities;

-Releasingaircrafttoservice.

ForcategoryAcertifyingstaff,theexperienceshouldincludeexercisingtheprivileges,

bymeansofperformingtasksrelatedtotheauthorizationonatleastoneaircrafttype

foreachlicencesubcategory.ThismeanstasksasmentionedinAMC145.A.30(g),in-

cludingservicing,componentchangesandsimpledefectrectifications.

ForcategoryB1andB2,foreveryaircrafttyperatingincludedintheauthorizationthe

experienceshouldbeonthatparticularaircraftoronasimilaraircraftwithinthesame

licencesub-category.Twoaircraftcanbeconsideredassimilarwhentheyhavesimilar

technology,constructionandcomparablesystems,whichmeansequallyequippedwith

thefollowing(asapplicabletothelicencecategory):

(a) Propulsionsystems(pistonorturboproporturbofanorturboshaftorjet-engine

orpushpropellers);and

(b) Flightcontrolsystems(onlymechanicalcontrolsorhydro-mechanicallypowered

controlsorelectro-mechanicallypoweredcontrols);and

(c) Avionicsystems(analogsystemsordigitalsystems);and

(d) Structure(manufacturedofmetalorcompositeorwood).

Forlicencesendorsedwith(sub)groupratings: InthecaseofB1licenceendorsedwith(sub)groupratings(eithermanufacturer

subgrouporfull(sub)group)asdefinedin66.A.45(g)theholdermayshowex-

perienceonatleastoneaircrafttypeper(sub)groupandperaircraftstructure

(metal,composite,wood).

InthecaseofaB2licenceendorsedwith(sub)groupratings(eithermanufacturer

grouporfull(sub)group)asdefinedin66.A.45(g)theholdermayshowexperi-

enceonatleastoneaircrafttypeper(sub)group.

ForcategoryC,theexperienceshouldcoveratleastoneoftheaircrafttypesendorsed

ontheauthorization.

Foracombinationofcategories,theexperienceshouldincludesomeactivitiesofthena-

tureshowninparagraph2ineachcategory.

CAR-66


Amaximumof20%oftheexperiencedurationrequiredmaybereplacedbythefollow-

ingrelevantactivitiesonanaircrafttypeofsimilartechnology,constructionandwith

comparablesystems:

Aircraftmaintenancerelatedtrainingasaninstructor/assessororasastudent;

Maintenancetechnicalsupport/engineering;

Maintenancemanagement/planning.

Theexperienceshouldbedocumentedinanindividuallogbookorinanyotherrecord-

ingsystem(whichmaybeanautomatedone)containingthefollowingdata:

(a) Dateandtime;

(b) Aircrafttype;

(c) Aircraftidentificationi.e.registration;

(d) ATAchapter;

(e) Operation performed i.e. 100FH check, MLG wheel change, engine oil check and

complement, SB embodiment, trouble shooting, structural repair, STC embodi-

ment…;

(f) Typeofmaintenancei.e.base,line;

(g) Typeofactivityi.e.perform,supervise,release;

(h) CategoryusedA,B1,B2orC.

(i) Durationindaysorpartial-days.

GM 66.A.20(b)2 Privileges

Thesentence“mettheprovisionfortheissueoftheappropriateprivileges”includedin

66.A.20(b)2meansthatduringtheprevious2yearsthepersonhasmetalltherequire-

mentsfortheendorsementofthecorrespondingaircraftrating(forexample,inthecase

ofaircraft inGroup1,theoreticalpluspracticalelementplus, ifapplicable,on-the-job

training).Thissupersedestheneedfor6monthsofexperienceforthefirst2years.How-

ever,therequirementof6monthsofexperienceinthepreceding2yearswillneedtobe

metafterthesecondyear.

AMC 66.A.20(b)3 Privileges

Thewording“hastheadequatecompetencetocertifymaintenanceonthecorrespond-

ing aircraft” means that the licence holder and, if applicable, the organisation where

he/sheiscontracted/employed,shouldensurethathe/shehasacquiredtheappropriate

knowledge,skills,attitudeandexperiencetoreleasetheaircraftbeingmaintained.This

isessentialbecausesomesystemsandtechnologypresentintheparticularaircraftbeing

CAR-66


maintained may not have been covered by the training/examination/experience re-

quiredtoobtainthelicenceandratings.

Thisistypicallythecase,amongothers,inthefollowingsituations:

TyperatingswhichhavebeenendorsedonalicenceinaccordancewithAppendix

ItoAMCtoCAR-66“ListofTypeRatings”afterattendingtypetraining/on-the-job

trainingwhichdidnotcoverallthemodels/variantsincludedinsuchrating.For

example, a licence endorsed with the rating Airbus A318/A319/A320/A321

(CFM56)afterattendingtypetraining/on-the-jobtrainingcoveringonlytheAir-

bus320(CFM56).

TyperatingswhichhavebeenendorsedonalicenceinaccordancewithAppendix

ItoAMCtoCAR-66“ListofTypeRatings”afteranewvarianthasbeenaddedto

therating inAppendixI,withoutperformingdifferencetraining.Forexample,a

licenceendorsedwiththeratingBoeing737-600/700/800/900forapersonwho

alreadyhadtheratingBoeing737-600/700/800,withoutperforminganydiffer-

encetrainingforthe737-900.

Work being carried out on a model/variant for which the technical design and

maintenancetechniqueshavesignificantlyevolvedfromtheoriginalmodelused

inthetypetraining/on-the-jobtraining.

Specific technologyandoptions selected byeachcustomerwhichmay not havebeencoveredbythetypetraining/on-the-jobtraining.

ChangesinthebasicknowledgerequirementsofAppendixItoCAR-66notrequir-

ingreexaminationofexistinglicenceholders(grandfatheredprivileges).

Theendorsementofgroup/subgroupratingsbasedonexperienceonarepresenta-

tivenumberoftasks/aircraftorbasedontypetraining/examinationonarepre-

sentativenumberofaircraft.

Personsmeetingtherequirementsof6monthsofexperienceevery2yearsonly

oncertainsimilaraircrafttypesasallowedbyAMC66.A.20(b)2.

PersonsholdingaCAR-66licencewithlimitations,obtainedthroughconversionof

pre-existingqualifications(66.A.70),wheresuchlimitationsaregoingtobelifted

afterperformingthe corresponding basic knowledgeexaminations. In this case,

thetyperatingsendorsedinthelicencemayhavebeenobtainedwithoutcovering

alltheaircraftsystems(becauseofthepreviouslimitations)andtherewillbeneed

toassessand,ifapplicable,totrainthispersononthemissingsystems.

AdditionalinformationisprovidedinAMC145.A.35(a).

CAR-66


GM 66. A. 20 (b) 4 Privileges

1.HoldersofaCAR-66aircraftmaintenancelicencemaynotexercisecertificationpriv-ilegesunlesstheyhaveageneralknowledgeofthelanguageusedwithinthemainte-nanceenvironmentincludingknowledgeofcommonaeronauticaltermsinthelan-guage.Thelevelofknowledgeshouldbesuchthatthelicenceholderisableto:

-readandunderstandtheinstructionsandtechnicalmanualsinusewithintheorganisation; makewrittentechnicalentriesandanymaintenancedocumentationentries,which

canbeunderstoodbythosewithwhomtheyarenormallyrequiredtocommuni-cate;

readandunderstandthemaintenanceorganisationprocedures; communicateatsuchalevelastopreventanymisunderstandingwhenexercising

certificationprivileges.

2. Inallcases,thelevelofunderstandingshouldbecompatiblewiththelevelofcertifi-cationprivilegesexercised.

GM 66.A.25(a) Basic knowledge requirements

Thelevelsofknowledgeforeachlicence(sub)categoryaredirectlyrelatedtothecom-

plexityof thecertificationsrelatedto thecorrespondinglicence(sub)category,which

meansthatcategoryAshoulddemonstratealimitedbutadequatelevelofknowledge,

whereascategoryB1,B2shoulddemonstrateacompletelevelofknowledgeintheap-

propriatesubjectmodule

AMC 66.A.30 (a) Experience requirements

1. Providedthattheexperiencerequirementspecifiedat66.A.30.a.(1)and(2)shallbereducedbyoneyearincaseofanapplicantwhohassatisfactorilycompletedtrain-inginanytrainingorganizationapprovedunderrule133BorwhohasacquiredaDegreeinanalliedfieldofEngineeringfromarecognizedUniversity;

2. WhileanapplicanttoaCAR-66CategoryClicencemaybequalifiedbyhaving3years

experienceascategoryB1orB2certifyingstaffonlyinlinemaintenance,itishowever

recommendedthatanyapplicantforacategoryCholdingaB1orB2licencedemon-

strateatleast12monthsexperienceasaB1orB2basemaintenancesupportstaff.

3.Askilledworkerisapersonwhohassuccessfullycompletedatrainingacceptableto

theDGCAandinvolvingthemanufacture,repair,overhaulorinspectionofmechani-

cal,electricalorelectronicequipment.Thetrainingwouldincludetheuseoftoolsand

measuringdevices.

CAR-66


4.Maintenanceexperienceonoperatingaircraft:

-Meanstheexperienceofbeinginvolvedinmaintenancetasksonaircraftwhicharebeingoperatedbyairlines,airtaxiorganisations,owners,etc.;

-Shouldcoverawiderangeoftasksinlength,complexityandvariety;-Aimsatgainingsufficientexperienceintherealenvironmentofmaintenanceas

opposedtoonlythetrainingschoolenvironment;-Maybegainedwithindifferenttypesofmaintenanceorganisations(CAR-145,

M.A.SubpartFetc.)orunderthesupervisionofindependentcertifyingstaff;-MaybecombinedwithCAR-147approvedtrainingsothatperiodsoftrainingcan

beintermixedwithperiodsofexperience,similartoanapprenticeship

AMC 66.A.30 (d) Experience requirements

Tobeconsideredasrecentexperience;atleast50%oftherequired12monthexperienceshouldbegainedwithinthe12monthperiodpriortothedateofapplicationfortheCAR-66 aircraft maintenance license. The remainder of the experience should have beengainedwithinthe7 yearperiodpriortoapplication. Itmustbenotedthattherestofthebasicexperiencerequiredby66.A.30mustbeobtainedwithinthe10yearspriortotheapplicationasrequiredby66.A.30(f).

AMC 66.A.30 (e) Experience requirements 1. For category A the additional experience of civil aircraft maintenance should be a

minimumof6months.ForcategoryB1orB2,theadditionalexperienceofcivilair-

craftmaintenanceshouldbeaminimumof12months.

2. Aircraftmaintenanceexperiencegainedoutsideacivilaircraftmaintenanceenviron-

ment can include aircraft maintenance experience gained in armed forces, coast

guards,policeetc.orinaircraftmanufacturing.

GM. 66. A. 35 Skill Test Requirements

Anapplicationforappearinginofskilltesttodemonstrateaircraftmaintenanceskill

shallbemadeonCAForm19-09(ReferAppendix-V)withnecessarydocumentsand

fees to DGCA. An applicant who fulfils the Aircraft Type Training and Examination

Standard,OnJobTrainingasdetailedinAppendix-IIItoCAR66shallonlybepermitted

toappearinskilltest.

ProceduresforappearingskilltestisdetailedinAPMChapter19.

CAR-66


GM 66.A.40 Continued validity of the aircraft maintenance licence

ValidityoftheCAR-66aircraftmaintenancelicenceisnotaffectedbyrecencyofmainte-nanceexperiencewhereasthevalidityofthe66.A.20privilegesisaffectedbymainte-nanceexperienceasspecifiedin66.A.20(a).

GM 66.A.45(b) Endorsement with aircraft ratings

Anaircrafttyperatingincludesalltheaircraftmodels/variantslistedincolumn2ofAp-pendixItoAMCtoCAR-66.

When a person already holds a type rating on the licence and such type rating isamendedintheAppendixItoAMCtoCAR-66inordertoincludeadditionalmodels/var-iants,thereisnoneedforadditionaltypetrainingforthepurposeofamendingthetyperatinginthelicence.Theratingshouldbeamendedtoincludethenewvariants,uponrequestbytheapplicant,withoutadditionalrequirements.However,itistheresponsi-bilityofthelicenceholderand,ifapplicable,themaintenanceorganisationwherehe/sheisemployedtocomplywith66.A.20(b)3,145.A.35(a)andM.A.607(a),asapplicable,be-forehe/sheexercisescertificationprivileges.

Similarly, type training courses covering certain, but not all the models/variants in-cludedinatyperating,arevalidforthepurposeofendorsingthefulltyperating

AMC 66.A.45(e) Endorsement with aircraft ratings

1. ForthegrantingofmanufacturersubgroupratingsforGroup2aircraft,forB1andC

licenceholders,thesentence“atleasttwoaircrafttypesfromthesamemanufacturer

whichcombinedarerepresentativeoftheapplicablemanufacturersubgroup”means

thattheselectedaircrafttypesshouldcoverallthetechnologiesrelevanttotheman-

ufacturersubgroupinthefollowingareas:

-Flightcontrolsystems(mechanicalcontrols/hydromechanicallypoweredcon-

trols/electromechanicallypoweredcontrols);and-Avionicsystems(analoguesystems/digitalsystems);and-Structure(manufacturedofmetal/composite/wood).

Incaseswherethereareverydifferentaircrafttypeswithinthesamemanufacturer

subgroup,itmaybenecessarytocovermorethantwoaircrafttypestoensureade-

quaterepresentation.

Forthispurposeitmaybepossibletouseaircrafttypesfromthesamemanufacturer

classifiedinGroup1aslongastheselectedaircraftbelongtothesamelicencesub

categoryforwhichtheratingwillbeendorsed.

2. Forthegrantingof fullsubgroupratings forGroup2aircraft, forB1 andC licence

holders, the sentence “at least three aircraft types from different manufacturers

CAR-66


whichcombinedarerepresentativeoftheapplicablesubgroup”meansthatthese-

lectedaircrafttypesshouldcoverallthetechnologiesrelevanttothemanufacturer

subgroupinthefollowingareas:

- Flight control systems (mechanical controls/hydromechanically powered con-

trols/electromechanicallypoweredcontrols);and-Avionicsystems(analoguesystems/digitalsystems);and-Structure(manufacturedofmetal/composite/wood).

Incaseswherethereareverydifferentaircrafttypeswithinthesamesubgroup,itmaybenecessarytocovermorethanthreeaircrafttypestoensureadequaterepresentation.ForthispurposeitmaybepossibletouseaircrafttypesfromdifferentmanufacturersclassifiedinGroup1aslongastheselectedaircraftbelongtothesamelicencesubcate-goryforwhichtheratingwillbeendorsed.3. Formanufacturersubgroupratings, the term“manufacturer”meanstheTCholder

definedinthecertificationdatasheet,whichisreflectedinthelistoftyperatingsin

AppendixItoAMCtoCAR-66.

InthecaseofanaircraftratingwherethetyperatingreferstoaTCholdermadeofacombinationoftwomanufacturerswhichproduceasimilaraircraft(i.e.AGUSTA/BEL-LELICOPTERTEXTRONoranycaseofaircraftsimilarlybuiltbyanothermanufacturer),thiscombinationshouldbeconsideredasonemanufacturer.Asaconsequence: Whenalicenceholdergetsamanufacturertypeoramanufacturersubgrouprating

madeofacombinationofmanufacturers,itcoversthecombinationofsuchmanu-facturers.

Whenalicenceholderwhointendstoendorseafullsubgroupratingselectsthree

aircraftfromdifferentmanufacturers,thismeansfromdifferentcombinationsofmanufacturersasapplicable.

AMC 66.A.45(d), (e)3, (f)1 and (g)1 Endorsement with aircraft ratings

1 The“practicalexperience”shouldcoverarepresentativecrosssectionincludingat

least50%oftaskscontainedinAppendixIItoAMCrelevanttothelicencecategory

and to the applicable aircraft type ratings or aircraft (sub)group ratings being en-

dorsed.ThisexperienceshouldcovertasksfromeachparagraphoftheAppendixII

list.OthertasksthanthoseintheAppendixIImaybeconsideredasareplacement

when they are relevant. In the case of (sub)group ratings, this experience may be

shownbycoveringoneorseveralaircrafttypesoftheapplicable(sub)groupandmay

includeexperienceonaircraftclassifiedingroup1,2and/or3aslongastheexperi-

enceisrelevant.Thepracticalexperienceshouldbeobtainedunderthesupervision

ofauthorisedcertifyingstaff.

CAR-66


2 InthecaseofendorsementofindividualtyperatingsforGroup2andGroup3aircraft,

forthesecondaircrafttypeofeachmanufacturer(sub)groupthepracticalexperience

shouldbereducedto30%ofthetaskscontainedinAppendixIItoAMCrelevantto

thelicencecategoryandtotheapplicableaircrafttype.Forsubsequentaircrafttypes

ofeachmanufacturer(sub)groupthisshouldbereducedto20%.

3.Practicalexperienceshouldbedemonstratedbythesubmissionofrecordsoralog-

bookshowingtheAppendixIItasksperformedbytheapplicant.Typicaldatatobe

recordedaresimilartothosedescribedinAMC66.A.20(b)2.

GM 66.A.45 Endorsement with aircraft ratings

Thefollowingtableshowsasummaryoftheaircraftratingrequirementscontainedin

66.A.45,66.A.50andAppendixIIItoCAR-66.

Thetablecontainsthefollowing: Thedifferentaircraftgroups;

Foreachlicence(sub)category,whichratingsarepossible(atthechoiceoftheappli-

cant)

oIndividualtyperatings;

oFulland/orManufacturer(sub)groupratings;

Foreachratingoption,whicharethequalificationoptions;

FortheB1.2licence(Group3aircraft) whicharethepossiblelimitationstobein-

cludedinthelicenceifnotsufficientexperiencecanbedemonstratedinthoseareas.

Note:OJTmeans“On-the-JobTraining”(AppendixIIItoCAR-66,Section6)andisonly

requiredforthefirstaircraftratinginthelicence(sub)category.

CAR-66


Aircraft rating requirements

Aircraft Groups B1 B2 licence C licence

Group 1

Complex motor powered

aircraft.

Multiple engine helicopters.

Aeroplanes certified above

FL290.

Aircraft equipped with

fly-by-wire.

Other aircraft when defined

DGCA

(For B1) Individual TYPE RATING Type training: - Theory + examination - Practical + assessment PLUS OJT (for first aircraft in licence subcat-egory

Individual TYPE RATING Type training: - Theory + examina-tion - Practical + assess-ment PLUS OJT (for first aircraft in licence category

Individual TYPE RATING Type training:

- Theory + exami-

nation

Group 2: Subgroups: 2a: single turboprop aeroplanes (*) 2b: single turbine engine helicopters (*) 2c: single piston-engine helicopters (*) (*) Except those classified in Group 1.

(For B1.1, B1.3, B1.4) Individual TYPE RATING (type training + OJT) or (type examination + practical experi-ence) Full SUBGROUP RATING (type training + OJT) or (type exami-nation + practical experience) on at least 3 aircraft representative of that subgroup Manufacturer SUBGROUP RATING (type training + OJT) or (type examination + practical experi-ence) on at least 2 aircraft representative of that manufacturer subgroup

Individual TYPE RATING (type training + OJT) or (type examination + practical experience) Full SUBGROUP RATING based on demonstra-tion of practical ex-perience Manufacturer SUBGROUP RAT-ING based on demonstra-tion of practical ex-perience

Individual TYPE RATING type training or type examination Full SUBGROUP RATING type training or type examination on at least 3 aircraft rep-resentative of that subgroup Manufacturer SUBGROUP RAT-ING type training or type examination on at least 2 aircraft rep-resentative of that manufacturer sub-group

Group 3 Piston-engine aeroplanes (except those classified in

Group 1.

(For B1.2) Individual TYPE RATING (type training + OJT) or (type examination + practical experi-ence) Full GROUP 3 RATING based on demonstration of practical experience Limitations:

Pressurised aeroplanes

Metal aeroplanes

Composite aeroplanes

Wooden aeroplanes

Metal tubing & fabric aeroplanes

Individual TYPE RATING (type training + OJT) or (type examination + practical experience) Full GROUP 3 RAT-ING based on demonstra-tion of practical ex-perience

Individual TYPE RATING type training or type examination Full GROUP 3 RATING based on demon-stration of practical experience

AMC 66.A.50(b) Limitations

1. The appropriate experience required to remove the limitations referred to in

66.A.45(f)shouldconsistoftheperformanceofavarietyoftasksappropriatetothe

limitationsunderthesupervisionofauthorisedcertifyingstaff.Thisshouldinclude

CAR-66


thetasksrequiredbya scheduledannual inspection.Alternatively, thisexperience

mayalsobegained,ifagreedbytheDGCA,bytheoreticalandpracticaltrainingpro-

videdbythemanufacturer,aslongasanassessmentisfurthercarriedoutandrec-

ordedbythismanufacturer.

2.Itmaybeacceptabletohavethisexperienceonjustoneaircrafttype,providedthat

this type is representativeof the (sub)group in relation to the limitation being re-

moved.

3.Theapplicationforthelimitationremovalshouldbesupportedbyarecordofexperi-

encesignedbytheauthorisedcertifyingstafforbyanassessmentsignedbytheman-

ufactureraftercompletionoftheapplicabletheoreticalandpracticaltraining.

GM 66.A.70 Conversion provisions

1. Asdescribedinpoint66.A.70,theconversionprovisionsapplytotheholderofaAME

LicencepriortothedateofentryintoforceofCAR-66..

2. Theconversionappliesto“certifyingstaffqualifications”suchas,forexample:

HoldingaAMElicence(orcompletedtheprocesstoobtainsuchalicence;)

Thisdoesnotmeanthatinordertobeentitledtoaconversionprocess,theapplicanthas

tobeexercisingcertificationprivileges.Apersonmayholda“certifyingstaffqualifica-

tion”whilenothavingcertificationprivileges(orwhileexercisingverylimitedcertifica-

tionprivilegesbelowhis/herqualification)fordifferentreasonssuchas, forexample,

thefollowing:

Thepersonisworkingas“supportstaff”inthebasemaintenanceenvironment;

Thepersonhasbeenauthorisedonlyforaverylimitedrangeoftasks(lowerthan

whathe/shewouldbeentitledifhis/herqualificationisconsidered)sincetheper-

sonisworkinginalinestationwherethescopeoftasksisverylimited;

Thepersonholdsalicencewithawiderscopethanthescopeoftheorganisation

wherehe/sheisemployed;

Thepersonisworkingoutsidetheaviationindustryoristemporarilyonleavedue

todifferentreasons(medical,personal,etc.).

Thesepersonsareentitledtohavetheconversionperformedinaccordancewiththefull

scopeoftheirqualificationandthefullprivilegesthattheywouldbeentitledtoholdon

thebasisofsuchqualification.

CAR-66


3. Asdescribedinpoint66.A.70,certifyingstaffqualificationseligibleforconversionare

thosevalid“priortothedateofentryintoforceofCAR-66”.

4.Althoughonlythosecertifyingstaffqualificationsgainedasindicatedaboveareeligi-

bleforconversion,thisdoesnotmeanthattheapplicationforconversionhastobe

submittedpriortothosedates.Theapplicantisentitledtohavetheconversionper-

formedirrespectiveofwhenhe/sheappliesforconversion.

5.Acertifyingstaffqualificationcanbesubjecttomorethanoneconversionprocessand

canalsobeconvertedtomorethanonelicence(withanyapplicablelimitations).This

couldbethecase,forexample,forapersonwhoalreadyhadthecertifyingstaffqual-

ificationconvertedtoaB1.2licencewithlimitationslinkedtosomemissingelements

oftheCAR-66AppendixIandIIstandard(following66.A.70(c)).Thispersonwould

beentitledtoapplyandhavehis/hercertifyingstaffqualificationconvertedtoaB1.2

onthebasisof66.A.70(d),whichwouldmeanthatthereisnoneedtocomparewith

theCAR-66AppendixIandIIstandard,introducingonlythoselimitationsrequired

tomaintaintheexistingprivileges.

GM 66.A.70(c) Conversion provisions

Forexample,alimitationcouldbewhereapersonholdsapre-existingcertifyingstaff

qualificationwhichcovered,tothestandardofCAR-66AppendixIandII,allthemod

ules/subjectscorrespondingtotheB1licenceexceptforelectricalpowersystems.This

personwouldreceiveaCAR-66aircraftmaintenancelicenceintheB1categorywitha

limitation(exclusion)onelectricalpowersystems.

Forremovaloflimitations,referto66.A.50(c).

GM 66.A.70(d) Conversion provisions

Inthecaseofaircraftnotinvolvedincommercialairtransportotherthanlargeaircraft,

an example of limitations could be where a person holds a pre CAR-66 qualification

whichcoveredprivilegestoreleaseworkperformedonaircraftstructures,powerplant,

mechanicalandelectricalsystemsbutexcludedprivilegesonaircraftequippedwithtur-

bineengine,aircraftabove2000kgMTOM,pressurisedaircraftandaircraftequipped

withretractablelandinggear.ThispersonwouldreceiveaCAR-66aircraftmaintenance

licenceintheB1.2(sub)categorywiththefollowinglimitations(exclusions):

Aircraftinvolvedincommercialairtransport(thislimitationalwaysexists);Air-

craftabove2000kgMTOM;

Pressurisedaircraft;

Aircraftequippedwithretractablelandinggear.

CAR-66


Anotherexampleoflimitationscouldbewhereapilot-ownerholdsapreCAR-66quali-

ficationwhichcoveredprivilegestoreleaseworkperformedonaircraftstructures,pow-

erplant,mechanicalandelectricalsystemsbutlimitedtohis/herownaircraftandtoa

particularaircrafttype(forexample,aCessna172).Thispilot-ownerwouldreceivea

CAR-66aircraftmaintenancelicenceintheB1.2(sub)categorywiththefollowinglimi-

tations(exclusions):

Aircraftinvolvedincommercialairtransport(thislimitationalwaysexists);

AircraftotherthanaCessna172;

Aircraftnotownedbythelicenceholder.

Theessentialaspectisthatthelimitationsareestablishedinordertomaintainthepriv-

ilegesofthepreCAR-66qualification,withoutcomparingthepreviousqualificationwith

thestandardofCAR-66AppendixIandII.

Forremovaloflimitations,referto66.A.50(c).

AMC to Section 1 of Appendix III to CAR-66 “Aircraft Type Training and Examina-

tion Standard. On-the-Job Training”

Aircrafttypetraining1.Aircrafttypetrainingmaybesubdividedinairframeand/orpowerplantand/or

avionics/electricalsystemstypetrainingcourses

i. Airframetypetrainingcoursemeansatypetrainingcourseincludingallrele-

vant aircraft structure and electrical and mechanical systems excluding the

powerplant.

ii. Powerplanttypetrainingcoursemeansatypetrainingcourseonthebareen-

gine,includingthebuild-uptoaquickenginechangeunit.

iii. Theinterfaceoftheengine/airframesystemsshouldbeaddressedbyeitherair-

frameorpowerplant type trainingcourse. Insomecases, suchas forgeneral

aviation,itmaybemoreappropriatetocovertheinterfaceduringtheairframe

courseduetothelargevarietyofaircraftthatcanhavethesameenginetype

installed.

iv. Avionics/electricalsystemstypetrainingcoursemeanstypetrainingonavion-

ics andelectrical systemscoveredbybut not necessarily limited toATA(Air

TransportAssociation)Chapters22,23,24,25,27,31,33,34,42,44,45,46,73

and77orequivalent.

CAR-66


2.Practicaltrainingmaybeperformedeitherfollowingorintegratedwiththetheoreti-

calelements.However,itshouldnotbeperformedbeforetheoreticaltraining.

3.Thecontentofthetheoreticalandpracticaltrainingshould:

i. addressthedifferentpartsoftheaircraftwhicharerepresentativeofthestruc-

ture,thesystems/componentsinstalledandthecabin;and

ii. includetrainingontheuseoftechnicalmanuals,maintenanceproceduresand

theinterfacewiththeoperationoftheaircraft.

iii. Therefore,itshouldbebasedonthefollowingelements:

a. Typedesignincludingrelevanttypedesignvariants,newtechnologyandtech-

niques;

b. Feedbackfromin-servicedifficulties,occurrencereporting,etc.;

c. Significantapplicableairworthinessdirectivesandservicebulletins;

d. Knownhumanfactorissuesassociatedwiththeparticularaircrafttype;

e. Useofcommonandspecificdocumentation,(whenapplicable,suchasMMEL,

AMM,MPD, TSM, SRM, WD, AFM, tool handbook), philosophy of the trouble-

shooting,etc.;

f. Knowledgeofthemaintenanceon-boardreportingsystemsandETOPSmainte-

nanceconditions,whenapplicable;

g. Useofspecial toolingand testequipment andspecificmaintenancepractises

includingcriticalsafetyitemsandsafetyprecautions;

h. Significant and critical tasks/aspects from the MMEL, CDL, Fuel Tank Safety

(FTS),airworthinesslimitationitems(ALI)includingCriticalDesignConfigura-

tionControlLimitations(CDCCL),CMRandallICAdocumentationsuchasMRB,

MPD,SRM,AMM,etc.,whenapplicable.

i. Maintenanceactionsandprocedurestobefollowedasaconsequenceofspecific

certificationrequirements,suchas,butnotlimitedto,RVSM(ReducedVertical

SeparationMinimum)andNVIS(NightVisionImagingSystems);

j. Knowledgeofrelevantinspectionsandlimitationsasapplicabletotheeffectsof

environmentalfactorsoroperationalproceduressuchascoldandhotclimates,

wind,moisture,sand,de-icing/anti-icing,etc.

CAR-66


ThetypetrainingdoesnotnecessarilyneedtoincludeallpossiblecustomeroptionscorrespondingtothetyperatingdescribedintheAppendixItoAMCtoCAR-66.4.LimitedavionicsystemtrainingshouldbeincludedinthecategoryB1typetraining

astheB1privilegesincludeworkonavionicssystemsrequiringsimpleteststoprove

theirserviceability.

5.ElectricalsystemsshouldbeincludedinbothcategoriesofB1andB2typetraining.

6.Thetheoreticalandpracticaltrainingshouldbecomplementaryandmaybe:

i. Integratedorsplit;

ii. Supportedbytheuseoftrainingaids,suchas,trainers,virtualaircraft,aircraft

components, synthetic training devices (STD), computer-based training de-

vices(CBT),etc.

AMC to Paragraph 3.1(d) of Appendix III to CAR-66 “Aircraft Type Training and Examination Standard. On-the-Job Training” Training Needs Analysis for the theoretical element of the aircraft type training 1.Theminimumdurationforthetheoreticalelementofthetyperatingtrainingcourse,

asdescribedinAppendixIIItoCAR-66,hasbeendeterminedbasedon:

i. genericcategoriesofaircraftandminimumstandardequipmentfit;ii. theestimatedaveragedurationofstandardcoursesimparted.

2.ThepurposeoftheTrainingNeedsAnalysis(TNA)istoadaptandjustifytheduration

ofthecourseforaspecificaircrafttype.ThismeansthattheTNAisthemaindriverfordeterminingthedurationofthecourse,regardlessofwhetheritisaboveorbelowtheminimumdurationdescribedinAppendixIIItoCAR-66.

Intheparticularcaseoftypetrainingcoursesapprovedonthebasisoftherequire-mentsvalidbeforeRegulationthisCARisapplicableandhavingadurationforthetheoreticalelementequaltoorabovetheminimumdurationcontainedinparagraph3.1(c)ofAppendixIIItoCAR-66,itisacceptablethattheTNAonlycoversthediffer-ences introducedby thisCAR inparagraph3.1(e) “Content” and thecriteria intro-ducedinparagraph3.1(d)“Justificationofcourseduration”relatedtotheminimumattendanceandthemaximumnumberoftraininghoursperday.ThisTNAmayresultinachangeinthedurationofthetheoreticalelement.

3.ThecontentandthedurationderivingfromtheTNAmaybesupportedbyananalysis

fromtheTypeCertificateholder.4.Inordertoapproveareductionofsuchminimumduration,theevaluationdoneby

theDGCAshouldbeperformedonacase-by-casebasisappropriatetotheaircrafttype.Forexample,whileitwouldbeexceptionalforatheoreticalcourseforalarge

CAR-66


transportcategoryaircraftsuchasanA330orB757tobebelowtheminimumdura-tionshown,itwouldnotnecessarilybeexceptionalinthecaseofaGeneralAviation(GA)businessaircraftsuchasaLearjet45orsimilar.Typically,theTNAforaGAair-craftcoursewoulddemonstratethatacourseofashorterdurationsatisfiesthere-quirements.

5.WhendevelopingtheTNA,thefollowingshouldbeconsidered:

a)TheTNAshouldincludeananalysisidentifyingalltheareasandelementswherethereisaneed fortrainingaswellas theassociatedlearningobjectives,consideringthedesignphilosophyoftheaircrafttype,theoperationalenvironment,thetypeofoper-ationsandtheoperationalexperience.Thisanalysisshouldbewritteninamannerwhichprovidesareasonableunderstandingofwhichareasandelementsconstitutethecoursetomeetthelearningobjectives.

b)Asaminimum,theTrainingNeedAnalysis(TNA)shouldtakeintoaccountallthe applicableelementscontainedinparagraph3.1ofCAR-66AppendixIIIandassociatedAMCs.c)TheTNAshouldsetupthecoursecontentconsideringtheAppendixIIIobjectivesfor

eachleveloftrainingandtheprescribedtopicsinthetheoreticalelementtablecon-tainedinparagraph3.1ofCAR-66AppendixIII.

d)ForeachChapterdescribedinthetheoreticalelementtablecontainedinparagraph

3.1ofCAR-66AppendixIII,thecorrespondingtrainingtimeshouldberecordede)Typicaldocumentstobeusedtoidentifytheareasandelementswherethereisaneed

fortrainingtypicallyinclude,amongothers,theAircraftMaintenanceManual,MRBreport,CMRs,airworthinesslimitations,TroubleshootingManual,StructuralRepairManual,IllustratedPartsCatalogue,AirworthinessDirectivesandServiceBulletins.

f)Duringtheanalysisofthesedocuments:

i) Considerationshouldbegiventothefollowingtypicalactivities:

1. Activation/reactivation;2. Removal/installation;3. Testing;4. Servicing;5. Inspection,checkandrepairs;6. Troubleshooting/diagnosis.

ii) Forthepurposeofidentifyingthespecificelementsconstitutingthetraining

course,itisacceptabletouseafilteringmethodbasedoncriteriasuchas:

1. Frequencyofthetask;2. Humanfactorissuesassociatedtothetask;3. Difficultyofthetask;

CAR-66


4. Criticalityandsafetyimpactofthetask;5. In-serviceexperience;6. Novelorunusualdesignfeatures(notcoveredbyCAR-66AppendixI);7. Similaritieswithotheraircrafttypes;8. Specialtestsandtools/equipment.

iii) Itisacceptabletofollowanapproachbasedon:

1. Tasksorgroupsoftasks;or2. Systemsorsubsystemsorcomponents.

g)TheTNAshould:

i. Identifythelearningobjectivesforeachtask,groupoftasks,system,subsystemorcomponent;

ii. Associatetheidentifiedtaskstobetrainedtotheregulatoryrequirements(ta-

bleinparagraph3.1ofAppendixIIItoCAR-66);

iii. Organisethetrainingintomodulesinalogicalsequence(adequatecombinationofchaptersasdefinedinAppendixIIIofCAR-66);

iv. Determinethesequenceoflearning(withinalessonandforthewholesylla-

bus);

v. IdentifythescopeofinformationandlevelofdetailwithregardtotheminimumstandardtowhichthetopicsoftheTNAshouldbetaughtaccordingtotheset-upobjectives.

vi. Addressthefollowing:

1. Descriptionofeachsystem/componentincludingthestructure(where

applicable);2. System/componentoperationtakingintoaccount:

a. Complexityofthesystem(e.g.theneedoffurtherbreakdownintosubsys-

tems,etc.);

b.Designspecificswhichmayrequiremoredetailedpresentationormaycontributetomaintenanceerrors;

b. Normalandemergencyfunctioning;

c. Troubleshooting;

d. Interpretationofindicationsandmalfunctions;

e. Useofmaintenancepublications;

f.Identificationofspecialtoolsandequipmentrequiredforservicingandmaintainingtheaircraft;

CAR-66


g.MaintenancePractices;h.Routineinspections,functionaloroperationaltests,rigging/adjustment,etc.

vii. Describethefollowing:

1. Theinstructionalmethodsandequipment,teachingmethodsandblendingof

theteachingmethodstoensuretheeffectivenessofthetraining;2. Themaintenancetrainingdocumentation/materialtobedeliveredtothestu-

dent;Facilitateddiscussions,questioningsession,additionalpractice-orientedtraining,etc.;

3. Thehomework,ifdeveloped;4. Thetrainingprovider’sresourcesavailabletothelearner.

h)Itisacceptabletodifferentiatebetweenissueswhichhavetobeledbyaninstructor

andissueswhichmaybedeliveredthroughinteractivesimulationtrainingdevicesand/orcoveredbyweb-basedelements.Overalltimeofthecoursewillbeallocatedaccordingly.

i)Themaximumnumberoftraininghoursperdayforthetheoreticalelementoftype

trainingshouldnotbemorethan6hours.Atraininghourmeans60minutesoftui-tionexcludinganybreaks,examination,revision,preparationandaircraftvisit.Inex-ceptionalcases,theDGCAmayallowdeviationfromthisstandardwhenitisproperlyjustifiedthattheproposednumberofhoursfollowspedagogicalandhumanfactorsprinciples.Theseprinciplesareespeciallyimportantinthosecaseswhere:

i. Theoreticalandpracticaltrainingareperformedatthesametime;

ii. Training and normal maintenance duty/apprenticeship are performed at thesametime.

j)Theminimumparticipationtimeforthetraineetomeettheobjectivesofthecourse

shouldnotbelessthan90%ofthetuitionhoursofthetheoreticaltrainingcourse.Additionaltrainingmaybeprovidedbythetrainingorganisationinordertomeettheminimumparticipationtime.Iftheminimumparticipationdefinedforthecourseisnotmet,acertificateofrecognitionshouldnotbeissued.

k)TheTNAisalivingprocessandshouldbereviewed/updatedbasedonoperationfeedback,maintenanceoccurrences,AirworthinessDirectives,majorservicebulle-

tinsimpactingmaintenanceactivitiesorrequiringnewcompetenciesformechanics,alertservicebulletins,feedbackfromtraineesorcustomersatisfaction,evolutionofthe maintenance documentation such as MRBs, MPDs, MMs, etc. The frequency atwhichtheTNAshouldbereviewed/updatedislefttothediscretionoftheorganisa-tionconductingthecourse.

NOTE: The examination is not part of the TNA. However, it should be prepared in accord-ance with the learning objectives described in the TNA.

CAR-66


AMC to Paragraphs 1(b), 3.2 and 4.2 of Appendix III to CAR-66 “Aircraft Type Training and Examination Standard. On-the-Job Training” Practical element of the aircraft type training 1.Thepracticaltrainingmayincludeinstructioninaclassroomorinsimulatorsbutpart

ofthepracticaltrainingshouldbeconductedinarealmaintenanceormanufacturerenvironment.

2.Thetasksshouldbeselectedbecauseoftheirfrequency,complexity,variety,safety,criticality,novelty,etc.Theselectedtasksshouldcoverallthechaptersdescribedin

thetablecontainedinparagraph3.2ofAppendixIIItoCAR-66.3.Thedurationofthepracticaltrainingshouldensurethatthecontentoftrainingre-

quiredbyparagraph3.2ofAppendix III to CAR-66 is completed.Nevertheless, foraeroplaneswithaMTOMequalorabove30000kg,thedurationforthepracticalele-ment of a type rating training course should not be less than two weeks unless ashorterdurationmeetingtheobjectivesofthetrainingandtakingintoaccountpeda-gogicalaspects(maximumdurationperday)isjustifiedtotheDGCA.

4.Theorganisationprovidingthepracticalelementofthetypetrainingshouldprovide

traineeswithascheduleorplan indicating thelistof taskstobeperformedunderinstructionorsupervision.Arecordofthetaskscompletedshouldbeenteredintoalogbookwhichshouldbedesignedsuchthateachtaskorgroupoftasksmaybecoun-tersignedbythedesignatedassessor.Thelogbookformatanditsuseshouldbeclearlydefined.

5.Inparagraph4.2ofAppendixIIItoCAR-66,theterm“designatedassessorsappropri-

atelyqualified”meansthattheassessorsshoulddemonstratetrainingandexperienceontheassessmentprocessbeingundertakenandbeauthorisedtodosobytheorgan-isation.

FurtherguidanceabouttheassessmentandthedesignatedassessorsisprovidedinAppendixIIItoAMCtoCAR-66.6.Thepracticalelement(forpowerplantandavionicsystems)oftheTypeRatingTrain-

ingmaybesubcontractedbytheapprovedCAR-147organisationunderitsqualitysystemaccordingtotheprovisionsof147.A.145(d)3andthecorrespondingGuidanceMaterial.

AMC to Paragraph 1(c) of Appendix III to CAR-66 “Aircraft Type Training and Ex-amination Standard. On-the-Job Training” Differences training

CAR-66


Approveddifferencetrainingisnotrequiredfordifferentvariantswithinthesameair-crafttyperating(asspecifiedinAppendixItoAMCtoCAR-66)forthepurposeoftyperatingendorsementontheaircraftmaintenancelicence.However,thisdoesnotnecessarilymeanthatnotrainingisrequiredbeforeacertifyingstaff authorisation can be issued by the maintenance organisation (refer to AMC66.A.20(b)3).

AMC to Section 5 of Appendix III to CAR-66 “Aircraft Type Training and Examina-tion Standard. On-the-Job Training” Type Examination Standard This Section 5 “Type Examination Standard” does not apply to the examination per-formedaspartoftypetraining.ThisSectiononlyappliestothosecaseswheretypeex-aminationisperformedasasubstitutefortypetraining.AMC to Section 6 of Appendix III to CAR-66 “Aircraft Type Training and Examina-tion Standard. On-the-Job Training” On-the-Job Training (OJT) 1.“Amaintenanceorganisationappropriatelyapprovedforthemaintenanceofthepar-

ticularaircrafttype”meansaCAR-145orM.A.SubpartFapprovedmaintenanceor-ganisationholdinganAratingforsuchaircraft.

2.TheOJTshouldincludeone-to-onesupervisionandshouldinvolveactualworktaskperformanceonaircraft/components,coveringlineand/orbasemaintenancetasks.3.TheuseofsimulatorsforOJTshouldnotbeallowed.4.TheOJTshouldcoveratleast50%ofthetaskscontainedinAppendixIItoAMCto

CAR-66.SometasksshouldbeselectedfromeachparagraphoftheAppendixIIlist.Tasksshouldbeselectedamongthoseapplicabletothetypeofaircraftandlicence(sub)categoryappliedfor.OthertasksthanthoseintheAppendixIImaybeconsid-eredasareplacementwhentheyarerelevant.Typically,inadditiontothevarietyandthecomplexity,theOJTtasksshouldbeselectedbecauseoftheirfrequency,safety,novelty,etc.

5.Upto50%oftherequiredOJTmaybeundertakenbeforetheaircrafttheoreticaltype

trainingstarts.6. The organisation providing the on-the-job training should provide trainees with a

scheduleorplanindicatingthelistoftaskstobeperformedundersupervision.Arec-ordofthetaskscompletedshouldbeenteredintoalogbookwhichshouldbedesignedsuchthateachtaskorgroupoftasksiscountersignedbythecorrespondingsupervi-sor.Thelogbookformatanditsuseshouldbeclearlydefined.

CAR-66


7.Regardingtheday-to-daysupervisionoftheOJTprogrammeintheapprovedmainte-nanceorganisationandtheroleofthesupervisor(s),thefollowingshouldbeconsid-ered:

i. It issufficient that the completionof individual OJTtasks isconfirmedbythe

directsupervisor(s),withoutbeingnecessarythedirectevaluationoftheasses-sor.

ii. Duringtheday-to-dayOJTperformance,thesupervisionaimsatoverseeingthe

completeprocess,includingtaskcompletion,useofmanualsandprocedures,ob-servanceofsafetymeasures,warningsandrecommendationsandadequatebe-haviourinthemaintenanceenvironment.

iii. Thesupervisor(s)shouldpersonallyobservetheworkbeingperformedtoen-

surethesafecompletenessandshouldbereadilyavailable forconsultation, ifneededduringtheOJTperformance.

iv. The supervisor(s) should countersign the tasks and release the maintenance

tasksasthetraineeisstillnotqualifiedtodoso.

v. Thesupervisor(s)shouldtherefore:

a) havecertifyingstafforsupportstaffprivilegesrelevanttotheOJTtasks;b) becompetentfortheselectedtasks;c) besafety-orientated;d) becapabletocoach(settingobjectives,givingtraining,performingsupervi-

sion,evaluating,handlingtrainee’sreactionsandculturalissues,managingobjectivelyandpositivelydebriefingsessions,determiningtheneedforex-tratrainingorreorientatethetraining,reporting,etc.);

e) bedesignatedbytheapprovedmaintenanceorganisationtocarryoutthe

supervision.

8.Regardingtheassessor,thefollowingshouldbeconsidered:

a) Thefunctionoftheassessor,asdescribedinSection6ofAppendixIIItoCAR-66,istoconductthefinalassessmentofthecompletedOJT.ThisassessmentshouldincludeconfirmationofthecompletionoftherequireddiversityandquantityofOJTandshouldbebasedonthesupervisor(s)reportsandfeedback.

b) InSection6ofAppendixIIItoCAR-66,theterm“designatedassessorappropri-atelyqualified”meansthattheassessorshoulddemonstratetrainingandexpe-rienceontheassessmentprocessbeingundertakenandshouldbeauthorisedtodosobytheorganisation.

FurtherguidanceabouttheassessmentandthedesignatedassessorsisprovidedinAp-pendixIIItoAMCtoCAR-66.

CAR-66


9 The procedures for OJT should be included into the Exposition Manual of the approvedmaintenanceorganisation(Chapter3.15,asindicatedinAMC145.A.70(a)).

TheseproceduresintheExpositionManualareapprovedbytheDGCA,andprovidingtrainingisnotoneoftheprivilegesofamaintenanceorganisation,theycanonlybeusedwhenthelicencingauthorityistheDGCA.Inothercases,itisuptothelicencingauthoritytodecidewhetheritacceptssuchproceduresforthepurposeofapprovingtheOJT(refertoAMC66.B.115).

AMC to Appendix III to CAR-66 “Aircraft Type Training and Examination Stand-ard. On-the-Job Training” Aircraft type training and On-the-Job Training Thetheoreticalandpracticaltrainingproviders,aswellastheOJTprovider,maycon-tracttheservicesofalanguagetranslatorinthecasewheretrainingisimpartedtostu-dentsnotconversantinthelanguageofthetrainingmaterial.Nevertheless,itremainsessentialthatthestudentsunderstandalltherelevantmaintenancedocumentation.Dur-ingtheperformanceofexaminationsandassessments,theassistanceofthetranslatorshouldbelimitedtothetranslationofthequestions,butshouldnotprovideclarifica-tionsorhelpinrelationtothosequestions.

CAR-66


APPENDICES to AMC for CAR-66

Appendix I

AIRCRAFT TYPE RATINGS

FOR CAR-66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE

The following aircraft type ratings should be used to ensure a common standard

throughoutIndia.

Theinclusionofanaircrafttypeinthelicencedoesnotindicatethattheaircrafttypehas

beengrantedatypecertificateundertheAircraftRuleNo.49AandCAR-21,thislistis

onlyintendedforthemaintenancepurposes.

Inordertokeepthislistcurrentandtyperatingsconsistent,suchinformationshouldbe

firstpassedontotheDGCAdaw@dgca.nic.inbyaffectedpersonnelororganizationsto

issueatyperatingthatisnotincludedinthislist.

Notes:

Whenamodificationisintroducedtoanaircrafttyperatingortoanenginedesignationintheratingwhichaffectlicencesalreadyissued,theratingsontheAMElicencesmaybemodifiedatthenextrenewalorwhenthelicenceisreceivedforendorsement/re-issued, unlessthereisanurgentreasontomodifythelicence.Notesonaircraftmodifiedby SupplementalTypeCertificate STC:.

WhenanaircrafthasbeenmodifiedbyanSTCforinstallationofanotherengine,

theCAR-66typeratingofthisaircraftmaychangei.e. fromGroup2toGroup1.

Thisisnotreflectedinthisdocument.Incasetheapplicanttoalicencefacessuch

acase,theholderofAMELicensemayinformtheDGCAandanewtyperatingwill

bedefinedbytheDGCA

Inthefollowingtables:

Thecolumn‘TCHolder’includestheTCholderasdefinedintheTypeCertificateDataSheetsTCDS(EASA,FAAorother)ortheSpecificAirworthinessSpecifications(SAS).

InGroup3,athirdcolumnhasbeenaddedwhichiscalled ‘Typeofstructure’and

whichintendstoassisttheDGCAinidentifyingtheexperiencerequiredforthistype

withaviewonremovingexistinglimitationsonthelicence.

CAR-66


Woodenstructurecoveredwithfabricisconsideredtofallunderwoodenstructure.

For Aeroplanes with a combination of structures; e.g. metal tubing fuselage and

woodenwings,bothexperience‘metaltubecoveredwithfabric’and‘woodenstruc-

ture’arerequired.

InGroup3,afourthcolumnhasbeenaddedwhichiscalled‘MTOM’andwhichintends

to assist in identifying the aeroplanes types where the Maximum Take-Off Mass

(MTOM)is:

—above2TandissubjecttoaB1.2licence,or

—2TandbelowandissubjecttoaB1.2orB3licence.

Column1includestheTCholderasdefinedintheTCDS(EASA,FAAorother).

Foraeroplanesofgroup1and2andhelicopters,theColumn2includestheaircraftmod-

elsasdefinedintherelevantTCDS(EASA,FAAorother).

Thefollowingcolumnincludesthe“commercialdesignation”whenavailable.

Column3includestherelevantindividualtyperating.Onlythedesignationsofratings

incolumn3shouldbeusedforendorsingindividualtyperatingsonCAR-66licences.

Note:aircraftSTCdataarenotincludedinthistable.

CAR-66


Group -1 Aeroplanes

Group -1 Aeroplanes

1. TC holder 2 Aeroplanes Model Commercial Desig-nation

3 Type Rating Endorsement

Airbus

A310-304

AirbusA310(GECF6)

A310-324 AirbusA310(PW4000)

A318-110series

Airbus A318/A319/A320/A321(CFM56)

A319-110series

A320-111

A320-210series

A321-110series

A321-210series

A319-130series

Airbus A319/A320/A321 (IAEV2500)

A320-230series

A321-130series

A321-230series

A330-200series

AirbusA330(GECF6)

A330-300series

A330-220series

AirbusA330(PW4000)

A330-320series

A330-240Series

AirbusA330(RRRB211Trent700)A330-340Series

A340-210

AirbusA340(CFM56)A340-310

AIRCRAFT IN-DUSTRIES

L410ML-410UVP-E9

Turbolet

LetL-410(WalterM601)

ATR-GIE Avionsde Transport Ré-gionals

ATR42-200

ATR 42-200/300 series (PWCPW120)

ATR42-320

ATR72-212 ATR72-200series(PWCPW120)

ATR42-50042-50042-600

ATR42-400/500/72-212A(PWCPW120)

CAR-66


Group -1 Aeroplanes



ATR72-212A72-500,72-600

BAESYSTEMS

BAeATP ATP(PWCPW120)

AVRO146-RJ70 BAe146/AVRO146-RJ(HoneywellALF500Series)

HS.748Series1

HS748(RRDDart)

HS.748Series2

HS748Series2A

HS748Series2B

Boeing

B737-200

Boeing737-200(PWJT8D)

B737-400, B737-300/500

Boeing737-300/400/500(CFM56)

B737-700

Boeing737-700/800/900(CFM56)

B737-800

B737-900

B737-900ER

B747-400

Boeing747-400(PW4000)B747-400F/SF(BCF)

B747-400 Boeing747-400(GECF6)

B747-400F/SF(BCF)

B757-200

Boeing757-200/300(PW2000)B757-200PF

B757-300

B757-200

Boeing757-200(RRRB211)

B777-200

Boeing777-200/300(GE90)B777-200LR

B777-300ER

B777-200

Boeing777-200/300(PW4000)

CAR-66


Group -1 Aeroplanes



B777-300

B787-8 DreamlinerBoeing 787-8 (GE GEnx)

B787-8 DreamlinerBoeing 787-8 (RR RB 211 Trent 1000)

BOMBARDIER

BD-100-1A10 Challenger300Bombardier BD-100-1A10 (Honey-wellAS907)

BD-700-1A10GlobalExpressGlobal6000

BombardierBD-700Series(RRDBR710)BD-700-1A11

Global5000Global5000GVFD

CL-600-2B16 (CL 604Variant)

Challenger-604(MSN<5701)

BombardierCL-600-2B16(variantCL604)(GECF34}

CL-600-2B16 (CL 604Variant)

Challenger-605(MSN>5701)

CL-600-2B19 Regional Jet Series100/200

BombardierCL-600-2B19(GECF34)

CRJ200BombardierCRJ200(GECF34)

CL-600-2C10Regional Jet Series700/701/702 Bombardier CL-600-2C10/-2D15/-

2D24/-2E25(GECF34)

CL-600-2D15Regional Jet Series705

DHC-8-401DHC-8-402

DHC-8 Series 400 Bombardier DHC-8-400 (PWC PW150)

CESSNA AIR-CRAFTCompany

525Citation Jet CJ1

Cessna 525/525A (Williams FJ 44)

525A

Citation Jet CJ2

525B CitationJetCJ3 CessnaC(WilliamsFJ44)

525C CitationJetCJ4 CessnaC(WilliamsFJ44)

550 CitationBravo

Cessna550/560(PWCPW530/535)560 CitationEncore

560 CitationEncore+

550 CitationII

Cessna550/560(PWCJT15D)

S550 CitationS/II

560 CitationV

560 CitationUltra

CAR-66


Group -1 Aeroplanes



560XL CitationExcel

Cessna560XL/XLS(PWCPW545)

560XLS CitationXLS

650 CitationIII–VIIV

Cessna650(HoneywellTFE731)

650 CitationVII

Cessana

680SovereignSovereign+

Cessna680(PWCPW306)

750 CitationX Cessna750(RRCorpAE3007C)

DassaultAviation

Falcon900EX Falcon900EX(HoneywellTFE731)

Falcon900EX F900EXEASy

Falcon 900EX EASy (HoneywellTFE731)

Falcon900EX F900DX

Falcon900EX F900LX

Falcon2000 Falcon2000(CFE738)

Falcon2000EX Falcon2000EX(PWCPW308)

Falcon2000EX F2000EXEASy

Falcon2000EXEASy(PWCPW308)

Falcon2000EX F2000DX

Falcon2000EX F2000LX

Falcon7X

Falcon7X(PWCPW307A)

RUAG AerospaceGmbH (DORN-IER)

228-200series Dornier228(HoneywellTPE331)

EMBRAER

EMB-500 Phenon-100 EmbraerEMB-500(PWCPW617)

EMB-135BJEMB145

Legacy600Legacy650

Embraer EMB-135/145 (RR CorpAE3007A)

ERJ170-100LRERJ170-200LR

ERJ-170ERJ-175

EmbraerERJ-170Series(GECF34)

ERJ190-100/200ERJ-190ERJ-195

EmbraerERJ-190Series(GECF34)

FOKKER SER-VICES

F27Mark100 Friendship

FokkerF27/FairchildF-27/FH-227(RRDDart)



CAR-66


Group -1 Aeroplanes





GULFSTREAM

AEROSPACELP

(GALP)c/oIsrael

Aircraft

Industries

Gulfstream200/Galaxy Galaxy200Gulfstream (IAI) 200/Galaxy (PWCPW306)

Gulfstream G150

Gulfstream G150 Gulfstream (IAI) G150 (Honeywell TFE731

G IV GIV / SP

Gulfstream G IV /GIV /SP

Gulfstream GIV Series (RRD Tay )

G V ?SP (G500) GV-SP ( G550)

Gulfstream G 500 Gulfstream G 550

Gulfstream G V SP Series ( RRD –BR710 )

G100 Gulfstream G 100 Gulfstream G 100 ( Honeywell TFE

731 )

HAWKERBEECHCRAFTCorporation

HS.125series700 "HawkerSiddeley"BAe 125 Series 700 (HoneywellTFE731)

Hawker750 Hawker750

BAe 125 Series750/800XP/850XP/900XP (Honey-wellTFE731)

Hawker800XP Hawker800XP



300 SuperKingAir

Beech300Series(PWCPT6)

300LW SuperKingAir

B300 SuperKingAir350

B300C SuperKingAir350C

400 BeechjetBeech 400 / Mitsubishi MU-300(PWCJT15)

400ABeechjet (Hawker400XP)

1900 Airliner

Beech1900(PWCPT6)1900C Airliner

1900D Airliner

4000 Hawker4000 Hawker4000(PWCPW308)

CAR-66


Group -1 Aeroplanes



LearJet

Learjet45 LJ45Learjet Model 45 (HoneywellTFE731)

Learjet40 LJ45

Learjet60 LJ60

LJ60XR

Learjet60(PWCPW305)

BEECHCRAFTCorporationBEECHCRAFT

Corporation

65-90

KingAir

Beech90Series(PWCPT6)

C90

C90A

C90GT

C90GTi

B200/B200C

Beech200Series(PWCPT6)B200CT

B200GT

B200T

390 Premier1,1A Beech390(WilliamsFJ44)

99/99A/100 KingAir Beech99/100Series(PWCPT6)

PIAGGIOAeroIn-dustries

P180 Avanti PiaggioP180Avanti/AvantiII(PWCPT6)

P180 AvantiII

PILATUS AIR-CRAFT

PC-12 PilatusPC-12(PWCPT6)

ASIAviation

F406 Caravan2 Reims-cessnaF406(PWCPT6)

VIKING AIR(Bombardier)(DeHavilland)

DHC-6-1 TwinOtter

DeHavillandDHC-6(PWCPT6)

DHC-6-100/110

DHC-6-200/210

DHC-6-300/310/320

DHC-6-400

CAR-66


Group 1 Helicopter

1 TC Holder 2 Aeroplanes Model Commercial Designation

3 Type rating endorsement

AGUSTAWestland A109E

Agusta A109 Series (PWCPW206/207)

A109S

AW109SP

AW/109N

A109

Agusta A109 Series (RR Corp250)

A109A

109C

AW139 AgustaAW139(PWCPT6)

BELL HELICOPTER TEX-TRON

212 Bell212/AgustaAB212(PWCPT6)

412 Bell412/AgustaAB412(PWCPT6)

412EP

412CF

BELL HELICOPTER CAN-ADA

427 Bell427(PWCPW207D)

222 Bell222(HoneywellLTS101)

222B

222U

230 230 Execu-tive

Bell230(RRCorp250)

230Utility

230EMS

429 Bell429(PWCPW207D)

430 Bell430(RRCorp250)

AIRBUSHELICOPTERS

AS355E Eurocopter AS 355 (RR Corp250)AS355F

CAR-66


Group 1 Helicopter

1 TC Holder 2 Aeroplanes Model Commercial Designation


AIRBUSHELICOPTERS

Contd---

AS355F1

AS355F2

AS355N EurocopterAS355(TurbomecaArrius1)

AS355NP

SA365N Dauphin Eurocopter SA 365 N (Tur-bomecaArriel1)

SA365N1 Dauphin Eurocopter SA 365 N1, AS 365N2(TurbomecaArriel1)

AS365N2

AS365N3 Dauphin Eurocopter AS 365 N3 (Tur-bomecaArriel2C)

EC155B EurocopterEC155(TurbomecaArriel2)

EC155B1

EUROCOPTERDeutschlandGMBH

EC135P1Series Eurocopter EC 135 (P&W206/207)

EC135P2Series

EC135P3Series

EC135T1

EurocopterEC135(TurbomecaArrius2B)

EC135T2

EC135T3

MBB-BK117C2 EC145 Eurocopter MBB-BK 117 C2(TurbomecaArriel1)

HINDUSTAN AERO-NAUTICSLtd.

DHRUV DHRUV

MDHELICOPTERS,INC. MD900 MD Helicopters MD900 (PWCPW206/207)

MOSCOWHELICOPTERSPLANT

MI172 M1 172 - Klimo TV/TB-3-117VM/BM

SIKORSKYAIRCRAFT

S-76C S-76C+ Sikorsky S-76C(Turbomeca Ar-riel2)S-76C S-76C++

S-76C Sikorsky S-76C(Turbomeca Ar-riel1)

CAR-66


SUBGROUP 2a: SINGLE TURBO-PROPELLER ENGINE AEROPLANES (Other than those in Group 1)

TC holder Type rating endorsement

CESSNAAIRCRAFTCompany Cessna208Series(PWCPT6)

PILATUSAIRCRAFT

PilatusPC-6Series(PWCPT6)

PilatusPC-6Series(TurbomecaAstazou)

PilatusPC-6Series(HoneywellTPE331)

CAR-66


SUBGROUP 2b: SINGLE TURBINE ENGINE HELICOPTERS (Other than those in Group 1)

1 TC Holder 2 Helicopter Model Commercial Designation


AGUSTA A119AW119MKII

Koala Agusta A119/Agusta AW119MKII(PWCPT6)

BELLHELICOPTERCANADA 407 Bell407(RRCorp250)

AGUSTA

AB206A

AgustaAB206/Bell206(RRCorp250)

AB206B

BELL HELICOPTER TEX-TRONCANADALIMITED

206seriesfromAtoL

THE ENSTROM HELICOP-TERCORPORATION

480 Enstrom480(RRCorp250)

480B

AIRBUS HELICOP-TERS

AS350 Ecureuil EurocopterAS350(TurbomecaArriel1)

AS350B1

AS350B2

AS350BA

AS350BB

AS350B3 EurocopterAS350(TurbomecaArriel2)

AS350D Eurocopter AS 350 (HoneywellLTS101)

EC120B Colibri EurocopterEC120(TurbomecaArrius2F)

EC130B4EC130T2

EurocopterEC130(TurbomecaArriel2)

SA315B Lama Eurocopter SA 315B (Tur-bomecaArtouste)

SA316BAlouetteIII

EurocopterSA316B(Tur-bomecaArtouste)

MDHELICOPTERSINC.(MDHI)

500N

MDHelicopters500NN/

AMD500N(RRCorp250)

MD600N

ROBINSONHELICOPTER R66 RobinsonR66(RRCorps250)

SCHEIZERAIRCRAFTCORP 269D Scgeizer269D(RRCorp250)

CAR-66


SUBGROUP 2C: SINGLE PISTON ENGINE HELICOPTERS (Other than those in Group 1)

1 TC Holder 2 Helicopter Model Commercial Designation


THE ENSTROM HELICOP-TERCORPORATION

F-28series

EnstromF-28(Lycoming)

SEI(BREDA-NARDI) NH300C Model300C Schweizer / Breda Nardi(Hughes)269/300(Lycoming)

SCHWEIZERAIRCRAFTCORPORATION

269A

269B

269C

ROBINSONHELICOPTERCOMPANY

R22R44

RobinsonR22/R44Series(Ly-coming)

CAR-66


GROUP – 3 PISTON ENGINE AEROPLANE ( Other than in Group – 1 )

TC holder Type rating endorsement Type of struc-ture

Maximum Take off Mass

2 T and Be-low

Above 2 T

AEROSTARAIRCRAFTCorporation

PiperPA-60/61Series(Ly-coming)

Metal X

AmericanChampion Champion8Series(Ly-coming)

Wood+Metaltubingfabrics

X

CESSNA AIRCRAFT Com-pany/REIMSAVIATION

Cessna310/320Series(Conti-nental)

Metal X

Cessna336(Continental) Metal X

Cessna421(Continental) Composite X

CessnaT303(Continental) Metal X

Beech55Series(Continental) Metal X

Beech58Series(Continental) Metal X

Beech58P(Continental) Metal+Pres-surised

X

Beech65-80Series(Ly-coming)

Metal X

Beech76(Lycoming) Metal X

Beech95Series(Lycoming) Metal X

PiperAircraft

PiperPA-30Series(Ly-coming)

Composite

X


Composite

X

PiperPA-31P(Lycoming) Metal+Pres-surised

X


Metal X

PiperPA-34Series(Continen-tal)

Metal X

VULCANAIR VulcanairP.68Series(Ly-coming)

Metal X

CessnaAircraftCompany

Cessna/Reims-Cessna150/F150Series(Continen-tal)

Metal X

Cessna/Reims-Cessna152/F152Series(Lycoming)

Metal X


Metal X


Metal X

Cessna172Series(Thielert) Metal X

CAR-66


GROUP – 3 PITON ENGINE AEROPLANE ( Other than in Group – 1 )

TC holder Type rating endorsement Type of struc-ture


2 T and Be-low

Above 2 T

Cessna175Series(Conti-nental)

Metal X

Cessna177Series(Ly-coming)

Metal X


Metal X


Metal X


Metal X

Cessna/Reims-Cessna182/F182Series(SMA)

Metal X


Metal X


Metal X

Cessna206Series(Ly-coming)

Metal X

HAWKERBEECHCRAFTCorporation

Beech35Series(Continen-tal)

Metal X

Beech36Series(Continen-tal)

Metal X

LAVIAArgentinaS.A(La-viasa)


Metal X

PILATUSAIRCRAFT PilatusPC-6Series(Ly-coming)

Metal X

PIPERAIRCRAFT PiperPA-23Aztec(Ly-coming)

Metal X


Metal X


Metal X

PiperPA-28Series(Conti-nental)

Metal X

PiperPA-28Series(Thielert) Metal X


Metal X


Metal X

PiperPA-36Series(Conti-nental)

Metal X

SKYInt AviatHuskyA(Lycoming) Metal

X

CAR-66


GROUP – 3 PITON ENGINE AEROPLANE ( Other than in Group – 1 )

TC holder Type rating endorsement Type of structure


2 T and Be-low

Above 2 T

DIAMONDAIRCRAFTIndus-tries

DiamondDA42Series(Thielert) Composite

X

DiamondDA42Series(AustroEn-gine)

Composite

X

CIRRUSDesignCorporation CirrusSR20(Continental) Composite

X

Cirrus SR22 Series (Continen-tal)

DIAMOND AIRCRAFT In-dustries

DiamondDA40(Lycoming) Composite

X

DiamondDA40D(Thielert) Composite

X

Diamond DA40 (Austro En-gine)

Composite

X

NATIONAL AEROSPACELABORATORIES

Hansa3(Rotax) Composite

X

ZlinAircraft(MoravanAvi-ation

ZlinZ-242L(Lycoming) Metal x

CAR-66


AppendixIItoAMCtoCAR-66

Aircraft type practical experience and On-the-Job Training

list of tasks

I Time limits/Maintenance checks (

ATA 05 ) a. 100hourcheck(generalaviation

aircraft). b. BorCCheckcheck(transport

categoryaircraft) c. Assistcarryingoutascheduled

maintenancechecki.a.w.AMMd. Reviewaircraftmaintenancelog

forcorrectcompletione. Reviewrecordsforcompliancewith

airworthinessdirectives. f. Reviewrecordsforcompliancewith

componentlifelimits.g. ProcedureforInspectionfollowing

heavylanding.h. ProcedureforInspectionfollowing

lightningstrike.II Dimensions/Areas(ATA 06)

a. Locatecomponent(s)bystationnumber.

b. Performsymmetrycheck.

III Lifting and Shoring(ATA 07) Assistin:

a. Jackaircraftnoseortailwheel.b. Jackcompleteaircraft.c. Slingortrestlemajorcomponent.

IV Leveling /Weighing(ATA 08) a. Levelaircraft.b. Weighaircraft.c. Prepareweightandbalanceamend-

ment.d. Checkaircraftagainstequipment

list.V Towing and Taxiing( ATA 09 )

a. Prepareforaircrafttowingb. Towaircraftc. Bepartofaircrafttowingteam.

VI Parking and mooring(ATA 10) a. Tiedownaircraft.b. Park,secureandcoveraircraft.c. Positionaircraftindock. d. Securerotorblades.

VII Placards and Marking ( ATA11) a. Checkaircraftforcorrectplacards.b. Checkaircraftforcorrectmarkings.

VII Servicing ( ATA 12 ) a. Refuelaircraft.b. Defuelaircraftc. Carryouttanktotankfueltransferd. Check/adjusttirepressures.e. Check/replenishoillevel.f. Check/replenishhydraulicfluid

level.g. Check/replenishaccumulatorpres-

sure.h. Chargepneumaticsystem.i. Greaseaircraft.j. Connectgroundpower.k. Servicetoilet/watersysteml. Performpre-flight/dailycheck

IX Vibration and Noise Analysis ( ATA 18 )

a. Analyzehelicoptervibrationprob-lem.

b. Analyzenoisespectrum. c. Analyseenginevibration.

X Air Conditioning ( ATA 21 )

a. Replacecombustionheater. b. Replaceflowcontrolvalve.c. Replaceoutflowvalve.d. Replacesafetyvalve.e. Replacevapourcycleunit.f. Replaceaircycleunit.g. Replacecabinblower.h. Replaceheatexchanger.i. Replacepressurizationcontroller.j. Cleanoutflowvalves.k. Deactivate/reactivatecargoisola-

tionvalve.l. Deactivate/reactivateavionicsventi-

lationcomponentsm. Checkoperationofair

conditioning/heatingsystemn. Checkoperationofpressurization

systemo. Troubleshootfaultysystem

XI Auto flight ( ATA 22)

a. Installservos.b. Rigbridlecablesc. Replacecontroller.d. Replaceamplifier.

CAR-66


e. Replacementoftheautoflightsys-temLRUsincaseoffly-by-wireair-craft

f. Checkoperationofauto-pilot.g. Checkoperationofauto-throttle/

autothrust.h. Checkoperationofyawdamper.i. Checkandadjustservoclutch.j. Performautopilotgainadjustments.k. Performmachtrimfunctionalcheck.l. Troubleshootfaultysystem.m. Checkautolandsystemn. Checkflightmanagementsystemso. Checkstabilityaugmentationsystem

XII Communications ( ATA 23 ) a. ReplaceVHFcomunit.b. ReplaceHFcomunit.c. Replaceexistingantenna.d. Replacestaticdischargewicks.e. Checkoperationofradios.f. PerformantennaVSWRcheck.g. PerformSelcaloperationalcheck.h. Performoperationalcheckofpas-

sengeraddresssystem.i. Functionallycheckaudiointegrating

system.j. Repairco-axialcable.k. Troubleshootfaultysyste

XIII Electrical Power ( ATA 24 )

a. Chargelead/acidbattery.b. Chargeni-cadbattery.c. Checkbatterycapacity.

d. Deep-cycleni-cadbattery.e. ReplaceIntegrateddrive/genera-

tor/alternator.f. Replaceswitches.

g. Replacecircuitbreakers.h. Adjustvoltageregulator.i. Amendelectricalloadanalysisre-

port.j. Repair/replaceelectricalfeederca-

ble.k. PerformfunctionalcheckofIDG/

Generator/Alternatorl. Performfunctionalcheckofvoltage

regulator.m. Performfunctionalcheckofemer-

gencygenerationsystem.n. Troubleshootfaultysystem

XIV Equipment/Furnishings (ATA 25 )

a. Replacecarpetsb. Replacecrewseats.c. Replacepassengerseats.

d. Checkinertiareels.e. Checkseats/beltsforsecurity.f. Checkemergencyequipment.g. CheckELTforcompliancewithregu-

lations.h. Repairtoiletwastecontainer.i. Repairupholstery.j. Changecabinconfiguration.

k. Replaceescapeslides/ropes

l. Replacecargoloadingsystemactua-tor.

m. Testcargoloadingsystem.XV Fire protection ( ATA 26)

a. Checkfirebottlecontents.

b. Check/testoperationoffire/smokedetectionandwarningsys-tem.

c. Checkcabinfireextinguishercon-tents.

d. Checklavatorysmokedetectorsys-tem.

e. Checkcargopanelsealing.f. Installnewfirebottle.g. Replacefirebottlesquib.h. Troubleshootfaultysystem.i. Inspectenginefirewiredetection

systems.XVI Flight Controls ( ATA 27 )

a. Inspectprimaryflightcontrolsandrelatedcomponentsi.a.w.AMM.

b. Extending/retractingflaps&slats.c. Replacehorizontalstabilizer.d. Replacespoiler/liftdamper.e. Replaceelevator.f. Deactivation/reactivationofaileron

servocontrol.g. Replaceaileron.h. Replacerudder.i. Replacetrimtabs.j. Installcontrolcableandfittings.k. Replaceslats.l. Replaceflaps.m. Replacepoweredflyingcontrolunit.n. Replaceflapactuatoro. Adjusttrimtab.p. Adjustcontrolcabletension.q. Checkcontrolrangeanddirectionof

movement.r. Checkforcorrectassemblyandlock-

ing.s. Troubleshootfaultysystem.t. Functionaltestofprimaryflightcon-

trols.u. Functionaltestofflapsystem.

CAR-66


v. Operationaltestofthesidestickas-sembly.

w. OperationaltestoftheTHS.

x. THSsystemwearcheck.

XVII Fuel ( ATA 28 )

a. Waterdrainsystem(operation).

b. Replaceboosterpump.

c. Replacefuelselector.

d. Replacefueltankcells.

e. Replace/testfuelcontrolvalves.

f. Replacemagneticfuellevelindica-tors.

g. Replacewaterdrainvalve.h. Checkfilters.i. Flowchecksystem.

j. Checkcalibrationoffuelquantitygauges.

k. Checkoperationfeed/selectorsl. Checkoperationoffueldump/jetti-

sonsystem.m. Fueltransferbetweentanks.n. Pressuredefuel.Pressurerefuel

(manualcontrol).o. Troubleshootfaultysystem.

XVIII Hydraulics ( ATA 29 ) a. Replaceenginedrivenpump.b. Check/replacecasedrainfilter.c. Replacehydraulicmotorpump/gen-

erator.d. Replacestandbypump.e. Replaceaccumulator.f. Checkoperationofshutoffvalve.g. Checkfilters/Clogindicators.h. Checkindicatingsystems.i. Performfunctionalchecks.j. Pressurisation/depressurisationof

thehydraulicsystem.k. PowerTransferUnit(PTU)opera-

tionl. ReplacementofPTU.m. Troubleshootfaultysystem.

XIX Ice and rain protection ( ATA 30 ) a. Replacepump.b. Replacetimer.c. Inspectrepairpropellerdeiceboot.d. Testpropellerde-icingsystem.e. Inspect/testwingleadingedgede-

icerboot.f. Replaceanti-ice/deicevalve.g. Installwipermotor.h. Checkoperationofsystems.

i. Operationaltestofthepitot-probeiceprotection.

j. OperationaltestoftheTATicepro-tection.

k. Operationaltestofthewingicepro-tectionsystem.

l. Assistancetotheoperationaltestoftheengineair-intakeiceprotection(withenginesoperating)

m. Troubleshootfaultysystem.

XX Indicating/recording systems (ATA 31 )

a. Replaceflightdatarecorder.b. Replacecockpitvoicerecorder.c. Replaceclock.d. Replacemastercautionunit.e. ReplaceFDR.f. PerformFDRdataretrieval.g. Troubleshootfaultysystem.h. ImplementESDSprocedures

i. InspectforHIRFrequirementsj. Start/stopEISprocedure.k. BitetestoftheCFDIU.l. Groundscanningofthecentral

warningsystem.XXI Landing Gear ( ATA 32 )

a. Buildupwheel.b. Replacemainwheel.c. Replacenosewheel.d. Replacesteeringactuator.e. Replacetrucktiltactuator.

f. Replacegearretractionactuator.g. Replaceuplock/downlockassembly.h. Replaceshimmydamper.i. Rignosewheelsteering.j. Replaceshockstrutseals.k. Servicingofshockstrut.l. Replacebrakeunit.m. Replacebrakecontrolvalve.n. Bleedbrakes.o. Replacebrakefan.p. Testantiskidunit.q. Testgearretraction.r. Changebungees.s. Adjustmicroswitches/sensors.t. Chargestrutswithoilandair.u. Troubleshootfaultysystem.v. Testauto-brakesystem.w. Replacerotorcraftskids.x. Replacerotorcraftskidshoes.

y. Packandcheckfloats.z. Flotationequipment.aa. Check/testemergencyblowdown

(emergencylandinggearextension).

CAR-66


bb. Operationaltestofthelandinggeardoors.

XXII Lights ( ATA 33 )

a. Repair/replacerotatingbeacon.b. Repair/replacelandinglights.c. Repair/replacenavigationlights.d. Repair/replaceinteriorlights.e. Replaceiceinspectionlights.

f. Repair/replacelogolights.g. Repair/replaceemergencylighting

system.h. Performemergencylightingsystem

checks.i. Troubleshootfaultysystem

XXIII Navigation ( ATA 34 )

a. Calibratemagneticdirectionindica-tor.

b. Replaceairspeedindicator.c. Replacealtimeter.d. Replaceairdatacomputer.e. ReplaceVORunit.f. ReplaceADI.g. ReplaceHSI.h. Checkpitotstaticsystemforleaks.i. Checkoperationofdirectionalgyro.j. Functionalcheckweatherradar.k. FunctionalcheckDoppler.

l. FunctionalcheckTCAS.m. FunctionalcheckDME.n. FunctionalcheckATCTransponder.o. Functionalcheckflightdirectorsys-

tem.p. Functionalcheckinertialnavsys-

tem.q. Completequadrantalerrorcorrec-

tionofADFsystem.r. Updateflightmanagementsystem

database.s. Checkcalibrationofpitotstaticin-

struments.

t. Checkcalibrationofpressurealti-tudereportingsystem.

u. Troubleshootfaultysystem.v. Checkmarkersystems.w. Compassreplacementdirect/indi-

rect.x. CheckSatcom.y. CheckGPS.z. TestAVM.

XXIV Oxygen ( ATA 35 )

a. Inspectonboardoxygenequipment.b. Purgeandrechargeoxygensystem.c. Replaceregulator.

d. Replaceoxygengenerator.e. Testcrewoxygensystem.f. Performautooxygensystemdeploy-

mentcheck.

g. Troubleshootfaultysystem.

XXV Pneumatic systems ( ATA 36 )

a. Replacefilter.

b. Replaceairshutoffvalve.

c. Replacepressureregulatingvalve.

d. Replacecompressor.

e. Rechargedessicators.

f. Adjustregulator.

g. Checkforleaks.

h. Troubleshootfaultysystem.XXVI Vacuum systems ( ATA 37 )

a. Inspectthevacuumsystemi.a.w.AMM.

b. Replacevacuumpump.

c. Check/replacefilters.

d. Adjustregulator.e. Troubleshootfaultysystem.

XXVII Water/Waste ( ATA 38 )

a. Replacewaterpump.

b. Replacetap.

c. Replacetoiletpump.

d. Performwaterheaterfunctionalcheck.

e. Troubleshootfaultysystem.

f. Inspectwastebinflapclosure.

XXVIII Central Maintenance System ( ATA45 )

a. RetrievedatafromCMU.

b. ReplaceCMU.

c. PerformBitecheck.

d. Troubleshootfaultysystem.

XXIX Airborne Auxiliary power (ATA 49)

a. Removal/InstallationofAPU.

b. Removal/installationoftheinletguide-vaneactuator.

c. OperationaltestoftheAPUemergencyshut-downtest.

d. OperationaltestofAPU.

XXX Structures ( ATA 51 )

a. Assessmentofdamage.

b. Sheetmetalrepair.

c. Fibreglassrepair.

CAR-66


d. Woodenrepair.

XXXI Fabric repair ( ATA 51 )

a. Recoverfabriccontrolsurface.

b. Treatcorrosion.

c. Applyprotectivetreatment.

XXXI Doors (ATA 52 )

a. Inspectpassengerdoori.a.w.AMM.b. Rig/adjustlockingmechanism.c. Adjustairstairsystem.d. Checkoperationofemergencyexits.e. Testdoorwarningsystem.f. Troubleshootfaultysystem.g. Removeandinstallpassengerdoor

i.a.w.AMM.h. Removeandinstallemergencyexit

i.a.w.AMM.i. Inspectcargodoori.a.w.AMM.

XXXII Windows ( ATA 56 )

a. Replacewindshield.b. Replacedirectvisionwindow.c. Replacecabinwindowd. Repairtransparency.

XXXIII Wings (ATA 57 )

e. Skinrepair.f. Recoverfabricwing.g. Replacetip.h. Replacerib.i. Replaceintegralfueltankpanel.j. Checkincidence/rig.

XXXIV Propeller (ATA 61 )

a. Assemblepropaftertransportation.b. Replacepropeller.c. Replacegovernor.d. Adjustgovernor.e. Performstaticfunctionalchecks.f. Checkoperationduringgroundrun.g. Checktrack.h. Checksettingofmicroswitches.i. Dressoutbladedamage.j. Dynamicallybalanceprop.k. Troubleshootfaultysystem.

XXXV Main Rotors ( ATA 62 )

a. Replaceblades.b. Replacedamperassembly.c. Checktrack.d. Checkstaticbalance.e. Checkdynamicbalance.f. Troubleshoot.

XXXVI Rotor Drive (ATA 63 )

a. Replacemast.

b. Replacedrivecoupling.

c. Replaceclutch/freewheelunit

d. Replacedrivebelt.

e. Installmaingearbox.

f. Overhaulmaingearbox.

g. Checkgearboxchipdetectors.

XXXVII Tail Rotors (ATA 64 )

a. Installrotorassembly.

b. Replaceblades.

c. Troubleshoot.

XXXVIII Tail Rotor Drive ( ATA 65 )

a. Replacebevelgearbox.b. Replaceuniversaljoints.c. Overhaulbevelgearbox.d. Installdriveassembly.e. Checkchipdetectors.f. Check/installbearingsandhangers.g. Check/service/assembleflexible

couplings.h. Checkalignmentofdriveshafts.i. Installandrigdriveshafts.

XXXIX Rotorcraft flight controls (ATA 67 )

a. Installswashplate.b. Installmixingbox.c. Adjustpitchlinks.d. Rigcollectivesystem.e. Rigcyclicsystem.f. Riganti-torquesystem.g. Checkcontrolsforassemblyand

locking.h. Checkcontrolsforoperationand

sense.i. Troubleshootfaultysystem.

XL Power Plant ( ATA 71 ) a. BuildupECU.b. Replaceengine.c. Repaircoolingbaffles.d. Repaircowling.e. Adjustcowlflaps.f. Repairfaultywiring.g. Troubleshoot.h. Assistindrymotoringcheck.i. Assistinwetmotoringcheck.j. Assistinenginestart(manual

mode).XLI Piston Engines(ATA 72 )

a. Remove/installreductiongear.b. Checkcrankshaftrun-out.c. Checktappetclearance.

d. Checkcompression.

e. Extractbrokenstud.

CAR-66


f. Installhelicoil.

g. Performgroundrun.

h. Establish/checkreferenceRPM.

i. Troubleshoot.

XLII Turbine Engines ( ATA 72 )

a. Replacemodule.b. Replacefanblade.

c. Hotsectioninspection/borescopecheck.

d. Carryoutengine/compressorwash.

e. Carryoutenginedrycycle.

f. Enginegroundrun.

g. Establishreferencepower.

h. Trendmonitoring/gaspathanalysis.

i. Troubleshoot.

XLIII Fuel and control, piston ( ATA 73 )

a. Replaceenginedrivenpump.

b. AdjustAMC.

c. AdjustABC.

d. Installcarburetor/injector.

e. Adjustcarburetor/injector.

f. Cleaninjectornozzles.

g. Replaceprimerline.

h. Checkcarburetorfloatsetting.

XLIV Fuel and control, turbine (ATA 73)

a. ReplaceFCU.

b. Replaceengineelectroniccontrolunit(FADEC).

c. Replacefuelmeteringunit(FADEC).

d. Replaceenginedrivenpump.

e. Clean/testfuelnozzles.

f. Clean/replacefilters.

g. AdjustFCU.

h. Troubleshootfaultysystem.

i. FunctionaltestofFADEC.

XLV Ignition systems, piston (ATA 74)

a. Changemagneto.

b. Changeignitionvibrator.

c. Changeplugs.

d. Testplugs.

e. CheckH.T.leads.

f. Installnewleads.

g. Checktiming.

h. Checksystembonding.

i. Troubleshootfaultysystem.

XLVI Ignition systems, turbine (ATA 74)

a. Performfunctionaltestoftheigni-tionsystem.

b. Checkglowplugs/ignitors.

c. CheckH.T.leads.

d. Checkignitionunit.

e. Replaceignitionunit.

f. Troubleshootfaultysystem.

XLVII Engine Controls( ATA 76 )

a. Rigthrustlever.

b. RigRPMcontrol.

c. RigmixtureHPcocklever.

d. Rigpowerlever.

e. Checkcontrolsync(multi-eng).

f. Checkcontrolsforcorrectassemblyandlocking.

g. Checkcontrolsforrangeanddirec-tionofmovement.

h. Adjustpedestalmicro-switches.


XLVIII Engine Indicating ( ATA 77 )

a. Replaceengineinstruments(s).

b. Replaceoiltemperaturebulb.

c. Replacethermocouples.

d. Checkcalibration.


XLIX Exhaust, piston ( ATA 78 )

a. Replaceexhaustgasket.

b. Inspectweldedrepair.

c. Pressurecheckcabinheatermuff.

d. Troubleshootfaultysystem.

L Exhaust, turbine ( ATA 78 )

a. Changejetpipe.

b. Changeshroudassembly.

c. Installtrimmers.

d. Inspect/replacethrustreverser.

e. Replacethrustreversercomponent.

f. Deactivate/reactivatethrustre-verser.

g. Operationaltestofthethrustre-versersystem.

LI Oil ( ATA 79 )

a. Changeoil.

b. Checkfilter(s).

c. Adjustpressurereliefvalve.

d. Replaceoiltank.

e. Replaceoilpump.

f. Replaceoilcooler.

CAR-66


g. Replacefirewallshutoffvalve.

h. Performoildilution.


LII

Starting ( ATA 80 )

a. Replacestarter.

b. Replacestartrelay.

c. Replacestartcontrolvalve.

d. Checkcrankingspeed.


LIII Turbines, piston engines ( 70 )

a. ReplacePRT.

b. Replaceturbo-blower.

c. Replaceheatshields.

d. Replacewastegate.

e. Adjustdensitycontroller.

LIV Engine water injection ( ATA 82 )

a. Replacewater/methanolpump.

b. Flowcheckwater/methanolsystem.

c. Adjustwater/methanolcontrolunit.

d. Checkfluidforquality.

e. Troubleshootfaultysystem

LV Accessory gear boxes ( ATA 83)

a. Replacegearbox.

b. Replacedriveshaft.

c. CheckChipdetector

CAR 66


APPENDIX III to AMC of CAR-66

Evaluation of the competence: assessment and assessors

ThisAppendixappliestothecompetenceassessmentperformedbythedesignatedas-sessors(andtheirqualifications).

1) What does “competence” mean and areas of focus for assessment

Theassessmentshouldaimatmeasuringthecompetencebyevaluatingthreemajorfac-torsassociatedtothelearningobjectives: Knowledge; Skills; Attitude.

Generally,knowledgeisevaluatedbyexamination.Thepurposeofthisdocumentisnotto describe the examination process: this material mainly addresses the evaluation of“skills” and “attitude” after training containing practical elements. Nevertheless, thetraineeneedstodemonstratesufficientknowledgetoperformtherequiredtasks.“Attitude”isindivisiblefromthe“skill”asthisgreatlycontributestothesafeperfor-manceofthetasks.Theevaluationofthecompetenceshouldbebasedonthelearningobjectivesofthetraining,inparticular: the(observable)desiredperformance.Thiscoverswhatthetraineeisexpectedtobe

abletodoandhowthetraineeisexpectedtobehaveattheendofthetraining; the(measurable)performancestandardthatmustbeattainedtoconfirmthe

trainee’slevelofcompetenceintheformoftolerances,constraints,limits,perfor-manceratesorqualitativestatements;and

theconditionsunderwhichthetraineewilldemonstratecompetence.Conditions

consistofthetrainingmethods,theenvironmental,situationalandregulatoryfac-tors.

Theassessmentshouldfocusonthecompetenciesrelevanttotheaircrafttypeanditsmaintenanceincluding,butnotlimitedto: Environmentalawareness(actsafely,applysafetyprecautionsandpreventdanger-

oussituations);

Systemsintegration(demonstrateunderstandingofaircraftsystemsinteraction,identify,describe,explain,plan,execute);

CAR 66


Knowledgeandunderstandingofareasrequiringspecialemphasisornovelty(areaspeculiartotheaircrafttype,domainsnotcoveredbyCAR66AppendixI,practicaltrainingelementsthatcannotbeimpartedthroughsimulationdevices,etc.);

Usingreportsandindications(theabilitytoreadandinterpret); Aircraftdocumentationfindingandhandling(identifytheappropriateaircraft documentation,navigate,executeandobeytheprescribedmaintenanceprocedures); Performmaintenanceactions(demonstratesafehandlingofaircraft,engines, componentsandtools); Aircraftfinal/close-upandreport(applycloseup,initiateappropriateactions/fol-

low-up/recordsoftesting,establishandsignmaintenancereords/logbooks).2) How to assess

Asfarasfeasible,theobjectivesoftheassessmentshouldbeassociatedwiththelearningobjectivesandthepassinglevel;itmeansthatobservablecriteriashouldbesettomeas-uretheperformanceandshouldremainasobjectiveaspossible.The general characteristics of effective assessment are: objective, flexible, acceptable,comprehensive, constructive, organised and thoughtful. At the conclusion, the traineeshould have no doubt about what he/she did well, what he/she did poorly and howhe/shecanimprove.Thefollowingisanon-exhaustivelistofquestionsthatmaybeposedtoassisttheas-sessment:

Whatarethesuccessfactorsforthejob? Whataretypicalcharacteristicsofacorrectbehaviourforthetask? Whatcriteriashouldbeobserved? Whatlevelofexpertiseisexpected? Isthereanystandardavailable? Whatisthepassmark?Forexample:

o“Go-nogo”situation;oHowtoallocatepoints?Minimumamounttosucceed;o“Mustknoworexecute”versus“Goodtoknoworexecute”versus“Don’texpectthecandidatetobeanexpert”.

Minimumormaximumtimetoachieve?Usetimeeffectivelyandefficiently. Whatifthetraineefails?Howmanytimesisthetraineeallowedtofail? Whenandhowshouldthetraineebepreparedfortheassessment? Whatproportionofjudgmentbytheinstructoroutofcollaborationwiththetrainee

isneededduringtheevaluationstage?

Theassessmentmaybe:

CAR 66


diagnostic(priortoacourse),formative(reorientatethecourseonareaswherethereisaneedtoreinforce)orsummative(partialorfinalevaluation);

performedtask-by-task,asagroupoftasksorasafinalassessment.Onemethodmightbeaninitialassessmenttobeperformedbythetraineehimself/her-self,thendiscussingareaswheretheperceptionsofthetrainee’sperformancebytheas-sessorsdifferinorderto: developtheself-assessmenthabits; maketheassessmentmoreacceptableandunderstandabletobothparties.A “box-ticking” exercise would be pointless. Experience has shown that assessmentsheetshave largelyevolvedover time intoassessmentofgroupsof “skills”because inpracticesuchthingseventuallydetractedfromthetrainingandassessmentthatitwasintendedtoserve:evaluateatapointoftime,encourageandorientatethetrainingneeds,improvesafetyandultimatelyqualifypeoplefortheirduties.Inaddition,manyotheraspectsshouldbeappropriatelyconsideredduringtheassess-mentprocesssuchasstressandenvironmentalconditions,difficultyofthetest,historyofevaluation(suchastangibleprogressesorsuddenandunexpectedpoorperformancemadebythetrainee),amountoftimenecessarytobuildcompetence,etc. Allthesereasonsplacemoreemphasisontheassessorandhighlightthefunctionoftheorganisation’sapproval. 3) Who should assess Inordertoqualify,theassessorshould: Beproficientandhavesufficientexperienceorknowledgein: o humanperformanceandsafetyculture;otheaircrafttype(necessarytohavethecertifyingstaffprivilegesincaseofCRSissuances);otraining/coaching/testingskills;oinstructionaltoolstouse;

Understandtheobjectiveandthecontentofthepracticalelementsofthetraining

thatisbeingassessed;

Haveinterpersonalskillstomanagetheassessmentprocess(professionalism,sincer-ityobjectivityandneutrality,analysisskills,senseofjudgement,flexibility,capabilityofevaluatingthesupervisor’sorinstructor’sreports,handlingoftrainee’sreactionstofailingassessmentwiththeculturalenvironment,beingconstructive,etc.);

Beultimatelydesignatedbytheorganisationtocarryouttheassessment.Therolesmaybecombinedfor:

CAR 66


theassessorandtheinstructorforthepracticalelementsoftheTypeRatingTrain-

ing;or theassessorandthesupervisorfortheOn-the-JobTrainingProvidedthattheobjectivesassociatedwitheachroleareclearlyunderstoodandthatthecompetenceandqualificationcriteriaaccordingtothecompany’sproceduresaremetforbothfunctions.Wheneverpossible(dependingonthesizeoftheorganisation),itisrecommendedtosplittheroles(twodifferentpersons)inordertoavoidanycon-flictsofinterests.Whenthefunctionsarenotcombined,theroleofeachfunctionshouldbeclearlyunder-stood

CAR 66


Appendix IV to AMC of CAR- 66. A. 45(d)

Fuel Tank Safety training

ThisappendixincludesgeneralinstructionsforprovidingtrainingonFuelTankSafety

issues.

1. LeveloftrainingrequiredbythisAnnexisonlylevel2.

Level2Detailedtraining

Objectives:Theattendantshould,afterthecompletionofthetraining:

1. knowthe historyand the theoretical andpractical elementsof the subject,havean

overviewofSpecialFederalAviationRegulations(SFARs)from14CFRSFAR88ofthe

FAAandofJAATGL47,beabletogiveadetaileddescriptionoftheconceptofCDCCL,

AirworthinessLimitationsItems(ALI)andusingtheoreticalfundamentalsandspecific

examples,

2. havethecapacitytocombineandapplytheseparateelementsofknowledgeinalogical

andcomprehensivemanner.

3. havedetailedinformationonhowtheaboveitemsaffecttheaircraftinthescopeofthe

activityoftheorganisationorinthefleet.

4. understandandcarryoutactivitieswiththeuseofmanufacturerandregulatoryau-

thoritydataprovidinginstructionsondesignandmaintenance,suchasServiceBulle-

tins,AirworthinessDirectives,AircraftMaintenanceManual,ComponentMaintenance

Manualetc.

5. useeasilythemanufacturer’sdocumentationfromvarioussourcesandapplycorrec-

tiveactionwhereappropriate.

6. identifythecomponentsorpartsortheaircraftsubjecttoFTSfromthemanufacturer’s

documentation,plantheactionorapplyaServiceBulletinandanAirworthinessDi-

rective.

Continuingtraining

The interval betweencontinuing trainingshallbe establishedbytheorganisation em-

ployingsuchpersonnel,butshouldnotexceedtwoyears.Thecontinuingtrainingshall

includeknowledgeonevolutionofmaterial,tools,documentationandmanufacturer’sor

DGCAdirectives.

2. ThepersonneldirectlyinvolvedinFuelTankSafety(FTS)systemsshallbequalifiedaccordingtothefollowingtable:

CAR 66


Organisation Personnel Level of

knowledge

Continuing

training

CAR-66licenceholdersina

continuing airworthiness

managementorganisation

Theairworthinessre-

viewstaffasrequired

byM.A.707.

2 Yes

CAR-66 licence holders in

aircraft and component

maintenanceorganisations

Maintenance organi-

sation support and

certifyingstaff

2 Yes

3. Generalrequirements

Thetrainingforthepersonneldesignatedintableabovehastobecarriedoutbeforeany

airworthinessreviewcertificateisissuedoranymaintenancetaskiscertifiedonanair-

craftoracomponent.

Thetrainingshouldbemadeinappropriatefacilitiescontainingexamplesofcomponents,

systems and parts affected by FTS issues and having access to aircraft or component

wheretypicalexamplesofFTSissuescanbeshown.Theuseofpictures,filmsandpracti-

calexamplesofthemaintenanceonfueltanksystemisrecommended.Thetrainingshall

includea representativenumberofrepair and inspections as requiredby the mainte-

nanceprogrammeshowingthenecessityofusingthemanufacturer’sdata.

4. Characteristicsofthetraining

Thefollowingcharacteristicsshallbetakenintoconsiderationwhenthelevel2training

programmearebeingestablished:

(a) understandingofthebackgroundandconceptsoffueltanksafetyasdevelopeddur-

ingthelast10years,and

(b) howinmaintenanceorganisationsmechanicscanrecognize,interpretandhandlethe

improvements that have been made or are being made during fuel tank system

maintenance,

(c) awarenessofanyhazardsworkingontheFuelSystem,andespeciallywithaFlam-

mabilityReductionSystemusingnitrogen.

a),b)andc)shouldbeintroducedinthetrainingprogrammeaddressingthefollowing

issues:

i) Thetheoreticalbackgroundbehindthefueltanksafety:theexplosionsofmixtures

offuelandair,thebehaviorofthosemixturesinanaviationenvironment,theeffects

oftemperatureandpressure,energyneededforignitionetc,the‘firetriangle’,-Ex-

plain2conceptstopreventexplosions:(1)ignitionsourcepreventionand(2)flam-

mabilityreduction,

CAR 66


ii) Themajoraccidentsandaccidentinvestigationsandtheirconclusions,

iii) SFARsfrom14CFRSFAR88oftheFAAandJAAInternalPolicyINTPOL25/12:

reasonofthesedocuments,andwhatwastheultimategoal,marginsoffuelsystem

safetyimprovements(from10-6to10-9,infactimprovementbyafactor100-1000,

to identifyunsafe conditions and to correct them, to systematically improvefuel

tankmaintenance),

iv) Explaintheconceptsthatarebeingused:theresultsofSFAR88oftheFAAandJAA

INT/POL25/12:modifications,airworthinesslimitationsandCDCCL,

v) Whererelevantinformationcanbefoundbythemechanicsandhowtouseandin-

terpretthisinformation(maintenancemanuals,componentmaintenancemanuals)

vi) FuelTankSafetyandMaintenance:fueltankentryandexitprocedures,cleanwork-

ingenvironment,whatismeantbyconfigurationcontrol,wireseparation,bonding

ofcomponentsetc,

vii) Flammabilityreductionsystems:reasonfortheirpresence,theireffects,thehaz-

ards of an FRS using nitrogen for maintenance, safety precautions in mainte-

nance/workingwithanFRS,

viii) Recordingmaintenanceactions,recordingmeasuresandresultsofinspections.

CAR 66


DGCA application forms for licenses and examinations

Form No Description

CA Form 19-01ApplicationForInitialIssueOfCAR-66AircraftMaintenanceEngineer’s

Licence

CA Form 19-02 ApplicationforextensionofCAR-66aircraftmaintenanceengineer’sli-

cence

CA Form 19-03 ApplicationforrenewalofCAR-66aircraftmaintenanceengineer’sli-

cence

CA Form 19-04 Applicationforconversion/removaloflimitationsofCAR-66aircraft

maintenanceengineer’slicence

CA Form 19-05 ApplicationforissueofduplicateCAR-66aircraftmaintenanceengineer’sli-

cence

CA Form 19-06 Medicalcertificate

CA Form 19-07 ApplicationforallotmentofcomputernumberforappearinginAMEli-

cenceexaminations

CA Form 19-08A Applicationforappearinginwrittenpaper(s)ofCAR66basicknowledge

examination

CA Form 19-08B Application for appearing in CAR 66 type examination

CA Form 19-09 ApplicationforappearinginskilltestofCAR-66AMElicence

CA Form 19-10 Formatofaircraftmaintenanceengineerworkrecord/logbook

CA Form 19-11 Applicationforissueofbasicknowledgeexaminationcertificate

CAR 66


HighlightsoftheCAR66Issue02

Sl.

No.

CAR66Issue02Reference Description

1. 66.A.01Scope ScopeandLicenceCategoriesSeparated

2. 66.A.3LicenceCategories

3. 66.A.5Aircraftgroups New para added to make provisions for Aircraft Groups for the

purposeofratingsonAMElicence.

4. 66.A.10Application Newpara66.A.10(f)addedtomakeprovisionforsupportingdoc-

umentationtodemonstratecompliancewithrequirementsforis-

sue/changeofAMElicence

5. 66.A.15Eligibility Newpara66.A.15(a)ofKnowledgerequirementsshiftedfromex-

istingpara66.A.25(a).

6. 66.A.25 Basic Knowledge re-

quirements

66.A.25(a)shiftedto66.A.15(a)asapartofeligibility.66.A.25

(b), (c),&(d)hasbeenaddedtomake provisionsforvalidityof

modulesandcreditfor10years.

7. 66.A.30 Experience require-

ments

InPara(c), (d)word“must”hasbeenreplacedwith“shall”and

para(f)hasbeenadded.

8. 66.A.33TypeTrainingandExam-

inationRequirements

66.A.33TypeTrainingandExaminationRequirementsadded

9. 66.A.35SkillTestRequirements 66.A.35SkillTestRequirementsadded.

10. 66.A.45 Endorsement with air-

craftratings

66A.45 has been replaced with new requirements for endorse-

mentswithaircraftratingsdependingupongroupofaircraftasper

66.A.05.

11. 66.A.50Limitations Newpara66.A.50hasbeenaddedtodetailstherequirementsfor

removaloflimitationonratingsintroducedonAMElicenceduring

conversion/issue.

12. 66.A.55Evidenceofqualification Provisionextendedtosupportstaff

13. 66.A.70Conversionprovisions

Minorchangesinpara(a)&(b)hasbeenmade(referenceofthe

conditions specified in 66.B.300 replaced with APM Chapter 17

beenrevisedtomakereferenceofCAR66.A.50.

14. SectionBProceduresforCAR-66

Section B – Licensingof Aircraft

MaintenanceEngineers

SectionBofCAR66(ProceduresforDGCA)forAircraftMainte-

nanceEngineersLicensinghasbeenremovedfromCAR66 and

shall be part of Airworthiness Proceduremanual which will be

availableonwebsite.

15. GM66.A.3Licencecategories NewParaonthesubjectofLicencecategoriesadded.

16. AMC.66.A.15(a)Eligibility AddedasperpubliccommentstoacceptDiplomainengineering

(Aeronautical,Mechanical,ElectricalandElectronics)atparwith

10+2PCMforthepurposeofAMElicenceissue.

CAR 66


17. GM66.A.20(a)Privileges

EarlierAMC20(a)replacedwithGM66.A.20(a)toexplainvari-

ous terms such as Electrical Systems, Avionics Systems, Simple

test,Troubleshooting,Line/BaseMaintenanceetc.

18. GM66.A.20(b)2Privileges

NewparaGM66.A.20(b)2hasbeenaddedtoexplaintheterm ‘

“mettheprovisionforissueofappropriateprivileges’’.

19. AMC66.A.20(b)3Privileges

NewAMC66.A.20(b)3hasbeenaddedtoexplaintheterm“ade-

quatecompetencetocertifymaintenance’’.

20 GM66.A.20(b)4Privileges

Numbering has been changed from GM 66.A.20(b)3 to GM

66.A.20(b)4.

21 GM 66.A.25(a) Basic knowledge

requirements

Thisparahasbeenamendedtoexplainlevelofknowledge..

22. AMC66.A.30(a)Basicknowledge

requirements

Para3&4ofAMC66.A.30(a)hasbeenamendedtoexplainskill

workerandmaintenanceexperience.

23. AMC 66.A.30 (d) Basic

knowledgerequirements

ParaAMC66.A.30(d)hasbeenrevisedtoincludethevalidityof

basicexperiencewithin10year.

24. GM 66.A.35 Skill Test Require-

ments

GuidanceforappearinginSkillTestasperrule61added.

25 GM 66.A.45 (b) Endorsement

withaircraftratings.

NewparaGM66.A.45(b)hasbeenaddedonthesubjecttoexplain

guidelinefortypetrainingforadditionalmodels/variants.

26 GM 66.A.45 (e) Endorsement

withaircraftratings.

Para GM 66.A.45 (e) has been added on the subject to explain

guidelineformanufacturergrouprating..

25. AMC66.A.45(d)(e)3,(f)1&(g)1

Endorsement with aircraft rat-

ings.

ParaAMC66.A.45(d)(e)3,(f)1&(g)1hasbeenamendedtoex-

plainguidelinesforpracticalexperience.

27. GM 66.A.45 Endorsement with

aircraftratings.

Newparahasbeenaddedtointroduceatableindicatingsummary

of theaircraftratingrequirementscontainedin66.A.45,66.A.50

andAppendixIIItoCAR66

28 AMC66.A.50(b)Limitations NewParaAMC66.A.50(b)addedtoexplainappropriateexperi-

encerequirementstoremovelimitation.

29 GM66.A.70Conversionprovi-sions

GM66.A.70hasbeenamendedtoexplainconversionofAMEli-cenceguidelines.

30. GM66.A.70(c)Conversionprovi-

sions

New Para GM 66.A.70(c) on the subject explaining provision of

LimitationsonAMELicenceratingadded.

31 GM66.A.70(d)Conversionprovi-

sions

NewParaGM66.A.70(d)onthesubjectexplainingexamplesof

Limitationsadded.

32 AppendixI-BasicKnowledgeRe-

quirements

Syllabusofmodules5,10,11,12,13and14revisedtoincludead-

ditionaltopics.

33. Appendix II –Basic Examination

Standard

No of questions for each modules increased to cover additional

topicsandmake itmultipleoffourforeasycalculationof%of

marksobtained.

34. AppendixIII -Typetrainingand

ExaminationStandard

RevisedtoprovidedetailrequirementsforOJT,practicaltasks,as-

sessors,minimumdurationoftypetrainingandcontentsofprac-

ticaltopics.introduced

35. AppendixItoAMCofCAR66Air-

craftTyperatings

List of Aircraft updated to include new aircraft inducted in thecountry.

CAR 66


36. Appendix II to AMC of CAR66

Aircraft Type Practical Experi-

enceandOJT

ListofOJTtasksupdatedtoincludetasksonoperation,functionaltestingofsystemsetc.

37. AppendixIIItoAMCofCAR-66on

evaluation of competence : as-

sessmentandassessors

NewAMCtoAppendixIIItoCAR-66toprovideguidelinesforas-sessment of competency and acceptance of practical assessorsadded.

38 AMCtoSection1ofAppendixIII

to CAR-66 “Aircraft Type Train-

ing and Examination Standard.

On-the-JobTraining

NewAMCtoSection1ofAppendixIIItoCAR-66onthesubjectex-plainingguidelinesfortypetrainingadded

39 AMCtoParagraphs3.1(d)ofAp-

pendix III to CAR-66 “Aircraft

Type Training and Examination

Standard.On-the-JobTraining

NewAMCtoParagraphs3.1(d)ofAppendixIIItoCAR-66onthesubjectexplainingguidelinesfortrainingneedanalysisadded

40. AMCtoParagraphs1(b),3.2and

4.2 of Appendix III to Part-66

“Aircraft Type Training and Ex-

amination Standard. On-the-Job

Training

NewAMCtoParagraphs1(b),3.2and4.2ofAppendixIIItoCAR-66onthesubjectexplainingpracticalelementsoftheaircrafttypetrainingadded

41 AMCtoParagraph1(c)ofAppen-

dix III to Part-66 “Aircraft Type

TrainingandExaminationStand-

ard.On-the-JobTraining

NewAMCtoParagraphs1(c)ofAppendixIIItoCAR-66onthesub-jectexplainingdifferenceaircrafttypetrainingadded

42. AMCtoSection5ofAppendixIII

to Part-66 “Aircraft Type Train-


On-the-JobTraining”

NewAMCtoSection5of AppendixIIItoCAR-66onthesubjectexplainingaircrafttypeexaminationstandardadded

43 AMCtoSection6ofAppendixIII

to Part-66 “Aircraft Type Train-


On-the-JobTraining

NewAMCtoSection6ofAppendixIIItoCAR-66onthesubjectexplainingOn-the-Jobtrainingadded

*********