Aircraft Technical Logs: RH Engine 1

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Transport
Canada
Transports
Canada
Aviation
Aviation
60-029
R/H ENGINE - PCE-305164
TP3910E
1 .
AIRCRAFT
TECHNICAL
LOGS
..
Section 3.
Second Edition
January 1987
Canada
ENGINE
ENGINE LOG
Make
2.
Model
3.
Specification
Cftl ETA
Manufacturer's Serial
Number
PCE-:x:>Sibf
4.
c-
I
1.
5.
Date of Manufacture
6.
Aircraft Inspection Cycle
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CRS KW3R646L
Tucson, Arizona
PACE 1
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23 CYCUS
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Customer:
Aircraft Mfg Type:
Aircraft Total Time:
Engine SIN :
i work Pertonneo:
Dallas Alnnotlvo
2049 High Ridge Rood
Boynton Beach, FL 33426
-------
RELIABLE JET MAINTENANCE, INC.
-------
LEAR 60
~
Engine Type:
Total Landings;
4729 7
PCE30516'
TT:
PW305A
411 6
TC:
4468 8
Rog. #:
En9. #
TSO:
4065
N11 9FD
S/N:
60·029
CSO:
NA
1
wor~ requested by cusiomer, as descl1bod on our Sales Ord
July 18 2012
F$27626
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1'HIS PA.GI!
TO'T"AL FPOM
l"'A~IOUS SU.MM-""'
_?,. ..L.
StUCF ... ~G
TSN: 4472.0
CSN: 4070
mphed wnh borescope evaluation check.
Complied with Nordam field eogin«ring disposition letter # NTRSD· 12-TPI 00 Dated July 23, 2012 signed by
Tom. Pryor Cusiomcr support engineer supervisor, by removing damaged inlei aoousric wire mtlh liner and
~\'Ith
c;no~
requires to be repair within IDO fli!!ht hours.
Compiled
Prati & Whiuiey
cnginttr evaluaiion leim OAA20 I2-6I2-1'W30SA-30S16-1 Ooicd July - -- 2012 sri:ncd by Serge Corriveau Service Engineer and Peter Boyd Chief Enginccr dctcnnined thot 1he engine
is rn serviccnbte condi1ion for a reposition Oigh1 from
Venezuela to Lincoln, Nebraska for the fan liner - -- -
~I:
Cara~.
_
Qrov ~~oir• or mamtcnnnee
is approved for rcnim to service.
•
Work
Order
#
The
above
described
---
ationYRRG491L
-Dallas Alrmotrvt' Repair St .
Signed ~
~
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A dc1:ii1ed record is on file under
-~
~
Page I of I
AuguSt. 01 2012
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Engine SIN: 305164
rcp1at(ment.
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Signed:~""·~
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-
Work Order: QPOV
TAT: ~732.9
Ensine Posilion: Ill
~
11c.comphshC?d and inspec1ed wilh reference 10 Instructions ror con11nued u1rwo11hiness and Curre ~r listed below was
01her data and methods acceptable to the ~dministralor with respect 10 the wor1< performed n1 AA re9utar.ons and
service Pertinent details of this repatr are on file al this FAA Certificated Repair Stallon
' •s approved tor return to
Date:
f,
C)
I __.....-/.r-.,--
IBR P/N 3002260 S/N 60A975 Next Duo Al 4768.B
Safes Order.
B)
~
Date: Augus1, 01 2012
SIN: 029
Model: PWJOSA
T~foll~wlng. maintenance was perfonnC?d by Duncan Aviation under Work Order# QPOVA
~
NA
Ren10V8d enyrr,.. wwtlll!IS. EEC. arrtrame 1n1e1. engine row cone fan assembl &
gain accMs to 1" stage IBR Complied v•th 1• stage IBR eddy current 1llS Y mner stator to
no1ed Compiled v.lh on v.ng coo-osoon repair Rernstalled inner stator f~'°" No etacks
nose cone airframe 111le1 EEC and engine cowling All maintenance has bee
embly engine
reference to Pran & Whitney Maintenance Manual 3081402 Rev# 59 dated n accomptr.she<l rn
Leal)et 60 Aircraft Marmenance Manual- MM-103 Revi$100 AS dated Octot>e 0oe;ember 02 2011
and methods acceptable to the adminls1rator
'
· 201 1 other data
This en1ry cen1fies that only the
I)
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Reg. II NI 19FD
Model: Lear 60
Make: P & WC
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-·
Ru
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~
Reg. # NI 19FO
Oare: Seplt mber 12. 201 2
Model: Lear 60
SIN: 029
Make: Prn 11 & Whirn cy Model: PWJOSA
Engmc SIN: PCE-305164 TSN . 4478.1
~
WorkOrder: QNJK
TAT: 4739.0
Engine Posi1ion: 112
CSN: 4073
~
-
d
_ The ab<>ve described repair or 11111imenn11ce is a1mrovcd for rc1urn 10 scivicc. A de1oiled record is on file under
_ Work Order~'IJKA.
Ott.~
Signed
- - - ,..,r
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1.!·107S?
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nt
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and pin ·
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10
IAW l'&W 305.1\ ~lM 79-20·01 . l<.~ chcci... T~~' P&:\\ ~A MM 72.()(M)O t.t::tk c:'h1:d: ;uod
2 Cumplti:d '' 11h ti 600hour/)6S cbyml chan~ Iii pin '"Oll6MJ..OI \\llh
J Ki:mon:d (.ngtn.: f~~l lill-:t tlnd u~allt:d :t ~;~.,~!'·r;\ W;,&W jOSA M~I 79·20·01 Ltal. 4htd. t(')()J
3 n1.:'' ~n ng ~n AS.J200- l~i Md pin A.SJ. -
----
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Removed fan case PIN 31041 18-01 SIN JF4S6 und ins1Dllcd fan case PIN 3105237-01SIN3L l29overha Id b
Prnu & Whi1ney Au10Air, Inc. CRS# QZAR320L und<r form 1rocki11g H ISl87J460IOOCJ0-121i871 dated Mn ,~ e Y
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TIMB SINCa
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To"I Eo:Jnt Cytl<s:
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IHSPl:C TIONS.
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MAINTENANCE RECORD
.. ·
£.---
AEPAJRS, A OJUSTMENTS, MOO I F' ICATION S
'-Oll THllllOU GM ........ UHUICO LtNCI IN 0 4T C A HO TIMI COLUMN•,.
CH f"flllCI. Olt AW & 0 1400N AL
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-----/
'
M"XIMOM HOU " '
BETWEEN ovl!AHAULS
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SIG NATUAI:
1..ICliNCC
NUMO!.R
RECORD OF ENGINE
AIRWORTHINESS DIRECTIVES IA/D), SERVICE BULLET INS (SIB),
OAT&:
iSeit MAR 1 7
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SPECIAL INSPECTIONS (S/11 Al'-.:D r-;iODIFICATIONS !MODS)
PEA~OAMED
=======================
DP
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D A
I NSPECT I ON
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1994 MAR 1 7
PlilA'fT 0. WH
1994 MAR 1 7
\.
(Q.o.r. COMP/\~~NEY CtUIADA INC.
Corn
APPROVA L No. 4·58)
Pany Au thorized Inspector
RECORD OF ENGINE
AIRWORTHINESS DIRECT IV :::'.S IA/DJ, SERVICE BULLETINS !S'BJ,
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PRATT & WHITNEY CANADA I NC.
PW305A FI NAL ACCEPTANCE TEST RECORD
Date: 17-MAR- 9 4
ENGINE S/N - 305164
E & TI
- 0565-C
BUILD SPE C. - 772
TEST CELL
- 22- 05
SLS ISA PERFORMANCE DATA @
PARAM ET ER
Nl/RTHO
N2/RTHO
P 3/ Pl
S PEC.
9341 9740
25450 - 26750
ACTUAL
9545
25924
16 . 7
4679 lbs . Fn .
PARAMETER
T45/THO (Deg . C)
SFC
AC TUAL
632
0 . 383
ACCEL TI ME - 4. 16
SEC. at 4 0 deg. F
lbs .
GROUND I DLE CORRECTED THRUST - 24 3
FLIGHT IDLE CORRE CTED THRUST - 430
lbs.
93 . 7
98 . 1
3
- 20
0
_
_
---:
..
..
___...
___..
__..,;
~-,.
OIL TYPE
- PWA521-2
FUEL TYPE
- CPW204
OIL CONSUMPTION - 0 . 11 lb/ hr
HIGH ROTOR TRIM BALANCE - FB25 F026 FA39
EIGH ROTOR TRIM BALANCE - R825 RD26 RA39
LOW ROTOR TRIM BALANCE - 033
, ('\~
DOT TYPE
FAA TY~ ~ AP PROVAL E- 22
~ ·~ CERTI FICATE E35NE
~~
GOVERNMENT SIGNATURE:
~
INSPECTION SIGNATURE:
~
..
~
__..,,.·
__..,,.
- --__..,,.
__.. ., - - __.,
__,,,:
_.-/
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__..,,,.~
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TH E UNDERSIGNED CERTIFIES THAT THIS RECORD ACCURATEL
THE EVENTS DURING THE TEST MADE ON THE ENGINE T!!ERE!y SETS FORT!!
N I DENT IF! ED
S SHJH
.
DAT£: 1994 MAR 1 7 FOREMAN, ASSY & TES T INS P . :
RE F:09584701 -040 17 REF - 4924
-·
-.
_::. .A-
PRODUCTION SIGNATURE:
P£Rjl!'0R M t 0
___..,,..
'
Hrs. 31 Mins.
lbs.
~
~·
lbs.
\
TOTAL RONNING TIME - 12
ENGINE HEIGHT (DRY ) - 986
IH" PE CTtO H
___..~
TRIM PLATE I NFORMATION
-
0'-:
___
__,,..,..
__,,.
ADDIT I ONA L INFORl'IATI ON
Nl REF .
N2 REF .
Nl TRI M CLASS
T45 TRIM cr.;.ss
VIGV TRIM CLASS
--:=-·
WORtc:
~·
SPEC.
648
0 . 388
NOTE : T45 is t r immed .
REFERENC E TRI M THRUST - 5225.
S PEC IAL INSPECTIONS !S/11 AND MODIFICATIONS !MODS)
~
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PRATT & WHITNEY CANADA INC.
lC OT CQ!!PAMYAppaoyAL No. 4·56)
Company Au1horized Inspector
{\ I ~· SHIH~ I /J.JJ "
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1994 MAR 1 7
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Transport
Canada
Transports
Canada
Aviation
Aviation
'·
CONFORMITY CERTIFICATE
CERTIFICAT DE CONFORMITE
REPAIR OR MODIFICATION
REPARATION OU MODIFICATION
INSTRUCTIONS
FOR INSTRUCTION SEE AIRWORTHINESS MANUAi. ADVISORY 575.219. ·POUR LES INFORl.IATIONS CONSUlTEA LA CIRCULAIRE CONSULTATIVE AU l.IANUEL DE NAVIGASIUTE 575 219
PRINT OR TYPE. DACTYLOGRAPHIER OU ECRIRE EN LETIRES l.IOULEEs
MAKE CONSTRUCTEUR
MODEL MODELE
1.
AIRCRAFT
AERONEF
2.
N/A
SERIALNO · N OE SERIE
N/A
N/A
ADDRESS·ADRESSE
NAME · NOM
OWNER
.
N/A
REGISTRATION MARKS· MARQUES D'IMMATRICULATION
N/A
N/A
PROPRIETAIRE
3.
IDENTITE DE l.'UNITE
MANUFACTURER · CONSTRUCTEUR
UNIT UNIT!:
TURBO-FAN
UNIT IDENTIFICATION
4. TYPE OF WORK· GENRE DE TRAVAIL
P&WC
~
SERIAL NO. · N ' DE SERIE
MODEL · MODELE
IWJOSA
MODIFICATION
PCE-305164
(!]
REPAIR
REPARATIO N
• USE A SEPARATE FORM FOR EACH UNIT BEING CERTIFIED· UTILISER UN FORMULA IRE SEPARE POUR CHAOUE UNIT!: CERTFIEE
I CERTIFY THAT THE WORK DETAILED ON THE REVERSE SIDE OF THIS
SHEET riAS BEEN ACCOMPLISHED IN ACCORDANCE WITH APPRO\IEO OATA
SPECIFIED THEREIN
5.
COllFORl.llTY
STATE~I EllT
DECLARATION
DE COllFORMITE
..>
~~~H~~
S»G#tATURE
IAUTl<OAIZED PERSOtl • PfRSOtl"<E AUTORISEEI
JE CERTIFIE OUE LE TRAVAIL OECRIT AU VERSO OE CE FORMULA!RE A
ETE EFFECTUE SELON LES METHOOES HOMOLOGUEES OUI y SONT
l.IENTIONNEES
1994 MAR 17
4-58
Aid£ UC:tM:E 00 A'JO APPflOVAL NO
u OELICEHClDUfCAOUO-OOUOEl MIO
ADDRESS ADllESSE
DATE
CATEGORY . CATEGOR!l:
1801 caJR'mEY PARK DRIVE
Ml.SSISS1\UG1\, ONrAR.I.O
L5T 1J3
THE MAINTENANCE REQUIRED TO INSTALL THIS COMPONENT ON THE
AIRCRAFT STATED ABOVE HAS SE.EN PERFORMED IN ACCORDANCE WITH
THE APPLICABLE STANDARDS OF AIRWORTHINESS.
6.
CERTIFICATION
SIGNATUR~
(AUfllOntZCO P~RSON · PEASONNE AUTORISEE)
LA MAINTENANCE REOUISE POUR INSTAUER LE COMPOSANT SUR
L'AERONEF MENTIONE Cl·HAUT A ETE EXECUTEE CONFORMEMENT AUX
NORMES DE NAVIGABILITE APPLICASLES.
AMF. LICENCS on AMO APPROVAL NO
N OE LICtNCh OU IEA OU O'APPllOOATION OE L' AMO
ADDRESS AOAESSE
CERTIFICATION OF AERONAUTICAL PRODUCTS BEING RETURNED TO
FOREIGN CUSTOMERS
DATE
CATEGORY · CATEGORIE
CERTIFICATION OE PRODUITS AERONAUTIOUES RETOURNl!S AUX
CLIENTS D ORIGINE ETRANGERE.
7.
FOR DEPARTMENT
OF TRAtlSPORT
OR APPROVED
LIAINTENAUCE
ORGAfllZATIOH USE
RESERVE
AU MINISTERE
DES TRANSPORTS OU
AUX ORGANISMES DE
MAINTENANCE
AGREES
AIRWORTHINESS OR AUTHORIZED INSPECTOR
INSPECTEUA AUTOAISE OU OE NAVIGABILITE
REGION 019H11Cr on 011GANl7ATION
REGION OISTn!CT OU Of10ANl$ATION
I
STAMP I CATE ESTAMPll.lE 1 OAIE
W04!i101 OOJ
Canada
____:...
WEIGHTIAND BALllNCE OR OPERATING LIMITATION CHANGES SHALL BE ENTERED IN THE
APPROPRIATE AIRCRAFT RECORDS A MODIFICATION MUST BE COMPATIBLE TO ALL
PREVIOUSLY INCORPORATED MODIFICATIONS TO ASSURE CONTINUED CONFORMITY WITH
THE APPLICABLE AIRWORTHINESS REQUIREMENTS
LES CHANGEMENTS DE MASSE ET CENTRAG E OU DE LIMITES D'UTILISATION DOIVENT
ETRE TRANSCRITS DANS LES DOSSIERS l\PPROPRIES DE L'AERONEF. UNE MODIFICATION
DOIT ETRE COMPATIBLE AVEC LES MODIFICATIONS PRECEDEMMENT INCORPOREES POUR
ASSURER LA CONFORMITE AUX NORMES DE NAV!GABILITIO APPLICABLES
8. DESCRIPTION OF WORK ACCOMPLISHED
(IF MORE SPACE IS REQUIRED ATIACH ADDITIONAL SHEETS · IDENTIFY WITH AIRCRAFT,
NATIONALITY AND REGISTRATION MARKS ANO DATE WORK COMPLETED.)
DESCRIPTION DES TRAVAUX EXECUTES
(AU BESOIN, UTILISER DES FEUILLES SUPPLEMENTAIRES - INDIOUER SUR CHAOUE
FEUILLE, LES MARQUES O'IMMATRICULATION OE L'AERONEF ET LA DATE A LAOUELLE LES
TRAVAUX ONT ETE EFFECTUES.)
EN:;INE S/N: 305164 RE'IURNED 'IO P&WC 'ro lNVESTIGA'IB SURGE AT
IDLE CCtIDITION AND K)[)IF!ED 'ro INCORPORA'l'E 'IHE P&~
SERVICE BULlEl'IN 24282.
Nr
EN:;INE M){)!FICATION, 'IHE FOLI.aflNG PARTS WERE OfANGIID:
3182199-01 TUBE REPLACED BY SAME P/N. (2 EA}.
31B4886-0l P2.8. B.O.V. S/N: 16A402 'RE}oi)VED. REPLACED
BY P/N: 31B4960-01 S/N: 18A494.
31B4469-02 H.M.U. S/N: 1891214 RE)i()VED, REPLAC'.ED BY
SAME P/N, S/N: 1891110.
30814998
TUBE REPI...ACED BY 30Bl499A.
END
~I
'--~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
D
D
WEIGHT ANO BALANCE
MASSE ET CENTRAGE
D
INDEPENDENT CONTRo'L CHECK '
VERIFICATION INDEPENDANTE OE~ COMMAN~ES
ELECTRICAL LOAD ANALYSIS
CALCUL DES CHARGES ELECTRlOUES
D
TEST FLIGHT
ESSMENVOL
00
D
LOG BOOK ENTRIES
INSCRIPTIONS AU CARNET D'AERONEF
ADDITIONAL SHEETS (IRE ATTACHED
FEUILLES 'suPPLEMENTAIRES JOiNTES
.
~
llilMIARDIER
(',enified Repafr Station No. SH5R197N ,
~
BOMBARDIER
AEROSPACE
PW 305 ENGINE OUTGOING CHECKLIST
NC SIN ~ 0 - Oc?. 9
NCN# 55KS
DATE: oS/l~/97'
MODEL
Pv-u 3 05
Engine SIN: Pc£. .3 os I Gt;
CUSTOMER ENGINE_/
W.0.#:
LOANER ENGINE_
1. Visually inspect Fan Inlet area to include Fan, Spinner and Inlet
2. Visually inspect By-pass Duct area to include Inner Duct and Ignitors
3. Turbine Area, includes Nl, ITT J Box and ITT Harness
4. Exhaust area to include Fire Loop Brackets, ExH Nozzles and LP Turbine
5. Visually inspect Accessory Gearbox
6. Visually inspect External Fuel and Oil Lines
7. Verify Shipping covers, caps and plugs are installed
8. Verify Oil Tanlc is drained and tagged
Record the following Components:
SIN ......l.....f'....~.....1__1"""'1(),,__ __
Fuel Control PIN
Fuel Pump
PIN
Pt~-0 ~
-(l (_
SIN
I"" }'(.'-~~ L\ (; t;"'6A-
.r
N2 Monopoles
Ch "A" PIN 30{5/ lj tf '1
Ch "B"PIN Jol) J'/t/9F
SIN C HGS 8
SIN
3oc;
Ignition Exciters
Ch "A"PIN Cjoi/ 7~ir0-(0
Ch "B"P/N <jo<171~c -10
SIN /JAJ 92 I 2. 03 7 5
SIN µJJ ?.2. / ZD3 7]'
EPA Can
SIN
13 G 3
3
K"'J/02.fC,5~ SIN ~
Engine Trim Plug
PIN
Heat Exchanger
PIN l~C, - <joo zo-tXJ<:>
11155
------=-SIN 2 S l/
--~----
Verify Engine Log Book matches Engine, is complete and installed in shipping container
Record any damage or missing items in remarks section and inform Lead Technician
o..c.:>sScr1l'~
/, ~ I~ C.
o ,,
bo,p./r
REMARKS: /3"1.ff'q.._
I
e·
c:az:wrn-~
t
----- -- ---1- ATTACH TO PRODUCT
Maintenance Release
P&WC 3440 ( 10-92)
Manufacturing Division
DOT Company Approval No. 4 - 58
m
UNITED
TECH NOLOGIES
PRATT & WHITNEY
CANADA
900247
Pratt & Whitney Canada Inc.
1000. Marie.Victorin
Longueuil. Ou6bec
Canada J4G IA I
Description --~- ____
FAN
_____________ Quantity __1___
Part Number _
3_184
__0_6_7_-_0_2_____ Serial Number PCE- 305164
Manufactured By _ __ _ P_
&_WC
__________ Model /Type
Work Order Number _ _ 1
_1_
59__4_4_____ Sales Order Number
Repaired
[X]
Overhauled
D
Tested
lKJ
_ _
CL. _ _ __
FW305A
409033717
Modified
Inspected
Previous Certification _ _ _ _ __ _ __ _ _ _ _ _ __ _ _ __ _ _ _ _ __
Total Time
89:30
Total Cycles --=1=-=5::.:3=--- --
Time Since 0/H
----
Cycles Since 0/H - - - - - -- - - -
Work performed
S/N: 305164 RETURNED 'ID P&WC 'ID
INVESTIGATE SURGE Nr IDLE CCT'IDlTirn AND
M)DlflED 'ID INCORPORATE '!HE P&WC SERVICE BULLETIN 24 82.
~INE
AT fill3INE MJDIFICATirn, '!HE FDLiailNG PARI'S WERE
OIANGED:
31B2199-01 TUBE REPLACED BY SAME P/N. (2EA).
31B4886-01 P.2.8. B.O.V. s/N: 16A402 ~VED.
REPLACED BY P/N: 3184960-01 S/N: 18A494.
3184469-02 H.M.U. S/N: 1891214 ~VED , REPLACED
BY SAME P/N, S/N: 1891110.
30Bl499B TUBE REPLACED BY 30Bl499A.
I certify that the maintenance stated above has been performed in accordance with
the applicable standards of airworthiness and the product is approved for return
to service. Records of the work performed are re tained under Work Order file.
1994 MAR 1 7
Date
Authorized Inspector
(Signature & Stamp)
'1....
l+I
Transpor1
Canada
Transports
Canada
Air
Air
CERTIFICATE OF AIRWORTHINESS
FOR EXPORT
• ..
CERTIFICAT DE NAVIGABILITE
POUR EXPORTATION
'I roR EXPORT TO' POUR EXPORTATION V£RS
U.S.A.
INSTRUCTIONS ON REVERSE - INSTRUCTIONS AU VERSO
2 EXPORTERS NAME· NOi.i DE LEXPORTATEUR
PRA'rr & WHI'mEY CANADA
nc.
3 AOORESS • AORESSE
1801 CXlJR'It£Y PARK DRIVE
MISSISSAIXiAr CNI'ARIO
CANAD!\
L5T 1J3
'' PRODUCT NAME NO.•~ OU PROOUIT
PW305A
5 p,\nT IJO ·ti OE PIECE
6 SERl>\Ll<O • N OE S(RlE
1
'9 TYP£ APPROVAL NO • II OE l HO'.IOl.OGMIOtl OE TYPE 10
8 t.•AOE BY • co•.STAUIT PAA
PRATI' & WHrit£Y
CANADA nc .
•., FORltlSTALLATICi.IOH-POURl/O:ITAGESUR
N/A
7 CUANTIT'I' • OUANTITE
PCE-305164
A31B4067-0l
IE\'/· NEUF
E-22
00VERHAULEO ·REVISE
EJSNE
0REPAIREO·REPARE
12 IWOICE"O ·fl OEFACTURE
400 033717
'13 REl.IAR~S • REMAROUES
• 15 TI1eaeronau1icalproductdosc11bcdabovo
conforms 10 the slated type approval, 1s 1n a
condi1Km for safe opera11on and. 1n lho caso ol
an engine or propeller. has been subJeclcd lo
a Ima! operahonal check
M.. ,
Lo produol a6ronaullque decnt ci-dessus correspond II l'homologa11on do 1ypo enoncee. esl
en c1a1 do foncuonnemencsecun1airc el. dans
IOC8S d·un moteur OU d'une h<ibce a Ctesaum1s
i\ un concrolc final de lonclionnement.
1993 AUS 2 4
CATE
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4
ATIACH TO PRODUCT
ATIACHERAU PROOUIT
Canada
INSTRUCTIONS
A. FORM PREPARATION
A. PREPARATION DU FORMULAIRE:
(a) Type or print clearly;
(a) Dactylographier
moulees;
(b) Can be completed in English or French,
as required by the foreign civil aviation
authority; and
(b) Peut etre complete en frarn;:ais ou en
anglais. selon !'exigence de l'autorite
de !'aviation civile etrangere; et,
(c) All blocks are to be completed to extent
applicable.
(c) Chaque case applicable doit etre
remplie.
B. COMPLETION INSTRUCTIONS FOR
BLOCKS DESIGNATED WITH AN
ASTERISK (*):
B. INSTRUCTIONS CONCERNANT LA
FA<;:ON DE REMPLIR LES CASES
ACCOMPAGNEES D'UN ASTERlQUE (*):
·1 Insert the name of country to which
product is being exported.
·1 lnscrire le nom du pays vers lequel le
produit est exporte.
•g To state foreign civil aviation authority
approval requirement (e.g., for U.S.A.
normally the TC. STC or TSO). If type
approval is pending, insert "pending''
and explain under "remarks" block.
·g lnscrire !'exigence d'homologation de
l'autorite de !'aviation civil~ etrangere
(e.g .. dans le cas des Etats-Unis.
typiquement le TC, STC, TSO). Si
l'homologation type est pendante,
l'inscrire, et l'expliquer dans la case
«remarques».
•11 Specify when identifiable, the make and
model of the aircraft, engine, propeller
or system on which subject product is
destined to be installed. For TSO
approved product enter NIA.
·11 Specifier, lorsqu'identifiable, la marque
et le modele de l'aeronef, du moteur, de
l'helice ou du systeme sur lequel le
produit vise est destine etre monte.
Dans le cas d'un produit homologue
TSO, inscrire NIA.
• 13 To include any statement required by
the approval document and specifi c
details of any authorized deviations to
approved data.
'13 Doil comporter toute declaration requise
dans le document d'approbation, ainsi
que les details specifiques de toute
derogation autorisee aux donnees
homologuees.
·15 To be signed either by a DOT Airworthiness Inspector or Airworthiness Inspection Representative, over typed or
printed name.
·15 Doil etre Signe par un lnspecteur de la
navigabilite du MdT ou par un Representant des services d'inspection de
l'etat de navigabilite des aeronefs; le
nom dactylographie ou en lettres
mou lees doit apparaTtre sous la
signature.
OU
ecrire en lettres
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Part Number
A3 1B4067-01
Longuou•I. Quebec
IOOO. Manc·V1ctonn.
Cannda J4G IAI
•
••
Manufacturer
Pratt & Whitney Canada Jnc .
Serial Number
_I>CE- 305 164
Model Number
PW305A
(1)
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g
R. N. No. 400
~
The item described above is new and conforms to approved design data, has been inspected and is in a
condition for safe operation.
(1)
0(1)
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TU HBO- F AJ\1
Pratt & Whitney Canada Inc.
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Nomenclature
UNITED
PRATT & WHITNEY
CANADA
TECt1NOLDGIES
0 33 71 7
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Authorized Inspector: _ _
/
S. ~H~/J
.JJ41-1JUm_L~j'- ~
Date:
i993 AU G 2 4