Download PT6A-66 S/N:PCE-RK0121 FINAL ACCEPTANCE TEST RECORD
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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 Ohms I TSN Description of all operations pertaining to Airworthiness Directives, Service Documents, Overhaul, Major or Minor Repair, and Inspections. TSO . . .. 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 I ITT Trim: fl.0 I C" I I --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 TSYE C~LUYN$. "IN. ( ~ U L Y /0~ & 1 0Y I1 0 ADIUSIYCNTI. ENT D ~ ~ AI W 1L O I &I 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 I SUB-TOTALS this page I I I ( TOTALS-Carry forward to next page 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. SUB-TOTALS this page TOTALS-Carry forward to next page 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. 1 I I . SUB-TOTALS t h ~ spage TOTALS-Carry forward to next page I 3 I I 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: * SUB-TOTALS this page I r I I 1 TOTALS-Carry forward to next page 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: - SUB-TOTAL this page TOTAL--Carry forward to next page