AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and...

34
. ' 1 ..&..1 Transport Transports ....,... Canada Canada Aviation Aviation Second Edition January 1987 Canada AIRCRAFT TECHNICAL LOGS Section 3. ENGINE Oc.- E P..:s o 2.'\'-\ TP3910E

Transcript of AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and...

Page 1: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

. '

1..&..1 Transport Transports ....,... Canada Canada

Aviation Aviation

Second Edition

January 1987

Canada

AIRCRAFT TECHNICAL

LOGS

Section 3. ENGINE

Oc.-E P..:so 2.'\'-\ TP3910E

Page 2: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

------ ------ ·------

MAKE PRATT & WHITNEY CANADA INC.

MODEL PT6A-42

SPECIFICATION 787 (E.T.C.E.-12)

SERIAL NO. PC-EPJ0244

DATE OF MANUFACTURE _,O~C..:..T:...;O~B""'E,..R,.,._.l""-99"'-'8><---------'.

. ' . i,

Page 3: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

,I i! 'i

ENGINE SERVICE AND

TIME RUN TIME SINCE OVERHAUL INSTALLATIONS, INSPECTIONS,

DATE

HRS. MIN. ~: USE BOTI-I PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETF~

HRS. MIN.

BROUGHT FORWARD -:r;;'/o.tt..,._c..f;,~ 8fl.()c.Hi'h ( ~I(""""' -ttt.d r-io"-

227'1. z t':J '•bliwH .,..~:>n·~ ----------1-----1---- ~~~':;'~.;.~\~~~~~~~~'~._ .. i~:.t;~·

---------+----+---- o ;>,.,.,...,,n,,..,...,,~"ll·JflhiS"mal.c.,-;:•ne1younLipcrt'o,_.runrmotiNXCOII'IIIhtb..-d.so <IIWPfl>"'Oc"""nD.:IIof.&_.,l,;calll.:n:lk:tilrli>fiiiC'<Iopcn!Or lfdl.ol9""nd pcrTilftN.IIc:e,.,....,s~lhrl<:ftljiM""'Ilberou«:cctoollrreoltn!JF.Io;!h!'.lll

::.;~::: ;,:·;:;:,;;;m.:,~.~;;";!;'!;;;''eu\:!·;;::..,~~ .. ~ ·"GrouoGI'~RIIIIRc;lort'

o lrtsww.tb.K:di.K<:__.ton.,.n:aama~;~Ribcooell!li:M-=n:rcc~:t~rdwotll~:a!JIIIC Anv !l.iKrtD'9' K£r19ftP .,...u be "'!'bi:cd >M 11! S"" wdl ht t!tr '""""'""'''''! ~( rht !!C:JMUII!l! "f!t""'M Jill ff1!1UI tf !hd f!IIIM. nu.~o:~oe~.-~~t.-.trortbc~lo¢ookerotno:~

:"f.l.nealtda4dl'ftlo(Openlor: Q~,v~"rf':J. 6 ~4 ---------+----+---- ?:':~:~~ ~::--.,~ ~~~-;:~-:.._

---------+----+---- Reata&EIIJIIM~odd:..<.?::;,•...:_•''-"''"--- SHIM:'f••bo!r: i'Jg;_'-•"'

O"D'i!!l A!!!Q atd Cufa: .u RagonJ·

---------+----+---- TISN:~ TCSN:_-_ nso·~ TCSO:~

U UNSIRVICABLE ---------+----+---- ~ SERVICABLE ~Dtfecuw~C-'&

" "-'

--------1------t--- ...,."Z'L tWf'

.

,•' ? .

~~o-~~'§:~. ~~~-,~~~:~~~::~·~-~:~.'~-~~-~--~'~-~~,,~"~~-:~.~--~·'~======= ~~C.'~~,,~04~!~~:~~~~-~~~l~~.~:·~-~--~~~~·~0~::~'::~::~%_,,~·--~'·========

~~~IAWMHI. ... --ACFT1T 40'fO.S ACI'TTC !lo?l.

.

----------------,_------t-----~~-----L------~--C-A_R __ R_I_E_O __ F_O_R_w __ A_R_o ____________________________________________ ~

TOTAL THIS PAGE

TOTAL FROM PREVIOUS SUMMARY

TOTAL SINCE MFG.

Page 4: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

----M A I N T E N A N ~ E .R E C 0 R D

REPAIRS, ADJUSTMENTS, MODIFICATIONS

ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS. SIGNATURE

-----------··- -

Pratt & Whitney Engine Services, Inc. 1525 Midway Park Road Pratt & Whitney Bridgeport, WV 26330 Certificate Number LM1R301K

A United Technologies Company

Manufacturer Description Modelffype Serial Nwnber

PRATT & WHITNEY GAS GENERATOR PT6A-42 PC-EPJ0244 MODULE

Time Since New Cycles Since New Time Since Overhaul Cycles Since Overhaul

2274.2 2025 ---- -----0 Overhaul lXI Repair C.T. Vane Class: N/D P.T. Vane Class: 19.36

DESCRIPTION OF WORK ACCOMPLISHED AND REFERENCE DOCUMENTATION: PBRFORMED A H.S.J. AND PERIODIC MAINTENANCE INSPECTION I/NW PRATT & WHITNEY PT6A-42 MAINTENANCE MANUAL PARTN0.3021442 REV.35 SECT. 72-00-00 TABLE 60l,AND OTHER P&WC APPROVED DOCUMENTATION,AND/OR ENGINEERING DOCUMENTATION ACCEPTABLE TO THE ADMINISTRATOR. INSTALLED NEW FUEL FILTER P/N:3070220-01. INSTALLED NEW OIL FILTER P/N:302S419. 118LMZ •••• MCDIWUO IdiltD. GAS GENERATOR MATED WITH SERVICEABLE POWER SECTION SIN: PJ0244-100 AND TEST RUN IJNW PRATT & WHITNEY PT6A-42 OVERHAUL MANUAL PARTN0.3021443 REV.34. INSTALLED OVERHAULED PROPELLER GOVERNOR PIN: 8210-024H S/N:2252058 AND IGNffiON EXCITER P/N:I0-381550-4C S/N:98254081 AT ENGINE PACKING.ENGINE IS APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF A DOCUMENTED SATISFACTORY LEAK CHECK,CONTROL SETIINGS,AND GROUND PERFORMANCE RUN. LT.T._!Y:LF ~C TRIMHARNESSRESISTANCE 22.4 OHMS.

This gas generator bas been repaired and inspected in accordance with current regulations of the Federal A via · and is approved for return to service. Pertinent details of the work performed are on file at this liBPd):)j~U~Mir'~/ work order No. 49821 13 Date 24-Aug-04 Approved lns]pec1tor)i~~~~~--=-=--=-=~~~~

l>UT\T. "l~ IU 4 V Oil\

MAXIMUM HOURS BETWEEN OVERHAULS _______ HOURS.

LICENCE NUMBER

...-

1

-+-------

Page 5: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

·' 1. Approving National Aviation 2. 3. Form Tracking Number: .) Authority/Country:

F AAIUNITED STATES AUTHORIZED RELEASE CERTIFICATE 4982113

FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG 4. Organization Name and Address: PRATT & WHITNEY ENGINE SERVICES, INC. 5. Work Order/ContracUinvoice

1525 MIDWAY PARK RD Number: BRIGEPORT, WV 26330 CERTIFICATE NO: LM1R301K 49821 13

6. Item: 7. Description: 8. Part Number: 9. Eligibility: * 10. Quantity: 11. Serial/Batch Number: 12. Status/Work:

ONE GAS GENERA TOR 3017690 PT6A-42 ONE PC-EPJ0244 REPAIR MODULE

13. Remarks: TTSN: 2274.2 TCSN: 2025 TTSO: ---- TCSO:---The gas generator identified hereon was inspected and repaired in accordance with Pratt & Whitney, Maintenance Manual PIN 3021442 Rev.35, Overhaul Manual PIN 3021443 Rev.34, other P&WC approved documentation, and /or Engineering documentation acceptable to the Administrator. Pertinent details of the work performed are on file at this repair station under the above work order number. Engine test certificate, life limited parts log, modification log, log of major parts replaced, and Engine check list are attached to the logbook. Certifies that the work Sl!ecified in block 12/13 was carried out in accordance with JAR 145 and with respect to that work the aircraft engine is considered read~ for release to service.

14. Certifies the items identified above were manufactured in conformity to: 19. [g) 14 CFR43.9 Return to Service D Other regulation specified in Block 13

D Approved design data and are in a condition for safe operation. Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with Title 14, Code of

D Non-approved design data specified in Block 13. Federal Regulations, part 43 and in respect to that work, the items are approved for return to service.

15. Authorized Signature: 16. ApprovaVAuthorization No.:

':QI~~ 21. ApprovaVCertificate No.:

LM1R301K

17. Name (Typed or Printed): 18. Date (rnld/y): 22. Name ('ryped or Printed): 23. Date (rnld/y):

R.L.FIGLIOLI QA COORDINATOR 24 August, 2004

U ser!lnstaller Responsibilities

It is important to understand that the existence of this document alone does not automatically constitute authority to install the parUcomponenUassembly.

Where the user/installer performs work in accordance with the national regulations of an airworthiness auttWrity different than the airworthiness authority of the country specified in Block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified in Block 1.

' Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user/installer before the aircraft may be flown.

FAA Form 8\30-3 (6-01) *Installer must cross-check eligibility with applicable technical data. NSN: 0052-00-012-9005

Page 6: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

PRATT & WHITNEY ENGINE SERVCIES,INC

PT6 ENGINE (LARGE) TEST CERTIFICATE

WORK ORDER NUMBER ENGINE MODEL REASON FOR REMOVAL

49821 13 PT6A-42 H.S.I./P.M.I.

GAS GENERATOR SERIAL NUMBER PC-E PJ0244

POWER SECTION SERIAL NUMBER PJ0244-100

C.T. VANE CLASS: N/D P.T. VANE CLASS: 19.36

CORRECTED PERFORMANCE

RATING SHP/DELRTH NG/RTH TtS/TH S.F.C.

850 35350 1681 .610 TAKE OFF

DATA PLATE SPEED = 35350 NG @ 850 S.H.P.

Ps3 PRESSURE RATIO 7.56 @ 35000 Ng/RTH

I.T.T. TRIM 46.6 o F. 83.8 0 c.

TRIM HARNESS RESISTANCE 22.4 ohms

THIS ENGINE HAS BEEN TESTED IN ACCORDANCE WITH THE MANUFACTURER'S RECOMMENDATIONS AND REQUIREMENTS.

DATE 24-Aug-04 ~~<d-AB

APPROVED INSPECTOR: .L. FIGLIOLI, Q.A~RDINATOR

PWV-3017 (JAN 98)

Page 7: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

PRATT & WHITNEY ENGINE SERVICES,INC. LOG OF MAJOR PARTS REPLACED

WORK ORDER NUMBER ENGINE MODEL SERIAL NUMBER

49821 13 PTGA-42 PC-E PJ0244

QTY PART NUMBER DESCRIPTION QTY PART NUMBER DESCRIPTION

NEW PARTS NEW PARTS

1 3028419 OIL FILTER ELEMENT

2 3032096 IGNITER PLUGS

1 3033492 FUEL NOZZLE ASSY.

2 3119919-01 FUEL NOZZLE SHEATHS

THE ABOVE LIST OF MAJOR ENGINE PARTS REPLACED DURING THIS SHOP VISIT IS ONLY A SUMMARY AND IS LISTED AS AN AID TO IDENTIFY PARTS REPLACED.FOR A COMPLETE LIST OF PARTS REPLACED AND ACTUAL PART NUMBERS INSTALLED, PLEASE REFER TO THE WORK ORDER ON FILE AT PRATT & WHITNEY ENGINE SERVICES INC.

1\

DATE 24-Aug-04 APPROVED INSPECTOR: ~~ ~;;;£ \___ ~';~\

L. FIGLIOLI, Q.A.~~INATOR PWV-3039 (MAR 00)

Page 8: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

PRATT & WHITNEY ENGINE SERVICES,INC.

PT6 ENGINE SHIPPING CHECK LIST

nnnThlV WORK ORDER NO. 49821 13 I ENGINE MODEL NO. PT6A-42

CUSTOMER PWC LEASING

POWER SECTION SERIAL NO. PJ0244-100

DESCRIPTION PART NO. SERIAL NO. TIME REMARKS

1 PROPELLER GOVERNOR 8210-024H 2252058 TSO -0-

2 TORQUE LIMITER 3244707-7 C12473 TSN 2274.2

3 TACH GENERATOR N/A

4 OVERSPEED GOVERNOR N/A

POWER .SECTION LOGBOOK QUANTITY: ONE COLOR: YELLOW TYPE: CANADIAN

GAS GENERATOR SERIAL NO. PC-E PJ0244

ITEM DESCRIPTION PART NO. SERIAL NO. TIME REMARKS

5 THERMO. BYPASS 3024996 TSN 2274.2

6 FUEL PUMP 399701-5 4307A TSN 2274.2

7 FUEL CONTROL 3244768-13 B12685 TSO 909.5

8 OIL/FUEL HEATER 10585J WA11440 TSN 2274.2

9 SOLENOID VA_LVE - N/A

10 IGNITION EXCITER 10-381550-4C 98254081 TSO -0-

11 COMP. BLEED VALVE 3123122-01 30A941 TSN 2274.2

12 COMP. BLEED VALVE 312323-01 30A835 TSN 2274.2

13 FLOW DIVIDER 26035-1 3199 TSN 2161.2

s GENERATOR LOGBOOK QUANTITY: ONE COLOR: YELLOW TYPE: CANADIAN

N/A - Not Applicable N/R - Not Received S/L - Ship Less

DATE 24 -Aug-04 ~1- ::J· - (~':.')

APPROVED INSPECTOR: :~t. FIGLIOLI, Q.~RDINATOR PWV-3056F (JAN 98)

Page 9: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

'--....--

'-----'

0 Pratt & Whitney Canad~ Una aoc11ilhi da Unned Tachnolo!Jias/ A lkutsd Tachnolog•• Cc 11p11nf

P&WCL

Pratt & Whitney Canada Leasing , Lirnjte9 Pa.-tn~ip 7007 de Ia Savanne Quebec ,Canada J3Y-3X7

PRE-REMOVAL GROUND PERFORMANCE RUN REPORT

ENGINE SIN X?c_~. I B;:Jo;L.~~

TSN/TSO /.::z <-/~~~ CSN /CSO I~ 108'

TFSN/TFSO TSSN/TSSO I RTO (Rapid Take Off) Scoop# 2 Yz Min Excursion OAT

/10 FIELDBARO. PRESS. ALT

.:29, 7.2. Oil Type I Brand Name TSN @ Last Oil Service RefSB's 1001, 3001,4001, 5001,

11001 , 13001, 14001 or Maintenance Manual 72-00-00

TARGET OBSERVED

NP .::ZOZ>D ~--------+TQ. 794o

NP TQ

~ 19(;.'0

. '---'

NG I Nl I NH CJ.t/,4 7., NGINl INH =]3% T5 I ITT I MGT_...::t..4..:::..~.::::..5'_-__ _ T5 I ITT I MGT tco/o WF G;o tl3s WF SDSO: N21NL N21NL OIL PRESS. //6 -130 i.J!>S OIL PRESS. --L...!/1...,.~~...----

CHIP DETECTORS Ol< OIL FIL TER(S) OK

REMARKS:

CERTWYINGSTATEMENT

This engine was tested and inspected in accordance with the applicable Maintenance Manual and Rental Agreement and found in a serviceable condition .

SIGNATURE ~~~=-q ~?A:: DATE

LICENSE OR STAMP fnr-YtJ~!£../2.87 J 3 COUNTRY

o;p~/o~ I I

c.J~)/i

Page 10: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

. ' ~

-----

0 ~ra~- ~ !lhit~~Y_ c~ii~-ila Pratt & WbitDey Cauada J...asing, ~ 7007 de Ia Sa~ " Quebec ,Cauada

JJY-3X7

P&WCL

POST INSTALLATION GROUND PERFORMANCE RUN REPORT

ENGINE SIN PC!£ P<T D::<.Ljq

TSN/TSO CSN/CSO / .9??q4, .::<. I ao:2.S

TFSNfl'FSO TSSN/TSSO

RTO (Rapid Take Oft) Scoop# 2 ~ Min Excursion OAT

13° FIELDBARO. PRESS. ALT

~'7.35 Oil Type I Brand Name TSN @ Last Oil Service RefSB's 1001, 3001,4001, 5001,

11001, 1300 1 , 1400 1 or

TARGET

NP .;l.OOO ·to--- · -- 197D

NG/Nl/NH %~ T5 /ill /MGT 7f0 6

WF St7 L6'S

N2/NL OIL PRESS. liD-- I@

REMARKS:

Maintenance Manual 72-()()..()()

OBSERVED

NP ;;;Lc;~ TQ-- -- ------ ---z97o· NG/Nl /NH 94,2"/o T5!m /MGT 47D WF N2/NL OILPRESS. _ CHIP DETECTORS OIL FILTER(S)

6/o L.BS'

L/5:_ D~

D~

CERTIFYING STATEMENT

This engine was tested and inspected in accordance with the applicable Maintenance Manual and Rental Agreement and found in a serviceable condition.

siGNATURE ~~. <?S28,a=zz.r:nATE 01 /.:2~/o/1 LICENSE OR ST .MfP COUNTRY USI1_

Page 11: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

ENGIN~.S~RVICE AND

-TIME RUN

TIME SINCE OVERHAUL INSTALLATIONS, INSPECTIONS,

DATE !i2,ll: USE BOTH PAGES AND AS MANY L.INES AS REQUIRED FOR COMPL.ETE

·~ HRS. MIN. HRS. MIN.

BROUGHT • FORWARD

-/4/ib&b f'"f i~t -;-;; -1. 11.. I £Kg ;..,J I!NI 1'$L-/::Z:l. :It: I Y-14 ~ CUQn /L ~lOY 111. - ' ,i':v witt.. '2E!.P:s ..._.. ... · ~J ~-..~a ... ~, eD ~j

mJ~ JU"- Y"uH. !J-ak dJ.!/!J. AIAA ,..,,.A' ..I?.. IAII!U~r~o" rtJM.

\.} BL· ·JZ2'3 AL7 7 "/~if.:JY!q .;r~c rL 9 i:J-9

/,;:51)~05 1-rT= l..2~7sZ ~ Rt»JI\lJL.n J:!vk.1AJ.?. & J PtJSrrJtJhl 1<6- Jz,z...-

-rc: 1~. l2:l~7 AGTT: ID '?nl. ~ Act' t,: q 'l '1~

lu 5,t..o'>_. 1-rr ·~t- 1 xt. J/1/SJAIL-A.J ~,.1;[.:...,,_,h{_ 1J.. I A=':) lrc..v ,1f- of, 'I ~.v<lr:..-•i. I

Ire. . r-

IAv7 r.• J J J,t7J. 1 /l,_.., i.. q 5ro-; / "bU7 tJ'II A t c, q1t .I"'""-~

.4 ... ? ,~/t,{ ~~·'\,;'1/)J...('.-t /}. wt.l 11tt t:,; I { .:..JU:./) I J

.

II eel a;- rr ~~-~ (<.11_.-.(.1,/.:;, £,.,t.--,~-t. a, ,4:; s,r;c .. .-~ xJJ o ,~ - 11 L- 12 )3 5"' Ad-r !Jilt,.> .1 /)'-I L. '1' ~10

oo_ 0--.

~

'-

. CARRIED FORWARD -

,~ __

TOTAL THIS PAGE

TOTAL FROM PREVIOUS SUI\Mo.AP'

Page 12: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

MAINTENANCE RECORD -~-~ 2

I REPAIRS, ADJUSTMENTS, MODIFICATIONS LICENCE

~ENTRIES. ORAW A OIAGONAI.. I..INE THROUGH ANY UNUSEO I..INES IN OATE AND TIME COI..UMNS, SIGNATURE NUMBER

' -.

~ 1,#/t/( ~0 &uJ~t~ Jl(,th..I/,._L ~ n~"" """ AJ --- A riSk w li.:J...~.~ .. ._t:l. IMAM./~~ &cd IJr~ r/JqJ./. MI:Ail.IJ.

~. _"'p_ ... J' . I -01

~ l~r~~g JU-id. &,u..:,.L. 1Jvllfr11Lhl w:41.. cit.. I."'· ~ ts.hJ. v I U.. /x"L - .1.

-:nTIIJ&,£ -, r.. , ,

rv;(~ JtHP .....

{/

~d ~ITP. J.~YeJ L.,[r,~, /~"/l_,u.,r~-..- ~«~iJ ,:f,.sSI;.,.:.... Aco ..... /l,s./"'-i•:?

~ 4 ~ t#rN]..-:1 .A.ur . .C (;,:,? l11A C4..,E_.;,~ f.v?- .~ ..... C.44f( (;..I( /)w,1

~

... . t- ......

-

.

-

MAXIMUM HOURS BETWEEN OVERHAULS _______ HOURS.

Page 13: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

Pratt & Whitney Canada Leasing, Limited Partnership 7007 de Ia Savanne " Quebec ,Canada J3Y-3X7

P&WCL ..#I

POST INSTALLATION GROUND PERFORMANCE RUN REPORT

ENGINE siN 'Pc E PJ o a..t-JL/ TSN /TSO

~<./05. 6 CSN /CSO :;2/0~

TFSN/TFSO ;l.t/ 05t ( TSSN/TSSO

CJ-.</Ot). -~ RTO (Rapid Take Oft) Scoop# 2 Yz Min Excursion

OAT ..rt/ (._ FIELD BAR0"[2Cf?9 PRESS. ALT

Oil Type I Brand Name TSN @ Last Oil Service RefSB's 1001,3001,4001,5001, 11001, 13001, 14001 or

T!X'ItJA/ t73W .a-- Maintenance Manual 72-00-00

TARGET OBSERVED

NP dOOJ TQ -{l.06-0 NGINl INH q~, 7 NGINl INH 9:2~s-T5 I ITT I MGT_--Io_6"-9_._Cf-'--- T5 I ITT I MGT _ __,6fl.O~""""'---WF 540 N21NL Nl~ ~INL 5j;£ OIL PRESS. 110-130 /6s OIL PRESS. /{) 5"

CHIP DETECTORS {),("" OIL FIL TER(S) tJK

REMARKS:

CERTWYINGSTATEMENT

This engine was tested and inspected in accordance with the applicable Maintenance Manual and Rental Agreement and found in a serviceable condition.

SIGNATURE ~. ~/~&~ DATE 17 ~60L LICENSE OR STAMP A?:%~d)Jt l(:.i)C! COUNTRY 0Sf1

~~--~~-~~-~-·-···-----·----------

Page 14: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

~~·''.

LCCS 8012, Exhibit F.

DYNCORP·

FIELD EUVATION · · or BAROMETRIC PRESSURE ~C(C( q

LH ENGINESN

RH ENGINE SN. _____ _

ITT P-ROP RPM N1 RPM FUEL FLOW

REMARKS:

.. (l

Page 15: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

. ·-..·

Pl'llt .t Whitney Cllllda Uasins • Llmittd Putnenblp 7007 d4 Ia 8avanne Quejlo!c , Cuwla J3Y-l~7

P&WCL

PRE-REMOVAL GROUND PERFORMANCE RUN REPORT

ENGINE SIN Pe-,; fJ'J o J4t.t

~ITSO CSN/CSO ~

'l.'ir'J). 5- 2·n)-TFSN!TFSO TSSN/TSSO

),1:/)J) 11 v-RTO (.]Upid Take Off) Scoop#

~1.~.t1in Excursion OAT FIELDBARO. PRESS. ALT

1c?.C)

Oil Type I Brand Name TSN @ Last Oil Service RefSB's 1001,3001,4001,5001, liOOl, 13001, 14001 or

;1,tJ 'l'H._. H·):'. Maintenance Manual 72...00..00 '"-

TARGET OBSERVED

NP :l.Or2Q NP 199., .... TQ '3 ~·!::I TQ jO.'l'.

NGi Nl /NIL fl..~-: :1 . NG/Nl /NH- q-LJ-

TS I ITT /MGT '2l T5/ITT /MGT ~ :s~ ... WF .-s-~" WF j"). 7 N2/NL .'II A· N2/NL (1/,}

OIL PRESS. ll(l. ·tw OIL PRESS. I q,-CHIP DE1ECTORS t;;ll...

t..___. OIL FIL TER(S) ,;)/(_

REM\RKS:

CERT~YTNGSTATEMffiNT

This engine was tested and insp~tcd in Accord11.11ce with the applicable Maintenance Manual and Rental Agreement and found in a serviceable condition .

SIGNATURE ~t-~·P~V~oll!pl)J~---- DATE ....JL-11 """'4· . ..:,_-; .l<l!f<L __

LICE>~SE OR STAMP COUNTRY

9t:rLt:r-£2:9-6 '11NI dJO:)UAO

\

Page 16: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

. ' '-

'l

Pratt & WbitDey Canada Leasing, Limited P:utuersbip

7007 de Ia Savannc " Quebec ,Canada JJY-3X7

.-- P&WCL

POST INSTALLATION GROUND PERFORMANCE RUN REPORT

ENGINE siN f'c .. >" /

II [;. j' 0 7- i-1 11 TSN /TSO CSN/CSO

2.(;;) )' 0 2-J.J.. I TFSNffFSO TSSN!fSSO

L£·)~_,;J ' 2-2-l-7 RTO (Rapid Take Off) Scoop# 2 Y:z Min Excursion

OAT FJELDBARO. PRESS. ALT _Jo"' C. :;ooi..-

Oil Type I Brand Name TSN @ Last Oil Service RefSB's 1001, 3001,4001, 5001, 11001, 13001, 14001 or

f),~ ). ) ~'/ 0 Maintenance Manual 72-00-00

TARGET OBSERVED

NP ; i)Ocl NP ;q 2~" TQ .-l J t(:;J.% TQ ~ c, s -NG/Nl/NH ~S:· 7 NG/Nl/NH q~.c T5/ITT /MGT :; ~j T5/ITI /MGT 62-0

WF /./. ,'2, q_t::!_ WF 5-...l ) -

N2/NL AlA N2/NL /<>~

OIL PRESS. ,tj.(;. t.l.~ I lt.J-}"',{) OIL PRESS. j(?J-

CHIP DETECTORS c.> I<-

OIL FILTER(S) oi<..

REMARKS:

CERTIFYING STATEMENT

This engine was tested and inspected in accordance with the applicable Maintenance Manual and Rental Agrm;;ound in a serviceable condition.

SIGNATURE t: DATE (t, Y•£ 2<'~,~ LICENSE OR ST~ ' .• ·. . . COUNTRY L I" f)

Page 17: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

LCCS 8012, Exhibit F

DYNCORP ENGINE PERFORMANCE CHECK

NOTE: Torque (Ftlb) = 30.57 x PSIG

OATE_.!.!:.L!_.:~'::' '• ..

SITE# -~.!L~--- ACFT SN {;)_£- o&j~

ACFT TT _..11 ~_q_cr, 1___ ACFT LNOGS_ C, \" cJ 3

FIELD ELIVATION or BAROMETRIC PRESSURE _ ']_£_ol::,__ OAT C +/- ___:_1_ 1 cJ _

PERFORMANCE TARGETS FROM P&W MM 71-00-00 FIG. 506/507

TORQUE ITT PROP N1 RPM FUEL FLOW

::,~, ~ {p7) 2000 RPM 9.>:l S~to

LH ENGINE SN {!_ kl~ /1 0 )..If Lj -

TSN CSN TSO cso TSHSI CSHSI

'-'7~ 0 ?.:D.l 1.-G Jr,o .2), ") J

TORQUE ITT PROP N1 RPM FUEL FLOW

10,J c~o 2000 RPM 9;,,Y C.>--0

RH ENGINESN -----------

TSN CSN TSO cso TSHSI CSH$1

TORQUE ITT PROP N1RPM FUEL FLOW

2000 RPM

REMARKS:

------------------- ·------------~-----------

Page 18: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

-- ...__ ___ _,L ----"---·"'""·. ·[· --~ ---Pratt& Whitney Canada Leasina. Limited Partnership 1525 Midway park Drive Sridg·~port, west Virginia 26330 Phont: 304--842·1262 &.12~6, Fax: 842-1345 0

Rental Engine Removal Form

Pratt & Whitney A United Technologies Company

• Prior to the removal of this rental engine a ground performance run must be accomplished so a:1 to provide assurance of a serviceable state for the next operator. If this ground p•:rrformanc;c run is not acsompli:shm. thi:s onginc will be routed to our testing facility in West Virginia to satisfy this requirement. Any and all associated costs will be the ~;soonsibility of the org!l!lization performing the removal. Utilize accompanying .. lJround Pertbrmance Run Repon. ·•

• L lSute that all accessories being returned are the ones that were received with this engine. Any discrepapt uscssories will be replaced and all costs will be the responsibilitY or the R.r&anization performing the remoxal of tbi1 enmne.

• This document does not replace the need for the appropriate logbook entries.

Pleast~ return the following infonnation along with the logbook or send it directly to: Atter~tion: Rental Pool Administrator Fu Number: 304-842-1345

Name and address of Operator: _fd:..,.; c l1 r1.,4 1'11h ,., s·" ,1, -l:l:, .~ J'4 ... K .u;. V • ..4...,.. {;,V ...,j£_ A.., l• .. s.?,w.(.. j" '-· l, l "9l_..

Rental Engine Model: .... e_.,""",..(,.;;;..:,...._~_-....... J..=------ Serial Number: .Pc.i 1'50).Atl:f

Qsrating Houn and ,Cycles at Removal:

l '( 1l-f'' TTSN: ~ TCSN: l-1 'i... TTSO: __ _

~ment of Senrieeability;

TCSO: __ _

TfW,~ confirm Ground Performance Runs at installation and removal have been exeo.:ted. I/We have found this engine to be in the following condition:

~ SERVICABLE U UNSERVICABLE

Discr~.:pancies, Defects or Pertinent Co~nments:

Date:

P& WCL would like to thank vou for your cooperation !

9t'Lt>·£~9-61lNI dJO:JUAO

Page 19: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

r OIL A•• ~~MQUES~ KEYPUNCH

~ CODE

TO OIL AN1"YSIS LAB Az::: ..,_,fl~ ~-? T-) 1·3

F MAJOR~ANO ------ 4

R 0 OPERATING ACTIVITY (lreduth ZIP Coth/APO) DODAAD 5-10

M

EQUIPMENT MODELIAPL PT 6 11 - '-( J._ 11-14

EQUIPMENT SER. NO. PCE- PJ tJc').. 'ft.f 11-20

END ITEM MODEL/HULL NO. 73L-!22-END ITEM SER. NO,JI!IC 8L}D'-J&-8' DAn sAMPLE TAK~ Jllll;,:o0 IP I LOCAL TIME SAMPLE

TAKEN I() 00 21·24

HOURS/MILES SINCE OVERHAUL . 21·21

HOURS/MILES SINCE OIL CHANGE 30.33

Rl(~N .. OR SAMPLE LM c: OTH •• M

•oun• 0 ••-- c lspui/7)

OIL ADDED SINCE LAST SAMPLE (Prs, Qts, Gills) ;;; ~fs 31-31

ACTION TAKEN /V (}tV'€_

DIICREFANT ITEM /L/11 HOW MAL .. UNCTIONED N/7 HOW .. OUND

0 LAB REQUEST J!rAIR OR GROUND CREW

HOWTAKEN tl SAMI'LE TEMPERATURE TYI'IEOI~ 37·31 0 D•AIN lif"TU• ~HOT 0 COLD Pf ..J-3 6 REMARKS $"'1'/~- /Jy L.JichtUUrV

o~-;).lfl-d-Y-18

FOR LAB USE ONLY SAMPLE RIUPONSE TIME

:~~~~: 31-40 ·- --.,

Ill' IE 41-43 AG ...... AL 47-41 CR so-sz cu .,. •• MG 1 .. 11 Nl IH1

" 12-14 Sl 11·17 SN 11·70 Tl 71·73 MO 74-71

LAB RECOMMENDATION

If~ ~~ 77·71

s,A~I'L\E r-o_.) --. I SIGNATURE 'I I"I&;;EMAINT DATA SEQ

IJ 1j ~ I L. I MAR I 4 2nns 71 10

\ 1 ,1 1 j

DD 1 ~8~~7 2028 PREVIOUS EDITION WILL BE USED

Page 20: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

n L (

,...... - OIL ANALYSIS REQUEST K£ INCH

'-----' -~~ -mE

TO OIL ANALYSIS LAB 1·3

F MAJOR COMMAND 4

R OPERATING ACTIVITY (lru:lNth ZIP Code/A.PO) DODAAD 0 5-10

M

EQUIPMENT MODEL/APL PT& ;:J -L/2- 11·14

EQUIPMENT SER. NO. f'LE ~ s-Jc 'V·+'f 15-20

END ITEM MODEL/HULL NO. 8/..._-I 'L '-END ITEM SI:R. NO./CIC J"'fD L/8"~ DATE SAMI't.E TAK'-J~;;.· y~ 1 LOCAL TIME ~~mE 'iJ_ TAKEN /

21·24

HOURS/MILES SINCE OVEIIAAUL 25·21

" :-MOURSIMILU SINCE OIL CHANGE 30.33

: ~N ~OR SAMI't.E LA8 a:! OTMall M

OUTt... 0 ... CIUUT 0 !)fUtfyl

OIL ADDED SINCE LAST SAMI't.E (fts, Qrs, Gills) :2-q_ t:r 35·31

ACTION TAKEN . -: --NdtYe_

DIICREFANT ITEM Nt:f

HOW MAL~UNCTIO-D JI/A-

HOW~OUND :l!r:"A111 OR GROUND CREW 0 LAB REQUEST

HOWTAI~I :I SAM~LE TEMNRATURE ~l37:33}o 37·31 0 DIIAIN TU- Q HOT )~"COLD

RE,ARKS s-.a ,,eo.c. L, t=idt~ (I) At__ Tl: 1D rG-,r: \. •i. o<J

5otf -241'-24 lg-

FOR LAB USE ONLY SAMI't.E RESI'ONSE TIME U-40

~· 41-43 AG ~ AL 47 .. 1 CR 50.52 CU 53-SS MG S .. SI Nl 5H1 .. 12 ... Sl IS-17 SN 11-70 Tl 71•73 MO 74-71

I LAB RECOMMENDATION

~ ~ 77·71

SAMPLE NO. 1 $Prt'Z~"'toos I I"ILI: MAINT DATA SEQ

i) [) 0 2 2 ; 71 10

. 00 1 :go•h 2028 PREVIOUS EDITION WILL BE USED

Page 21: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

OIL ANALYSIS REQUEST

FE AO AL CR MG NA

Nl P8 Sl SN 8 MO

ZN LAB RECOMMENDATION

SAMPLE NUMBEACSI

Page 22: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

l •.

-· .. ENGINE SERVICE AND

TIME SINCE TIME RUN

OVERHAUL. INST AL.L. AT IONS, INSPECTIONS, DATE

HRS. I MIN. HRS. ~: USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE

MIN.

BROUGHT ~ FORWARD

Pratt & Whitney Engine Services, Inc. 1525 Midway Park Road Bridgeport. WV 26330 Certificate Number LM1R301K

Manufacturer Description

0 Pratt & Whitney A United Technologies Company

ModeVfype Serial Number

PRATT & WIDTNEY GAS GENERATOR PT6A-42 PC-EPJ0244 MODULE

Time Since New Cycles Since New Time Since Overhaul Cycles Since Overhaul

2833.5 2335 ------ ----Overhaul rEI Repair C.T. Vane Class: N/D P.T. Vane Class: N/D DESCRIPTION OF WORK ACCOMPLISHED AND REFERENCE DOCUMENTATION:

GAS GENERATOR DISASSEMBLED AS NECESSARY TO OVERHAUL INSPECT C.T. DISK AND BLADES FOR WRONG FUEL NOZZLE CONFIGURA TTl ON INSTALLED If AlW PRATT & WHITNEY PT6A-42 OVERHAUL MANUAL PART NO. 3021443 REV.37 DATED 10/21105, AND OTHER P&WC APPROVED DOCUMENT ATION,AND/OR ENGINEERING DOCUMENTATION ACCEPT ABLE TO THE ADMINISTRATOR

GAS GENERTOR MATED WITH SERVICEABLE POWER SECTION SIN: PJ0244-100 AND TEST RUN.

LT.T. TRIM 88.2 F 49.0 C TRIM HARNESS RESISTANCE 20.8 OHMS.

This gas generator has been repaired and inspected in accordance with current regulations of the F Al:bninistration and is approved for return to service. Pertinent details of the work perl1 fil sales order No. 136514 Date 3-Feb-06 Approved

PWV-3096 (MAY 98) .

~n\1/Hn 0 () .!lRq_~ Is ~I""'\,') \~o. ~--\(""\..~eA. . ' ' .._)

CARRIED FORWARD

TOTAL. THIS PAGE

TOTAL. FROM PREVIOUS SUMMARY

TOTAL. SINCE MFG.

-., 1.

:.~..~ ~ -- · .. ~c

Page 23: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

1. Approving National Aviation Authority/Country:

F AAIUNITED STATES

4. Organization Name and Address:

ONE GAS GENERATOR MODULE PT6A-42

2.

AUTHORIZED RELEASE CERTIFICATE FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG

PRATT & WHITNEY ENGINE SERVICES, INC. 1525 MIDWAY PARK RD BRIGEPORT, WV 26330 CERTIFICATE NO: LM1R301K

3017690 N/A ONE PC-EPJ0244

3. Form Tracking Number:

136514

5. Sales Order/Contract/Invoice Number:

REPAIR

13. Remarks: TTSN: 2833.5 TCSN: 2335 TTSO: - TCSO: -The gas generator identified hereon was inspected and repaired in accordance with Pratt & Whitney, Overhaul Manual PIN 3021443 Rev.37 Dated 10/21105, other P&WC approved documentation, and /or Engineering documentation acceptable to the Administrator. Engine test certificate, life limited parts log, modification log, log of major parts replaced, and Engine check list are attached to the logbook. Pertinent details of the work performed are on file at this repair station under the above sales order number. With respect to that work the aircraft

for release to service.

[81 14 CFR 43.9 Return to Service D Other regulation specified in Block 13

Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations, part 43 and in respect to that work, the items are approved for return to service.

21. Approval/Certificate No.:

LM1R301K

23. Date (rnldly):

R.L.FIGLIOLI QA COORD INA TOR February 3, 2006

User/Installer Responsibilities

It is important to understand that the existence of this document alone does not automatically constitute authority to install the part/component/assembly.

Where the user/installer performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified in Block 1.

Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user/installer before the aircraft may be flown.

FAA Form 8130-3 (6-01) *Installer must cross-check eligibility with applicable technical data. NSN: 0052-00-012-9005

Page 24: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

PRATT & WHITNEY ENGINE SERVICES,INC. PT6 ENGINE LIFE LIMITED PARTS LOG

DATE SALES ORDER ENGINE SERIAL MODEL CUSTOMER NUMBER NUMBER

3-FEB-06 136514 PC-E PJ0244 PT6A-42 PWCLEASING T.T.S.N. T.C.S.N. T.T.S.O. T.C.S.O.

REFERENCE: SB 3002 REV. 24

GAS GENERATOR 2833.5 2335 ------ ------

POWER SECTION 2833.5 2335 ------ ------

PART NAME PIN SIN T.S.N. C.S.N. REMAININ p MAX CYCLE CYLCES LIMIT

HUB ASSEMBLY N/D

2ND STG COMP DISK N/D

3RD STG COMP DISK N/D

IMPELLER N/D

C.T. DISK 3049291-01 A0001Tl0 2833.5 2335 7665 10000

1ST STG P.T. DISK N/D

2ND STG P.T. DISK NID

C.T.BLADES 3123131-02 ------ ------ ------ ------ 0/H INSPECTED

1 sr STG BUSHING N/D

OIL FILTER 3028419 ------ 559.2 ------ ------ ------

REMARKS:

*NOTE:TIMES AND CYCLES REMAINING MUST BE REVIEWED AT EACH SUBSEQUENT REVISION OF THE APPLICABLE SERVICE BULLETIN.THE CYCLES REMAINING ON THIS FORM ARE ONLY VALID FOR THE CURRENT REVISION OF THE SERVICE BULLETIN.

flU.~~ ::oo~OR APPROVED INSPECTOR: R.L. FIGLIOLI, QA

PWV-3048D (MAY 01)

-- ---- ~--

Page 25: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

0 Pratt & Whitney A United Technologies Company

Liste des pieces remplacees List of Parts Replaced Dossier qualite - Quality Record P&WC JR3_6934_E [6934] (2004-10)

N° de serie Module Modele ~~~~:!i~~Je~~~~ Serial No. Model

PJ0244 GG PT6A-42 136514

N° de Ia tf.iece Part o.

Des~nation de Ia piece art Description

NEW

3014660 RING-SEALING,POWER TURBINE

3033356 PARTS KIT-FIL TER,FUEL PUMP

3059779-01 FILTER ELEMENT OPTION (IC)

3100453-03 ADAPTER ASSY-FUEL MANF,INLET

3100456-03 ADAPTER ASSY-FUEL MANIFOLD,PRIMARY

3100458-03 ADAPTER ASSY-FUEL MANIFOLD,SECONDAR

3119920-01 SHEATH-FUEL NOZZLE

AKWV-42AIRINLET KIT

AKWV-42EXTGG KIT

AKWV-42GASGEN KIT

AKWV-420FHSG KIT

AKWV-42PKGGG kit

AKWV-42SHIPPINGGC kit . . .. J 2006-02-02 12.58.04 R3 2006.02.02 12.57.39 PR1 400 PW41572 lopllumqlqueue/tmplpltB1so02021258038

PWCL(CSSP)

Qte Qty

2

1

1

1

7

6

14

1

1

1

1

1

1

Pratt & Whitney Engine Services, Inc 1525 Miavay Park Ro"ad Bridgeport, West Virginia 26330 USA Phone: 304-842-5421 Fax : 304-842-4933

Page 1 81 1

Date 2006.02.02

Client Customer

Non Facture Not Charged

Substitution Switch Flag

Fm du document End-of-document

Page 26: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

PRATT & WHITNEY ENGINE SERVCIES,INC

PT6 ENGINE (LARGE) TEST CERTIFICATE

SALES ORDER NUMBER ENGINE MODEL REASON FOR REMOVAL

136514 PT6A-42 RETURN ENGINE-INCORRECT FUEL NOZZLES INSTALLED

GAS GENERATOR SERIAL NUMBER PC-E PJ0244

POWER SECTION SERIAL NUMBER PJ0244-100

C.T. VANE CLASS: N/D P.T. VANE CLASS: N/D

CORRECTED PERFORMANCE

RATING SHP/DELRTH NG/RTH TtS/TH S.F.C.

850 35350 1685 .612 TAKE OFF

DATA PLATE SPEED = 35350 NG @ 850 S.H.P.

Ps3 PRESSURE RATIO 7.57 @ 35000 Ng/RTH

I.T.T. TRIM 88.2 o F. 49.0 0 c.

TRIM HARNESS RESISTANCE 20.8 ohms

THIS ENGINE HAS BEEN TESTED IN ACCORDANCE WITH THE MANUFACTURER'S RECOMMENDATIONS AND REQUIREMENTS.

YfL. /~ r:·"'

Q.A. ~db~INATOR DATE 3-Feb-06 APPROVED INSPECTOR: FIGLTOLI,

PWV-3017 (JAN 98)

Page 27: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

PRATT & WHITNEY ENGINE SERVICES,INC.

PT6 ENGINE SHIPPING CHECK LIST

ENGINE SALES ORDER NO. 136514 I ENGINE MODEL NO. PT6A-42

I CUSTOMER PWC LEASING

I I POWER SECTION SERIAL NO. PJ0244-100 I

ITEM DESCRIPTION PART NO. SERIAL NO. TIME REMARKS

1 PROPELLER GOVERNOR 8210-024H 2252058 ---------

2 TORQUE LIMITER 3244707-7 C12473 ---------

3 TACH GENERATOR N/A

4 OVERSPEED GOVERNOR N/A

POWER SECTION LOGBOOK QUANTITY: ONE COLOR: YELLOW TYPE: CANADIAN

GAS GENERATOR SERIAL NO. PC-E PJ0244

ITEM DESCRIPTION PART NO. SERIAL NO. TIME REMARKS

5 THERMO. BYPASS 3024996 ------------ ---------

6 FUEL PUMP 399701-5 43074 ---------7 FUEL CONTROL 3244768-13 B12685 ---------

8 OIL/FUEL HEATER 10585J WA11440 ---------9 SOLENOID VALVE N/A

10 IGNITION EXCITER 10-381550-4C NN97178085 TSO -0-

11 COMP. BLEED VALVE 3123122-01 30A941 ---------12 COMP. BLEED VALVE 3123123-01 30A835 ---------13 FLOW DIVIDER 26035-1 3199 ---------

ENGINE LOGBOOK QUANTITY: ONE COLOR: YELLOW TYPE: CANADA IN

N/A - Not Applicable N/R - Not Received S/L - Ship Less ---· #A/-:1_~ ia1J

DATE 3-Feb-06 APPROVED INSPECTOR: R.L. FI LIOLI, Q.A. CO~DINATOR

PWV-3056F (JAN 98)

Page 28: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

PRATT & WHITNEY ENGINE SERVICES,INC.

ENGINE MODIFICATION LOG

WORK ORDER NUMBER ENGINE MODEL SERIAL NUMBER

49821 13 PT6A-42 PC-E PJ0244

THE FOLLOWING SERVICE BULLETINS WERE FOUND PREVIOUSLY INCORPORATED:

3142,3147,3149,3152,3158,3162,3164,3165,3167,3174,3175,3178,3179,3180,3183,3184,3185, 3191,3193,3194,3197,3208,3211,3213,3237,3240,3241,3245,3246,3252,3253,3257,3258,3259, 3274,3277,3279,3281,3283,3286,3296,3301,3302,3310,3317,3341,3344,3347,3350,3358,3360, 3361.

THE FOLLOWING SERVICE BULLETINS WERE INCORPORATED THIS VISIT:

THE FOLLOWING AIRWORTHINESS DIRECTIVES WERE CHECKED FOR PREVIOUS COMPLIANCE OR COMPLIED WITH THIS VISIT:

AD(97-04-12) AD(CF-96-24)

THE FOLLOWING AIRWORTHINESS DIRECTIVES WERE CHECKED AND FOUND NOT APPLICABLE:

AD{86-10-05) AD(CF-83-28)

I HEREBY CERTIFY THAT THE ABOVE MODIFICATIONS HAVE BEEN INCORPORATED IN THIS ENGINE PER THE MANUFACTURER'S RECOMMENDATIONS.

DATE 24-Aug-04

PWV-3018 (REV. MAY 02)

Page 29: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

Alberta Central Airways Ltd.

PUBLICATION REVIEW FORM

Date Reviewed :...:A~pr=ii_.4:.L.. =20=0=6::,__ _____ _

Publication Pratt & Whitney PT6A-42 AWD's FAA Reference No. April 4/06

Forwarded to GM 0 CPO MCD Other 0 _______ _

Review Notes Reviewed Pratt & Whitney PT6A-42 A WD's and found them to be embodied. See log book.

Review notes entered on document n/a Q/ yesO lnitals ~£. Review notes entered in journey log n/a [!d/' yesO lnitals ~·

QAUSERONLY

Inspection sheets updated n/a 0 yes [3" lnitals

ICA generated n/a [j' yesO lnitals

Amend aircraft Maintenance Schedule n/a [j" yes 0 lnitals

Copy of document filed in RFM/FMS n/a [?"" yesO lnitals

Copy of document filed in library n/a 0 yesC¥ lnitals

Computer tracking updated n/a 0 yes cg/ lnitals

Staff training required n/a~ yesO lnitals

Review Notes

Date Closed A.fJtZ... '-1/ 0 G

June 2, 2005

Page 30: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

Airworfuiness Directives

PT6A-42 v-9'7-04-12 tA6-10-05

03/14/97

06/05/86

Compressor Bleed-off Valve

First Stage Compressor Hub

Page 1 of 1

http://www.airweb.faa.gov/Regulatory _and_ Guidance_Library/rgAD.nsf/CurrentADFRMakeModel!Ope... 04/04/2006

Page 31: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

Alberta Central Airways Ltd.

PUBLICATION REVIEW FORM

Date Reviewed '-'A:I'<-p'-"ril_4'-'-, =2=00=6=--------

Publication Pratt & Whitney PT6A-42 AWD's T.C. Reference No. April 4/06

Forwarded to GM D CPO McD Other D --------Review Notes Reviewed Pratt & Whitney PT6A-42 A WD's and found them to be embodied. See log

book.

Review notes entered on document n/a C1J"' yesD lnitals JJ. Review notes entered in journey log n/a G;V yesD lnitals cW·

QAUSERONLY

Inspection sheets updated n/a D yes~ lnitals

ICA generated n/a W yes D lnitals

Amend aircraft Maintenance Schedule n/a [J/ yesD lnitals

Copy of document filed in RFM/FMS n/a fY yesD lnitals

Copy of document filed in library n/a D yes [i)/ lnitals

Computer tracking updated n/a D yesGr lnitals

Staff training required n/a~ yesD lnitals

Review Notes

Date Closed

June 2, 2005

Page 32: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

C,.AWIS - AD Record List ·

••• Transcf:rt Cana a

Trans:rts Cana a Can ad~

Franc;ais Contact Us Help Search Canada Site Home About us Media room Environment Emergencies

CAWIS

Airworthiness Directives • Recent

CF Registration Mark

C- @ AD Number

[i] (Do not include revision numbers in the search criteria) • Advanc:<~c:L§earch

Air Marine Rail

All airworthiness directives applicable to: Manufacturer: PRATI & WHITNEY-CAN Model: PT6A-42

New Model

PT6A-42

PT6A-42

Ctry. AD Number

CF v(f-96-24

CF ~83-28

Last updated: 2005-09-22

Road Major issues

AD Record List

AD Subject

D BLEED OFF VALVE (BOV)

D COMPRESSOR HUB

Important Notices

htto:/ /www.tc.gc.ca/aviation/applications/cawis-swimn/awd-lv-cs 140 1.asp?rand=

Page 1 of 1

Service Bulletin or Reference Re In~

y 1538R2,3344,4204 y

04/04/2006

Page 33: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

-Service Centre - PL81 - WV FAA ARS, No. LM1R301K

Pratt & Whitney Engine Service Inc. - 1525 Midway Park Road

Bridgeport, West Virginia United States, 26330 FAA ARS, No. LM1R301K

Status of Airworthiness Directives for This Shop Visit

Sales Order: 136514 Customer: PWCL(CSSP) Description: GAS GENERATOR MODULE MOdel: PT6A-42

Print Date: 02-FEB-2006 Page: 001 of 001

Serial Number: PJ0244

Document No. Revision No. Status Description

AWD CF-83-28 000 00 Embodied COMPRESSOR HUB LOW CYCLE FATIGUE LIFE.

AWD CF-96-24 000 00 Embodied BLEED OFF VALVE COVER - INSPECTION/

FAA 86-10-05 000 00 Embodied FIRST STAGE COMPRESSOR HUB

FAA 97-04-12 000 00 Embodied COMPRESSOR BLEED OFF VALVES

I hereby certify that the above airworthiness directives with status have been incorporated or found embodied in this engine as per the manufacturer's recommendations.

d?L-A~ Authorized Inspector: ~~~

"EMBODIED"

Page 34: AIRCRAFT TECHNICAL LOGS - Aviation Technologies Eng 8.24.044.7.06.pdf,i i! 'i engine service and time run time since overhaul installations, inspections, date hrs. min. ~: use boti-i

Service Centre - PL81 - WV FAA ARS, No. LM1R301K

-Pratt & Whitney Engine Service Inc.

1525 Midway Park Road Bridgeport, West Virginia

United States, 26330 FAA ARS, No. LM1R301K

List of Service Bulletins Incorporated This Visit

Sales Order: 136514 CUstomer: PWCL(CSSP) Module Name: GAS GENERATOR MODULE Model: PT6A-42 Serial Number: PJ0244

Document No. Revision # Class

:SB 3003 000 SB 3250 000 SB 3328 000

20 3 04 8 00 8

Description

Print Date: 02-FEB-2006 Page: 001 of 001

OPERATING TIME BETWEEN OVERHAULS .AND IMPROVED C.C LINER,EXIT DUCT .AND FUEL NOZZLE SHEATH - INTRODUCTION OF

I hereby certify that the above modifications have been incorporated in this engine as per the manufacturer's recommendations.

Authorized Inspector: