challenger juofsbreport 06/12/03

Challenger JUOFSB Report

APPENDIX 1 Operational Acceptability Checklist for FAR PARTS 91/135BD-100-1A10 Compliance Checklist Issue: --

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Date: March 2003

FAR REQUIREMENT COMPLIANCE REMARKS

91. 9(a)

91.9(b)

91. 9(b)(I)

91. 9(b)(2)

Compliance with Flight Manual, Markings, and PlacardMarkings

Except as provided in paragraph (d) of this section, no personmay operate a civil aircraft without complying with theoperating limitations specified in the approved Airplane orRotorcraft Flight Manual, markings, and placards, or asotherwise prescribed by the certificating authority of thecountry of registry.

Each operator must keep a current copy of each approvedmanual at its principal base of operations and must make eachmanual available for inspection upon request by theAdministrator.

For which an Airplane or Rotorcraft Flight Manual is requiredby ~ 21.5 of this chapter unless there is available in theaircraft a current, approved Airplane or Rotorcraft FlightManual or the manual provided for in ~ 121.141 (b); and

Operator's responsibility. SA provides an approvedAFM for Green aircraft configuration. CompletionCenter to supplement AFM if affected.

SA provides approved AFM, QRM and FCOM forgreen aircraft configuration.

SA provides approved AFM, QRM aand FCOM forgreen aircraft configuration or an FAA approvedAirplane Flight Manual complying with FAR 25.1581is provided with each aircraft. For green aleconfiguration, completion center to supplement ifaffected.

The Internal! External Markings of thegreen aircraft configuration comply withFAR 25 requirements. Registrationmarking to be addressed by deliverycenter at completion.

Completion Center to supplement ifrequired/affected.

91. 9(c)

For which an Airplane or Rotorcraft Flight Manual is not Not applicable.required by ~ 21.5 of this chapter, unless there is available inthe aircraft a current approved Airplane or Rotorcraft FlightManual, approved manual material, markings, and placards, orany combination thereof.

No person may operate a U.S.-registered civil aircraft unlessthat aircraft is identified in accordance with part 45 of this

A fireproof identification plate complying with FAR45 is included in the baseline configuration

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Operational Acceptability for FAR PARTS 91/135BO - 100 - Compliance Checklist

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RAZ-BAIOO-I06Issue: --Date: March 2003

FAR REQUIREMENT COMI'L1ANCE REMARKS

91. 9(d)

91.191(a)

Compliance with Flight Manual, Markings, and PlacardMarkings

Any person taking off or landing a helicopter certificated Not applicableunder part 29 of this chapter at a heliport constructed overwater may make such momentary flight as is necessary fortakeoff or landing through the prohibited range of the limitingheight-speed envelope established for the helicopter if thatflight through the prohibited range takes place over water onwhich a safe ditching can be accomplished and if thehelicopter is amphibious or is equipped with floats or otheremergency flotation gear adequate to accomplish a safeemergency ditching on open water.

Category II and Category 111manualExcept as provided in paragraph (c) of this section, after Operator's responsibilityAugust 4, 1997, no person may operate a U.S.-registered civilaircraft in a Category II or a Category III operation unless -- (I)There is available in the aircraft a current and approvedCategory II or Category III manual, as appropriate, for thataircraft;

(2) The operation is conducted in accordance with theprocedures, instructions, and limitations in the appropriatemanual; and

(3) The instruments and equipment listed in the manual thatare required for a particular Category II or Category IIIoperation have been inspected and maintained in accordancewith the maintenance program contained in the manual.

Certification for Cat II operations will beconducted after initial Type Certification.An approved Airplane Flight Manual,including Category II procedures,instructions and limitations, will beprovided with each aircraft.An approved maintenance schedule asper the Maintenance Review Board(MRB) Report, derived from the MSG-3process, and an Aircraft MaintenanceManual complying with FAR 25.1529 &Appendix H are provided to eachoperator. These documenls reflect thegreen aircraft as designed by BombardierAerospace and supplemented byCompletion Center additions.

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91.191(b)

91.191(c)

Category II and Category III manualEach operator must keep a current copy of each approved Operator's Responsibility.manual at its principal base of operations and must make eachmanual available for inspection upon request of theAdministrator.

This section does not apply to operations conducted by aholder of a certificate issued under part 121 or part 135 of thischapter.

91.203(a) Civil Aircraft: Certifications RequiredExcept as provided in 91.715, no person may operate a civilaircraft unless it has within it the following: (I) An appropriateand current airworthiness certificate. Each U.S. airworthinesscertificate used to comply with this subparagraph (except aspecial flight pennit, a copy of the applicable operationsspecifications issued under 2 1.197(c) of this chapter,appropriate sections of the air carrier manual required by parts121 and 135 of this chapter containing that portion of theoperations specifications issued under 21.197(c) or anauthorization under 91.611) must have on it the registrationnumber assigned to the aircraft under part 47 of this chapter.However the airworthiness certificate need not have on it anassigned special identification number, that has been affixedto an aircraft, may only be obtained upon application to anFAA Flight Standards district office. (2) An effective U.S.registration certificate issued to its owner or, for operationwithin the United States, the second duplicate copy (pink) ofthe Aircraft Registration Application as provided for in47.31(b), or a registration certificate issued under the laws of aforeign country.

CofA issued by FAA for the green alc configurationwill be provided for each aircraft under 21.197(c). USregistration certificate to be issued by FAA via SACompletion Center.

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Operational Acceptability for FAR PARTS 91/135SO -100 - Compliance Checklist

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91.203(b)

91.203(c)

91.203(d)

Civil Aircraft: Certifications RequiredNo person may operate a civil aircraft unless the airworthinesscertificate required by paragraph (a) of this section or aspecial flight authorization issued under 91.715 is displayed atthe cabin or cockpit entrance so that it is legible to passengeror crew,

No person may operate an aircraft with a fuel tank instaHedwithin the passenger compartment or a baggage compartmentunless the instaHation was accomplished pursuant to part 43ofthis chapter, and a copy of FAA Form 337 authorizing thatinstaHation is on board the aircraft.

No person may operate a evil airplane (domestic or foreign)into or out of an airport in the United States unless it complieswith the fuel venting and exhaust emission requirements ofpart 34 of this chapter.

Operator's responsibility. Valid C of A for greenaircraft will be provided at aircraft delivery and wiH besupplemented by Completion Centre for completedaircraft. It is operator responsibility to keep theaircraft continuously airworthy.

Not applicable. No fuel tank instaHed within thepassenger compartment or baggaged compartment inChallenger 300 for the Green Aircraft Configuration.

Compliance with FAR 34 requirements has beendemonstrated during Type Certification, as weH asICAO Annex 16 Volume 2 for fuel venting andexhaust emission requirement.

91.205(a) Powered civil aircraft with standard category U.S.airworthiness certificates: Instrument and equipmentrequirements

General. Except as provided in paragraphs (c)(3) and (e) of this For ChaHenger 300 green configuration a Mastersection, no person may operate a powered civil aircraft with a Minimum Equipment List (MMEL) approved by FAAstandard category U.s. airworthiness certificate in any is provided.operation described in paragraphs (b) through (I) of thissection unless that aircraft contains the instruments andequipment specified in those paragraphs (or FAA-aprrovedequivalents) for that type of operation, and those instrumentsand items of equipment are in operable condition.

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Operational Acceptability for FAR PARTS 91/135SO - 100 - Compliance Checklist

RAZ. BAI00- I 06Issue: .-Date: March 2003


91.205(b) Powered civil aircraft with standard category U.S.airworthiness certificates: Instrnment and equipmentrequirements

All equipment specified for Day VFR, as applicable toa turbine engine aircraft is included in the baselineconfiguration RAL-IOO-OOOI;except for Items;(I) - (10) are part of the baseline green configuration.;

(II) The Challenger 300 is a large transport categoryairplane type certificated under Part 25. Anticollision lighting system is provided as part of the

6) Temperature gauge for each liquid-cooled engine; baseline green configuration.7) Oil temperature gauge for each air-cooled engine; (12) Part of Ferry Kit for green ale. Completion center8) Manifold pressure gauge for each altitude engine; to address for completed aircraft.;9) Fuel gauge indicating the quantity of fuel in each tank; (13) Completion center to address for completed10) Landing gear position indicator, if the aircraft has a aircraft.;retractable landing gear; (14) The Challenger 300 is a large transport categoryII) For small civil airplanes certificated after March II, 1996, in airplane type certificated under Part 25. Green aleaccordance with part 23 of this chapter, an approved aviation configuration completed for pilots seats only.red or aviation white anticollision light system. In the event of Completion center to re-address for completedfailure of any light of the anti collision light system, operation aircraft.;of the aircraft may continue to a location where repairs or (15) ELT part of the green ale configuration.;replacement can be made; (16) The Challenger 300 is a large transport category12) If the aircraft is operated for hire over water and beyond airplane type certificated under Part 25. Completionpower-off gliding from shore, approved flotation gear readily center to address for Cabin Seats.available to each occupant and at least one pyrotechnic (17) Not Applicable. The Challenger 300 is a fixedsignaling device. As used in this section, "shore" means that wing airplane.area of the land adjacent to the water which is above the highwater mark and excludes land areas which are intermittentlyunder water.13) An approved safety belt with an approved metal-to-metallatching device for each occupant 2 years of age or older.14) For small civil airplanes manufactured after July 18, 1978,an approved shoulder harness for each front seat. Theshoulder harness must be designed to protect the occupantfrom serious head injury when the occupant experiences the

Visual-flight rules (day). For VFR flight during the day, thefollowing instruments and equipment are required:I) Airspeed indicator;2) Altimeter;3) Magnetic direction indicator;4) Tachometer for each engine;5) Oil pressure gauge for each engine using pressure system;

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ultimate inertia forces specified in 23.561(b)(2) of this chapter.Each shoulder harness installed at a flight crewmember stationmust permit the crewmember, when seated and with the safety

belt and shoulder harness fastened, to perform all functionsnecessary for flight operations. For purposes of thisparagraph --i) The date of manufacture of an airplane is the date theinspection acceptance records reflect that the airplane iscomplete and meets the FAA-approved type design data; and

ii) A front seat is a seat located at a flight crewmember stationor any seat located alongside such a seat.15) An emergency locator transmitter if required by 91.207.16) For normal, utility, and acrobatic category airplanes with aseating configuration, excluding pilot seats, of 9 or less,manufactured after December 12, 1986, a shoulder harness for

i) Each front seat that meets the requirements of23.785 (g) and(h) of this chapter in effect on December 12, 1985;ii) Each additional seat that meets the requirements of23.785(g) of this chapter in effect on December 12, 1985;17) For rotorcraft manufactured after September 16, 1992, ashoulder harness for each seat that meets the requirements of27.2 or 29.2 of this chapter in effect on September 16,1991.

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91.205(c)

91.205(d)

Powered civil aircraft with standard category U.S.airworthiness certificates: Instrument and equipmentrequirements

Visual flight rules (night). For VFR flight at night, thefollowing instruments and equipment are required:(I) Instruments and equipment specified in paragraph (b) ofthis section.(2) Approved position lights(3) An approved aviation red or aviation white anti-collisionlight on all U.S.- registered civil aircraft. Anti.collision lightsystems initially installed after August II, 1971, on aircraft forwhich a type certificate was issued or applied for beforeAugust II, 1971, must at least meet the anti.collision lightstandards of part 23, 25, 27, or 29 of this chapter, as applicable,that were in effect on August 10, 1971, except that the colormay be either aviation red or aviation white. In the event offailure of any light of the anti.collision light system,operations with the aircraft may be continued to a stop whererepairs or replacement can be made.(4) If the aircraft is operated for hire, one electric landing light.

(5) An adequate source of electrical energy for all installedelectrical and radio equipment.(6) One spare set of fuses, or three spare fuses of each kindrequired, that are accesible to the pilot in flight.


Instrument flight rules. For IFR flight, the followinginstruments and equipent are required:(1) Instruments and equipment specified in paragraph (b) ofthis section, and, for night flight, instruments and equipmentspecified in paragraph (c) of this section.(2) Two-way radio communications system and navigational

All equipment specified for Night VFR, Items (2) thru(6) are included in the baseline configurationRAL.l 00.000 I, except for:Item (6) - Spare fuses are not provided since allre-sertable circuits by the flight crew are protected bycircuit breakers.

All equipment specified for IFR flight, Items (2) thru(9) are included in the baseline configurationRAL.j 00.000 1.

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equipment appropriate to the ground facilities to be used.(3) Gyroscopic rate-of-turn indicator, except on the followingaircraft:(i) Airplanes with a third attitude instrument system usablethrough flight attitude 0060 degrees of pitch and roll andinstalled in accordance with the instrument requirementsprescribed in 121.305 U) of this chapter; and(ii) Rotorcraft with a third attitude instrument system usablethrough flight attitudes of +/-80 degrees of pitch and +/-120degrees of roll and installed in accordance with 29.1303 (g) ofthis chapter.(4) Slip-skid indicator(5) Sensitive altimeter adjustable for barometric pressure(6) A clock displaying hours, minutes, and seconds with asweep-second pointer or digital presentation.(7) Generator or alternator of adequate capacity(8) Gyroscopic pitch and bank indicator (artificial horizon)(9) Gyroscopic direction indicator (directional gyro orequi valent)

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91.205(e)

91.205(0


Flight at and above 24,000 ft MSL (FL 240). If VORnavigational equipment is required under paragraph (d)(2) ofthis section, no person may operate a U.S. registered civilaircraft within the 50 states and the District of Columbia at orabove FL 240 unless that aircraft is equipped with approveddistance measuring equipment (DME). When DME requiredby this paragraph fails at and above FL 240, the pilot incommand of the aircraft shall notify ATC immediately, andthen may continue operations at and above FL 240 to the nextairport of intended landing at which repairs or replacement ofthe equipment can be made.

Category II operations. The requirements for Category IIoperations are the instruments and equipment specified in --(I) Paragraph (d) of this section; and(2) Appendix A to this part.

One DME system is provided as part of the baselineconfiguration RAL-1 00.000 1.

Not applicable at this time. Certification for Cat IIoperations will be conducted after initial TypeCertification. Insturments and equipment are part ofbaseline Green Aircraft Configuration.

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91.205(g)Category III operations. The instruments and equipment Aircraft will not address Cat III operations.required for Category lJ[ operations are specified in paragraph(d) of this section.

91.205(h)

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91.215(a)

91.215(b)

Exclusions. Paragraph (I) and (g) of this section do not applyto operations conducted by a holder of a certificate issuedunder part 121 or part 135 of this chapter.

ATC Transponder and Altitude Reporting Equipment andUse

All airspace: U.S.- registered civil aircraft. For operations notconducted underpal1121 or 135 of this chapter, ATCtransponder equipment installed must meet the performanceand environmental requiremnets of any class of TSO-C74b(Mode A) or any class ofTSO-C74c (Mode A with altitudereporting capability) as appropriate, or the appropriate class ofTSO-CI12 (Mode S)

ATC Transponder and Altitude Reporting Equipment andUse

All airspace. Unless otherwise authorized or directed by ATC,no person may operate an aircraft in the airspace described inparagraphs (b)(l) through (b)(5) of this section, unless thataircraft is equipped with an operable coded radar beacontransponder having either Mode 3/A 4096 code capability,replying to Mode 3/A interrogations with the code specifiedby ATC, or a Mode S capability, replying to Mode 3/Ainterrogations with the code specified by ATC and imermodeand Mode S interrogations in accordance with the applicableprovisions specified in TSO C-112, and that aircraft isequipped with automatic pressure altitude reportingequipment having a Mode C capability that automaticallyreplies to Mode C interrogations by transmitting pressurealtitude information in 100-foot increments. This requirementapplies --

Part (I) & (g) are addreed for operators of Certificateholders under Part 91.

Aircraft/Operators conducts operation under Part 91Mode S transponder is part of the baseline greenAlC configuration.

Operator's responsibility. The green aircraft isequipped with a transponder that complies with thisrequirement.

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(1) All aircraft. In Class A, Class B, and Class C airspace areas;

(2) All aircraft. In all airspace within 30 nautical miles of anairpon listed in appendix D, section I of this pan from thesurface upward to 10,000 feet MSL;(3) Norwithstanding paragraph (b)(2) of this section, anyaircraft which was not originally cenificated with anengine-driven electrical system or which has notsubsequently been cenified with such a system installed,balloon or glider may conduct operations in the airspacewithin 30 nautical miles of an airpon listed in appendix D,section I of this part provided such operations are conducted -(i) Outside any Class A, Class B, or Class C airspace area; and

(ii) Below the altitude of the ceiling of a Class B or Class Cairspace area designated for an airpon or 10,000 feet MSL,whichever is lower; and(4) All aircraft in all airspace above the ceiling and within thelateral boundaries of a Class B or Class C airspace areadesignated for an airpon upward to 10,000 feet MSL; and(5) All aircraft except any aircraft which was not originallycertificated with an engine-driven electrical system or whichhas not subsequently been certified with such a systeminstalled, balloon, or glider -- --(i) In all airspace of the 48 contiguous states and the Districtof Columbia at and above 10,000 feet MSL, excluding theairspace at and below 2,500 feet above the surface; and(ii) In the airspace from the surface to 10,000 feet MSL within a10-nautical-mile radius of any airport listed in appendix D,section 2 of this pan, excluding the airspace below 1,200 feetoutside of the lateral boundaries of the surface area of theairspace designated for that airport.

91.215(c)Transponder-on operation. While in the airspace as specified Operator's responsibility.in parargraph (b) of this section or in all controlled airspace,each person operating an aircraft equipped with an operableATC transponder maintained in accordance with 91.413 of thispan shall operate the transponder, including Mode C

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equipment if installed, and shall reply on the appropriate codeor as assigned by ATC.

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91.215(d)

91.217

91.217(a)

ATe Transponder and Altitude Reportiug Equipment andUse

ATC authorized deviations. Requests for ATC authorized Operator's responsibility.deviations must be made to the ATC facility havingjurisdiction over the concerned airspace within the timeperiods specified as follows:(1) For operation of an aircraft with an operating transponderbut without operating automatic pressure attitude reportingequipment having a Mode C capability, the request may bemade at any time.(2) For operation of an aircraft with an inoperative transponderto the airport of ultimate destination including anyintermediate stops, or to proceed to a place where suitablerepairs can be made at any time.(3) For operation of an aircraft that is not equipped with atransponder, the request must be made at lest one hour beforethe proposed operation. (Approved by the Office ofManagement and Budget under control number 2120-0005)

Data correspondence between automatically reportedpressure altitude data and the pilot's altitude reference

No person may operate any automatic pressure altitudereporting equipment associated with a radar beacontransponder --

91.217(b)

When deactivation of that equipment is directed by ATC;

Operational Acceptability for FAR PARTS 91/

Data correspondence between automatically reportedpressure altitude data and the pilot's altitude reference

Operator's responsibility

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Unless, as installed, that equipment was tested and calibrated Mode C altitude - encoding equipment capable of Periodic testing and calibration is anto transmit altitude data corresponding within 125 feet (on a 95 transmitting altitude with at least 125-foot accuracy is operator responsibility.percent probability basis) of the indicated or calibrated datum provided in the baseline configurationof the altimeter normally used to maintain flight altitude, with RAL-I 00-000 I.that altimeter referenced to 29.92 inches of mercury foraltitudes from sea level to the maximum operating altitude ofthe aircraft; or

91.217(c)Unless the altimeters and digitizers in that equipment meet the Altimeters conform to TSO-C IOb and TSO-C88standards ofTSO-CIOb and TSO-C88, respectively.

91.219(a)

91.219(b)

Altitude alerting system or device: Turbojet-powered civilairplanes

Except as provided in paragraph (d) of this section, no person Operator's responsibilitymay operate a turbojet-powered U.S.-registered civil airplaneunless that airplane is equipped with an approved altitudealerting system or device that is in operable condition andmeets the requirements of paragraph (b) of this section.

Altitude alerting system or device: Turbojet-powered civilairplanes

Each altitude alerting system or device required by paragraph Operator's responsibility.(a) of this section must be able to--(l) Alert the pilot --(i) Upon approaching a preselected altitude in either ascent ordescent, by a sequence of both aural and visual signals insufficient time to establish level flight at that preselectedaltitude; or(ii) Upon approaching a preselected altitude in either ascent ordescent, by a sequence of visual signals in sufficient time toestablish level flight at that preselected altitude, and whendeviating above and below that preselected altitude, by anaural signal;(2) Provide the required signals from sea level to the highestoperating altitude approved for the airplane in which it isinstalled;(3) Preselect altitudes in increments that are commensuratewith the altitudes at which the aircraft is operated;

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(4) Be resred without special equipment to determine properoperation of the alerting signals; and(5) Accept necessary barometric pressure settings if thesystem or device operates on barometric pressure. However,for operation below 3,000 feet AGL, the system or device needonly provide one signal, either visual or aural, to comply withthis paragraph. A radio altimeter may be included to providethe signal if the operator has an approved procedure for itsuse to determine DH or MDA, as appropriate.

91.219(c)

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Each operator to which this section applies must establish andassign procedures for the use of the altitude alerting systcmor device and each flight crewmember must comply with thoseprocedures assigned to him.

A enhanced GPWS (TSO C92/C 117) which complies Operator's responsibility to maintainwith Requirements (I) thru (5) is included in the system in an operable condition.baseline configuration RAL-IOO-OOO1. The enhancedportion of the EGPWS will be certified after initialtype cert

91.219(d) Altitude alerting system or device: Turbojet-powered civilairplanes

Paragraph (a) of this section does not apply to any operation Operator's responsibility.of an airplane that has an experimental certificate or to theoperation of any airplane for the following purposes:(I) Ferrying a newly acquired airplane from the place wherepossession of it was taken to a place where the altitudealerting system or device is to be installed.(2) Continuing a flight as originally planned, if the altitudealerting system or device becomes inoperative after theairplane has taken off; however, the flight may not depart froma place where repair or replacement can be made.(3) Ferrying an airplane with any inoperative altitude alertingsystem or device from a place where repairs or replacementscannot be made to a place where it can be made.(4) Conducting an airworthiness flight test of the airplane.(5) Ferrying an airplane to a place outside the United Statesfor the purpose of registering it in a foreign country.(6) Conducting a sales demonstration of the operation of theairplane.

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(7) Training foreign flight crews in the operation of theairplane before ferrying it to a place outside the United Statesfor the purpose of registering it in a foreign country.

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91.409(a)

91A09(b)

91.409(c)

InspectionsExcept as provided in paragraph (c) of this section, no person Operator's responsibility.may operate an aircraft unless, within the preceding 12calendar months, it has had ••(1) An annual inspection in accordance with part 43 of thischapter and has been approved for return to service by aperson authorized by ~ 43.7 of this chapter; or(2) An inspection for the issuance of an airworthinesscertificate in accordance with part 21 of this chapter. Noinspection performed under paragraph (b) of this section maybe substituted for any inspection required by this paragraphunless it is performed by a person authorized to performannual inspections and is entered as an "annual" inspectionin the required maintenance records.

Except as provided in paragraph (c) of this section, no personmay operate an aircraft carrying any person (other than acrewmember) for hire, and no person may give flightinstruction for hire in an aircraft which that person provides,unless within the preceding 100 hours of time in service theaircraft has received an annual or 100-hour inspection andbeen approved for return to service in accordance with part 43of this chapter or has received an inspection for the issuanceof an airworthiness certificate in accordance with part 21 ofthis chapter. The 100-hour limitation may be exceeded by notmore than 10 hours while en route to reach a place where theinspection can be done. The excess time used to reach a placewhere the inspection can be done must be included incomputing the next 100 hours of time in servic

InspectionsParagraphs (a) and (b) of this section do not apply to.-(1) An aircraft that carries a special flight permit, a currentexperimental certificate, or a provisional airworthinesscertificate;(2) An aircraft inspected in accordance with an approved

An approved maintenance schedule asper the Maintenance Review Board(MRB) Report, derived from the MSG-3process, and an Aircraft MaintenanceManual complying with FAR 25.1529 &Appendix H are provided to eachoperator. These documents reflect thegreen aircraft as designed by BombardierAerospace and supplemented byCompletion Center additions.

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aircraft inspection program under part 125 or 135 of thischapter and so identified by the registration number in theoperations specifications of the certificate holder having theapproved inspection program;(3) An aircraft subject to the requirements of paragraph (d) or(e) of this section; or(4) Turbine-powered rotorcraft when the operator elects toinspect that rotorcraft in accordance with paragraph (e) of thissection.

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Operational Acceptability for FAR PARTS 91/135SO. 100. Compliance Checklist

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91.409(d) InspectionsProgressive inspection. Each registered owner or operator ofan aircraft desiring to use a progressive inspection programmust submit a written request to the FAA Flight Standardsdistrict office having jurisdiction over the area in which theapplicant is located, and shall provide --(I) A certificated mechanic holding an inspectionauthorization, a certificated airframe repair station, or themanufacturer of the aircraft to supervise or conduct theprogressive inspection;(2) A current inspection procedures manual available andreadily understandable to pilot and maintenance personnelcontaining, in detail --(i) An explanation of the progressive inspection, including thecontinuity of inspection responsibility, the making of reports,and the keeping of records and technical reference material;(ii) An inspection schedule, specifYing the intervals in hoursor days when routine and detailed inspections will beperformed and including instructions for exceeding aninspection interval by not more than 10 hours while en routeand for changing an inspection interval because of serviceexperience;(iii) Sample routine and detailed inspection forms andinstructions for their use; and(iv) Sample reports and records and instructions for their use;

(3) Enough housing and equipment for necessary disassemblyand proper inspection of the aircraft; and(4) Appropriate current technical information for the aircraft.The frequency and detail of the progressive inspection shallprovide for the complete inspection of the aircraft within each12 calendar months and be consistent with the manufacturer'srecommendations, field service experience, and the kind ofoperation in which the aircraft is engaged. The progressiveinspection schedule must ensure that the aircraft, at all times,will be airworthy and will conform to all applicable FAA

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aircraft specifications, type certificate data sheets,airworthiness directives, and other approved data. If theprogressive inspection is discontinued, the owner or operator shall immediately notify the local FAA Flight Standardsdistrict office, in writing, of the discontinuance. After thediscontinuance, the first annual inspection under ~91.409(a)(I) is due within 12 calendar months afterthe lastcomplete inspection of the aircraft under the progressiveinspection. The 100-hour inspection under ~ 91.409(b) is duewithin 100 hours after that complete inspection. A completeinspection of the aircraft, for the purpose of determining whenthe annual and 100-hour inspections are due, requires adetailed inspection of the aircraft and all its components inaccordance with the progressive inspection. A routineinspection of the aircraft and a detailed inspection of severalcomponents is not considered to be a complete inspection.

91.409(e)Large airplanes (to which part 125 is not applicable), turbojetmultiengine airplanes, turbopropeller-powered muItiengineairplanes, and turbine-powered rotorcraft. No person mayoperate a large airplane, turbojet multi engine airplane,turbopropeller-powered muItiengine airplane, orturbine-powered rotorcraft unless the replacement times forlife-limited parts specified in the aircraft specifications, typedata sheets, or other documents approved by theAdministrator are complied with and the airplane orturbine-powered rotorcraft, including the aimame, engines,propellers, rotors, appliances, survival equipment, andemergency equipment, is inspected in accordance with aninspection program selected under the provisions ofparagraph (I) of this section, except that, the owner oroperator of a turbine-powered rotorcraft may elect to use theinspection provisions of ~ 91.409(a), (b), (c), or (d) in lieu of aninspection option of ~ 91.409(1).

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91.409(1) InspectionsSelection of inspection program under paragraph (e) of thissection. The registered owner or operator of each airplane orturbine-powered rotorcraft described in paragraph (e) of thissection must select, identify in the aircraft maintenancerecords, and use one of the following programs for theinspection of the aircraft:(1) A continuous airworthiness inspection program that is partof a continuous airworthiness maintenance program currentlyin use by a person holding an air carrier operating cenificateor an operating cenificate issued under pan 121 or 135 of thischapter and operating that make and model aircraft under part121 of this chapter or operating that make and model underpart 135 of this chapter and maintaining it under S135.41 I(a)(2) of this chapter.(2) An approved aircraft inspection program approved under S135.419 of this chapter and currently in use by a personholding an operating certificate issued under part 135 of thischapter.(3) A current inspection program recommended by themanufacturer.(4) Any other inspection program established by theregistered owner or operator of that airplane orturbine-powered rotorcraft and approved by the Administratorunder paragraph (g) of this section. However, theAdministrator may require revision of this inspection programin accordance with the provisions of S 91.415. Each operatorshall include in the selected program the name aud address ofthe person responsible for scheduling the inspectionsrequired by the program and make a copy of that programavailable to the person performing inspections on the aircraftand, upon request, to the Administrator.

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FAR

91.409(g)

91.409(h)

REQUIREMENT

InspectionsInspection program approved under paragraph (e) of thissection. Each operator of an airplane or turbine-poweredrotorcraft desiring to establish or change an approvedinspection program under paragraph (f)(4) of this section mustsubmit the program for approval to the local FAA FlightStandards district office having jurisdiction over the area inwhich the aircraft is based. The program must be in writingand include at least the following information:(I) Instructions and procedures for the conduct of inspectionsfor the particular make and model airplane or turbine-poweredrotorcraft, including necessary tests and checks. Theinstructions and procedures must set forth in detail the partsand areas of the airframe, engines, propellers, rotors, andappliances, including survival and emergency equipmentrequired to be inspected.(2) A schedule for performing the inspections that must beperformed under the program expressed in terms of the time inservice, calendar time, number of system operations, or anycombination of these.

Changes from one inspection program to another. When anoperator changes from one inspection program underparagraph (f) of this section to another, the time in service,calendar times, or cycles of operation accumulated under theprevious program must be applied in determining inspectiondue times under the new program.

COMPLIANCE REMARKS

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91.411(a)

91.411(b)

Altimeter system and altitude reporting equipment tests andinspections

No person may operate an airplane, or helicopter, in controlledairspace under IFR unless --(1) Within the preceding 24 calendar months, each staticpressure system, each altimeter instrument, and eachautomatic pressure altitude reporting system has been testedand inspected and found to comply with appendix E of part 43of this chapter;(2) Except for the use of system drain and alternate staticpressure valves, following any opening and closing of thestatic pressure system, that system has been tested andinspected and found to comply with paragraph (a),appendices E and F, of part 43 of this chapter; and(3) Following installation or maintenance on the automaticpressure altitude reporting system of the ATC transponderwhere data correspondence error could be introduced, theintegrated system has been tested, inspected, and found tocomply with paragraph (c), appendix E, of part 43 of thischapter.

The tests required by paragraph (a) of this section must beconducted by -- (I) Themanufacturer of the airplane, orhelicopter, on which the tests and inspections are to beperformed; (2) A certificated repair station properly equippedto perform those functions and holding-- (i) An instrumentreating, Class I; (ii) A limited instrument rating appropriate tothe make and model of appliance to be tested; (iii) A limitedrating appropriate to the test to be performed; (iv) An airframerating appropriate to the airplane, or helicopter, to be tested;(v) A limited rating for a manufacturer issued for the appliancein accordance with 145.IOl(b)(4) of this chapter; (3) A

The Maintenance Manual includes the tests and Operator responsible for conducting testsinspections required by Appendix E of FAR 43. The and inspections.FAR 43 tests and inspections are conducted as a partof the Canadair Functional Test Plan for each aircraftprior to delivery.

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certificated mechanic with an airframe rating (static pressuresystem tests and inspections only);

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91.4l1(c)

9IAI1(d)

91.413(a)

91.413(b)

Altimeter system and altitude reporting equipment tests andinspections

Altimeter and altitude reporting equipment approved underTechnical Standard Orders are considered to be tested andinspected as of the date of their manufacture.

No person may operate an airplane, or helicopter, in controlledairspace under IFR at an altitude above the maximum altitudeat which all altimeters and the automatic altitude reportingsystem of that airplane, or helicopter, have been tested.

ATe transponder tests and inspectionsNo persons may use an ATC transponder that is specified in91.215(a), 121.345(c), or ~ 135.143(c) of this chapter unless,within the preceding 24 calendar months, the ATCtransponder has been tested and inspected and found tocomply with appendix F of part 43 of this chapter; and

Following any installation or maintenance on an ATCtransponder where data correspondence error could beintroduced, the integrated system has been tested, inspected,and found to comply with paragraph (c), appendix E, of part 43of this chapter.

The Maintenance Manual includes the tests and Operator responsible for conducting testsinspections required by Appendix E of FAR 43. The and inspections.FAR 43 tests and inspections are conducted as a partof the Canadair Functional Test Plan for each aircraftprior to delivery.

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91.413(c)

91.503(a)

ATC transponder tests and inspectionsThe tests and inspections specified in this section must beconducted by --(1) A certificated repair station properly equipped to performthose functions and holding --(i) A radio rating, Class III;(ii) A limited radio rating appropriate to the make and modeltransponder to be tested;(iii) A limited rating appropriate to the test to be performed;(iv) A limited rating for a manufacturer issued for thetransponder in accordance with ~ 145.IOI(b)(4) of thischapter; or(2) A holder ofa continuous airworthiness maintenanceprogram as provided in part 121 or ~ 135.411(a)(2) of thischapter; or(3) The manufacturer of the aircraft on which the transponderto be tested is installed, if the transponder was installed bythat manufacturer.

Flying equipment and operating informationThe pilot in command of an airplane shall ensure that thefollowing flying equipment and aeronautical charts and data,in current and appropriate form, are accessible for each flightat the pilot station of the airplane:(I) A flashlight having at least two size "D" cells, or theequivalent, that is in good working order.(2) A cockpit checklist containing the procedures required byparagraph (b) of this section.(3) Pertinent aeronautical charts.(4) For IFR, VFR over-the-top, or night operations, eachpertinent navigational en route, terminal area, and approachand letdown chart.(5) In the case ofmuitiengine airplanes, one-engineinoperative climb performance data.

Operator's responsibility.

The green aircraft includes the following:- Flashlight- Checklist & QRH- AFM Performance Chart

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Issue: ..Date: March 2003

FAR

91.503(b)

91.503(c)

91.503(d)

REQUIREMENT

Flying equipment and operating informationEach cockpit checklist must contain the following proceduresand shall be used by the flight crewmembers when operatingthe airplane:(I) Before starting engines.(2) Before takeoff.(3) Cruise.(4) Before landing.(5) After landing.(6) Stopping engines.(7) Emergencies.

Each emergency cockpit checklist procedure required byparagraph (b)(7) of this section must contain the followingprocedures, as appropriate:(I) Emergency operation of fuel, hydraulic, electrical, andmechanical systems.(2) Emergency operation of instruments and controls.(3) Engine inoperative procedures.(4) Any other procedures necessary for safety.

COMPLIANCE

Cockpit Checklist provided in the green aircraftaddresses items I to 7


REMARKS

Checklists are provided in the AirplaneFlight Manual I Flight Crew OperatingManual.

The equipment, charts, and data prescribed in this section Operator's responsibility.shall be used by the pilot in command and other members ofthe flight crew, when pertinent.

91.603 Aural speed warning deviceNo person may operate a transport category airplane in aircommerce unless that airplane is equipped with an aural speedwarning device that complies with ~ 25.1303(c)(I).

Speed warning devices which comply with FAR25. 1303(c)( I) are included in the baselineconfiguration RAL-I 00-000 1.

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Operational Acceptability for FAR PARTS 91/135RAZ- BA 100-1 06


FAR

91.609(a)

REQUIREMENT

Flight recorders and cockpit voice recordersNo holder of an air carrier operating certificate or an operatingcertificate may conduct any operation under this part with anaircraft listed in the holder's operations specifications orcurrent list of aircraft used in air transportation unless thataircraft complies with any applicable flight recorder andcockpit voice recorder requirements of the part under whichits certificate is issued except that the operator may --(1) Ferry an aircraft with an inoperative flight recorder orcockpit voice recorder from a place where repair orreplacement cannot be made to a place where they can bemade;(2) Continue a flight as originally planned, if the flight recorderor cockpit voice recorder becomes inoperative after theaircraft has taken off;(3) Conduct an airworthiness flight test during which the flightrecorder or cockpit voice recorder is turned off to test it or totest any communications or electrical equipment installed inthe aircraft; or(4) Ferry a newly acquired aircraft from the place wherepossession of it is taken to a place where the flight recorder orcockpit voice recorder is to be installed.

COMPLIANCE REMARKS

A digital flight data recorder conformingto TSO C 124 is included in the baselineconfiguration RAL-l 00-000 1, inaccordance with FAR 25.1459. The FDRwill be fully operational prior to aircraftentry into service.

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FAR

91.609(b)

REQUIREMENT

Flighl recorders and cockpil voice recordersNotwithstanding paragraphs (c) and (e) of this section, anoperator other than the holder of an air carrier or a commercialoperator certificate may--(I) Ferry an aircraft with an inoperative flight recorder orcockpit voice recorder from a place where repair orreplacement cannot be made to a place where they can bemade;(2) Continue a flight as originally planned if the flight recorderor cockpit voice recorder becomes inoperative after the aircrafthas taken off;(3) Conduct an airworthiness flight test during which the flightrecorder or cockpit voice recorder is turned off to test it or totest any communications or electrical equipment installed inthe aircraft;(4) Ferry a newly acquired aircraft from a place wherepossession of it was taken to a place where the flight recorderor cockpit voice recorder is to be installed; or(5) Operate an aircraft:(i) For not more than 15 days while the flight recorder and/orcockpit voice recorder is inoperative and/or removed for repairprovided that the aircraft maintenance records contain anentry that indicates the date offailure, and a placard is locatedin view of the pilot to show that the flight recorder or cockpitvoice recorder is inoperative.(ii) For not more than an additional 15 days, provided that therequirements in paragraph (b)(5)(i) are met and that acertificated pilot, or a certificated person authorized to returnan aircraft to service under ~ 43.7 of this chapter, certifies inthe aircraft maintenance records that additional time isrequired to complete repairs or obtain a replacement unit

COMPLIANCE

Operator's responsibility. The green aircraft has anapproved MMEL.

REMARKS

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FAR

91.609(c)

91.609(d)

REQUIREMENT

Flight recorders and cockpit voice recordersNo person may operate a U.S. civil registered, multiengine,turbine-powered airplane or rotorcraft having a passengerseating configuration, excluding any pilot seats of 10 or morethat has been manufactured after October II, 1991, unless it isequipped with one or more approved flight recorders thatutilize a digital method of recording and storing data and amethod of readily retrieving that data from the storagemedium, that are capable of recording the data specified inappendix E to this part, for an airplane, or appendix F to thispart, for a rotorcraft, of this part within the range, accuracy,and recording interval specified, and that are capable ofretaining no less than 8 hours of aircraft operation.

Whenever a flight recorder, required by this section, isinstalled, it must be operated continuously from the instantthe airplane begins the takeoff roll or the rotorcraft beginslift-off until the airplane has completed the landing roll or therotorcraft has landed at its dest

COMPLIANCE


The green aircraft is equipped with a CVR whichmeets this requirement.


The green aircraft is equipped with a CVR whichmeets this requirement.

REMARKS

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91.609(e)

91.609(1)

Flight recorders and cockpit voice recordersUnless orherwise authorized by the Administrator, after The green aircraft configuration complies with theOctober 11, 1991, no person may operate a U.S. civil registered applicable regulations of part 25 for CVR.multiengine, turbine-powered airplane or rotorcraft having a

passenger seating configuration of six passengers or moreand for which two pilots are required by type certification oroperating rule unless it is equipped with an approved cockpitvoice recorder that:(I) Is installed in compliance with ~ 23.1457(a) (1) and (2), (b),(c), (d), (e), (I), and (g); ~ 25.1457(a) (I) and (2), (b), (c), (d), (e),(I), and (g); ~ 27. 1457(a) (I) and (2), (b), (c), (d), (e), (I), and (g);or ~ 29. 1457(a) (I) and (2), (b), (c), (d), (e), (I), and (g) ofthis

chapter, as applicable; and(2) Is operated continuously ITom the use of the checklistbefore the flight to completion of the final checklist at the endof the flight.

In complying with this section, an approved cockpit voice The CVR installed in the green aircraft complies.recorder having an erasure feature may be used, so that at anytime during the operation of the recorder, information

recorded more than 15 minutes earlier may be erased orotherwise obli

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91.609(g)

91.App A

Flight recorders and cockpit voice recordersIn the event of an accident or occurrence requiring immediate Operator's responsibility.notification to the National Transportation Safety Board underpart 830 of its regulations that results in the termination of the\light, any operator who has installed approved flightrecorders and approved cockpit voice recorders shall keep therecorded information for at least 60 days or, ifrequested bythe Administrator or the Board, for a longer period.Information obtained from the record is used to assist indetermining the cause of accidents or occurrences inconnection with the investigation under part 830. TheAdministrator does not use the cockpit voice recorder recordin any civil penalty or certifica

Category II Operations: Manual, Instruments, Equipment,and Maintenance

I. Category II Manual(a) Application for approval. An applicant for approval of aCategory II manual or an amendment to an approved CategoryII manual must submit the proposed manual or amendment tothe Flight Standards District Omce having jurisdiction of thearea in which the applicant is located. (fthe applicationrequests an evaluation program, it must include the following:

(I) The location of the aircraft and the place where thedemonstrations are to be conducted; and(2) The date the demonstrations are to commence (at least 10days after filing the application).(b) Contents. Each Category II manual must contain:(I) The registration number, make, and model of the aircraft towhich it applies;(2) A maintenance program as specified in section 4 of thisappendix; and

Certification for Category II operations will beconducted after initial Type certification. Anapproved Airplane Flight Manual, includingprocedures, instructions and limitations will beprovided with each aircraft. A maintenanceDocument, derived from MSG-3 process, and anaircraft Maintenance Manual are provided with eachaircraft.

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Challenger JVOFSB Report

(3) The procedures and instructions related to recognition ofdecision height, use of runway visual range information,approach monitoring, the decision region (the region betweenthe middle marker and the decision height), the maximumpermissible deviations of the basic ILS indicator within thedecision region, a missed approach, use of airborne lowapproach equipment, minimum altitude for the use of theautopilot, instrument and equipment failure warning systems,instrument failure, and other procedures, instructions, andlimitations that may be found necessary by the Administrator.2. Required Instruments and EquipmentThe instruments and equipment listed in this section must beinstalled in each aircraft operated in a Category II operation.This section does not require duplication of instruments andequipment required by ~ 91.205 or any other provisions of thischapter.

(a) Group l. (I) Two localizer and glide slope receivingsystems. Each system must provide a basic ILS display andeach side of the instrument panel must have a basic ILS. However, a single localizer antenna and a single glideslope antenna may be used.(2) A communications system that does not affect theoperation of at least one of the ILS systems.(3) A marker beacon receiver that provides distinctive auraland visual indications of the outer and the middle markers.(4) Two gyroscopic pitch and bank indicating systems.(5) Two gyroscopic direction indicating systems.(6) Two airspeed indicators.(7) Two sensitive altimeters adjustable for barometricpressure, each having a placarded correction for altimeterscale error and for the wheel height of the aircraft. After June26, 1979, two sensitive altimeters adjustable for barometricpressure, having markings at 20-foot intervals and eachhaving a placarded correction for altimeter scale error and forthe wheel height of the aircraft.(8) Two vertical speed indicators.(9) A flight control guidance system that consists of either anautomatic approach coupler or a flight director system. Aflight director system must display computed information assteering command in relation to an ILS localizer and, on thesarne instrument, either computed information as pitchcommand in relation to an ILS glide slope or basic ILS glide

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')Challenger" lIO FSB Report

slope infonnation. An automatic approach coupler mustprovide at least automatic steering in relation to an ILSlocalizer. The night control guidance system may be operatedfrom one of the receiving systems required by subparagraph(I) of this paragraph.(10) For Category II operations with decision heights below150 feet either a marker beacon receiver providing aural andvisual indications ofthe inner marker or a radio altimeter.(b) Group II. (I) Warning systems for immediate detection bythe pilot of system faults in items (I), (4), (5), and (9) of GroupI and, if installed for use in Category 1II operations, the radioaltimeter and autothrottle system.(2) Dual controls.(3) An externally vented static pressure system with an alternate static pressure source.(4) A windshield wiper or equivalent means of providingadequate cockpit visibility for a safe visual transition by eitherpilot to touchdown and rollout.(5) A heat source for each airspeed system pitot tube installedor an equivalent means of preventing malfunctioning due toicing of the pitot system.3. Instruments and Equipment Approval(a) General. The instruments and equipment required bysection 2 of this appendix must be approved as provided inthis section before being used in Category II operations.Before presenting an aircraft for approval of the instrumentsand equipment, it must be shown that since the beginning ofthe 12th calendar month before the date of submission --(I) The ILS localizer and glide slope equipment were benchchecked according to the manufacturer's instructions andfound to meet those standards specified in RTCA Paper23-63/00-117 dated March 14, 1963, "Standard AdjustmentCriteria for Airborne Localizer and Glide Slope Receivers,"which may be obtained from the RTCA Secretariat, 1425 K St.,NW., Washington, DC 20005.(2) The altimeters and the static pressure systems were testedand inspected in accordance with appendix E to part 43 of thischapter; and(3) All other instruments and items of equipment specified insection 2(a) of this appendix that are listed in the proposedmaintenance program were bench checked and found to meetthe manufacturer's specifications.(b) Flight control guidance system. All components of the

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)Challengel ~uOFSB Report

f1ighl control guidance system musl be approved as installedby lhe evalualion program specified in paragraph (e) oflhisseclion if they have not been approved for Category IIIoperations under applicable type or supplemental typecertification procedures. In addition, subsequent changes tomake, model, or design of the components must be approvedunder this paragraph. Related systems or devices, such as theautothrottle and computed missed approach guidance(3) An externally vented static pressure system with anmust be approved in the same manner if they are to be usedfor Category II operations.(c) Radio altimeter. A radio altimeter must meet theperformance criteria of this paragraph for original approvaland after each subsequent alteration.(I) It must display to the flight crew clearly and positively thewheel height of the main landing gear above the terrain.(2) It must display wheel height above the terrain to anaccuracy of plus or minus 5 feet or 5 percent, whichever isgreater, under the following conditions:(i) Pitch angles of zero to plus or minus 5 degrees about themean approach attitude.(ii) Roll angles of zero to 20 degrees in either direction.(iii) Forward velocities from minimum approach speed up to200 knots.(iv) Sink rates from zero to 15 feet per second at altitudes from100 to 200 feet.(3) Over level ground, it must track the actual altitude oftheaircraft without significant lag or oscillation.(4) With the aircraft at an altitude of200 feet or less, anyabrupt change in terrain representing no more than 10 percentof the aircraft's altitude must not cause the altimeter to unlock,and indicator response to such changes must not exceed O. Iseconds and, in addition, if the system unlocks for greaterchanges, it must reacquire the signal in less than I second.(5) Systems that contain a push-to-test feature must test theentire system (with or without an antenna) at a simulatedaltitude of less than 500 feet.(6) The system must provide to the flight crew a positivefailure warning display any time there is a loss of power or anabsence of ground return signals within the designed range ofoperating altitudes.(d) Other insIruments and equipment. All other insIruments

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)Challenger ~clO FSB Report

and items of equipment required by 9 2 of this appendix mustbe capable of perfonning as necessary for Category IIoperations. Approval is also required after each subsequentalteration to these instruments and items of equipment.

(e) Evaluation program -- (I) Application. Approval byevaluation is requested as a part of the application forapproval of the Category II manual.(2) Demonstrations. Unless otherwise authorized by theAdministrator, the evaluation program for each aircraftrequires the demonstrations specified in this paragraph. Atleast 50 ILS approaches must be flown with at least fiveapproaches on each of three different ILS facilities and nomore than one half of the total approaches on anyone ILSfacility. All approaches shall be flown under simulatedinstrument conditions to a 1OO-footdecision height and 90percent of the total approaches made must be successful. Asuccessful approach is one in which --(i) At the 1OO-footdecision height, the indicated airspeed andheading are satisfactory for a nonnal flare and landing (speedmust be plus or minus 5 knots of programmed airspeed, butmay not be less than computed threshold speed ifautothrottles are used);(ii) The aircraft at the IOO-footdecision height, is positionedso that the cockpit is within, and tracking so as to remainwithin, the lateral confines of the runway extended;(iii) Deviation from glide slope after leaving the outer markerdoes not exceed 50 percent of full-scale deflection asdisplayed on the ILS indicator;(iv) No unusual roughness or excessive attitude changesoccur after leaving the middle marker; and(v) In the case of an aircraft equipped with an approachcoupler, the aircraft is sufficiently in trim when the approachcoupler is disconnected at the decision height to allow for thecontinuation of a nonnal approach and landing.(3) Records. During the evaluation program the followinginfonnation must be maintained by the applicant for theaircraft with respect to each approach and made available tothe Adninistrator upon request:(i) Each deficiency in airborne instruments and equipment thatprevented the initiation of an approach.

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')Challenger ~VOFSB Report

(ii) The reasons for discontinuing an approach, including the

altitude above the runway at which it was discontinued.(iii) Speed control at the 100-foot decision height if autothrottles are used.(iv) Trim condition of the aircraft upon disconnecting the autocoupler with respect to continuation to flare and landing.(v) Position of the aircraft at the middle marker and at thedecision height indicated both on a diagram of the basic ILSdisplay and a diagram of the runway extended to the middlemarker. Estimated touchdown point must be indicated on therunway diagram.(vi) Compatibility of flight director with the auto coupler, ifapplicable.(vii) Quality of overall system performance.(4) Evaluation. A final evaluation of the flight controlguidance system is made upon successful completion of thedemonstrations. If no hazardous tendencies have beendisplayed or are otherwise known to exist, the system isapproved as installed.4. Maintenance program(a) Each maintenance program must contain the following:(I) A list of each instrument and item of equipment specifiedin 9 2 of this appendix that is installed in the aircraft andapproved for Category II operations, including the make andmodel of those specified in 92(a).(2) A schedule that provides for the performance ofinspections under subparagraph (5) of this paragraph within 3calendar months after the date of the previous inspection. Theinspection must be performed by a person authorized by pan43 of this chapter, except that each alternate inspection maybe replaced by a functional flight check. This functional flightcheck must be performed by a pilot holding a Category II pilotauthorization for the type aircraft checked.(3) A schedule that provides for the performance of benchchecks for each listed instrument and item of equipment that isspecified in section 2(a) within 12 calendar months after thedate of the previous bench check.(4) A schedule that provides for the performance of a test and

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inspection of each static pressure system in accordance withappendix E to part 43 of this chapter within 12 calendarmonths after the date of the previous test and inspection.(5) The procedures for the performance of the periodicinspections and functional flight checks to determine theability of each listed instrument and item of equipmentspecified in section 2(a) of this appendix to perform asapproved for Category II operations including a procedure forrecording functional flight checks.(6) A procedure for assuring that the pilot is informed of alldefects in listed instruments and items of equipment.(7) A procedure for assuring that the condition of each listedinstrument and item of equipment upon which maintenance isperformed is at least equal to its Category II approvalcondition before it is returned to service for Category IIoperations.(8) A procedure for an entry in the maintenance recordsrequired by 9 43.9 of this chapter that shows the date, airport,and reasons for each discontinued Category II operationbecause of a malfunction of a listed instrument or item ofequipment.(b) Bench check. A bench check required by this section mustcomply with this paragraph.(1) It must be performed by a certificated repair station holdingone of the following ratings as appropriate to the equipmentchecked:(i) An instrument rating.(ii) A radio rating.(iii) A rating issued under subpart D of part 145 of thischapter.(2) It must consist of removal of an instrument or item ofequipment and performance of the following:(i) A visual inspection for cleanliness, impending failure, andthe need for lubrication, repair, or replacement of parts;(ii) Correction of items found by that visual inspection; and(iii) Calibration to at least the manufacturer's specificationsunless otherwise specified in the approved Category II manu

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)


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RAZ-BAI00-106Issue: --Date: March 2003

FAR

91.App C

REQUIREMENT

for the aircraft in which the instrument or item of equipment isinstalled.(c) Extensions. After the completion of one maintenance cycleof 12 calendar months, a request to extend the period forchecks, tests, and inspections is approved if it is shown thatthe performance of particular equipment justifies therequested extension.

Operations in the North Atlantic (NAT) MinimumNavigation Performance Specifications (MNPS) Airspace

Section INAT MNPS airspace is that volume of airspace between FL285 and FL 420 extending between latitude 27 degrees northand the North Pole, bounded in the east by the easternboundaries of control areas Santa Maria Oceanic, ShanwickOceanic, and Reykjavik Oceanic and in the west by thewestern boundary of Reykjavik Oceanic Control Area, thewestern boundary of Gander Oceanic Control Area, and thewestern boundary of New York Oceanic Control Area,excluding the areas west of 60 degrees west and south of 38degrees 30 minutes north.Section 2The navigation performance capability required for aircraft tobe operated in the airspace defined in section I of thisappendix is as follows:(a) The standard deviation of lateral track errors shall be lessthan 6.3 NM (1 1.7 Km). Standard deviation is a statisticalmeasure of data about a mean value. The mean is zero nauticalmiles. The overall form of data is such that the plus and minus1 standard deviation about the mean encompasses

COMPLIANCE

Aircraft navigation performance capability exceedsthe minimum specifications.

REMARKS

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