PT6A-66 S/N:PCE-RK0121 FINAL ACCEPTANCE TEST RECORD
Contents
1. Temps de E P Temps de i Ob ti onctionnemen Ari nctionnemen 2 3 servations i Num ro de s rie i Cumul de cette installati Cumul pr sent ion d i isi depuis depuis umul de cette instalation jusqu a presen Installation d entretien de r vision bon de l installation du TOM Mod le l enl vement Accumulated This Installation Total Accumulated To Date du v rificateur matne du materiel ngine Module Eng Module Remarks SN When Engine TSN When Maintenance Overhaul Facility Work Material Material Temps Time Cycles Temps Time Cycles Order amp inspection stamp Installed Removed PCE RK0121 PT6A 66 ins rer le pr sent historique dans le livre du moteur ou du module o la pi ce est install e This record must be kept with the engine module logbook where this part is installed ree z Pratt amp Whitney Canada Cie Historique du mat riel dur e de vie limit e Pratt amp Whitney Canada Pratt amp Whitney Canada Corp Life Limited Mater ial History Record Une soci t de United Technologies A United Technologies Company Longueuil Qu bec Canada J4G 1A1 Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation du mat riel Material Name DISC TURBINE Num ro du mat riel Nota Pour conna tre les dur es de2. afin ess Pratt amp Whitney Canada Cie Historique du mat riel dur e de vie limit e Pratt amp Whitney Canada Pratt amp Whitney Canada Corp H imi i 1000 Marie Victorin Life Limited Material History Record Una aa Longueuil Qu bec Canada J4G 1A1 Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation du mat riel Code de traitement thermique mis le AM Material Name Heat Code Issue Date Y M D ROTOR COMPRESSOR EPDDH 2004 07 28 Num ro du mat riel Num ro de s rie du mat riel N de s rie du matl forg Temps de Material Number Material Serial Number Forging Mat l Serial No fonction fonction Time Since New Cycles Since N 3040942 EAAA000F800 130 ime v ew Cycles Since New Donn es sur le moteur module Engine Module Data Donn es sur le mat riel Material Data Nota Pour connaitre les dur es de vie accumul e et r siduelle du mat riel consulter le Manuel d entretien du moteur ou le Bulletin de service appropri selon le cas Note For determination of accumulated and remaining lives on this material refer to the engine Maintenance Manual or Service Bulletin as applicable Temps de Temps de ent Fame da s rt fonctionnement Cumul de cette installation Cumul jusqu pr sent de l installation du modul renlevement Accumulated This Instal
3. 1 t i servations depuis i Cumul de cette installation Cumul jusqu pr sent ion d i instalation du Mod le BC Qu Accumulated This Installation Total Accumulated To Date CR d entretien de revision Don mat riel du mat riel Engine Module Eng Module Remarks SN When Engine Module TEN When Maintenanoe Overhaul Faclity Work ateria Ti Ti on s installa Removed Ternps Time Cycles Temps Time Cycles rder amp Inspec mp PCE RK0121 PT6A 66 ins rer le pr sent historique dans le livre du moteur ou du module o la pi ce est install e This record must be kept with the engine module logbook where this part is installed Historique du mat riel dur e de vie limit e i Life Limited Material History Record Pratt Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation du mat riel Materia Name DISC TURBINE mis le A M J Issue Date Y M D 2004 07 28 Code de traitement thermique Heat Code LARYB Num ro du mat riel Num ro de s rie du mat riel N de s rie du forg Temps de Cycles de Material Number Material Serial Number Forging Mat Serial No fonction Ime since New es since New 3037312 A001K246 0727 ies 0 Donn es su
4. Pour connaitre les dur es de vie accumul e et r siduelle du mat riel consulter le Manuel d entretien du moteur ou le Bulletin de service appropri selon le cas Note For determination of accumulated and remaining lives on this material refer to the engine Maintenance Manual or Service Bulletin as applicable Observations Installation d entretien de r vision bon de travail et timbre du v rificateur Remarks Maintenance Overhaul Facility Work Order amp inspection stamp Ins rer le pr sent historique dans le livre du moteur ou du module o la pi ce est install e This record must be kept with the engine module logbook where this part is installed v nee Pratt amp Whitney Canada Cie Historique du mat riel dur e de vie limit e Pratt amp Whitney Canada Pratt amp Whitney Canada Corp S 9 1000 Marie Victorin Life Limited Material History Record Une soci t de United Technologies A United Technologies Company Longueuil Quebec anada Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation du mat riel Material Name ROTOR COMPRESSOR Num ro du mat riel Nota Pour connaitre les dur es de vie accumul e et r siduelle du mat riel Code de traitement thermique Heat Code Emis le Oe Issue Date Y M D 2004 07 28 Cycles de fonction consulter le Manue d
5. M NINE DN 2927025 avantair 4 03 05 HARTZELL PROPELLER PN HC ESN 3A SN KU041 146 4 PROPTT THIS PROPELLER IS PRESENTLY INSTALLED ON AIRCRAFT N 307SL SN 1091 COMPLIED WITH 150 HOUR INSPECTION OF THE 1 L H PROPELLER PIAGGIO P 180 M M REV C7 11 30 04 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 PERFORMED NO FAULTS FOUND PROPELLER APPROVED FOR SERVICE AUTHORIZED SIGNATURE LEA APIA 4 7 26 va TOTALS Carry forward to next page TOTAL TACH OR TIME RECORDING N METEA TIME DESCRIPTION OF WORK PERFORMED SIGNATURE amp CERTIFICATE NO OF PERSON PERFORMING WORK SERVICE TOTAL brought forward from previous page Date 4 3 05 avantair N 30761 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 AAIP Section II Page 2 and Piaggio P 180 chap 5 and Pratt amp Whitney PT6A 66 Maintenance Manuals chapt 72 00 00 1 C W AD 2000 07 11 Leaking Brake Fluid by inspection satisfactory Next due _296 4 2 C W FAR 91 207 D by inspection satisfactory 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 INS
6. WIRING HARNESS ELECTRICAL DUCT TURBINE EXHAUST ASYO GEAR RING FIRST STAGE REDUCTION DISC TURBINE SHAFT PROPELLER LINER COMB CHMBR OUTER ASYO HEATER OIL TO FUEL CARRIER FIRST STAGE REDUCTION BEARING BALL FLANGED PKAAO00F386 PKAAO00R894 PKAAO00R898 PKAAO000R931 PKAA000R936 PKAA000K237 PKAA000K641 PKAA000L893 PKAA000Y202 BB0036570 BB0036572 BB0036711 PKAA000H090 PKAA000F733 NNA04267624 EAAA000H236 TXA1A4734 PKAA000N529 PKAA000N542 PKAA000N548 A001K246 A001K73F PKAA000L492 A000A116 NR01979 A001K0E5 PKAA000T242 A004K78L EAAA000C797 FTAA000A588 WA20931 PKAA000R449 BB0037040 Pratt amp Whitney Canada Prat amp Whiney Canada Corp z 2 8 Une soci t de United Technologies A United Technologies Company Marie Victorin Liste des composants moteur num ros de s rie xk TUNES Engine Serialized Component Summary ee Page 2 P amp WC JR3 6830 E 05 1998 Serial No Build Spec NO bri i i i Code de trait de s rie du N de en t pour trait ri i N du mat riel D signation du mat riel N de s rie i N de mat riel du fournisseur Material Number aterial Name Serial No thermique eab forg No thermig TASS Batch No Vendor Material No L Date 2004 07 28 Modele PT6A 66 N de s rie PCE RK0121 Caract de montage BS676 PKAAO000R637 3109239 01 BUS BAR NEGATIVE TERMINAL T5 NR06047 3109240 01 BUS BAR POSITIVE TERMINAL T
7. engine module logbook where this part is installed Historique du mat riel dur e de vie limit e Life Limited Material History Record Pratt amp Whitney Canada Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation du mat riel Material Name DISC TURBINE Num ro du mat riel Code de traitement thermique Emis le A M J Heat Code Issue Date Y M D 2004 07 28 Cycles de fonction Num ro de s rie du mat riel Material Number Material Serial Number 3037313 A001K73F Donn es sur le moteur module Engine Module Data N de s rie du mati forg Forging Mat Serial No 0997 Donn es sur le mat riel Material Data Temps de forces t f depuis en puree Senie nt Cumul de cette installation Cumul jusqu pr sent installation du modulo l enl vement Accumulated This Installation Total Accumulated To Date mat riel du mat riel i Jg Material ora Material Ti Installed Temps Time Cycles Temps Time Cycles 0 121 PT6A 66 Une soci t de United Technologies A United Technologies Company Pratt amp Whitney Canada Cie Pratt amp Whitney Canada Corp 1000 Marie Victorin Longueuil Qu bec Canada J4G 1A1 Nota
8. entretien du moteur ou le Bulletin de service appropri selon le cas Code de traitement thermique Cod mis le A M J Heat e MD Issue Date Y 2004 07 28 Temps de Cycles de fonction fonction Time Since New Cycles Since New 0 0 Donn es sur le mat riel Material Data PZBLH N de s rie du mat forg Forging Mat l Serial No 052 Num ro de s rie du mat riel Material Number Material Serial Number 3036898 EAAA000H236 Donn es sur le moteur module Engine Module Data Note For determination of accumulated and remaining lives on this material refer to the engine Maintenance Manual or Service Bulletin as applicable Gann mak fo Temps t Ob ti ctionne nctionnemen servations Num ro de s rie i s oe depuis depuis Cumul de cette installation Cumul jusqu pr sent Installation d entretien de r vision bon de l installation du rre l enl vement Accumulated This Installation Total Accumulated To Date travail et timbre du v rificateur mat riel du mat riel En iy wawa Engine Module Material Serial Number Installed Eng Module Remarks TSN Wh Maintenance Overhaul Facility Work Order amp inspection stamp ins rer le pr sent historique dans le livre du moteur ou du module o la pi ce est install e This
9. entretien du moteur ou le Bulletin de service appropri selon le cas EPDEC N de s rie du mat l forg Forging Mat i Serial No 74 Num ro de s rie du mat riel Material Number Material Serial Number 3040933 TXA1A4711 Donn es sur le moteur module Engine Module Data Temps de Temps de Num ro de s rie one instalation du Mod le l enl vement mat riel u mat riel En ht Sr Engine Module Model En K Vaule en H en Material Serial Number Material Installed Removed PCE RK0121 PT6A 66 Temps de fonction 0 Donn es sur le mat riel Material Data Note For determination of accumulated and remaining lives on this material refer to the engine Maintenance Manual or Service Bulletin as applicable Observations _ Installation d entretien de r vision bon de travail et timbre du v rificateur Cumul de cette installation Accumulated This Installation Cumul jusqu pr sent Total Accumulated To Date TEE Remarks Maintenance Overhaul Facility Work Order amp inspection stamp z 3 a a ins rer le pr sent historique dans le livre du moteur ou du module o la pi ce est install e This record must be kept with the engine module logbook where this part is installed M T CUN
10. record must be kept with the engine module logbook where this part is installed Pratt amp Whitney Canada Cie Historique du mat riel a dur e de vie limit e i Pratt amp Whitney Canada Corp Life Limited Material History Record Pratt amp WhitneyCanada 1000 Marie Victorin Une soci t de United Technologies A United Technologies Company Longueuil Qu bec Canada J4G 1A1 Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation mat riel Material Name Nota Pour connaitre les dur es de vie accumul e et r siduelle du mat riel Code de traitement thermique mis le MY Heat Code Issue Date Y M D EPDEC 2004 07 28 N de s rie du forg Temps de Cycles de Forging Mat l Serial No fonction fonction 87 consulter le Manuel d entretien du moteur ou le Bulletin de service appropri selon le cas ROTOR COMPRESSOR Num ro du mat riel Material Number 3037001 Num ro de s rie du mat riel Material Serial Number TXA1A4734 Note For determination of accumulated and remaining lives on this material refer to the engine Maintenance Manual or Service Bulletin as applicable Donn es sur le moteur module Engine Module Data Donn es sur le mat riel Material Data fonction m t f s t Ob ti lonnement Num ro de s rie
11. BP piu 3420832262 siv 43862454 HAS BEEN 40 ias eco PIN 3420832 02 s w 43301590 HAS BEEN amp LICENCE NUMBER TOTAL THIS PAGE TOTAL FROM H i CARRIED FORWARD PREVIOUS SUMMARY pn 4 TOTAL SINCE MFG MAXIMUM HOURS BETWEEN OVERHAULS HOURS mS mcis Mr A ne 4 TOTAL TOTAL TACH OR DATE TIME TIME RECORDING DESCRIPTION OF WORK PERFORMED IN SINCE METER SIGNATURE amp CERTIFICATE NO OF PERSON PERFORMING WORK SERVICE OVERHAUL TIME TOTALS brought forward from previous page OF 438 z OTE A Pes E m a eH AIT LAT YE 2 2 dz Er 4 Rep STEVENS AVIATION INC GREENVILLE SC N307SL SN 1091 3 30 2005 HM 138 3 LEFT ENGINE 101 Serviced engine with Mobile Jet 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 s Are On File At This Agency Under Work Order No GYH 33758 125 SIGNED D Af Hekk For STEVENS AVIATION INC GREENVILLE SC CRS VIBR368K avantair 4 3 05 PT6A 66 SN PCE RK0122 1 ENGTT 146 4 CYCLES 109 THIS ENGINE IS PRESENTLY INSTALLED ON AIRCRAFT P 180 N 307L SN 1091 COMPLETED 150 HOUR ENGINE MINOR INSPECTION INSTALLED A PT6 O RING KIT AND SERVICED ENGINE
12. ED 34900 RPM IDLE SPEED 222 272 RPM ACCEL TIME F I TO MAX T1 2 23 SECS 70 8 DEGF ENGINE DRY WEIGHT 452 5 LBS 2 d d 1 PRODUCTION INSPECTION SIGNATURE GOVERNMENT INSPECTOR THE UNDERSIGNED CERTIFIES THAT THIS RECORD ACCURATELY SETS FORTH THE EVENTS DURING THE TEST MADE ON T GINE THEREIN IDENTIFIED 4 58 044 k i E JUL 28 04 FOREMAN ASSY amp TEST INSP index of Engine Documentation Engine Number PCE RK0121 Document Name Quantity of Documents Final Acceptance Test Record Sheet Quantity of set X Quantity per set 1X 2 Engine Serialized Component Summary Life Limited Material History Record i H Life Limited Blades History N A Record when applicable Quantity of set X Quantity per set 1X 1 Engine Build Record Status Report SB Note 1 copy or set is staple in the SB section of the Yellow Book Engine Log Book Yellow Book Final Vibration Survey N A when applicable Authorized Released Certificate Form 24 0078 Date July 28 2004 H Note This index reflects the quantity of Shipping Documentation supplied with the engine Issue Date June 10 2000 Pratt amp Whitney Canada Cie Pratt amp Whitney Canada Corp 1000 Marie Victorin Longueuil Qu bec Canada J4G 1A1 450 677 9411 Pratt amp Whitney Canada Liste des composants moteur a num ros de s rie Engine Serialized Co
13. ES IN DATE AND TIME COLUMNS NUMBER BROUGHT FORWARD gt NNNM This Power Section module is combined with 2 o o o New engine final acceptance test completed S N M PE kal T satisfactorily and is in condition for safe operation NGNO 24 400 Rpm at 850 Shp 5V0 ITT Trim O c 5 Trim resistance CX Ohms aE ey Ee U 5 E s a j SOL SLEE Cone AND TOTAL FROM MAXIMUM HOURS BETWEEN OVERHAULS HOURS PREVIOUS SUMMARY TOTAL SINCE MFG TOTAL THIS PAGE Propeller AIG Description of all operations pertaining to Airworthiness Directives TSN TSO Hrs Service Documents Overhaul Major or Minor Repair and Inspections Baalo O ELICA NOOVA ASSENBLATA SECONDO CARTONE DO RE INCRE DESY MRE remm x rrr NRE ER TR D R irit RIAA ETRE ems cape e cem ed OE se cnn mes m wa oem toe Description of all operations pertaining to Airworthiness Directives Service Documents Overhaul Major or Minor Repair and Inspections Propeller TSN TSO Hrs H 1 P Page 1 RECORD OF ENGINE AIRWORTHINESS DIRECTIVES A D SERVICE BULLETINS 5 8 1 SPECIAL INSPECTIONS 5 1 AND MODIFICATIONS MODS DATE A D 5 8 5 1 MODS DETAILS OF 1 WORK OR IN
14. MED NO FAULTS FOUND MAINTENANCE DONE I A W PRATT amp WHITNEY PT6A 66 M M REV 26 9 17 04 AND THE AVANTAIR P 180 AAIP SECTION 2 PAGE 2 ENGINE APPROVED FOR SERVICE AUTHORIZED nime 2 Z 6 44 A TOTAL L TOTAL TACH OR TIM TIME RECORDING DATE IN SINCE METER SERVICE OVERHAUL TIME DESCRIPTION OF WORK PERFORMED SIGNATURE amp CERTIFICATE NO OF PERSON PERFORMING WORK TOTALS brought forward from Ay r E EAA I N avantair 4 03 05 HARTZELL PROPELLER PN HC ESN 3AL SN HF184 146 4 PROPTT THIS PROPELLER IS PRESENTLY INSTALLED ON AIRCRAFT N 307SL SN 1091 COMPLIED WITH 150 HOUR INSPECTION OF THE 2 R H PROPELLER l A W PIAGGIO P 180 M M REV C7 11 30 04 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 PERFORMED NO FAULTS FOUND PROPELLER APPROVED FOR SERVICE AUTHORIZED S K Qf 4 2 a SUB TOTALS this page TOTALS Carry forward to next page TOTAL TOTAL TACH OR TIME TIME RECORDING DESCRIPTION OF WORK PERFORMED IN SINCE METER SERVICE OVERHAUL TIME SIGNATURE amp CERTIFICATE NO OF PERSON PERFORMING WORK TOTALS brought forward from previous page D mm P PP 4 2 j FA
15. PRATT amp WHITNEY CANADA CORP P68 PROGR 29 ce ee ee a ee mu mm ee am ww mm em mm mm A a 9 2004 JUL 27 TEST CELL 0113 BUILD SPEC 676 ENGINE TESTED AND ACCEPTED IN ACCORDANCE WITH E amp TI 453 FINAL VANE FLOW AREAS FIRST STAGE 13529 1S5 7 18 SECOND STAGE 01466 262 24 04 PERFORMANCE DATA TAKE OFF PART POWER me cem 452 SPEC ACTUAL SPEC ACTUAL PROP SPEED A 200 2000 2000 S L S STD DAY POWER 850 850 650 I T T T5A TRIMMED DEG R 1681 1645 1597 TSD DERIVED DEG R 1720 1630 1580 GAS GEN SPEED RPM 34550 35150 34900 34150 SFC 18400 BTU LB LB SHP HR 0 683 0 656 0 754 PRESSURE RATIO 34500 RPM 7 91 7 80 FUEL TYPE CPW 204 TEST LHV 18502 BTU LB S G 0 812 81 DEG F OIL TYPE PWA 521 TYPE OIL CONSUMPTION 0 0 LB HR OIL PRESSURE 114 5 PSI OIL TEMPERATURE 150 DEG F I T T TRIM DELTA T UNTRIMMED TRIMMED 0 0 DEG F TRIM DELTA UNTRIMMED TRIMMED 0 0 DEG C I T T TRIM CLASS 20 TRIM RESISTANCE C OHMS COLD HARNESS RESISTANCE 1 44 OHMS B O V SEAT CLASS AS TESTED 13 B O V SEAT CLASS AS SHIPPED 16 2 mm mm lt Ll oL lt oc lt Z lt lt TRIMMED MAX NG N A RPM UNTRIMMED MAX NG 39000 RPM DATA PLATE SPE
16. S NR06030 3109251 01 SHAFT POWER TURBINE RWA01A610 3112272 01 HOUSING ASSY PROP REDN G B FR A001HEMD BEARING ROLLER FLANGED 94X1 65X 47 FA0413771 FA0413777 FA0413780 FA0413783 FA0413785 FA0413792 FA0413793 FA0413800 FA0413804 FA0413808 3112368 01 3112612 01 COUPLING COMPRESSOR REAR HUB PKA45W405 3112696 03 BEARING BALL 1 181X2 8345X 743 FLG FC139066 3113589 01 BEARING BALL 1 450X3 600X1 000 FA0409723 3113744 01 COUPLING POWER TURBINE SHAFT PKAAO00M574 3116790 01 LINER COMB CHMBR INNER ASYO FTAA000A165 3118495 03 GOVERNOR PROPELLER 13904897 3120663 01 SHAFT STUB COMPRESSOR ROTOR RWA01A656 3120832 02 FUEL CONTROL TURBOPROP 438624641390 75 3123229 01 CASE ASYO GAS GENERATOR RWA04A150 tae 3123532 01 Z N Approv l Approved By 2 4 A AHX001595 TET D ies i da Cie Historique du mat riel dur e de vie limit e Pratt amp Whitney Canada Pratt amp Whitney Canada Corp imi i 1000 Marie Victori Life Limited Mate rial H istory Record Une soci t de United Technologies A United Technologies Company Mr Canada J4G 1 1 Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation du mat riel Material Name IMPELLER CENTRIFUGAL Num ro du mat riel Nota Pour conna tre les dur es de vie accumul e et r siduelle du mat riel consulter le Manuel d
17. SPECTION PERFORMED RUNDEN E SIGNATURE A pone ee pe Lee LICENCE NUMBER 5 P an ot 200 CF 96 24 TO PRECLUDE MALFUNCTION OF THE COMPRESSOR BLEED OFF VALVE ae ae SB 1538R2 3344 4204 12134 13287 amp 14251 OR THEIR LATER REVISIO OR SUPERSEDING B INCORPORATED MANUFACTURE Set cicls oe ee STATUS REPORT SHEET y gia NO 044 gt E E o o o z 7 m o o m m 3 gt e m z m m e r 2 Q 2 c 11 D 44360 LON PLY WIT 0 4 Ut m Juan ENGINE SERVICE AND MAINTENANCE RECORD TIME SINCE OVERHAUL INSTALLATIONS INSPECTIONS i REPAIRS ADJUSTMENTS MODIFICATIONS DATE us 9 NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE A ENTRIES DRAW DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS SIGNAT tabs Ponwanp A i This Gas Generator module is combined with Se ER EC E Power Section EET e LXI New engine final acceptance test and DEI em a as SIN PS Rk Ojal inhibiting run completed satisfactorily and is I See SSS EENI in condition for safe operation pe NGNO 34 200 Rpm at 850 Shp 8v0 prise Tie e ITT Trim 0 c TS Trim resistance Of 2 Ohms LLL DE AERE DUE Z Ze BEET FL 2 du A
18. TALLED A NEW UNIT PN 028 357 0 SN 4247W00188 12 REPLACED 2 PROP BETA BLOCK PN A3026 I certify that this airframe has been inspected in accordance with a an A Check inspection and determined to be in airworthy condition and approved for return to service Signature APIA 6622624 SUB TOTAL this page TOTAL Carry forward to next page
19. WITH MOBIL JET II TURBINE OIL SECURITY LEAK AND FUNTION CHECK PERFORMED NO FAULTS FOUND MAINTENANCE DONE I A W PRATT amp WHITNEY PT64 66 M M REV 26 9 17 04 AND THE AVANT AIR P 180 AAIP SECTION 2 PAGE 2 ENGINE APPROVED FOR SERVICE AUTHORIZED SIGNATURE A APIA Z 6 29 Jd MEN TOTALS Carry forward to next page TOTAL TOTAL TACH OR TIME TIME RECORDING DESCRIPTION OF WORK PERFORMED IN SINCE METER SIGNATURE amp CERTIFICATE NO OF PERSON PERFORMING WORK SERVICE OVERHAUL TIME TOTALS brought forward from previous page 3 Dispel Lik 7 25 LA WA D AAAS STEVENS AVIATION INC GREENVILLE SC 3 30 2005 RIGHT ENGINE N307SL SN 1091 101 Serviced engine with Mobile Jet II 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 s Are On File At This Agency Under Work Order No GYH 33758 125 SIGNED Aled te For STEVENS A INC GREENVILLE SC CRS VIBR368K avantalr 4 3 05 PT6A 66 SN PCE RK0121 2 ENGTT 146 4 CYCLES 109 THIS ENGINE IS PRESENTLY INSTALLED ON AIRCRAFT P 180 N 307SL SN 1091 COMPLETED 150 HOUR ENGINE MINOR INSPECTION INSTALLED PT6 O RING KIT AND SERVICED ENGINE WITH MOBIL JET H TURBINE OIL SECURITY LEAK AND FUNTION CHECK PERFOR
20. ique dans le livre du moteur ou du module la pi ce est install e This record must be kept with the engine module logbook where this part is installed PRATT amp WHITNEY CANADA ENGINE BUILD RECORD STATUS THE FOLLOWING SERVICE BULLETINS ARE BASIC TO ENGINE SERIAL NO PCE RK0121 ENGINE MODEL PT6A 66 BUILD SPEC 676 SERVICE BULLETINS 14005 14013 14014 14017 14019 14021 14027 14032 14034 14036 14037 14038 14047 14048 14051 14052 14055 14061 14075 14077 14078 14080 14086 14087 14094 14096 14097 14098 14100 14101 14106 14107 14108 14110 14111 14112 14122 14124 14125 14127 14129 14144 14159 14163 14164 14165 14167 14168 14182 14189 14198 14202 14207 14213 14218 14219 14222 14223 14225 14233 14253 14258 14259 14260 14266 14269 14277 14280 14283 14289 14294 14295 14314 14317 14329 14332 14333 14337 14353 14362 NO APPROVED Eo DENIS 14022 14039 14067 14089 14103 14115 14145 14169 14214 14239 14272 14297 14342 DATE Page no 1 14025 14026 14042 14043 14071 14072 14092 14093 14104 14105 14117 14119 14147 14156 14174 14175 14215 14216 14244 14252 14273 14275 14299 14308 14344 14346 2004 08 17 ENGINE SERVICE AND MAINTENANCE RECORD 1 TINENUN TIME SINCE DATE OVERHAUL INSTALLATIONS INSPECTIONS REPAIRS ADJUSTMENTS MODIFICATIONS Larne LICENCE mns uns NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE ENTRIES ORAW A DIAGONAL LINE THROUGH ANY UNUSED LIN
21. lation Total Accumulated To Date Date mat riel du mat riel A M J Engine Moduie Engine Module Eng Module SN Wh x Maintenance ON F ility Work en i TSN When aintenance Overhaul Facility Wor Material Serial Number Material Temps Time Cycles Temps Time Cycles Order amp inspection stamp Installed Removed PCE RK0121 Observations _ Installation d entretien de r vision bon de travail et timbre du v rificateur Ins rer le pr sent historique dans le livre du moteur ou du module la pi ce est install e This record must be kept with the engine module logbook where this part is installed Pratt amp Whitney Canada Cie Historique du mat riel dur e de vie limit e Pratt amp Whitney Canada Pratt amp Whitney Canada Corp PPB u 1000 Marie Victorin Life Limited Material History Record Une soci t de United Technolgies JA United Technologies Company Longueuil Qu bec Canada J4G 1A1 Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation du mat riel Material Name COMPRESSOR Num ro du mat riel Nota Pour conna tre les dur es de vie accumul e et r siduelle du mat riel Code de traitement thermique mis le A M Heat Code M Issue Date Y M D 2004 07 28 Temps de Cycles de fonction fonction Time Since New Cycles Since New 0 0 Don
22. mponent Summary Page 4 P amp WC JR3 6830 E 05 1998 Mod le PT6A 66 N de s rie Model Caract de montage Serial No PCE RK0121 Build Spec NO BS676 Code de trait thermique Heat Code N de s rie du mat riel forg Forging Serial No N du mat riel N de lot pour trait Material Number thermique Heat Treat Batch No D signation du mat riel N de s rie aterial Name N de mat riel du fournisseur Serial No Vendor Material No 3008012 3012286 3023250 3023252 3027977 3028004 3028007 3028455 3028683 3035889 3036898 3037001 3037305 3037312 3037313 3038472 3040760 3040931CL0710 3040933 3040942 3040944 3040982CL02 3041123 3043063 3043705 01 3043825 01 3043919 01 3053085 01 3053740 01 3054489 01 3055663 01 3057249 01 3101419 01 3102227 01 GEAR PLANET SECOND STAGE REDUCTION COUPLING SHAFT FLEX 2ND STAGE RED N GEAR SUN 2STG RDCN 46 TEETH ADAPTER 1ST STAGE CARRIER CARRIER SECOND STAGE REDUCTION BEARING OPTION BEARING ROLLER FLANGED GEAR SUN 1ST STAGE REDUCTION 26 TEET GEAR RING 2ND STAGE RED N EXCITER IGNITION IMPELLER CENTRIFUGAL ROTOR COMPRESSOR GEAR PLANET 1ST STAGE REDUCTION 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
23. n es sur le mat riel Material Data consulter le Manuel d entretien du moteur ou le Bulletin de service appropri selon le cas EPCZU N de s rie du mati forg Forging Mat l Serial No 126 2 Num ro de s rie du mat riel Materia Number Material Serial Number 3040944 EAAA000F494 Donn es sur le moteur module Engine Module Data Note For determination of accumulated and remaining lives on this material refer to the engine Maintenance Manual or Service Bulletin as applicable Temps de Temps de Installed Removed fonctionnement fonctionnement A A Observations i Num ro de s rie i Cumul de cette instal ati Cumul pr sent ion n visi depuis depuis umul de cette instalation jusqu presen Installation d entretien de r vision bon de l instal ation du du moteur Mod le reni vement Accumulated This Installation Total Accumulated To Date Pate travail et timbre du v rificateur mat rie u mat riel NE Engine Module Engine Module Mode Eng Module MD Remarks SN When S rial Number TSN When Maintenance Overhaul Facility Work Material Material Temps Time Cycles Order amp inspection stamp 121 66 Ins rer le pr sent historique dans le livre du moteur ou du module o la pi ce es
24. r le mat riel Material Data 0 Donn es sur le moteur module Engine Module Data Temps de Temps de n ni Ons Num ro de s rie bros ia Cumul de cette installation Cumul jusqu pr sent l installation du cure Mod le l enl vement Accumulated This Installation Total Accumulated To Date um RE ngint i n ule bimen eger ue TEM atena Ti lt Installed Roma ved Temps Time Cycles Temps Time Cycles ne mu 0 PCE RK0121 PT6A 66 Pratt amp Whitney Canada Cie Pratt amp Whitney Canada Corp 1000 Marie Victorin Une soci t de United Technologies A United Technologies Company Longueuil Qu bec Canada J4G 1 1 Nota Pour conna tre les dur es de vie accumul e et r siduelle du mat riel consulter le Manuel d entretien du moteur ou le Bulletin de service appropri selon le cas Note For determination of accumulated and remaining lives on this material refer to the engine Maintenance Manual or Service Bulletin as applicable Observations Installation d entretien de r vision bon de travail et timbre du v rificateur Remarks Maintenance Overhaul Facility Work Order amp inspection stamp Ins rer le pr sent historique dans le livre du moteur ou du module la pi ce est install e This record must be kept with the
25. t install e This record must be kept with the engine module logbook where this part is installed os A Pratt amp Whitney Canada Cie Historique du mat riel dur e de vie limit e Pratt amp Whitney Canada Pratt amp Whitney Canada Corp aal 1000 Marie Victorin Life Limited Material History Record soci t de United Teohnologies7A United Technologies Company Longueuil Qu bec Canada J4G 1A1 Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation du mat riel Code de traitement thermique mis le Gen Material Name Heat Code Issue Date Y M D SHAFT STUB COMPRESSOR ROTOR EPDBK 2004 07 28 Num ro du mat riel Num ro de s rie du mat riel Material Number Material Serial Number 3043063 PKAA000L492 Donn es sur le moteur module Engine Module Data Nota Pour connaitre les dur es de vie accumul e et r siduelle du mat riel consulter ie Manuel d entretien du moteur ou le Bulletin de service appropri selon le cas N de s rie du mati forg Temps de Cycles de Forging Mat Serial No fonction nction 47 Time Since New Cycles Since New 0 Donn es sur le mat riel Material Data Note For determination of accumulated and remaining lives on this material refer to the engine aintenance Manual or Service Bulletin as applicable
26. vie accumul e et r siduelle du mat riel consulter le Manuel d entretien du moteur ou le Bulletin de service appropri selon le cas Code de traitement thermique mis ie AMD Heat Code D Issue Date Y 2004 07 28 Cycles de fonction 1 Num ro de s rie du mat riel Material Number Material Serial Number 3053740 01 A001K78L Donn es sur le moteur module Engine Module Data N de s rie du forg Forging Mat Serial No 32 Temps de Fc Note For determination of accumulated i i and remaining lives on this material refer to the engine Maintenance Manual or Service Bulletin as applicable Donn es sur le mat riel Material Data Temps de 1 Temps de fonctionnement fonctionnement Observations i Num ro de s rie i Cumul de cette installation Cumul jusqu pr sent ilation d entretien de r vision bon de l installation du du moteur Accumulated This Installation Total Accumulated To Date osm travail et timbre du v rificateur E materiel i e EM materal Remarks ngin ule n ule When pon TSN When Maintenance Overhaul Facility Work Material Material Order amp inspection stamp Installed Removed ins rer le pr sent histor
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