Download PT6A-66 S/N:PCE-RK0121 FINAL ACCEPTANCE TEST RECORD

PRATT
& WHITNEY CANADA CORP. P68 PROGR
.29
================================================================
PT6A-66
S/N:PCE-RK0121 FINAL ACCEPTANCE TEST RECORD
......................................................
2004 JUL 27 TEST CELL : 0113 BUILD SPEC.: 676
ENGINE TESTED AND ACCEPTED IN ACCORDANCE WITH E&TI : 453
FINAL VANE FLOW AREAS
FIRST STAGE : 13529 IS5
SECOND STAGE : 01466 2S2
7.18
24.04
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..
PERFORMANCE DATA
TAKE-OFF
PART-POWER
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
SPEC ACTUAL
SPEC ACTUAL
. . . . . . . . . . . . . . . . . . . . . .
PROP SPEED
S.L.S. STD.DAY POWER
I.T.T. (T5A TRIMMED)
DEG R
T5D (DERIVED)
DEG R
GAS GEN. SPEED
RPM
SFC @ 18400 BTU/LB LB/SHP.HR
PRESSURE RATIO @ 34500
2000.
850.
1681.
1720.
34550-35150
0.683
RPM
7.91
2000.
650.
1597.
1580.
34150.
0.754
2000.
850.
1645.
1630.
34900.
0.656
7.80
FUEL TYPE : CPW 204
BTU/LB
TEST LHV : 18502.
S.G. :0.812 @ 81. 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 :
B.O.V. SEAT CLASS AS TESTED :
B.O.V. SEAT CLASS AS SHIPPED :
PWA 521
0.0
114.5
150
TYPE I1
LB/ HR
PSI
DEG F
0.0
0.0
20
0
0
1.44
13
16
DEG F
DEG C
OHMS
OHMS
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
HANDLING AND CONTROL SETTINGS
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
RPM
TRIMMED MAX NG : N/A
RPM
UNTRIMMED MAX NG : 39000
RPM
DATA PLATE SPEED : 34900
IDLE SPEED : ;)0 2 9 =L RPM
ACCEL. TIME F.I. TO MAX @ TI : 2.23 SECS @ 70.8 DEGF
ENGINE DRY WEIGHT : 452.5
LBS .
fls-
PRODUCTION SIGNATURE
0
INSPECTION SIGNATURE
.
GOVERNMENT INSPECTOR
:
THE UNDERSIGNED CERTIFIES THAT THIS RECORD ACCURATELY SETS
FORTH THE EVENTS DURING THE TEST MADE ON TbfET-EAIGINE THEREIN IDENTIFIED.
1
.E
JUL
8
FOREMAN,ASSY .&TEST INSP
:
Index of Engine Documentation
Engine Number: PCE- RK0121
Quantity of
Documents
Document Name
I
I
Final Acceptance Test
~ e c o r dSheet
I
Engine Serialized
Component Summary
(Quantity of set) X (Quantity per set)
Life Limited Material
History Record
1
Life Limited Blades History
Record(when applicable)
Engine Build Record Status
I
(Quantity of set) X (Quantity per set)
Report (SB)
Note: (1) copy or set is staple in the
SB section of the Yellow Book
Engine Log Book
(Yellow Book)
I
1
Final Vibration Survey
(when applicable)
1
Authorized Released
Certificate(Form 24-0078)
Date
Note: This index reflects the quantity of Shipping
Documentation supplied with the engine
Issue Date: June 10,2000
Pratl8 Whihriay Canada Cis. 1
Prail8 Wh'tney Canada Corp.
Pratt & Whitney Canada
Une .odOMde W i d Techn&+slAUniledT~(ihnologim
Liste des composants moteur a numeros de serie
Engine Serialized Component Summary
I
Aod&le
Aodel
3008012
I
:ode de trait.
hermique
leat Code
2OUPLING SHAFT FLEX 2ND STAGE RED'N
>EAR-SUN.2STG RDCN.46 TEETH
4DAPTER-1ST STAGE CARRIER
SARRIER-SECOND STAGE REDUCTION
3EARING OPTION
DISC TURBINE
DISC-TURBINE
FLOW DIVIDER AND PURGE VALVE
PUMP-FUEL
- COMPRESSOR-TURBINE STATOR,ASSY OF
ROTOR COMPRESSOR
ROTOR - COMPRESSOR
ROTOR COMPRESSOR
VANE RING-POWER TURBINE
VANE RING-TURBINE
SHAFT-STUB.COMPRESSOR ROTOR
HOUSING-POWER TURBINE STATOR
WIRING HARNESS - ELECTRICAL
DUCT-TURBINE EXHAUST,ASYO
GEAR - RlNG FIRST STAGE REDUCTION
DISC -TURBINE
SHAFT-PROPELLER
LINER-COMB CHMBR,OUTER,ASYO
HEATER-OIL TO FUEL
CARRIER-FIRST STAGE REDUCTION
BEARING-BALL FLANGED
-
Carad. de montage
BUIM Spec NO.
I
Node serie
Serial No.
;EAR-PLANET,SECOND STAGE REDUCTiON
3EARING-ROLLER FIANGED
SEAR - SUN, 1ST STAGE REDUCTION, 26 TEET
SEAR RlNG 2ND STAGE RED'N
IXCITER-IGNITION
MPELLER-CENTRIFUGAL
?OTOR-COMPRESSOR
SEAR-PLANET.1ST STAGE REDUCTION
:",",",.u~~:"d~~~~~Canada
J4G 1Al
Node s e i e
Serial No.
Desi nation du materiel
gaterial Name
Nodu materiel
Mater~alNumber
Company
PZBLH
EPDEC
LARYB
LASW
EPDEC
EPDDH
EPCZU
EPDBK
EPDEM
PFOPZ
lode s6rie du
lat6nel forge
orging Ser~alNo.
de lot pour trait.
bermique
eat Treat Batch No.
de materiel du fournisseur
endor Material No.
Pratt & Whitney Canada
Une r
Liste des composants moteur a numeros de serie
Engine Serialized Component Summary
PT6A-66
Nodu materiel
Mater~alNumber
450-677-941I
310752501
310923401
3109240-01
3109251-01
3112272-01
311236801
I
COUPLING-POWER,TURBINE
BUS BAR-NEGATIVE TERMINAL,T5
BUS BAR-POSITIVE TERMINAL,T5
SHAFT-POWER.TURBINE
HOUSING ASSY-PROP REDN G.B.FR.
BEARING-ROLLER FLANGED..94X1.65X.47
COUPLING-COMPRESSOR,REAR HUB
BEARING BALL,1.181X2.8345X.743,FLG
BEARING-BALL,1.450X3.600X1.000
COUPLING-POWER TURBINE SHAFT
LINER-COMB CHMBR INNER,ASYO
GOVERNOR-PROPELLER
SHAFT-STURCOMPRESSOR-ROTOR
FUEL CONTROL-TURBOPROP
CASE ASYO-GAS GENERATOR
VPLVE-CYPRESSOR BLEED, ASSY
Approve ar \
~pprove8~y
BAA
0
I
,
-
I
PCE-RKO121
Nodeserie
Serial No.
D6si nation du materiel
gaterial Name
I
: ~ ~ ; , " ~ ~ ~ ~ ~ ~ ~ ~ C a n a
J4G IAI
P I W C JR36830-E (05-1998)
Modhle
Model
W de United Technolo~nIAUnitedTsohnoloplss Mrnpany
Pran & Whisiey Canada Cie. 1
Pratt & Whitney Canada Corp.
Node serie
Serial No.
PKAAOOOR637
NR06047
NR06030
RWAOlA610
A001HEMD
FA0413771
FA0413777
FA0413780
FA0413783
FA0413785
FA0413792
:ode de trait.
iermtque
leat Code
EPBTO
avuu
EPDCB
-
Page
2
I
Carad. de montage
Build Spec NO.
I' de .&rie du
iat6nel forge
orging Serial No.
lode!ot pour trait.
hermlque
leat Treat Batch No.
de materiel du fournisseur
endor Material No.
Historique du materiel a duree'de vie limitee
Life Limited Material History Record
Pratt & Whitney Canada
Urn sad616 da Un tsd Teohmlodw/A UnnedTechnoloped Company
Nurnero d u dessin ST3582-01 - Drawing Number ST3582-01
P8WC JR3-6834-E [6834] (199846)
Dbignation du materiel
Material Name
I
:ode de traitement thermique
{eat Code
IMPELLER-CENTRIFUGAL
-
Nurnero de sene du materiel
Material Serial Number
de serie du mall. forge
aging Mat'l. Senal No.
052
nn&s sur le moteur Imodule - Engine IModule Data
Temps de
fonctionnernent
Engine IModule
Serial Number
Model
2004.07.28
Iaooroorie. selon le cas.
I
Temps de
Cydes de
fonction.
fonction.
Time Since New Cycles S~nceNew
0
0
D o n n h sur le mt&riel- Material Data
b
Temps de
mctionnement
Numero de sene
du moteur I
module
rnis le (A-M-J
$sue Date (Y-h-D)
1
PZBLH
-
Numero du materiel
Material Number
1
Pratt 8 Whitney Canada Cie. I
Pratt 8 Whitney Canada Corp.
1000. Marie-Victorin
L~ngUeUllQuebec
Canada J ~ G
1Al
depuis
I'enlevement
du maOriel
En IModule
men
Material
Removed
TEN
Cumul. de cetle installation
4ccumulated This Installahon
Cumul. jus u'8 present
Total ~ccum8atedTo Date
Date
c
remps -Time
Cycles
Temps -Time
Cycles
Observations
(Installation d'entretien de revision, bon de
trava~let timbre du venficateur)
@
:I:;
)
Remarks
(MaintenanceIOverhauI, Facility, Work
Order 8 inspection stamp)
Historique du materiel a duree de vie limitee
Life Limited Material History Record
Pratt & Whitney Canada
Urn s
d M de UnnedT.EhmlogieslAUn(tadTeohndwieaMrnpny
Nurnero du dessin ST3582-01 - Drawing Number ST3582-01
Pratt & Whitney Canada Cie. /
Pratt & Whitney Canada Corp.
1000, Marie-Victorin
L o ~ ~ u Quebec
~uI~
1Al
Canada J ~ G
&WC JR3-6634-E [6834] (199866)
Xsignation du materiel
daterial Name
Code de traitement thermique
Heat Code
NuMro de SBrie du materiel
Material Senal Number
3037001
No de serie du r@l. forge
Forgmg Marl. Senal No.
TXAI A4734
87
I
Donnees sur le rnoteur 1module - Engine IModule Data
2004.07.28
Temps de
Cycles de
fonction.
foncfron.
Time Since New Cycles Smce New
0
0
D o n n b sur le maOriel - Material Data
foncz$sment
Temps de
Numero de sBrie
dU
module
Modele
Model
Ey&el$g,"'
eEngine
IModule
Serial Number
Material
Installed
D
mis le (A-M-J
Esue Date (Y-LD)
EPDEC
ROTOR-COMPRESSOR
qumero du materiel
Material Number
Temps de
fonctionnement
depuis
I'installation du
materiel
I
PCE-RKDlZ1
PT6A-66
renpvement
du materiel
En /Module
When
Material
Removed
TEN
0
Cumul. de cette installatiqn
Accumulated This Installabon
Temps -Time
Cycles
Cumul. jus u'a prbent
Total ~ccumiatedTo Date
-
Temps Time
Cycles
Obse~ation~
Installation d'entretien, de revision, bon de
trava~let bmbre du venficateur)
Remarks
(Maintenance/Ove~t~aul,
Facility Work
&
inspection
stampj
Order
I
Historique du materiel a duree de vie limitee
Life Limited Material History Record
Pratt & Whitney Canada Cie. 1
Pratt
1000.&~arie-victorin
Whitney Canada corp.
Pratt & Whitney Canada
Une so*
& UnnedTechmlopies/A UnitsdTecnndcqie. Crmpany
Numbro du dessin ST3582-01 - Drawing Number ST3582-01
Longueull Quebec
1Al
Canada J ~ G
&WC JR34834-E (68341(199805)
Iesignationdu matbriel
flakrial Name
Code de traitement thermique
Heat Code
DISC TURBINE
mis le (A-M-J
:sue Date (Y-h-D)
LARYB
Vu&ro du materiel
Watenal Number
Num6ro de sene du materiel
Material Senal Number
3037312
NO de sene du FYI. forge
Forging Mat'l. Ser~alNo.
A001K246
Donnks
sur le moteur Imodule - Engine IModule Data
Temps de
fonctionnement NuMro de sene
de uis
du moteur I
l'instal/km du
module
materiel
En ineIModule Engine IModule
QSN m e n
Serial Number
Material
Installed
I
I
Temps de
Cycles de
fon@on.
fonction.
Time S ~ n wNew Cycles Slnw New
0
0
Donnees sur le mat6riel- Material Data
Modele
Model
0727
2004.07.28
accumulee et r6siduelle du materiel,
consulter le Manuel d'entretien du
moteur ou le Bulletin de service
l a ~ ~ r o o r iselon
b , le cas.
Date
En /Module
T!N When
Inserer le Present historique dans le livre du moteur ou du module ou la piece est install&.
Observations
Installation d'entretien de r+&o
.in,
bon de
trava~let timbre du venficateur)
Remarks
stamp) Work
(MaintenancelOverhaul.
Order & inspectionFacility,
- This record must be kept with the enginelmodule logbook where this part is installed.
Historique du materiel a duree de vie limitee
Life Limited Material History Record
Uw todOte de UnitsdT.Fhrmlodas/AUnitsdTffihnolopiesCcinpany
Numero du dessin ST3582-01 - Drawing Number ST3582-C
.
.
DCignation du matbriel
Material Name
I
:ode de traitement thermique
ieat Code
DISC-TURBINE
-
-
N u M o du magriel
Mater~alNumber
Nume~ode eerie du magriel
Matenal Senal Number
3037313
LASWY
f de sene du marl. forge
-orglng Mat'l. Senal No.
A00 1K73F
I
I
I
1
Emis le (A-M-J
Issue Date (Y-h-D)
2004.07.28
Temps de
Cycles de
fonction.
foneon.
Time Since New Cycles S~nceNew
I
I
Longueull Quebec
1Al
Canada J ~ G
accumulee et rbiduelle du pateriel.
consulter le Manue! d'entreben du
moteur ou le Bulletin de servlce
a ~ ~ r o ~ selon
r i e , le cas.
I
I
Obsetvations
(Installation d'entretien, de revision, bon de
travail et timbre du venficateur)
Modele
Model
IModule
E ~ ~ $ N e / ~ ~Engine
l e Number
Serial
Material
Installed
1
n
l
n
Donn&es sur le maYriel - Material Data
0997
D o n n b sur le moteur 1 module - Engine 1 Module Data
Temps de
fonctionnement NuMro de serie
depuis
dUmodule
mteur I
I'installation du
mateliel
Pratt & Whitney Canada Cie. I
Pratt
1000,&~Whitney
a r i e - vCanada
e r i n Corp.
Pratt & Whitney Canada
remps - Time
Remarks
(MaintenancelOverhaul. Facility, Work
Order & inspection stamp)
I
Inserer le present historique dans le livre du moteur ou du module ou la piece est install&.
- This record must be kept with the enginelmodule logbook where this part is installed.
Historique du materiel a duree de vie limitee
Life Limited Material History Record
Pratt & Whitney Canada
Une s&&6
&a Unitsd TwhrwlodesIA UnitsdTechnolwiesCompany
-
Pratt & Whitney Canada Cie. 1
Pratt & Whitney Canada Corp.
1000, Marie-Victorin
L0ngueull Quebec
1Al
Canada J ~ G
Numero du dessin ST3582-01 Drawing Number ST3582-01
LWC JR3-6834-E I68341 (199806)
Iesignation du materiel
Aaterial Name
Code de traitement thermique
Heat Code
ROTOR - COMPRESSOR
2004.07.28
EPDDH
4umero du materiel
vlatenal Number
Numb~ode sene du materiel
Matenal Senal Number
3040942
EAAAOOOF800
-
No de sene du mat'l. forge
Forging Mat'l. Senal No.
130
Cycles de
Temps de
fonction.
fonction.
Time Since New Cycles Since New
0
-
D o n n k sur le moteur / module Engine I Module Data
Temps de
ionctionnement
depuis
I'installatipn du
matenel
mis le (A-M-J
t s u e Date ( Y - k ~ )
0
Donn6es sur le materiel Material Data
foncz$sment
Temps de
de serie
I
module
dU
Ey$f$i'e
Material
Engine / Module
Serial Number
0
PCE-RKO12I
Modele
Model
Installed
PT6A-66
renl&vement
du mat6nel
En IModule
men
Material
Removed
TEN
Cumul. de cette installatiqn
Accumulated This Installabon
Temps -Time
Cycles
Cumul. jus u'a present
Total ~ccumiatedTo Date
Temps -Time
Cycles
Note: For.determination of accumulated
and remalnln lives on thls material, refer
to the en Ine%aintenance Manual or
Service 8ulletin. as applicable.
Date
Observations,
(Installation d'entretien de revision, bon de
trava~let timbre du verificateur)
Remarks
(MaintenancelOverhauI,Facility, Work
Order & inspection stamp)
0
Inserer le present historique dans le livre du moteur ou du module ou la pibce est install&. -This record must be kept with the enginelmodule logbook where Mis part is installed.
Historique du materiel a duree de vie limitee
Life Limited Material History Record
Pratt & Whitney Canada
Une d 6 t d de United T.ohmldstrlA UnltodTochndonies Company
Numero du dessin ST3582-01 - Drawing Number ST3582-01
Pratt & Whitney Canada Cie. I
Pratt & Whitney Canada Corp.
1000. Marie-Victorin
Longueull Quebec
Canada J ~ G
1Al
P&WC JRM834-E 168341 (1998-06)
r~bsignationdu magriel
Material Name
Code de traitement thermique
Heat Code
ROTOR - COMPRESSOR
Num4ro de sene du magriel
Material Senal Number
3040944
EAAAOOOF494
0
0
.
Temps de
dU
module
I
Modele
Model
Engine 1 Module
Serial Number
PCE-RK0121
PT6A-66
..
DonnCs sur le rnatbriel Material Data
foncz$Sment
de serie
Installed
0
126
Cydes de
Temps de
foneon.
fon@on.
Time Slnce New Cycles Slnce New
-
-
Donnbes sur le mteur Imodule Engine IModule Data
'T!{fi:Material
le
No de sene du rn?'I. forge
Forging Mat'l. Senal No.
accumulee et rbiduelle du magriel,
wnsulter le Manue! d'entreben du
moteur ou le Bullebn de servlce
a ~ ~ r w r iselon
e . le cas.
2004.07.28
EPCZU
Nu&ro du materiel
Material Number
Temps de
fonctionnernent
de uis
hxtalttion du
materiel
mis le (A-M-J
i s u e Date (Y-&-D)
renlevement
du materiel
En IModule
T ~m
Ne n
Material
Removed
Cumul. de cette installation
Accumulated This Installabon
Cumul. jus u'd prbsent
Total ~ccumiatedTo Date
)A:!$
Temps - Time
Cycles
Temps -Time
Cydes
Date
Observations,
(Installation d'entretien de revision, bon de
trava~let bmbre du venficateur)
Remarks
(MaintenanceIOverhaul Facility, Work
Order & inspectiohstamp)
0
Inserer le prbsent historique dans le livre du moteur ou du module ou la piece est installee. -This record must be kept with the enginelmodule logbook where this part is installed.
Historique du materiel a duree de vie limitee
Life Limited Material History Record
Pratt & Whitney Canada
Une s&O
d.UniUdT.ohmlodes/AUnbdToohndwis. Company
Nurnero du dessin ST3582-01 - Drawing Number ST3582-01
Pratt & Whitney Canada Cie. I
~ r a t&t Whitney Canada Corp.
1000 Marie-Victorin
L ~ ~ Q ' U ~Quebec
U~I
Canada J ~ G
IAl
PWC JR34834-E [MU41(199806)
)&signation du materiel
daterial Name
Code de traitement thermique
Heat Code
SHAFT-STUB,COMPRESSOR ROTOR
qumero du materiel
daterial Number
EPDBK
NuMro de sene du matbriel
Material Senal Number
3043063
No de sene du marl. forge
Forgmg Marl. Ser~alNo.
PKAAOOOL492
D o n n h sur le moteur Imodule - Engine IModule Data
Temps de
fonctionnement
de uis
l'instal&ion du
materiel
ET!t(,","Ie
mis le (A-MJ
:sue Date (Y-AD)
47
2004.07.28
Temps de
Cycles de
fonction.
foneon.
Time Since New Cycles Slnce New
0
-
0
accumul6e et r6siduelle du materiel,
consulter le Manuel d'entretien du
moteur ou le Bulletin de service
Note: For,determinationof accumulated
and remalnln lives on this material refer
to the en ine%aintenance Manual br
Service &letin, as applicable.
Donnees sur le matbriel Material Data
I
de serie
dUmodule I
Engine
IModule
Serial Number
Modele
Model
Installed
Inserer le prhsent historique dans le livre du moteur ou du d u l e ou la piece est install&.
- This record must be kept with the enginelmodulelogbook where this part is installed.
Historique du materiel a duree de vie limitee
Life Limited Material History Record
Pratt & Whitney Canada
Une sodw da unitsdT.Ehnoio~sr/A
UniWTechnologiasC a p a n y
Nurnero du dessin ST3582-01 - Drawing Number ST3582-01
NC JR36834-E [6834] (199806)
Bsignation du materiel
atenal Name
I
DISC - TURBINE
um6ro du maOriel
atenal Number
Numero de sene du materiel
Material Serial Number
3053740-01
A001K78L
mbes sur le motet Imodule - Engine IModule Data
Temps de
mtionnement
depuis
installation du
matenel
.n inelModule
QSN m e n
Material
Installed
Num6ro de serie
du moteur I
module
Engine IModule
Serial Number
I
Code de traitemnt thermique
Heat Code
32
mis le (A-M-J
k.ue Date (Y-lh-D)
1
EPDEM
No de sene du m+t'I. forge
Forgmg Mat'l. Senal No.
Pratt & Whitney Canada Cie. I
Pratt & Whitney Canada Corp.
1000 Marie-Victorin
L W ~ ~ Quebec
U ~ I
G
Canada J ~ 1Al
2004.07.28
l a ~ ~ r o ~ selon
r i e , le cas.
I
Temps de
Cycles de
fonction.
fonction.
Time Since New Cycles S~ncaNew
0
0
Donnees sur le materiel - Material Data
I
Modele
Model
Temps de
fonctionnement
Cumul. de cette installation
depuis
Accumulated This Installation
I'enlevement
du materiel
En 1Module
T
N
!
When
Material
Temps - T i m
Cycles
Removed
Cumul. jus u'A present
Total ~ccum8atedTo Date
I
Temps - T i m
Cycles
Observations
(Installation d'entretien de,rcvision, ban de
trava~let hmbre du venficateur)
Remarks
(MaintenanceQverhafl, Facility, Work
stamp)
Order & ~nspechon
Inserer le present historique dans le livre du mteur ou du module oh la piece est install&. -This record must be kept with the enginelmodule logbook where this part is installed.
Page no :
PRATT & WHITNEY CANADA
ENGINE BUILD RECORD STATUS
THE FOLLOWING SERVICE BULLETINS ARE BASIC TO :
ENGINE SERIATJ NO.
PCE-RKO121
ENGINE MODEL
PT6A- 6 6
BUILD SPEC
676
SERVICE BULLETINS
1
ENGINE SERVICE AND
MAINTENANCE RECORD
1
\
I
operation.
ITT Trim:
T5 Trim resistance:
0.0 C'
00
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TSN
Description of all operations pertaining to Airworthiness Directives,
Service Documents, Overhaul, Major or Minor Repair, and Inspections.
TSO
.
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Page 1
Date
Propeller
TSN TSO
AIC
Hrs
Description of all operations pertaining to Airworthiness Directives,
Service Documents, Overhaul, Major or Minor Repair, and Inspections.
RECORD OF ENGINE
AIRWORTHINESS DIRECTIVES IA/Dl, SERVICE BULLETINS (W,
CF-9624 TO PRECLUDEMALFUNCTION OF THE COMPRESSOR BLEED OFF VALVE
FAAAD. SB 1538R2,3344,42M. 12134, 13287 & 14251 OR THEIR LATER REVlSlO
97-04-12 OR SUPERSEDING SB INCORPORATED AT MANUFACTURE.
FOR LIST OF SB'S INCORPORATED SEE ATTACHED ENGINE BUILD RECOR
STATUS REPORT SHEET.
NAME PRINTED:
-
1
SPECIAL INSPECTIONS (SYIJ AND MODIFICATIONS (MODS]
IUN
DATE
HIS.
BROUGHT
FORWIRD
"IN.
ENGINE SERVICE AND
MAINTENANCE RECORD
I
T l Y C SINCE
INITALLITIOML.
OVERHAUL
NOTE
S
.
USE m.7~
P A a E s r-O
INSPECTIONS,
r l M A N Y L I N E S -1 . I E O Y I " T O
-0-
REPAIRS.
Y0OIFICAIIOH.I
YNU.CD
LINL. I N D A T E A N D
1
10
,,""Be"
New engine final acceptance test and
inhibiting run completed satisfactorily and is
in condition for safe operation.
1
This Gas Generator module is combined with
Power Section.
sm: PS&
ma/
1
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ITT Trim:
fl.0
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--T O T A L THIS PAGE
Y I X l Y U Y HOURS BETWEEN O V E R H A U L S
T O T A L FROM
PFtEVI0U.I I Y Y I A R I
s
TOT*L
SINCE YFO.
LlCEHCL
s'=YAT"RE
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"IN.
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ADIUSIYCNTI.
ENT
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S.
D U L L LlUL I H I O U G Y .U1
COY-LSIE
1
1
H0UI.L.
I
Page No.
TOTAL
TOTAL
TACH OR
DESCRIPTION OF WORK PERFORMEDSIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK
TIME
R M N S AVIATION lNC
GREENVILLE. SC
-
3/30/2005
LEFT ENGINE
101 Serviced engine with Mobile Jet I1 per Maintenance Manual Specifications.
The Maintenance Identified In This Work Order Package Has Been Inspected And The Item(s) Are
Approved For Return To Service. Pertinent Details Of The Repair@)Are On File At This Agency
Under Work Order No. GYH.33758/I25.
SIGNED
A ~ A T Z O NZNC...
.
GREENVZLLE.SC CRS VZBR368K
1-1
4/3/05 P ~ 6 ~ - 11
6 SN-PCE-RKO122.
6
/I #1
ENGTT: 146.4
i
CYCLES: 109
"THIS ENGINE IS PRESENTLY INSTALLED ON AIRCRAFT P-180, N-307L, SN-1091"
t-
COMPLETED 150 HOUR ENGINE MINOR INSPECTION. INSTALLED A PT6 O-RING KIT AND SERVICED ENGINE
WITH MOBIL JET I1 TURBINE OIL. SECURITY LEAK AND FUNTION CHECK PERFORMED NO FAULTS FOUND.
MAINTENANCE DONE V A N PRATT & WAITNEY PT6A-66 M/M REV-26 (9-17-04) AND THE AVANTAIR P-180 AAIP
SECTION 2 PAGE 2.
ENGINE APPROVED FOR SERVICE.
AUTHORIZED SIGNATURE
APIA
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Page No.
TOTAL
DATE
TIME
IN
SERVICE
x\
TOTAL
TIME
SINCE
OVERHAUL
TACH OR
RECORDING
METER
TIME
DESCRIPTION OF WORK PERFORMEDSIGNATURE &CERTIFICATE NO. OF PERSON PERFORMING WORK
SEEK AVIATION INC
GREENVILLE. SC
N307SL
SN 1091
3/30/2005
RIGHT ENGINE
101 Serviced engine with Mobile Jet I1 per Maintenance Manual Specifications.
The Maintenance Identified In This Work Order Package Has Been Inspected And The Item@)Are
Approved For Return To Service. Pertinent Details Of The Repair(s) Are On File At This Agency
Under Work Order No. GYH.33758A25.
SIGNED
IhC,GREENVILLE, SC CRS VIBR368K
4/3/05 PT6A-66 I/ SN-PCE-RKO121. 11 #2
ENGTT: 146.4
CYCLES: 109
*THISENGINE IS PRESENTLY INSTALLED ON AIRCRAFT P-180, N-307SL, SN-1091"
COMPLETED 150 HOUR ENGINE MINOR INSPECTION. INSTALLED A PT6 O-RING KIT AND SERVICED ENGINE
WITH MOBIL JET I1 TURBINE OIL. SECURITY LEAK AND FUNTION CHECK PERFORMED NO FAULTS POUND.
MAINTENANCE DONE IIAIW PRATT & WHITNEY PT6A-66 hUM REV-26 (9-17-04) AND THE AVANTAIR P-180 AAIP
SECTION 2 PAGE 2.
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Page No. RK PERFORMED-
HARTZELL PROPELLER N PN-HC-ESN-3AL 11 SN-HF184. I/ 146.4 {PROPTT}
*THIS PROPELLER IS PRESENTLY INSTALLED ON AIRCRAFT N-307SL, SN-10911
1
1
COMPLIED WITH 150 HOUR INSPECTION OF THE #2 RIB:PROPELLER YAlW
PIAGGIO P-180 M/MREV C7 (11130104) CHAPTER 61 AND THE AVANTAIR P-180 AAIP
SECTION 2 PAGE 2. CLEANED AND DRESSED LEADING EDGES. PAINTED PROPELLER AS
REQUIRED. SECURITY AND FUNCTION CHECK PERWORMED NO FAULTS FOUND.
PROPELLER APPROVED FOR SERVICE.
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4-03-05
HARTZELL PROPELLER N PN-HC-E5N3A /I SN-KU041. /I 146.4 {PROPTT}
"THIS PROPELLER IS PRESENTLY INSTALLED ON AIRCRAFT N-307SL, SN-1091*
COMPLIED WITH 150 HOUR INSPECTION OF THE #1 WH PROPELLER YAlW
PIAGGIO P-180 M/M REV C7 (llN0104) CHAPTER 61 AND THE AVANTAIR P-180 AMP
SECTION 2 PAGE 2. CLEANED AND DRESSED LEADING EDGES. PAINTED PROPELLER AS
REQUIRED. SECURITY AND FUNCTION CHECK PERFORMED NO FAULTS FOUND.
PROPELLER APPROVED FOR SERVICE.
AUTHORIZED SIGNATURE:
*
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Page No. -
DATE
TOTAL
TACH OR
TIME
RECORDING
IN
METER
TIME
SERVICE
I
DESCRIPTION OF WORK PERFORMEDSIGNATURE 8 CERTIFICATE NO. OF PERSON PERFORMING WORK
I
TOTAL brought forward from previous page
Date: 4-3-05
N#: 307SL
ACTT: 146.4
CYCLES: 109
LANDINGS: 109
Complied with a 150 hr "A"Check and 150 hour minor inspections on the
#1 and #2 engines in accordance with the Avantair P-180 AMP Section 11,
Page 2 and Piaggio P-180 chap-5 and Pratt & Whitney PT6A-66
Maintenance Manuals chapt-72-00-00.
1) C/W AD 2000-07-1 1 Leaking Brake Fluid by inspection satisfactory. Next d u e 296.4
2) C/W FAR 91.207 @) by inspection satisfactoty. Next due@ 4/06
10) REPLACED L/H MAIN TIRE. INSTALLED A NEW UNIT. PN= 028-357-0,
SN- 4247W00201.
11) REPLACED R/H MAIN TIRE. INSTALLED A NEW UNIT PN= 028-357-0,
SN-4247WOO188.
12) REPLACED #2 PROP, BETA BLOCK. PN= A3026.
I certify that this airframe has been inspected in accordance with a h A
Check inspection and determined to be in airworthy condition and approved
for return to service.
Signature:
-
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