, -...-

.. ENGINE LOGBOOK PT6A Turboprop

PCE-RB0334

1. Approving national aviation authority /country - 2. 3, Form tracking No. - Numero de sui .... i du formulaire Autorite de I' aviation du pays d 'approbation I pays AUTHORIZED RELEASE CERTIFICATE · BON DE SORTIE AUTORISEE Transport Canada TCCA 24-0078 SEE BLOCK 5

4. Approved organization name and address - Nom el adre~~ de l'organisme agree Pratt & Whitney Ganada Cie .I Pratt & Whitney Canada Corp 5. Work orderlcontracUinvoice-

Prall & Whitney Canada 4045 - 26 AVE. I,ORTH Bon de travail/contra! /facture

0 LETHBRIDGE, P.LBERTA Una societe de United TeehnologiesJA United Technologies Company T1H 6G2 P.O.# 4000377344

6. Item 7. pescription 8. Part No. - N° de piece 9. Eligibility' - AdmlSsibilite" 10. Qty - QU~e 11 . Serialfbatch No.- N° de serie/de lot 12. Status/work - Etat/t ravail

Free Turbine Turbo-Prop 01 PT6A-34 , 3020800 VARIOUS 1 PCE-RB0334 MANUFACTURED

13. Remarks - .Remarq.ues

. , ,

CANADIAN TYPE c:;ERTIFICATE E-6, FAA TYPE CERTIF.ICATE E4EA

THIS ENGINE CONFORMS TO !TS UNITED STATES TYpg DES!GN (TYPE CERTIFICATE NUMBER E4EA) AND IS IN CONDITION FOR SAFE OPERATION. THIS ENGINE HAS BEEN SUBJECTED BY THE MANUFACTURER TO A FINAL OPERATION CHECK AND IS IN A PROPER STATE OF AIRWORTHINESS.

,. " , .. , , .

I . . , "

, , -;-

'. " .

- . . , .

14. Certifies that the items identified above were manufactured in conformity to: ,

Le present bon cert ifie que les articles Indiques ci-dessus ant ele construits conformement a : c: 571.10 Maintenance release. - Certification apres maintenance en vertu du RAe 571

~ Approved design data and are in condi tion for safe operation. ,

des donnees de conceotion aoorouvees et au'ils oeuvent eIre utilises en louIe securile 0 Other re~ulalio ecifled in block 13. - Autre reQlemenlalion precisee a se 13.

0 Non Approved design data specified in block 13.- C:fifies that, except where otherwise ified in block 13, the work . led in block 12 and described in

des donnees de conception non approuvees indiquees ell la case 13. bl k 13 was performed in accordance wi th 571. l e I>resent bon certifie que, a moins d'indication ire raissant a la case 13, Ie travail indique a la cas~ 12 et d'krit a la case 13 a ele effectue confor u RAC 571.

15. Authorized signature - Signature autorisee 16.Certificate I Approval Ref. No. 20. Authorized s;9natu,. ~ 21. C.rtmc;~

~ N° d'agremenUd'autorisation (f::) T.e.4-&8

N° d'agremen ' torisation

~ NO. 024

17. Name - Nom 18. Date (dd/month/yyyy) 2V 23. Date (dd/mmmlyyyy)

~ K.PMDOR 1 3 DEC 2006 ,

2HXl78 (12/0912001 ) I P&WC 5720 (200S.03) Installer must cross.check eligibility With approved data - Le monleur 001 conlre-venfier I adflSSlbil lte avec les donnees approlNees 1. Le pl'esenl document n'autolise aucunement Ie montage de la piece. - 1. This document does not consblute authority to mslall the part. 2. 8; Ie monleur se base sur la reglementaUon naUonale d'une autorite de nav. igabilite autre Que celie indiQuee a la case 1, il 001 s'assurer que I't0rit£! d. e navigabilite doni i.1 releve accepte les prod. uils ou les travaux de maintenance de l'auloril9 de. navigabilile indiquee a la case 1, • 2. Where the Installer works in accordance with the national regulations 0/ an airworthiness authority other than the auth' ty specified In ~ock 1, the inSlalier must ensure that his!her ahworthiness authority accepts producls or maintenance from the airworthiness aulhority specified in block 1, . 3. Les enonces des cases 14 et19 ne constituent en aucune fa~on une certification du montage. Dans laus les cas, Ie dossier technique de t'ae r~€f 001 renfermer une certification de montage c\ellvree confo(foomenl a la regiementation de l'Etal d'lmmalriculation, et ce, avant que tout vol puisse avoir lieu. - 3. Statements 14 and 19 do not constitute installation certitication. In all cases the aircraft technical record must contain an installation certification, issued in accordance with the national regulations of the slale of registry, before the aircraft may be Hown

PRATT & WHITNEY CANADA CORP. P68 PROGRAM 4.3.44 ================================================================ PT6A-34 S/N : PCE-RB0334 FINAL ACCEPTANCE TEST RECORD ------------------------------------------------------

2006 DEC 12 TEST CELL: 3202 BUILD SPEC.: ENGINE TESTED AND ACCEPTED IN ACCORDANCE WITH E&TI

FINAL VANE FLOW AREAS FIRST STAGE SECOND STAGE

1009 245 29501 3S3 29501 4S2

======= = = ::; = ::; ::; ::; ::; ::; ::; ::; ::; ::; ::; ::; ::; ::; ::; ::; ::; = = = =

6 . 11 15 . 38 = = =

PERFORMANCE DATA TAKE-OFF MAX-CRUISE ::; ::; ::; ::; ::; ::; = ::; = ::; ::; = ::; ::; ::; = = = = =

PROP SPEED S . L.S. STD. DAY POWER TRIMMED INTERTURBINE TEMP T5D (DERIVED) GAS GEN. SPEED FUEL FLOW @ 18400 BTU / LB

DEG R DEG R RPM LB / HR

::; ::; ::; =

- - - = = = = = = - - - = = = SPEC ACTUAL SPEC = = = = = = = = = - - -- - -2200. 2200. 2200 .

750. 750. 700. 1785. 1755. 1745.

1812. 36800 36500.

467. 445. 443.

FUEL TYPE : CPW 204

= = = = ACTUAL

- - - -- - - -2200.

700. 1715. 1773 .

36000. 422.

TEST LHV : 18540. BTU/LB S.G. :0.812 @ 49. DEG F

OIL TYPE OIL CONSUMPTION

T.O. OIL PRESSURE OIL TEMPERATURE

I . T.T . TRIM DELTA T (UNTRIMMED-TRIMMED) I.T . T. TRIM DELTA T (UNTRIMMED-TRIMMED)

I.T.T. TRIM CLASS TRIM RESISTANCE

COLD HARNESS RESISTANCE = ::; = = ::; ::; ::; ::; ::; = ::; ::; ::; ::; = ::; ::; ::; ::; ::; ::; ::; ::; = HANDL I NG AND CONTROL SETTINGS ::; ::; = ::; ::; ::; ::; = ::; ::; ::; ::; ::; ::; = = = = ::; = ::; ::; ::; ::; = =

=

=

PWA 521 0 . 0 93.8 154.5

54.6 30.3 50 19.1

0 .71 = = =

= = = 35579 38100 35579 19736

TYPE LB/HR PSI DEG F

DEG F DEG C

OHMS OHMS

= = = = =

= = = = = RPM RPM RPM RPM

II

=

=

= =

= =

= =

= = = =

TRIMMED MAX NG UNTRIMMED MAX NG DATA PLATE SPEED

IDLE SPEED ACCEL . TIME F . I . TO MAX @ Tl

SG DOME FINAL SETTING ENGINE DRY WEIGHT

2.37 SECS @ 4l. 1 DEGF INDEX CLICK 333 . 5 LBS.

PRODUCTION SIGNATURE

INSPECTION SIGNATURE

GOVERNMENT INSPECTOR

THE UNDERSIGNED CERTIFIES THAT THIS RECORD ACCURATELY SETS THE EVENTS DURING THE TEST MADE ON THE ENGINE THEREIN IDENTIFIED .

~ (f:\ T.C. '" / ~0NO.04~

~JjPZ1~ G. HERMANN

FORTH

DATE 1 3 DEC 2006 FOREMAN, ASSY . &TEST INSP i I

Liste des composants moteur a numeros de serie Engine Serialized Component Summary

P&WC JR3-6830-E (0 5-1998)

Modele PT6A-34 I N° de serie PCE-RB0334 Model Serial No.

N° du materiel DeSi~ation du materiel N° de serle Code de trait.

Material Number aterial Name Serial No. thermique Heat Code

3007338 GEAR-RING,SECOND STAGE REDUCTION PKAAA072678 3011 095 SHAFT-POWER TURBINE RWA59A104 HSCJW 3011713 DISC-COMPRESSOR A0023XCK KAWAD 3012286 COUPLING SHAFT FLEX 2ND STAGE RED'N PKAAA074029 3013111 HUB-COMPRESSOR,REAR RWA56A145 KAWBX 3013132 CARRIER-SECOND STAGE REDUCTION PKAAA042862 3013176 IMPELLER - CENTRIFUGAL EAAAOooC029 PZBSB 3013411 DISC-TURBINE A0024342 PZBTM 3013712 DISC-COMPRESSOR A0023W07 KAWAD 3018834 COUPLING POWER TURBINE SHAFT PKAAA073909 3019906 FLOW DIVIDER AND DUMP GATE 9959512919 3022339 RING-CONTAINMENT RWA60A258 SGEAJ 3023250 GEAR-SUN,2STG RDCN,46 TEETH PKAAA066119 3023252 ADAPTER-1 ST STAGE CARRIER PKAAA073085 3024765 GEAR-SUN,1ST STAGE RDCN,27 TEETH PKAAA058959 3026812 DISC-TURBINE A00244CC PZBXX 3027629 BUS BAR-T5 THERMOCOUPLE,ASSY OF HR22986 3028004 BEARING OPTION BB0052498

BB0052601 3028007 BEARING-ROLLER FLANGED BB0053121 3028266 HOUSING ASSY-PROP RED GBOX,FRONT RWA59A756 3032151CL03 VANE RING-TURBINE HLA046C 3032710 HEATER-OIL TO FUEL WA28298

-'3034794_ PUMP-FUEL 002503 3035889 EXCITER-IGNITION NNA06423888 3035926 GOVERNOR-PROPELLER 14995496AE 3037305 GEAR-PLANET, 1ST STAGE REDUCTION PKAAA075571

PKAAA075578 PKAAA075585

3043672CL02 VANE RING-POWER TURBINE(MACH) HLAX031 3045839 GEAR-PLANET,SECOND STAGE REDUCTION PKAAA074287

PKAAA074293 PKAAA074294 PKAAA074295 PKAAA074297

3048695-01 SHAFT-PROPELLER EAAAOOOB088 KAWCB 3053085-01 GEAR - RING FIRST STAGE REDUCTION PKAAA075453 3058201-01 GEARSHAFT - DRIVE, ACCESSORY GEARBOX PKAAA071051 3058264-01 COUPLING-COMPRESSOR REAR HUB PKAAA064177 3058641-01 HOUSING-POWER TURBINE STATOR,ASSY OF A001A805 3070218-01 GEARSHAFT STARTER GENERATOR DRIVE PKAAA069111

Pratt & Whitney Canada Unit sociti te dEl United Technologies fA Unitod Tochnologies Company

Pratt & \. CanaOa Cie. I Prall & Whitney Canada Corp 1000 , Marie-Victorin Longueuil. Quebec. Canada J4G 1A1 450-677-9411

Page 1

I Caract. de montage Build Spec NO. BS1009

N° de serle du N° de lot pour trait. N° de materiel du foumisseur materiel forae thermique Vendor Material No. Forging Sen al No. Heat Treat Batch No.

44138

44069

061 164

44138

044

l....onL'O

Liste des composants moteur it numeros de serie Engine Serialized Component Summary

P&WC JR3-6830-E (05- \ 998)

Modele PT6A-34 I N° de serie PCE-RB0334 Model Serial No.

N° du materie l Desi't1'ation du materiel N° de serie Code de trait.

Material Number aterial Name Serial No. thermique Heat Code

3100829-03 VALVE ASSY-COMPRESSOR BLEED AHX007259 3101419-01 CARRIER-FIRST STAGE REDUCTION PKAAA046523 3101635-01 BEARING-BALL FLANGED FAA0633938 3101864-01 BEARING-BALL FAA0634054 31 02227-01 BEARING-BALL FLANGED B80052942 3102336-01 SHAFT-STUB,COMPRESSOR,FRONT RWA57A738 EPEIB 3110863-07 CASE ASSY-GAS GENERATOR RWA65A180 3111780-01 DUCT-TURBINE EXHAUST, ASYO RWA64A117 3112368-01 BEARING-ROLLER FLANGED,.94X1 .65X.47 FAA0635034

FAA0635035 FAA0635045 FAA0635046 FAA0635060 FAA0635061 FAA0635062 FAA0635112 FAA0635113 FAA0635114 FAA0635828 FAA0635829

3117924-01 WIRING HARN-T5,THERMOCOUPLE NRA23739 31 22633-01 LINER-COMBUSTION CHAMBER,ASSY OF RWA64A330 3122696-03 FUEL CON}:R0L-TURBOPROP C25819

Approve sar Approve By /~/I 1/'/'/'/'/1/ G. HERMANN

~ TC 4·58 ,... ",NO 049

,

Pratt & Whitney Canada Une sociatli de United Technole>gies fA Uniled Technologies Company

Pratt & \' 2canada Cie. I Pratt & WI ,0111 Y Canada Corp. 1000, Marie-Victorin l ongueuil, Quebec, Canada J 4G 1A1 450-677-9411

Page 2

I Caract. de montage Build Spec NO. B51009

N° de serie du N° de lot pour trait. N° de materiel du fournisseur materiel forge thermique Vendor Material No. Forging Senal No. Heat Treat Batch No.

Date 2006.12.13

Historique du materiel a duree de vie limitee Life Limited Material History Record

Numero du dessin ST3582-01 - Drawing Number ST3582-01

P&WC JR3-6834·E [66341 (2004-02)

Designation du materiel Material Name

DISC-COMPRESSOR N° du materiel N° de sene du materiel Material No. Material Serial No.

3011713 AOO23XCK

Donnees sur Ie moteur / module - Engine / Module Data

Temps de Temps de fonctionnement fonctionnement

depuis N° de serie du depuis I'installation du moteur I module Modele I'enlewement

materiel du materiel E~ine/Module En~ne / Module Model En~ / Module

SNWhen erial No. T N When Material Material Installed Removed

0 PCE-RB0334 PT6A-34 0

Pratt & Whitney Canada c Uoe societe de United Technologi&SJA United Technologies Company

Pratt & Whitney Canada Cie .1 Pratt & Whitney Canada Corp. 1000, Marie.victorin Longueuil, Quebec Canada J4G 1 A 1

Nota; Pour connaitre les durees de vie Code de traitement thermique !Omis Ie (A-M-J ~ accumulee et residuelle du materiel , Heat Cooe Issue Dale (Y- ·0) consulter Ie Manuel d'entretien du

KAWAD 2006.12.13 meteur ou Ie Bulletin de service approprie, selon Ie cas.

N° de sene du marL forge Temps depuis Cycles depuis Forging Mat'l. Serial No. neuf neuf Note: For determination of accumulated

Time Since New Cycles Since New and remainin~jVeS on this material, refer

0 0 to the en~ine aintenance Manual or Service ulletin, as applicable.

Donnees sur Ie materiel - Material Data

Cumul. de cette installation Cumul. jus~u'a present Observations

(Installation d'entretien , de revision, Bulletin Accumulated This Instal lation Total Accumu ated To Date Date de vente et timbre du verificateur)

/¢-M-J\ -M-D Remarks

(Maintenance/Overhaul, Facility, Sales Temps - Time Cycles Temps - Time Cycles Order & inspection stamp)

Inserer Ie present historique dans Ie livre du moteur ou du module aU la piece est installee. - This record must be kept with the engine/module logbook where this part is installed.

Historique du materiel a duree de vie limitee Life Limited Material History Record

Numero du dessin ST3582-01 - Drawing Number ST3582-01

P&WC JR3-6834·E (6834] (2004-()2)

Designation du materiel Material Name

HUB-COMPRESSOR,REAR N° du materiel N° de serie du materiel Material No. Material Serial No.

3013111 RWA56A145

Donnees sur Ie moteur I module - Engine I Module Data

Temps de fonctionnement

Temps de fonctionnement

depuis N° de serie du depuis !'installation du moteur I module Modele I'enlevement

materiel du materiel E~ine{ModUle En~ne I Module Model En~ I Module

SNWhen erial No. T N When Material Material Installed Removed

0 PCE-RB0334 PT6A-34 0

Pratt & Whitney Canada c Une societe de United Technologies/A United Technologies Company

Pratt & Whitney can,,"_2e.1 Pratt & Whitney Canada Corp. 1000, Marie·Victorin Longueuit, Quebec Canada J4G 1A1

Nota ; Pour connaitre Jes dUrE~~es de vie Code de traitement thermique I !'.mis Ie (A-M-J ~ accumulee et residueHe du materiel , Heat Code Issue Date (Y- -0) consulter Ie Manuel d'entretien du

KAWBX 2006.12.13 meteur ou Ie Bulletin de service approprie, selon Ie cas.

N° de sene du mat'l. forge Temps depuis Cycles depuis Forging Mat'l. Serial No. neuf neuf Note: For determination of accumulated

Time Since New Cycles Since New and remainin~ives on this material, refer

0 0 to the eneine aintenance Manual or Service ulletin, as applicable.

Donnees sur Ie materiel - Material Data

Observations Cumu!. de cette installation Cumu1. jusqu 'a present (Installation d'entretien, de revision, Bulletin

Accumulated This Installation Total Accumulated To Date Date de vente et timbre du verificateur) !¢-M-J\

-M-O Remarks (Maintenance/Overhaul, Facility, Sales

Temps - Time Cycles Temps - Time Cycles Order & inspection stamp)

Inserer Ie present historique dans Ie livre du moteur ou du module ou la piece est installee. - This record must be kept with the engine/module logbook where this part is installed.

Historique du materiel a duree de vie limitee Life Limited Material History Record

Numero du dessin ST3582-01 - Drawing Number ST3582-01

P&WC JR3-6834·E [6834] (2004-02)

Designation du materiel Material Name

IMPELLER - CENTRIFUGAL N° du materiel N° de serie du materiel Material No. Material Serial No.

3013176 EAAAOOOC029

Donnees sur Ie moteur I module· Engine I Mcx:lule Data

Temps de fonctionnement

Temps de fonctionnement

depuis N° de serie du depuis I'installation du moteur I module Modele I'enh~vement

materiel du materiel E~ine'Module En~ne I Module Model En~ 1 Module

SN When erial No. T N When Material Material Installed Removed

0 PCE-RB0334 PT6A-34 0

Pratt & Whitney Canada Url9 societe de United Technologle, fA United Technologies Company

Pratt & Whitney Canav. )e.1 Pratt & Whitney Canada Corp. 1000, MarieNictorin Longueuil, Quebec Canada J4G lA 1

Nota: Pour connaitre les dunres de vie Code de traitement thermique ~mis Ie (A-M-J ~ accumulee et residuelle du materiel , Heat Gode Issue Date (Y- -0) consulter Ie Manuel d'entretien du

PZBSB 2006.12.13 moteur au Ie Bulletin de service approprie , selon Ie cas.

N° de serie du man forge Temps depuis Cycles depuis Forging Mat'l. Serial No. neuf neuf Note: For determination of accumulated

Time Since New Cycles Since New and remainin~ives on this material, refer 061 0 0 to the en~ine aintenance Manual or

Service ulletin, as applicable. Donnees sur Ie materiel - Material Data

Cumul. de cette installation Cumul. jus~u'a present Observations

(Installation d'entretien, de revision, Bulletin Accumulated This Installation Total Accumu ated To Date Date de vente et timbre du verificateur)

~-M-J\ -M-D Remarks (MaintenanceJOverhaul , Facility, Sales

Temps - Time Cycles Temps - Time Cycles Order & inspection stamp)

Inserer Ie present historique dans Ie livre du moteur ou du module au la piece est instaliee. - This record must be kept with the engine/module logbook where this part is installed.

Historique du materiel a duree de vie limitee Life Limited Material History Record

Numero du dessin ST3582-01 - Drawing Number ST3582-01

P&WC JR3--6834-E [6834] (2004-02)

Designation du materiel Material Name

DISC-TURBINE N° du materiel N° de serie du materiel Material No. Material Serial No.

3013411 A0024342

Donnees sur Ie meteur I module - Engine I Module Data

Temps de Temps de fonctionnement fonctionnement

depuis N° de serie du depuis l'installation du mateur I module Modele I'enlevement

materiel du materiel E~ine/Module En~ne I Module Model En~1 Module

SNWhen erial No. T N When Material Material Installed Removed

0 PCE·RB0334 PT6A-34 0

Pratt & Whitney Canada c Une societe de UnitedTechnologies /A United Technologies Company

Pratt & WI1itney CanaOd de. I Pratt & Whitney Canada Corp. 1000, Marie·Victorin LongueUiJI Quebec Canada 4G 1A1

Nota : Pour connaitre les durees de vie Code de trailement thermique I Emis Ie (A-M-J~ accumulee et residuelle du materiel, Heat Code Issue Date (Y- -0) consulter Ie Manuel d'entretien du

PZBTM 2006.12.13 moteur ou Ie Bulletin de service approprie, selon Ie cas.

N° de serle du mat'!. forge Temps depuis Cycles depuis Forging Mat'1. Serial No. neuf neuf Note: For determination of accumulated

Time Since New Cycles Since New and remainin~ives on this material, refer 164 0 0 to the en~ine aintenance Manual or

Service ulletin, as applicable. Donnees sur Ie materiel - Material Data

Observations Cumu!. de cette installation Cumu!. jus~u'a present (Installation d'entretien, de revision, Bulletin

Accumulated This Installation Total Accumu ated To Date Date de vente et timbre du verificateur) !¢-M-J\

-M-D Remarks (MaintenanceJOverhaul, Facility, Sales

Temps - Time Cycles Temps - Time Cycles Order & inspection stamp)

Inserer Ie present historique dans Ie livre du mateur au du module au la piece est installee. - This record must be kept with the engine/module logbook where this part is installed.

Historique du materiel a duree de vie limitee Life Limited Material History Record

Numero du dessin ST3582-01 - Drawing Number ST3582-01

P&WC JR3-6834·E [6834] (2004..(12)

Designation du materiel Material Name

DISC-COMPRESSOR N° du materiel N° de serie du materiel Material No. Material Serial No.

3013712 AOO23W07

Donnees sur Ie moteur I module - Engine I Module Data

Temps de Temps de fonctionnement fonctionnement

depuis N° de serie du depuis l'instaUation du moteur I module Modele I'enlevement

materiel du materiel E1line/Module En~ne I Module Model En~ 1 Module

SNWhen erial No. T N When Material Material Installed Removed

0 PCE-RB0334 PT6A-34 0

Pratt & Whitney Canada c Une $oci9tt de United Technologies /A United Technologies Company

Pratt & Whitney Cana"O 2 e. I Pratt & Whitney Canada Corp. 1000, Marie-Victorin Longueuil

l Quebec

Canada J4G 1A1

Nota : Pour connaitre les durees de vie Gode de traitement thermique Emis Ie (A-M-J~ accumulee et residuelle du materiel . Heat Code Issue Date (Y- -D) consulter Ie Manuel d'entretien du

KAWAD 2006.12.13 moteur ou Ie Bulletin de service approprie, selon Ie cas.

N° de serie du mat'!. forge Temps depuis Cycles depuis Forging Mat'l . Serial No. neuf neuf Note: For determination of accumulated

Time Since New Cycles Since New and remaininflJives on this material, refer

0 0 to the en~ine aintenance Manual or Service ulletin, as applicable.

Donnees sur Ie materiel - Material Data

Cumu!. de cette installation Cumu!. jus~u'a present Observations

(Installation d'entretien, de revision, Bulletin Accumulated This Installation Total Accumu ated To Date Date de vente et timbre du verificateur)

/¢-M-J\ -M-D Remarks

(Maintenance/Overhaul , Facillty, Sales Temps - Time Cycles Temps- Time Cycles Order & inspection stamp

Inserer Ie present historique dans Ie livre du moteur ou du module ou la piece est instaUee. - This record must be kept with the engine/module logbook where this part is installed.

Historique du materiel it duree de vie limitee Life Limited Material History Record

Numero du dessin ST3582-01 - Drawing Number ST3582-01

P&WC JR3-6834-E {6834J (2004"()2)

Designation du materiel Material Name

DISC-TURBINE N° du materiel N° de serie du materiel Material No. Material Serial No.

3026812 A00244CC

Donnees sur Ie rnoteur Il'1l<XIule - Engine / Module Data

Temps de Temps de fonctionnement fonctionnement

depuis N° de serle du depuis I'installation du moteur I module Modele I'enlevement

materiel du materiel E~ine1ModUle En~ne I Module Model En~ I Module

SNWhen erial No. T N When Material Material Installed Removed

0 PCE-RB0334 PT6A-34 0

Pratt & Whitney Canada Una socUlI' de United Technologies/A UniledTechnoiogies Company

Pratt & Whitney Canaad 2e.1 Pratt & Whitney Canada Corp. 1000, Marie·Victorin Longueuil , Quebec Canada J4G 1A1

Nota : Pour connaitre les dun~es de vie Gode de traitement thermique Emis Ie (A-M-J ~ accumulee et residuel1e du materiel, Heat Code Issue Date (Y- -D) consulter Ie Manuel d'entretien du

PZBXX 2006.12.13 moteur au Ie Bulletin de service approprie, selon Ie cas.

N° de serie du mat'1. forge Temps depuis Cycles depuis Forging Mal'!. Serial No. neuf neuf Note: For determination of accumulated

Time Since New Cycles Since New and remainin~ives on this material. refer 044 0 0 to the en~ine aintenance Manual or

Service ulletin, as applicable. Donnees sur Ie materiel - Material Data

Cumul. de cette installation Cumul. jUs~u'a present Observations

(Installation d'entretien, de revision , Bulletin Accumulated This Installation Total Accumu ated To Date Date de vente et timbre du verificateur)

/¢-M-J\ -M-D Remarks

(Maintenance/Overhaul, Facility) Sales Temps - Time Cydes Temps - Time Cycles Order & inspection stamp

Inserer Ie present historique dans Ie livre du moteur au du module ou la piece est installee. - This record must be kept with the engine/module logbook where this part is installed.

1. Approving N ... I Aviation 2. AUTHORIZED RELEA~._lERTIFICATE 3. Form Trucking Number: )-Authority/Country:

FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG F AAfUNITED STATES 73240

4. Organilatioll Name and Address: Internationa l Governor Services LLC 5. Work Order/Contract/Invoice Number:

([CiS-7290 W I 18TH PLACE BROOMFIELD CO US ( IGOR976N )

Wor k Order 1524913 / ....",.

6. Item: 7. 0clleription: 8. Part Number: 9. Eligibility;* to. Quantity: II. SeriaVBateh Number: 12. S tat us/Work:

I IIONEYWELI. FUEL CONTROL 3244809·8 N/A I C218 19 PP26680- 1 OVERI IALI LED.

13. ",emarks:

I Overhauled and rccalibrated fuc l control with reference to Honeywell ('MM 73-20-36 Rev 2 (5/08) and other data acccplable to the administrator TSO,O.O

A C()I1lI)lete record of the work is on file at this station under 15249 13 . International Governor Service ccniles that the work sp..'Cilied in Block 13 was carried out in accordance with EASA 145 and in respect to that work the aircra ft component is considered ready tor release to serv ice under EASA Acceptance Ceni ficate Number: 145.4575

14. Certifies the items identified ahove were manufactured in conformity to: 19. [!I 14 CFR 43.9 ",eturn to Service [!] Other regulation specified in Block 13

0 Approved dCllign data and arc in condition for safe operation. Certifies that unless otherwise specified in block 13, the work identified in block 12 and dClleribcd in Block 13 wn:; at:eomplishcd in accordance wiHl. Title 14, Code of Federal Regulations, part 43 and in respect to

0 Non -approved design data specified in Block 13. that work, the items are approved for return to service.

/"\ ~

15. Au,hodz,d Signa~ 16. Approval/Authorization No.: If A'd:~bI" 21. Approval/Certificate No.:

IGOR976N

~,p'inted)' 18. Date (MonIJ)O!""Y"): 22. Name (Typed or Printed): 23. Dale (MoniD O/Y""Y): CIIADQUEEN OCT/25/20 13

User/ Installer Responsibilities

It is important to understand that the clt istence orthis Document alone docs not automatically constitute authority 10 insLalithe part/component/assembly.

Where the user/installer working accordance with the national regulations of an Airworthiness Authority different than the Airworthiness Authority of the country sJX.'Cifil.'<i in block 1 it is essential that the user/installer ensures that his/her I\ irwOlthiness Authority accepts p<lns/componentslassembl ics from the Airworthiness Authority of the COWltry specilied in block 1.

Statements in block 14 and 19 do not constitute installation certi fi cation . In all cases aircraft maintenance records must conwin an installation certification issued in accordance with the national regulations by the user/insta ller before the aircrall may be Ilawn .

FAA FomlS 130·3 (6-0 1) ·Installer mus t cross check eligibi lity w ith applicable tt.'Chnical data NSN:0052·00·012·9005

OIL REPORT

MAKEIMODEL. Pratt & Whitney PT6A-34 FUEL TYPE· Jet A ADDITIONAL INFO Confldenlia!. Screen

CHUCK ARMSTRONG XP SERVICES 105 NWTAXIWAY LANE TULLAHOMA TN 37388

LAB NUMBER: GO!50~1

REPORT DATE; 4i21 ,'2014

CODE: 63/75

UNIT 10: N382SB-FR

CLIENT 10: 72386

PAYMENT: CC Visa

OIL T iPE & GRADE BP 2380 OIL USE 'NTERVAL 25 Hours

PHONE 19~1 260-8645 FAX. ALl PHONE EMAIL ~'uck armstrong@xpse-rvlces us

CHUCK/DON· No problems to report here. Metals are nice ana low and the 011 was phYSically in good shape. There was 1 ppm of silver but we're not ready to call that a problem at thrs porn! This orl should be fine for continued use.

• THIS COLUMN APPLIES ONLY TO THE CURRENT SAMPLE

416 E. PETTIT AVE. FORT WAYNE, IN 46806 (260) 744-2380 www.blackstone-Iabs.com ClCOPYRIGHT BLACKSTONE lABORATOR!E$ 2012 LIABtUH l.MITED TO COST OF ANALYSIS

Gear Box FUEL TYPE

OIL REPORT

ADDITIONAL INFO COnflden".' P,ep

~======== CHUCK ilR',1 Q TRO ,c XF SERVICES 105 NW TAXIW!\Y LANe

TULLAHOMA N 37388

LAB NUMBER: G07556

REPORT DATE: ,121/2014

UNIT 10: N382SB-GB

CLIENT 10: 72386

PAYMENT. CC, V,sa CODE: S3'i5

'IL TYPE & GRADE OIL JSE INTERVAl

PHCN~ C' r ... r.864:

FAA ALT FHUNE

BP ,380 Hou~!>

!:M.AiL Ch,:':K armstro:rq\~xoser;.:ces.llS

~============~~-~~~========~ CHUCK/DON: Solids were kind of hlghn this sample showing some Qxidalloo of Ihe 01, But other than that, metals were low If you haven't changed this 0:1 yet, it wouldn't be a bad Idea 10 do so,

I ,

, i

• THIS COLUMN APPLIES ONLY TO THE CURRENT SAMPLE

41 6 E. PETTIT AVE. FORT WAYNE, IN 46806 (260) 744-2380 www.blackstone-Iabs.com

@COPYRIGHTBLACKSTONE LABORATORIES 2012 .IABI ... r"y LIMITED TO CCST OF ANA,- .... 5:S

9'19/2014 If'l NorkspaCB Nl;!omail

Manual References Braun. Jeff ).

'""'\ Sert 8/6/20141158 AM

To chuck.armstrong@xpservices.u>

Chuck, I neglecter!:o '1'llltion "Py k,nd of refe·e~ce 'T'3teriallast week when I sent this note recapping my visit.

I referenced the following procedures from the Pratt & Whitney Milintenance Manual 3021242 rev 52, dated 27 January 2014; 1) Part Power Trim Check Sec 71.00.00 paragraph 11, sub seclior A (Titled "Fuel Control Unit Maximum Gas Generator Speed Setting") ?) Bleed Valve Closing c;ec 71 (10 00 rr~ri12r"ph 1 R sub section A (Titled "Bleed Valve Closing Check \Post S81683),,) 3) Idle Speed Adiusl"er' Se 711)00C l ',or'Dr 11 sub section C (Titled "Fuel Control Unit Idle Speed Adjustment' )

Also, with regards to the engine rigging ti~a~ I assis,ed you With we followed the procedures set forth from the instruction contained In the document NCSA Engine Control Rigging Procedures, Document # SER-38000033rev 1.

Regards, .JI ff ~\ ~~ ~-t ~ ~~ ~~ ~e\'IP'.o

~ J\AA -Ja{\. ~f\c.w..",- ~ St-~"",.o Q,,-t . .

" Jeffrey L Braun ~Chm .O~~< :s

PT6 Field Service StandardAero

lOS Sawyer Lalle Pickens. Soutn Carolina 29071 Un'ted Stales of Amenca

MOb" •. 864.517.8998 Jf).ff .oraUll@standardaero.c(·m IN .,>/"IJ .stanaarOocro. com

StandardAero A Do'? Comp,my

r}f 31 TIn

-::r:: Cl. 4-\ 5 9.. 2> t'S "'\ ~

~l~)JtoL.:i~-;lI; --=R

''The trusted service partner"

o

Ttl .. \~;Tla,1 ;11';j:.J.IL, (,11m nt!.'., ,., I,; jill 1:111: ::lf1d 1,1 eliOt J I, 1I C ,j~e cf !!1e IlldIViduc.I(S) to whom It is addressed. If you are not the intended Io:'upler.! bEl :::trly'se{1 thal t'll) '.,,-1" (t""r.BWE'd tl em. 'I. (fror elnff·hrl! all" l;"'~ dlS~tmllnatlon. forwarding, printing. or copying of this t:m,1.11 "., SIn! t!y' prurb Ie :r y'.:J ',lA' rceeil/e, !nh enliliin p-rro: "f€'~:.3e C ie::'le It ~ selloar and lher. delete It from your system Although thiS email and any attacnmen~s arc o€:loe'.'(;d:o be rrel:! oi any 1/1" ... .:;es C~ ,h .. , .::.!t;,eCiS Il Ci:1nnot be guaranteec to be secure and error free as It can be intercepted. amenoed. Ics~ r)r '-'BSTr!Jycd. Oub~1 Aerosr<l(,~ En~l~q'r,s(" (OAE) Ltd ar:d StandardAero accept no responsibility for any loss or damage arising in <:lily 'lAdy fr0m Its reGe:pl elr ,I"e.

From: Braun, Jeff Sent: Monday, August 04, 2014 ·':53 Pr-'I To: 'chuck.armstrong@xpservices.us'; 'John,humohrres@xpservices.us'

tIUp::,·, /tornall i 5.~ecurt;~E>(·/er .n~oJ WlllcJUWI pr InU?!· .r,lll ,U~n;;.;22034:)5~,3c.ul· 113

1+1 Transport Canada

Transports Canada

Engine Logbook

TP 14182E

1111 111 11 11 11111111111 11111111111111111 11111111 111

(Revised OS/2005)

Canada

Other related Transport Canada Publications: TP 14089B TP 140S8E/F

Previous Edition: TP 391OE, 2nd Edition (Jan. 1987) TP 14182E (Dec. 2003)

Printed in Canada.

Please direct your comments, orders and inquiries to:

Transport Canada Civil Aviation Communications Centre (AARC) Place de Ville, Tower C, Sth Floor 330 Sparks Street Ottawa, ON KIA ON8

Telephone: Fax: E-mail :

1 800 30S-20S9 613 957-4208 services@tc.gc.ca

© Her Majesty the Qu~en in Right of Canada , as represented by the Minister of Transport (200S).

® Permiss ion granted fo r internal use only :

This publication may be reproduced for internal use only without permiss ion, provided the source is full y acknowledged. However, multiple copy reproduction of this publication in whole or in part for purposes of resale or redi stribution requires prior written permission from the Minister of Public Works and Government Services, Ottawa, Ontario, Canada KIA OSS or at copyright.droitdauteur@communication.gc.ca.

TP 14182E (OS/2005) TC-1001l8S Catalogue No. TS2-4/2-2003E

Volume #: ~ Opened on: 1 3 DEC 2006

ENGINE DETAILS

1. Manufacturer __ Pratt & Whitney Canada Corp.

2. Type/Model/Series PT6A- 3 4 B/S: IDDe:;

3. Serial Number peE- RB 6)334

(i)

Section 1: Record of engine maintenance and elementary work

Date --/--/ - -

1 3 DEC 2005

Time since new

D·D

Time since overhaul

(9.0

Total cycles

o

Details of task

New engine final acceptance test and inhibiting run completed satisfactoril -and is in coridition for safe operation

l =

Date: 04119112 Engine SIN: PCE-RB0334

I Time since new: 0.0 I TSMOH: NIA I Total Engine Cycles: 0.0 MAINTINEANCE PERFORMED:

Removed all propeller reversing system parts listed in Table 1 of PWC IPC Chapter 76-10-00, FIG 1 and PWC maintenance manual chapter 76-10-00. Installed 2 new MS9320-12 washers on on prop reduction gearbox cover studs after removal of reverseing lever guide pin assy.

T~rqued all faste~!ff/~W PW~e::ce manual PIN 3011244 Chapter 76-10-00. SIgnature: ~~A.ff O~ William Ostrander Cert. No: 3278840

0 - 1 NIA \ ~ t\)OV 2D{.~ 0 ' 3

~---------+--------4-------~~------~--------------------------~~'~ TTSN 0.0

Serial #: PCE-RB0334

Model #: PT6A-34

N382SB

I certify that this engine has been inspected in

accordance with the Pratt and Whitney maintenance

manual Part # 3021242 and was deemed safe for flight.

~~~~~, Charles M. Armstrong Jr.

IA415981577

j~,.(' &0 .'!'\A. (>,~.o oA ° ~ ~~<,~ -=l3:~O -GO a.<:a 7. 0'E{ ~:I\.<.l '\i).I'). J)~ . ~ , ~m,O ~:~ ~('u "JJ..-. 1Me1.~t..n-,"j .k ..\o~""",,~~b ~"';~ L~ .. ~ "'R\~D -3 '

I

c~ AME

'1\ 'CP Signature ACA/AMO

! SCA/AMO -'"! ad . , . . ,

)ril\ I TRIMSPEEDNg 35517 ,% NgMAX: 14/1. on. .. G. J:j~~MANN 1 . /

- I -@ /Ill VI/' //l44/Vl/ G<e!;..J. T.C. 4·58 \,A!;." NO . 049

, ~ .f -----.~

.----------~ ~

/

I ~. I

-C J,~ I ,

I I

'j

I

I

I J ~Jt.. .

LC ,~ ....,./

'i} ) l

.

Sect ion 1: Record of engine maint enance and elementary w ork

Date -- /--/--

------

Time since new

Time since overhaul

Total cycles

--~ ------

Details of task

~~l\ltl1tc\ F.Miu S1u ttG ~60"?>1>LI Oe-f'­:Vet W M"'\N\ [d ~ro-oo ()1f\2_:~O;;l~t{l.

, rSl0FJ M~~3()"t{I~ ef~"~~ FM.iof\.f./ iiV Pf'tsC(u~Jif)1f\

J

~--~--~~--~----------~~

I

I

(

(

Engine Airworthiness Directives pwc 2371(2000-01)

Reference AD.'s

To ensure the early detection of reduction gearbox FAA A.D . deterioration and for improved blade containment. 75-06-01 S.B. 1138, 1216& 1220 or their later revision or

superseding S.B. incorporated at manufacture.

Sign

d'/tdt£t// G.HERMANN

For engine incorporating an unmodified power £~ / FAA A.D . turbine shaft housing assembly part number / I %iAf/ 75-11-04 3010548. Not applicable due to part number.

Modification incorporated at manufacture. G.HERMANN

Engine incorporates the inproved power turbine ~4zf(fol/~ CF-78-03 containment modification. S.B. 1217 & 1220 or their later revision or superseding S.B. incorporated at manufacture. G.HERMANN

CF-96-24 To preclude malfunction of the compressor bleed of vri£ywv /' FAA A.D . valve. S.B 1538 or its later revision or superseding _ 97-04-12 S.B .. incorporated at manufacture. G. iiERMANN

Pratt & Whitney Canada Corp_ 1000, Marie-Victorin Longueuil, Quebec Canada J4G 1 A 1

IEnginel ~/N PCE-RB0334

Lic. # Date

or Stamp

(!::) T.C. 4-58 "-,. 0NO.04g 1 3 DEC 2D95

(Jr) T.C. 4-58 "-'- NO . 049 o - 1 3 DEC 2006

~ T.C.4-58 1 3 DEC 2006 "-'- NO . 049 · (0) -

(!::) T.C. 4·58 "-,. NO. 049 o - 1 3 DEC 2006

l Page no 1

PRATT & WHITNEY CANADA

ENGINE BUILD RECORD STATUS

THE FOLLOWING SERVICE BULLETINS ARE BASIC TO

ENGINE SERIAL NO. PCE-RB0334

ENGINE MODEL PT6A-34

BUILD SPEC 1009

SERVICE BULLETINS

1103 1129 1148 1165 1167 1168 1169 1170 1173 1176 1178 1179 1183 1185 1190 1191 1192 1194 1200 1201 1202 1203 1207 1211 1212 1215 1216 1217 1219 1220 1223 1224 1225 1226 1227 .1228 1229 1231 1232 1236 1242 1247 1248 1249 1251 1254 1255 1259 1261 1263 1270 1275 1276 1277 1280 1281 1288 1293 1300 1310 1316 1318 1320 1321 1322 1326 1327 1331 1332 1334 1336 1338 1339 1352 1354 1357 1358 1361 1367 1370 1372 1374 1379 1381 1388 1389 1390 1391 1393 1394 1395 1397 1404 1409 1410 1416 1418 1427 1428 1430 1434 1439 1441 1446 1457 1459 1470 1473

( 1474 1490* 1493* 1498 1500 1503 1508 1513 1518 1519 1520 1524 1527 1528 1534 1537 1540 1544 1545 1553 1554 1556 1560 1562 1564 1567 1570 1572 1591 1598 1613 1614 1621 1627 1630 1637 1638 1647 1650 1651 1652 1654 1655

* DENOTES PARTIAL INCORPORATION OF SERVICE BULLETIN SB# PARTS INTRODUCED AT ENGINE BUILD. 1490 3039939 3116033-01 1493 3117225-01 3117228-01 3117230-02 3117233-01

APPROVED BY DATE 2006.12.13