Second Edition - Starman Auctions
Contents
1. l installation du N de s rie du l enl vement Accumulated This Installation Total ARCU ated To Date r vision bon de travail et timbre du v rificateur R f rence mat riel moteur module Mod le du mat riel mat riel Engine Module Engine Module Engine Module Model Eng Module Remarks TSN When p on Maintenance Overhaul Facility ateria ork Order amp Inspection Stam Material Installed Installed Removed Reference i 3 059 RK0125 PT6A 66 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 Ins rer 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 i H Pratt amp Whitney Canada Cie 7 re Pratt amp Whitney amp Whitney Canada Pratt 8 Whitney Canada Carp Pratt amp Whitney Canada amp Whitney Canada Pratt amp Whitney Canada Corp Una soci t de United Technologies United Technologies Company 7007 Chemin De La Savane Une soci t de United Technolagies A United Tachnologlas Company 7007 Chemin De La Savane St Hubert2. EPDHB N de s rie du matl forg Forging Mat Serial DISC TURBINE Num ro du mat riel Material Number 3053740 01 N de s rie du mat riel Material Serial No A001L27Y Timbre du v rificateur NIL Inspection Stamp 4 073 2 Donn es sur le moteur module Engine Module Data Donn es sur le mat riel Material Data Temps depuis Observations _ neuf Cumul de cette installation Cumul jusqu pr sent Installation d entretien de l installation du Accumulated This Installation Total Accumulated To Date r vision bon de travail et timbre du mat riel v rificateur R f rence Remarks Maintenance Overhaul Facility Work Order amp Inspection Stamp Reference Engine Module SN When Materiali Installed Cycles depuis Temps depuis neuf neuf l installation du N de s rie du 1 l enl vement mat riel moteur module Mod le du mat riel Engine Module Engine Module Model Eng Module SN When erial No TSN When Material Material Installed Removed 3 059 RK0125 PT6A 66 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 o
3. _ Serviceable Cleaned amp Inspected a 1 261302 AS3209 009 _ Fuel Flow Divider 1 9050624042 9959524042 Cleaned amp Visually inspected 7 CC LINER ASSEMBLY REMARKS Cleaned and Inspected Inner CC Liner Assembly P N 3116790 01 S N A001L2LB and Outer Liner Assembly 3055663 01 S N FTAA000A743 Results Satisfactory All Work Performed AW The Pratt amp Whitney Canada Maintenance Manual P N 3036122 Revision 30 dated Dec 8 2006 section 72 40 01 FUEL NOZZLE ASSEMBLY REMARKS Inspected Pressure Tested Spray Tested and Cross Manifold Leak Checked Fuel Manifold Assemblies Found One 1 Nozzle Tip Streaking Replaced Nozzle Tip and Re Tested Results Satisfactory All Work Performed The Pratt amp Whitney Canada Maintenance Manual P N 3036122 Revision 30 dated Dec 8 2006 section 73 10 04 and 73 11 05 repair are on file at this AIRCRAFT REG N109SL AIRCRAFT S N 1092 DISTRIBUTION 1 CUSTOMER 2 SHOP _ 3 FILE The aircraft and or component identified above was repaired and inspected in accordance with current federal air regulations This overhaul or repair does not include installation on an aircraft Pertinent details of the agency on the above work order mu DATE COMPLETED MAY 21 2007 APPROVED DATE SHIPPED Ba MCO QA 001 9 06 a Bus 0156 RP PO i 8440 Tradeport Drive Suite 105 woRK oRDER WA22290 n
4. T UT N109SL SERIAL 1092 DATE 4 16 2008 Pratt amp Whitney PT6A 66 LAC CSN 2776 _ _ SERIAL RK0125 ENGTSN SDX T0 TT POSITION 2 ENG CSN 2780 CSO Performed 150 HOUR INSPECTION in accordance with Pratt amp Whitney PT6A 66 M M 3036122 Complied with the following Scheduled inspection items 150 hr 1 Year Engine Mounts and Vibration Isolators Inspection 150 hr Applicable Portions P amp W Periodic Inspection Guide 100 hr P3 Air Filter Inspection 150 hr T Year Engine Controls Inspection 100 hr Engine Oil Filter Inspection 100 hr Engine Magnetic Chip Detector Inspection o N 300hrFuelNozzle Leak and Functional Test Complied with the following AD s and SB s None complied with at this time Performed the following Maintenance Installed A PT6 O Ring kit e Serviced Engine with BP 2380 Turbine oil Security leak and functional checks performed with no faults found Sey The above maintenance was performed in accordance with Piaggio Pratt amp Whitney and Hartzell maintenance and component aR manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with current Federal Aviation Regulations and is approved to return to service Pertinent details are on file with Avantair Inc s Quality Assurance Department Authorized Signature Z Z Certificate Number 27 5 99 2
5. LINES DATE AND TIME COLUMNS SIGNATURE ener Pes win nas NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE s EN TRIES DRAW DIAGONAL k u E i F r F a L 2 ee Arun T aq der es e NI09SL SERIAL 1092 103 w si sett AC TSN 2749 1 DATE 62607 __ Pratt amp Whimey PT6a 66 ACCSNI2H M a __ SERIAL RK0125 ENG TSN 2749 1 TSO Fu Ff POSITION 2 ENGCSN 2121 CSO T Performed 150 HOUR INSPECTION in accordance with Pratt amp Whitney PT6A 66 M M 3036122 Complied with the following Scheduled Inspection items e 150 hr l Year Engine Mounts and Vibration Isolators Inspection 150 hr Applicable Portions P amp W Periodic Inspection Guide 100 hr P3 Air Filter Inspection 150 hr l Year Engine Controls Inspection D 100 hr Engine Oil Filter Inspection 100 hr Engine Magnetic Chip Detector Inspection 300 hr Fuel Nozzle Leak and Functional Test Complied with the following AD s and SB s gt None complied with at this time m Performed the following Maintenance Installed A PT6 O Ring kit Serviced Engine with 2380 Turbine oil Security leak and functional checks performed with no faults found R R P3 Filter Element P N P 1018 250 Hour Borescope Inspection The above maintenance was performed in accordance with Pia
6. Pratt amp Whitney Canada Corp 7007 chemin de la Savane 5t Hubert Qu bec Canada 3X7 Registre de maintenance Ls Pratt amp Whitney Canada P 77 re Une seciets de United Technetescs A Uniled Technelagies Company Maintenance Log Centre de service r vision St Saint Hubert Service Centre St Hubert P amp WC 6461 2004 05 Fabricant Manufacturer N de s rie Serial No DesignationD signation Description Mod le Model PRATT AND WHITNEY TURBOPROP GAS PT6A 66 CANADA GENERATOR MODULE 125 Bon de vente Sales Order TSN CSN Depart SSN FSN 155100 4073 2 3059 N A N A Travail effectu WorkPerformed TSO SSO FSO OVERHAULED 0 0 THIS GAS GENERATOR MODULE HAS BEEN OVERHAULED MODIFIED TESTED AND PROCESSED IN PT6A 66 OVERHAUL MANUAL REV 25 DAA APPROVED DATA AND SPECIFICATION NO G PT6ALL REV 1 4 1 ALL AD S WERE VERIFIED NO AD S APPLY TO THIS MODULE 2 NEW C T BLADES QTY 43 INSTALLED THIS VISIT 3 FUEL NOZZLE SET WAS OVERHAULED IN A W PT6A 66 OVERHAUL MANUAL 4 NEW OIL AND FUEL FILTERS INSTALLED 5 AND TESTED WITH POWER SECTION MODULE S N PS RK0125 S O 155100 P T VANE RING AREA 24 02 CAVITY 252 C T VANE RING AREA 7 08 6 TEST RUN PERFORMED AND FOUND SATISFACTORY Fr CLAUDE MONGRAIN 35 C Pa SVCE CENTRE T C AMO No 20
7. Transport BB canada Aviation Second Edition January 1987 LE Transports Aviation TECHNICAL gaw Section 3 ENGINE UE ad Her Majesty the Queen in Right of Canada represented by the Minister of Public Works and Government Services 1987 Available through your local bookseller or by mail from Canadian Government Publishing Communication Canada Ottawa Ontario KIA OS9 Telephone 613 941 5995 Orders only 1 800 635 7943 Canada and U S A Fax 613 954 5779 or 1 800 565 7757 Canada and U S A Internet http publications communication gc ca Catalogue No T52 2365 3 ISBN 0 660 11857 2 Reprinted 1988 1989 1991 1993 1994 1995 1998 1999 2003 1 2 3 qq 5 Make Model Specification Manufacturer s Serial Number Date of Manufacture Aircraft Inspection Cycle ENGINE LOG Pratt amp Whitney Canada Corp PT6A 66 B S E T C E 21 pce RKO AS gt S E and ENGINE SERVICE AND MAINTENANCE RECORD 1 i TIME RUN TIME since Ey uda ares IN D MEDIE DATE a m OVERHAUL INSTALLATIONS INSPECTIONS REPAIRS ACJUSTMENTS MOOIFICATIONS LICENCE Ours om NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE CY T Ses nana DIZONEE LINE TAROUCA ANY NDS TEE ES m T SEP n B u x SIGNATURE NUMBER BROUGHT NE
8. t MAXIMUM HOURS BETWEEN OVERHAULS HOURS LICENCE NUMBER ENGINE SERVICE AND MAINTENANCE RECORD TIM SINCE TIME RUN CERTA INSTALLATIONS INSPECTIONS REPAIRS ADJUSTMENTS MODIFICATIONS DATE SIGNATURE NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE E ET US EN TRIES DRAW DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS G HRS MIN HRS MIN 5 V1I 2001 8AT 03 45 AM 002 005 o _ ALT Avantair Camarillo CMA NIO9SL _ SERIAL 1092 ACTSN 31347 j _ DATE 11 12 07 Pratt amp Whitney PT6A 66 AC CSN 2383 SERIAL RE0125 ENG TSN 3134 7_TSO LV POSITION 2 ENG CEN 2387 C50 WO 1985 150 hr Applicable Portions P amp W Periodic Inspection Guide 100 hr P3 Air Filter Inspection 100 hr Engine Oil Filter Inspection 100 hr Engine Magnetic Chip Detector Inspection a 150 br Year Engine Controls Inspection a 300 hr Fuel Nozzle Leak and Functional Test None complied with at this time LOT do owing i iarmtemsnce Installed A FTS O Ring kit Serviced Engine with BP 2380 Turbine oil a Security leak and functional checks performed with no faults found 400 Hour Borescope Inspection 8 a Th above maintenance was performed in accordance with Piageio Pratt amp Whitney amd Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or
9. t a Ar li l 5 i li i p IE f i TE 1 A d JL I A i Macr bh K p I n wn f F E c 7 iH eS RM O DES S K AL TOTAL THIS PAGE Q TOTAL FROM T MAXIMUM HOURS BETWEEN OVERHAULS HOURS PREVIOUS SUMMARY U r O Ba hs tc w I 1 A f u D a Se ENGINE SERVICE AND MAINTENANCE RECORD 2 1231 1 ji TIME RUN TIME SINCE OVERHAUL INSTALLATIONS INSPECTIONS REPAIRS ADJUSTMENTS MODIFICATIONS LICENCE DATE pcs SIGNATURE Tues waw mn NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE gt Ar 5 ENTRIES DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS NUMBER 1 RS U U I L rmm mne n8 C C Cl a arts M _ mu FORWARD M E ro o G s sa gt _ L 11 21 06 2112 DATE 08 25 06 ENG P N PT6A 66 i ENG P N PT6A 66 SN PCE RK 0125 ih E SN PCE RK0125 ENG TT 2029 9 ENG TSN 17396 0 0 ENG TC 1579 ENG CSN 1368 POSITION 42 POSITION 2 4 ACFT N109SL 1092 ACFT N109SL 1092 i i GAS GENERATOR OR COMPLIED WITH 150 HO
10. Temps depuis Observations neuf maia Cumul de cette installation Cumul jusqu pr sent Installation d entretien de l installation du N de S rie du l enl vement i i r vision bon de travail et timbre du ere du materiel moteur i module mat riel Accumulated This Installation Total Accumulated To Date v rificateur R f rence Mode Engine Module Engine Module sa Modig Remarks SN When SN When erial No N When Maintenance Overhaul Facility Material Material Work Order amp Inspection Stam Material Installed Installed Removed Reference 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 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 Pratt amp Whitney Canada Prat amp Whiney Canada Corp Historique des piece a duree de vie limit e Une soci t de United Technologies A United Technologies Company Longueuil Qu bec G Saada Life Limited Parts History Record A50 err giii Centre de revision P amp WC JR3_6904_E 2007 05 Service Center
11. N de bulletin de vente Sales Order No 155100 Overhaul Manuel amp R vision Manual amp Revision SB14002 REV 19 D signation de la pi ce Part Name mis le A M J Issue Date Y M D 2008 10 31 Temps depuis neuf Cycles depuis neuf Time Since New Cycles Since New 3 059 Code de traitement thermique Heat Code Service EPDEC de s rie du mat forg Forging Mat l Serial ROTOR COMPRESSOR Num ro du mat riel Material Number 3037001 N de s rie du mat riel Material Senal No 565 Timbre du v rificateur Inspection Stamp 8 4 073 2 Donn es sur le moteur module Engine Module Data Donn es sur le mat riel Material Data 2 Cycles depuis Observations Temps depuis neut 3P neuf See Cumul de cette installation Cumul jusqu pr sent Installation d entretien de l installation du sen du Eon Le eu Accumulated This Installation Total Accumulated To Date r vision bon de travail et timbre du mat riel v rificateur R f rence Engine Module Engine Module Remarks Engine Module When M en erial No Facility ateria ork Order amp Inspection Stam patenalinsiales Installed Reference Temps depuis neuf l enl vement Mod le du mat riel Model Eng Module TSN When Material Removed N
12. Orlando FL 32827 _ 146336 m M MAY 15 2007 RIGHT ENGINE CUSTOMER MODEL DATE SERIAL RE 6 P amp WC ESP AVANTAIR INC PT6A 66 MAY 15 2007 PCE RK0125 E onn 2643 0 N A NA 3053740 01 A001L27Y 26439 2036 PARTNUMBER ro T ary DESORPTION SNO smon CONDIIONANDIORREWORKINSTRUCTIONS 1 30394001 CT Disk Agsy 1 A027Y A001L27Y DIA REC D 9 526 Skim cut and balanced Doc LANES 4 Balance Rivet CE Balance CT Disk 1 312330201 Small Exit Duct LA ADMKWES A001KWES Serviceable clean and inspect 1 3040831 lt CT Vane Ring Assy _ LA NB6716 NB6715 FIC 3 1 311281801 No 2 Bearing Cover Ass Ab mpm spect _1 3024881 TCT Vene Ring Lock Plate 5 1 Serviceable clean and inspect __1_ 907039102 307030102 1 Sea 1 PT 1 lOnetimeue _ CT DISK ASSY REMARKS PART NUMBER 2305397401 S N AQ01L27 Y CYCLES REMAINING 5 964 SB 14002 Rev 17 Cleaned and Inspected CT Disk Assembly Pratt amp Whitney Canada Maintenance Manual P N 3036122 Rev 30 Dated Dec 08 2006 section 72 50 02 Removed Detail Weights Skim Cut and Balanced CT Disk Assembly Pratt amp Whitney Canada Overhaul Manual P N 3036123 Rev 23 Dated Dec 01 2006 Se
13. oll S N PCE RK0125 ENG TSN 2455 2 POSITION 2 ACFT N109SL 1092 ACTT 2455 2 i _ COMPLIED WITH 150 HOUR MINOR INSPECTION INSTALLED A PT6 O RING KIT SERVICED ENGINE oe WITH BP2380 TURBINE OIL SECURITY LEAK AND FUNCTION CHECKS PERFORMED WITH NO FAULTS FOUND MAINTENANCE DONE I A W PRATT amp WHITNEY PT6A 66 M M Lo ENGINE APPROVED FOR SERVICE ALS CARRIED FORWARD 4 d E L a m n A1Fa bes o KF L im T TOTAL misi v TOTAL FROM m PREVIOUS SUMMARY T TOTAL UNCLE _ MAXIMUM HOURS BETWEEN OVERHAULS HOURS r ENGINE SERVICE AND MAINTENANCE RECORD TIME SINCE TIME RUN OVERHAUL INSTALLATIONS INSPECTIONS REPAIRS ADJUSTMENTS MODIFICATIONS DATE NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE ENTRIES DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS SIGNATURE n SE SS SS rg u u u E a _ BROUGHT FORWARD LICENCE NUMBER __ NISE SERIAL 1092 AC TSN 2602 2 635 DATE 42707 Pratt amp Whitney 66 ACCSN 302 a O o o OT SERALE RKO 2ZS ENG TSN 26022 T50 POSITION 2 ENG CSN 2005 CSO Performed 150 HOUR INSPECT
14. C ss SERIAL 4 RK0125 ENG TSN 34284 TSO Re o3 POSITION 2 ENG CSN 2581 CSO ae ae Performed 150 HOUR INSPECTION in accordance with Pratt amp Whitney PT6A 66 M M 3036122 Complied with the following Scheduled Inspection items 150 hr l Year Engine Mounts and Vibration Isolators Inspection 150 hr Applicable Portions P amp W Periodic Inspection Guide 100 hr P3 Air Filter Inspection 156 hr Year Engine Controls Inspection 100 hr Engine Oil Filter Inspection 100 hr Engine Magnetic Chip Detector Inspection 300 hr Fuel Nozzle Leak and Functional Test e 400 hr Engine Borescope Inspection Complied with the following AD s and SB s e None complied with at this time Performed the following Maintenance Installed A PT6 O Ring kit e Engine with BP 2380 Turbine oil e Security leak and functional checks performed with no faults found t G The above maintenance was performed in accordance with Piaggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with current Federal Aviation Regulations and is approved to return to service Pertinent details are on file with Avantair Inc s Quality Assurance Department Authorized Signature LLL Z Certificate Number 2 SA TOTAL THIS PAGE TOTAL FROM MAXIMUM HOURS B
15. CPW 204 TEST LHV 18524 S G 0 805 72 OLL X pus PWA 521 OIL CONSUMPTION O00 T O OIL PRESSURE LI5b OIL TEMPERATURE 154 I T T TRIM DELTA T UNTRIMMED TRIMMED 0 0 I T T TRIM DELTA T UNTRIMMED TRIMMED 0 0 Ewer TRIM CLASS 20 TRIM RESISTANCE ex COLD HARNESS RESISTANCE D OU B O V SEAT CLASS AS TESTED 12 B O V SEAT CLASS AS SHIPPED 16 HANDLING AND CONTROL SETTINGS i i TRIMMED MAX NG N A UNTRIMMED MAX NG 39000 DATA PLATE SPEED 35050 IDLE SPEED 20316 ACCEL TIME F I TO MAX G T1 ENGINE DRY WEIGHT THE UNDERSIGNED CERTIFIES THAT THIS IS AN ACCURATE RECORD OF THE EVE TS DURING THE TEST OF SECTION PCE RK0125 7 2 TEST CELL OPERATOR RPM 2 47 SECS 68 6 DEGF LBS Service Centre St Hubert T C AMO Approval No 20 00 Pratt amp Whitney Canada Corp 7007 Chemin de la Savane St Hubert Quebec Canada J3Y 3X7 List of Service Bulletins and Special Instruction incorporated this visit Sales Order 159367 Module Name GAS GENERATOR MODULE Model PT6A 66 Serial Number RK0125 Customer Avantair Print Date 31 JUL 2009 Page 001 of 001 Document No Revision 4 Class Description SB 14360 000 00 3 INTERCONNECT ROD INSPECTION OF I hereby certify that the above modifications and directives have been incorporated in this engine as per the manufacturer s recommendations L MOORE C2 Authorized Inspector M PRWC SVCE CENTRE UN i a w C
16. Controls Inspection 100 hr Engine Oil Filter Inspection 100 hr Engine Magnetic Chip Detector Inspection e 300 hr Fuel Nozzle Leak and Functional Test Complied with the following AD s and SB s e None complied with at this time Performed the following Maintenance Installed A PT6 O Ring kit e Serviced Engine with BP 2380 Turbine a Security leak and functional checks performed with no faults found e R R Oil Filter Element P N 3028419 The above maintenance was performed in accordance with Piaggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with current Federal Aviation Regulations and is approved to return to service Pertinent details are on file with Avantair Inc s Quality Assurance Department LZ Lb ZO Authorized Signa Certificate Number SSE CFEC EM MM C _ _ P TOTAL THIS PAGE F Vas LI MAXIMUM HOURS BETWEEN OVERHAUL S HOURS TOTAL FROM PREVIOUS SUMMARY TOTAL LICENCE NUMBER ENGINE SERVICE AND MAINTENANCE RECORD TIME SINCE OVERHAUL INSTALLATIONS INSPECTIONS NOTE USE BOTH PAGES AND AS MANY L f c INES AS REQUIRED FOR COMPLETE HRS MIN NIOS _ SERIAL 1092 AC TSN 3428 4 WO425502 DATE 1 31 08 Pratt amp Whitney PT6A 66 LAC CSN 2577 CC C CC
17. DATE AND TIME COLUMNS I H SIGMATURE 2 SERIAL 1092 AC TSN 2895 6 WO f 1310 ERIAL RK0125 ENG TSN 2895 6 TSO 150 hr 1 Year Engine Mounts and Vibration Isolators Inspection 150 hr Applicable Portions P amp W Periodic Inspection Guide 100 hr P3 Air Filter Inspection 150 hr 1 Year Engine Controls Inspection 100 hr Engine Oil Filter Inspection 100 hr Engine Magnetic Chip Detector Inspection Fuel Nozzle Leak and Functional Test Fuel Pump inlet Screen Inspection Sundstrand Fuei Pump In Situ Inspection Engine Magnetic Chip Detector Inspection Engine Magnetic Chip Detector Bridge Inspection 400 Hr Borescope Inspection None complied with at this time Installed A PT6 O Ring kit Serviced Engine with BP 2380 Turbine oil Security Jeak and functional checks performed with no faults found R R Fuel Nozzles P N 3119855 01 R R Oil Filter Element P N 3028419 The above maintenance was performed in accordance with Piaggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with current Federal Aviation Regulations and is approved to return to service Pertinent details are on file with Avantair Inc s Quality Assurance Department m Authorized Signature Certificate Number 7 227 2 0 TOTAL SINCE MFG CARRIED FORWARD LLL
18. Gas Generator Engine Log Book 1 YELLOW CANADIAN Remarques Remarks Ver par namet mbre Checkedouby name amp stamp Dale V rfcaton inal nom et imere Final Inspection ame asamp De F CHENIER 1020 31 Oct 08 A R PEPIN SC86 31 Oct 08 NA Sans objet NR Non re u SL Non exp di TSN Temps depuis neuf TSO Temps depuis r visions Not Applicable Not Received Ship Less Time Since New Tine Since Overhaul Pratt amp Whitney Canada Cie Pratt amp Wh itney Canada Pratt amp Whitney Canada Corp Una soci t de United Technologies A United Tachnologies Company 1000 Marie Victorin Historique des pi ce dur e de vie limit e 1000 Mane Mctorin Life Limited Parts History Record J4G 1 1 450 677 9411 Centre de revision P amp WC JR3 6904 E 2007 05 Service Center D signation de la pi ce Code de traitement thermique mis le A M J N de bulletin de vente i Part ame Heat Code ende Bate Y M D Sales Order No ROTOR COMPRESSOR EPDEH 2008 10 31 155100 Overhaul Num ro du mat riel N de s rie du mat riel N de s rie du mat Temps depuis neuf Cycles depuis neuf AMANAN as Material Number Material Serial No forg Forging Mat Serial Time Since New Cycles Since New SB14002 REV 19 3040942 rat s 40732 3 059 Er Donn es sur le moteur module Engine Module Data Donn es sur le mat riel Material Data Temps depuis
19. Maintenance e Installed A PT6 O Ring kit Serviced Engine with BP 2380 Turbine oil Security leak and functional checks performed with no faults found R R Fuel Control P N 8063 016 S N Off 14066372 S N On 13991223 R R Fuel Pump P N 825601 5 S N Off 006932 S N On 0149 dance with Piaggio Pratt amp Whitney and Hartzell maintenance and component llers or Appliances stated above was repaired and inspected in accordance with Pertinent details are on file with Avantair Inc s Quality The above maintenance was performed in accor manuals The Aircraft Airframe Engines Prope current Federal Aviation Regulations and is approved to return to service Assurance Department Z Authorized Signature gt Certificate Number 8 27774 p I 1 i I 1 I I H A TOTAL THIS Pace TOTAL FROM PREVIOUS SUMMARY MAXIMUM HOURS BETWEEN OVERHAULS HOURS ENGINE SERVICE AND SS TNT n CE p TIME SINCE pare OVERHAUL INSTALLATIONS INSPECTIONS NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE nns mn EN f i TIME RUN BROUGHT FORWARD v F m l r 80g d Avantair Camarillo o CMA N109SL SERIAL 1092 AC TSN 4009 8 DATE 7 29 2008 Pratt amp Whitney PT6A 66 AC CS
20. No Material Installed poe Remarks Maintenance Overhaul Facility Work Order amp Inspection Stamp Reference Engine Module Eng Module When T N When Material Removed 4 073 2 3 059 RKO125 PT6A 66 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 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 Z Pratt amp Whitney Canada Pratt amp Whithey Canada Corp Historique des pi ce dur e de vie limit e Une soci t de United Technologies A United Technologies Company ede P ongueuil Qu bec Canada Life Limited Parts History Record 450 677 9411 Centre de revision P amp WC 6904 E 2007 05 Service Center N de bulletin de vente Sales Order No Service 155100 Overhaul Manuel amp R vision Manual amp Revision SB14002 REV 19 D signation de la pi ce Part Name mis le A M J Issue Date Y M D 2008 10 31 Temps depuis neuf Cycles depuis neuf Time Since New Cycles Since New 3 059 Code de traitement thermique Heat Code
21. Piaggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with current Federal Aviation Regulations and is approved to retum to service Pertinent details are on file with Avantair Inc s Quality Assurance Department 575 Aviation Dr Camarillo 93010 Phone 805 383 1100 Fax 805 383 2037 Signed For Avantair inc 4781 PT6A 66 Twi AL cinerem TOTAL FROM PREVIOUS SUMMARY TOTAL SINCE MFG SERIAL 1083 DATE 6 22 09 Pratt amp Whitne ES MAINTENANCE RECORD REPAIRS ST HUBERT QUEBEC T C AMO 20 00 MAXIMUM HOURS BETWEEN OVERHAULS ADJUSTMENTS MODIFICATIONS EN TRIES ORAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS LOGBOOK CLOSED BY P amp WC SERVICE CENTRE _HOURS SIGNATURE k E 20 LICENCE NUMBER I Hi 1 Un 6 r3 H Cn m Ad Pe Ji STATUS REPORT SHEET RECORD OF ENGINE AIRWORTHINESS DIRECTIVES SERVICE BULLETINS S B SPECIAL INSPECTIONS 5 1 AND MODIFICATIONS MODS T 3 DETAILS OF Wa WORK OR INSPECTION PERFORMED SIGNATURE EE J _ M d me i SIGNATURE _ LICENCE NUMBER TO PRECLUDE MALFUNCTION OF THE COMPRESSOR BLEED OFF VALVE DOT APPROVAL 4 58 SB 1538R2 3344 4204 12134 1
22. Quebec St Hubert Queb anada Canada J3Y 3X7 Liste des pi ces remplac es List of Parts Replaced Dossier qualit Quality Record Liste des pi ces remplac es List of Parts Replaced Dossier qualit Quality Record De gt Page 2 Or 2 Page 1 Of Date 31 10 2008 P amp WC JR3 6934 E 6934 2004 10 Date 31 10 2008 P amp WC JR3 6934 E 6934 2004 10 RKO125 PT6A 66 455100 551 00 Avantair 000 RK0125 PT6A 66 155100 N de la pi ce Designation de la pi ce 08 mos N dela pl c Designation de la place EXCHANGE 3119836 01 CABLE IGNITION EXCITER TO IGNITER 2 3040931CL07 COMPRESSOR TURBINE STATOR ASSY OF 3120816 01 SEAL PLAIN 865 DIA X 1 3805 X 312 1 3108781 01 HOUSING ASSY SCAVENGE PUMP 3123386 01 RING SEALING COMPRESSOR 1 3118471 01 COMPRESSOR STATOR 1ST STG ASSY OF AK66 10 Kit Assy 1 AK66 100 Kit Assy 1 NEW AK66 15 Kit Assy 1 3014791 SPRING HLCL CPRSN 572X 072X14 COILS 1 AK66 20 Kit Assy 1 3026785 TUBE FUEL PRESSURE PRIMARY ASSY OF 1 AK66 25 Kit Assy 1 3029268 FILTER ELEMENT IC AK66 30 Kit Assy 1 3032096 IGNITER IC AK66 35 Kit Assy 1 3033736 HOSE NONMETALLIC 1 AK66 40 Kit Assy 1 3036777 SEAL FACE OPTION iC AK66 45 Kit Assy 1 3038419 TUBE FUEL PRESS PRIMARY ASSY OF 1 AK66 46 Kit Assy 1 3039465CL22 SHROUD SEGMENT COMPRESSOR TURBINE 10 AK66 5 Kit Assy 1 3045458 01 OIL LEVEL SENSOR IND ATOR 1 AK66 50 Kit Assy 1 3057818 01 RING SEALING POWER TURBINE HOUSING 1 AK60 55 Kit Ass
23. de turbine de puissance Power Turbine Governor R gulateur survitesse d h lice Propeller Overspeed Governor Limiteur de couple Torque Limiter N A Valve de mise en drapeau automatique N A Auto Feather Valve G n rateur de tachym tre Tach Generator MA Livret Section Motrice Quantit Quantity Couleur Colour Type Power Section Log Book 1 YELLOW CANADIAN Sectlon du g n rateur de gaz N de s rie sur la plaque Bon de commande Gas Generator Section signal tique PCE RK0125 Order No 155100 Unit s n s de s rie Serialized Units N de pi ce Part Number N de s rie Serial Number TSN TSO Remarques Remarks Compensateur de temperature Temperature Compensator Pompe carburant Gerr Pump 8256015 5 os T50 2119 1 9 REPAIRED R gulateur de carburant Control 8063016A 6A 139903227 TSO 2119 1 9 REPAIRED changeur thermique Oil to Fuel Heater TSO 0 0 SONIS MEM changeur thermique N A Fuel to Oil Cooler Commande de d marrage N A Starting Control R gulateur d allumage haute nergie 10 381550 4 NNA04267624 TSO 0 0 OVERHAULED Vanne de d charge compresseur Compressor Eus 3059835 01 AHX001911 TSO 0 0 OVERHAULED Compressor Bleed Valve Diviseur de d bit soupage de d charge Clapet antiretour Valve 30382420 PWCO8L2678 TS0 0 0 O OVERHAULED Livret g n rateur de gaz moteur Quantit Quantity Couleur Colour Type
24. 00 October 31 2008 Date M rificateur autoris Authorized Inspects MAXIMUM HOURS BETWEEN QVERHAULS HOURS MAINTENANCE RECORD 17 REPAIRS ADJUSTMENTS MODIFICATIONS LICENCE ENTRIES DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS SIGNATURE NUMBER THE DAT TIME RUN DATE BROUGHT FORWARD m Wt Tr EE TIME SINCE OVERHAUL Ee Installed TOTAL THIS PAGE TOTAL FROM PREVIOUS SUMMARY TOTAL SINCE MFG ENGINE SERVICE AND E EEE INSTALLATIONS INSPECTIONS REPAIRS re gt __ E n cM m nFdAs mu a n Q zu Mr is ae MI n l N147SL SERIAL 4 1083 AC TSN 52452 DATE 2 14 09 Pratt amp Whitne AC CSN 3862 PT6A 66 SERIAL RK0125 TL POSITION 2 ENG CSN 3059 CRS Number V2JRO78L LEM tp GE CARRIED FORWARD a ENG TSN 4073 2 TSO 0 0 aay CSO 0 MAXIMUM HOURS MAINTENANCE RECORD ADJUSTMENTS MODIFICATIONS wis NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE F 1 ENTRIES DRAW DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS wes min dhe rs te BETWEEN OVERHAULS HOURS SIGNATURE 18 LICENCE NUMBER I FJ Il E 5 GZ SI PF CEE ENGINE SERVICE AND TIME SINCE TIM
25. 14214 14239 14272 14297 14342 DATE Page 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 10 14 POS 8440 Tradeport Drive Suite 105 SALES ORDER WA22290 m Orlando FL 32827 146336 ISSUE DATE OR REV NO DETAIL INSPECTION RECORD CRS HN4D238M unir MARCH 15 2007 RIGHT ENGINE MER CUSTO MODEL DATE m SERIAL ax P amp WC ESP AVANTAIR INC d PT6A 66 MAY 15 2007 PCE RK0125 TSN CSN TsO CSO m 2643 9 2036 N A N A 3 Tory PART mumeeR paru L ary ST smon CONDITION ANDIORREWORKINSTRUCTIONS _1_ 305560201 CCLinerAssy Outer 1 FTAA000A743 FTAA000A743 Inspected Serviceable _1 2311678001 CC Liner Assy Inner 1 A001L21B AO01L2LB Inspected Serviceable 13 311985501 303849 X 1 Duplex Fuel Nozzle Assy 42 1 Sevieable inspected Quantity 1 Streaking 1 311085601 Inlet Duplex Fuel Nozzle Assy 1 Sevioeable Cleaned Inspected amp Spray Checked 10 31029110 Nozzle Sheath 10 J Sericeable Cleaned amp Inspected 28 3024731 53209 009 28 Strainer Element 28
26. 277 CARRIED FORWARD HOURS MAXIMUM HOURS BETWEEN OVERHAULS TOTAL FROM PREVIOUS SUMMARY TOTAL SINCE MFG 14 LICENCE NUMBER ENGINE SERVICE A ND MAINTENANCE RECORD n TIME RUN E SINCE EL mes DATE RH AUL RSEN Ours min m NOTE UsE BOTH LIEN DE INSPECTIONS p o Pi es S AND AS MANY LINES AS REQUIRED FOR mmu a COMPLETE REPAIRS ADJUSTMENTS SEE Es Hese E x ENTRIES DRAW A DIAGONAL LINE THROUGH ANY n 4 SED LINES IN DATE AND TIME COLUMNS SIGNATURE NISL SERIAL 1092 AC TSN 38613 Pratt amp Whitney PT6A 66 CACCSN 288 DATE 610008 V SMALERKOUS ENGISNLS TS porion ENG CSN 2886 6001 Performed 150 HOUR INSPECTION in accordance with Pratt amp Whitney PT6A 66 M M 3036122 Complied with the following Scheduled Inspection items e 150 hr 1 Year Engine Mounts and Vibration Isolators Inspection 150 hr Applicable Portions P amp W Periodic Inspection Guide 100 hr P3 Air Filter Inspection 150 hr l Year Engine Controls Inspection 100 hr Engine Oil Filter Inspection 100 hr Engine Magnetic Chip Detector Inspection e 300 hr Fuel Nozzle Leak and Functional Test Complied with the following AD s and SE s e None complied with at this time Performed the following
27. 3287 amp 14251 OR THEIR LATER REVISION EN roses OL y o 97 04 12 OR SUPERSEDING SB INCORPORATED AT MANUFACTURE HO 044 FOR LIST OF S B S INCORPORATED SEE ATTACHED ENGINE BUILD RECORD Al Hi PX te ant Y R M UNER X ve 80 048 __ m NAME PRINTED Ses DO er ad EE m Po 2 E z ri e I i DM CONNECT Qcp iNSGEZTION OK COMPLIED WITH a ruEL cowTneL UNTT LEPLACETZENT OE QoHPLIED WITA _ Y _ a SUM 77 cui AME RR o THIS Mey _ Kerek de ATTAcHEds med hob KEINE nan LATED THIS VISITE i IBI P HH i 1 II I l x t i a l l II I I 4 l l LICENCE NUMBER P50 P50 CLAUDE MONGHA 9 awe SVCE CENTRE V Mmo Service Centre St Hubert T C AMO Approval No 20 00 Sales Order 155100 Module Name GAS GENERATOR MODULE PT6A 66 Model Serial Number RK0125 Document SB SB SB SB SB SB SB SB 14002 14360 14364 14395 14408 14411 14603 A14410 000 No 000 000 000 000 000 000 000 Revision Class 19 00 02 03 02 02 14 01 hereby certify that the engine as p
28. 39 0071 Fax 272 539 7007 Signed For Avantair Inc CARRIED FORWARD TOTAL THIS PAGE TOTAL FROM PREVIOUS SUMMARY WENN TOTAL SINCE MFG EN TRIES MAINTENANCE RECORD REPAIRS ADJUSTMENTS MODIFICATIONS DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS MAXIMUM HOURS BETWEEN OVERHAULS HOURS SIGNATURE 19 LICENCE NUMBER Hi G AH In nj Hom i DATE BROUGHT FORWARD Complied with the Following Items TIME SINCE TIME R 2 Engine Logbook N147SL Piaggio P 180 S N 1083 ENGINE SERVICE AND NOTE Airframe Hours 5475 1 2 Engine Hours 4303 1 2 Engine Cyc Lndgs 3228 Pratt amp Whitney PT6A 66 S N PCE RK 0125 WO 1165 N147SL INSTALL ATIONS USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE INSPECTIONS 06 08 2009 Airframe Landings 4031 32 000 COMPLIED WITH 2 ENGINE APPLICABLE PORTIONS OF P amp W PERIODIC INSPECTION GUIDE 150 HOUR IAW P amp W MM 72 00 00 32 001 Complied with 720007 Air Filter Inspection Engine 2 32 002 Complied with 720011 Power Turbine Blade Inspection Engine 2 32 003 Complied with 790005 Engine Oil Filter Inspection Engine 2 32 004 Complied with 790009 Engine Magnetic Chip Detector Inspection Engine 2 Maintenance Notes Complied with The above maintenance was performed in accordance with
29. AIRS ADJUSTMENTS MODIFICATIONS ENTRIES DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS t Il MAXIMUM HOURS BETWEEN OVERHAULS HOURS i 16 LICENCE NUMBER PRATT amp WHITNEY CANADA CORP P68 PROGRAM 4 4 10 uo URS maa msc ar aa kaa Han ew ei ee ua ra rs s arm M sm sa a a ui m m s s massa waw e e e e e maa ram ar aaa ma t s r rra mm mama rm maa am maa m m w m 0 mam mamam aaa fra ara maw amas maaa aa a mam mamata maa a maa aa a a sma rasa rra m u w wam w w x lt w i mmm mm m ai mm m s s mm mm u m m m m w w w F mam RE mms ms kam OR um um Luo NO ieee n 2009 JUL 31 TEST CELL 00502 TESTED AS PER OH MANUAL REV 44 APPLICABLE SB FINAL VANE FLOW AREAS REL _ _ 7 FIRST STAGE SECOND STAGE noc xd kamami BTU LB DEG F TYPE LB HR ESI DEG DEG F DEG C ERFORMANCE DATA TAKE OFF REP SPEC ACTUAL PROP SPEED 2000 2000 S L S STD DAY POWER S50 e IDIOT T5A TRIMMED DEG R 1681 1649 T5D DERIVED DEG R 1732 T635 GAS GEN SPEED RPM 35261 85050 SFC 18400 BTU LB LB SHP HR 0 691 0 660 PRESSURE RATIO 34500 RPM qu gu Teos BURL TYPE
30. Appliances stated above was repaired and inspected in accordance with Federal Aviation Regulations and is approved to return to service Pertinent details are on file with Avaritair Inc s Quality Assurance Department Authorized Signature ptf de Certificate Number R LS Le zt j Ys Ns a a HI M MAXIMUM HOURS BETWEEN OVERHAULS HOURS TOTAL FROM PREVIOUS SUMMARY TOTAL x SINCE MFG ee LICENCE NUMBER ENGINE SERVICE AND MAINTENANCE RECORD TIME RUN TIME SINCE putem OVERHAUL INSTALLATIONS INSPECTIONS REPAIRS ADJUSTMENTS MODIFICATIONS sama m ee nntu Dante amh AC IMEE AE DENIIIREN END POMBI ETF gt are ENTRIES DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS SIGNATURE r D T C m N109SL SERIAL 1092 ACTSN 32812 0 2206 DATE 12 24 07 Pran amp Whimey PT6A 66 ACCSN 2480 O 7 7 OS ENG TSN 32812 _ POSITION 2 ENGCSN 2484 CSO Z o SSS Performed 150 HOUR INSPECTION in accordance with Pratt amp Whitney PT6A 66 M M 3036122 Complied with the following Scheduled Inspection items 150 hr 1 Year Engine Mounts and Vibration Isolators Inspection 150 hr Applicable Portions P amp W Periodic Inspection Guide 100 hr P3 Air Filter Inspection 150 hr 1 Year Engine
31. D ENGINE WITH BP2380 TURBINE OIL SECURITY LEAK AND FUNTION CHECKS PERFORMED WITH NO FAULTS FOUND MAINTENANCE DONE I A W PRATT amp WHITNEY PT6A 66 M M ENGINE APPROVED FOR SERVICE AUTHORIZED SIGNATURE AvP 2542573 Im pum E g TOTAL THIS PAGE AUTHORIZED SIGNATURE MAXIMUM HOURS BETWEEN OVERHAULS HOURS TOTAL FROM PREVIOUS SUMMARY TOTAL SINCE MFG ENGINE SERVICE AND MAINTENANCE RECORD TIME RUN TIME SINCE REPAIRS ADJUSTMENTS MODIFICATIONS Mm ORTE OVERHAUL INSTALLATIONS INSPECTIONS SIGNATURE NUMBER 2 NOT E USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE I4 ls EN TRIES DRAW A Cl GON AL LINE THROUGH AM Y UNK SEQ LINES IN DATE ANO TIME COLUMNS Ours min p 1 rcm rm D E ER m DATE 02 04 07 ENG P N PT6A 66 S N PCE RK0125 ENG TSN 2318 7 ENG CSN 1794 POSITION 2 N109SL 1092 ACTT 2318 7 ACTC 1791 GAS GENERATOR COMPLIED WITH 150 MINOR amp 600 BORESCOPE HOUR ENGINE INSPECTIONS R R ENG FUEL NOZZLES 13 ea INSTALLED A PT6 O RING KIT SERVICED ENGINE WITH 2380 TURBINE OIL SECURITY LEAK AND FUNCTION CHECKS PERFORMED WITH NO FAULTS FOUND MAINTENANCE DONE I A W PRATT amp WHITNEY PT6A 66 MM ENGINE APPROVED FOR SERVICE AUTHORIZED SIGNATURE z Z 27 e 39 dr Dur y m mi DATE 3 18 07 d ENG P N PT6A 66
32. E RUN QVERH AUL INSTALL ATIONS INSPECTIONS DAVE Duns waw L uns NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE BROUGHT B FORWARD CERN a zum I RS er CE TT ee ll rete Ya EE ss Eu V ELS 2 Engine Logbook WO 293 N147SL 04 18 2009 IE N147SL Piaggio P 180 S N 1083 Airframe Hours 5334 5 Airframe Landings 3912 2 Engine Hours 4162 5 2 Engine Cyc Lndgs 3109 Pratt amp Whitney PT6A 66 S N PCE RK 0125 12 000 Complied with 720005 Comply with Applicable Portions P amp W Periodic Inspect Guide Engine 2 72 00 00 14 000 Complied with 720007 P3 Air Filter Inspection Engine 2 72 00 00 16 000 Complied with 720011 Power Turbine Biade Inspection Engine 2 72 00 00 18 000 Complied with 790005 Engine Oil Filter Inspection Engine 2 72 00 00 20 000 Complied with 790009 Engine Magnetic Chip Detector Inspection Engine 2 72 00 00 Complied with the Following Items The above maintenance was performed in accordance with Piaggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with current Federal Aviation Regulations and is approved to return to service Pertinent details are on file with Avantair Inc s Quality Assurance Department Certificate Number V2JRO78L 4311 General Howard Drive Clearwater FL 33762 Phone 727 5
33. ETWEEN OVERHAULS HOURS PREVIOUS SUMMARY SINCE MFG ENGINE SERVICE AND MAINTENANCE RECORD OVERHAUL INSTALLATIONS INSPECTIONS REPAIRS ADJUSTMENTS MODIFICATIONS UGH ANY UNUSED LINES IN DATE AND TIME COLUMNS Mi NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE sa ENTRIES DRAW A DIAGONAL LINE THRO Hm MIN min lI O I IIS ZS s f I A A mn P e o E E E em x m TIME SINCE DATE P _ SIGNATURE N109SL SERIAL 1092 AC TSN 3578 7 DATE 3 11 08 Pratt amp Whitney PT6A 66 AC CSN 2677 SERIAL RK0125 ENG TSN 3578 7 TSO 22088 160 POSITION 2 ENG CSN 2681 CSO fC Performed 600 HOUR INSPECTION in accordance with Pratt amp Whitney PT6A 66 M M 3036122 Complied with the following Scheduled Inspection items 150 hr 1 Year Engine Mounts and Vibration Isolators Inspection 150 hr Applicable Portions P amp W Periodic Inspection Guide 100 hr P3 Air Filter Inspection 150 hr 1 Year Engine Controls Inspection 100 hr Engine Oil Filter Inspection 100 hr Engine Magnetic Chip Detector Inspection Fuel Nozzle Leak and Functional Test Fuel Pump Iniet Screen Inspection Sundstrand Fuel Pump In Situ Inspection Engine Magnetic Chip Detector Inspection Engine Magnetic Chip Detector Bridge Inspection 400 Hr Borescope Inspection s aa Complied with the follo
34. HIS IS AN HE EVENTS DURING THE TEST OF SECTION PCE RK012 ATE m TEST CELI OPERATOR CT 31 2008 INSPECTOR OR L ERTIFIED OPERATOR MR probe OF KEFER Te OVERKUAOL TEST nf 3 1 2008 31 Aal 4 20069 1 g AUDE MONGRANN ES x lt SVCE CENTRE Pratt amp Whitney Canada Cie Liste de v rifications du moteur s rie PT6A Pratt amp Whitney Canada Pratt amp Whitney Canada Corp Une soci t da United Tachrologlac United Tachnologigs Campan i PT6A Engine Check List Canada J4G 1 1 P amp WC 9442 2003 11 Conteneur Container Couvercle Cover z gt Ce moteur est muni de l quipement standard figurant sur la liste illustr es des pi ces de P amp WC sauf E exception mention e sur le pr sent document Palette Skid GOOD This unit is complete with standard equipment as listed in the P amp WC Illustrated Parts List except as noted Berceau Cradle GOOD herein Manchon Sleeve N de s rie du conteneur de m tal Metal Container SN 2 Client Customer AVANTAIR Mod le de P amp WC P amp WC Model PT6A 66 Section Motrice N de s rie sur la plaque Bon de commande signal tique P S RK0125 sales Order No 122109 Unit s n s de s rie Serialized Units N de pi ce Part Number N de s rie Serial Number TSN TSO Remarques Remarks R gulateur d h lice Propeller Governor 3118495 03 1631 2258 TSN 0 0 R gulateur
35. ION in accordance with Pratt amp Whitney PT6A 66 M M 3036122 Complied with the following Scheduled Inspection items 150 hr 1 Year Engine Mounts and Vibration Isolators inspection 150 hr Applicable Portions P amp W Periodic Inspection Guide 100 hr P3 Air Filter Inspection 150 hr Year Engine Controls Inspection 100 hr Engine Oil Filter Inspection 100 hr Engine Magnetic Chip Detector Inspection 300 hr Fuel Nozzle Leak and Functional Test Complied with the following AD s and SB s 9 None complied with at this time Performed the following Maintenance 0 e Installed A PT6 O Ring kit e Serviced Engine with BP 2380 Turbine oil Security leak and functional checks performed with no faults found The above maintenance was performed in accordance with Piaggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with current Federal Aviation Regulations and is approved to return to service Pertinent details are on file with Avantair Inc s Quality Assurance Department License Number S 29 9 2 p AUTRE HELL AH N TOTAL FROM PREVIOUS SUMMARY TOTAL 1 SINCE MFG i MAXIMUM HOURS BETWEEN OVERHAULS HOURS ENGINE SERVICE AND MAINTENANCE RECORD TIME SINCE E DIFICATIONS TUNES RER OVERHAUL INSTALLATIONS INSPECTIONS E pee R
36. N 2996 po SERIAL f RK0125 ENG TSN 4009 8 TSO POSITION 2 ENGCSN 3008 CS Performed 150 HOUR INSPECTION in accordance with Pratt amp Whitn ey PT6A 66 M M 3036122 Complied with the foll wing Scheduled Inspection items 150 hr l Year Engine Mounts and Vibration Isolators Inspection 150 hr Applicable Portions P amp W Periodic Inspection Guide 100 hr P3 Air Filter Inspection 150 hr 1 Year Engine Controls Inspection 100 hr Engine Oil Filter Inspection 100 hr Engine Magnetic Chip Detector Inspection 300 Fuel Nozzle Leak and Functional Test Complied with the following AD s and SB s None complied with at this time Performed the following Maintenance e Installed A PT6 O Ring kit e Serviced Engine with BP 2380 Turbine oil ed Security leak and functional checks performed with no faults found R R Engine Oil Filter P N 3059258 01 WO 3893 The above maintenance was performed in accordance with Piaggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with current Federal Aviation Regulations and is approved to return to service Pertinent details are on file with Avantair Inc s Quality ssurance Department fe Certificate Number 2727724 TOTAL THIS PAGE TOTAL FROM PREVIOUS SUMMARY TOTAL SINCE MFG MAINTENANCE RECORD REP
37. N NUM ma _ _ nn st Y FORWARD This Gas Generator module is combined with C Bera Q 0 o o x Power Section j New engine final acceptance test and Ko 125 D HE x New en S N PS inhibiting run completed satisfactorily and is _ G si in condition for safe operation me NG V0 2495 Rpm at _ 2 O Shp dv0 1 LE 2 HE EEE Myr FF Np FTE e n M 4 06 _ 2206 a 5 ao LT Low DIVIDER gt 203 G7 2 LEMOVED sw PIS 9 PE INSTALLED s A S fe 22072 E mom ED FUEL W022LE FLV 311 55 4 Qty 13 anb PW 3419 5 amp 04 Qty 4 _ AN 2005 Le T Dm LEPACED LVEL Control AS fer Pewee CE 14 136 7 Mo 14 365 LeHoven PA 31208 32 02 s DE Pr Ef TECA tm EE UM mmc t RN INSTALLED LL 21720832 05 sp A406E372 m E oo aa i MEN DLL L OL LL LE are aul a r E m _ gr n H I 1h 3l th 1 T M j k 1 I I ar H I e 1 li J n EET u 5 Tu k h li WIL T I j 8 ui Ht i A HE Awa 8 B Es ALT INE E Ls S V EN IE NS
38. Technolagies A United Technologies Company 1000 Marie Victorin Historique des pi ce dur e de vie limit e 1000 Mare Victorin a Life Limited Parts History Record JAG 1 1 450 677 9411 Centre de revision P amp WC JR3_6904_E 2007 05 Service Center D si i apa _M N de bulletin d t ze n de la pi ce s Co omen thermique m Kx D ud E S ide ven Service ROTOR COMPRESSOR EPDBR 2008 10 31 155100 Overhaul Manuel amp R vision Manual amp Revision SB14002 REV 19 Num ro du mat riel Material Number 3040933 N de s rie du mafl forg Forging Matl Serial N de s rie du mat riel Material Serial No EAAAO000F872 Temps depuis neuf Cycles depuis neuf Time Since New Cycles Since New 3 059 Timbre du v rificateur Inspection Stamp 13 4 073 2 Donn es sur le moteur module Engine Module Data Donn es sur le mat riel Material Data G Temps depuis neuf Cumul de cette installation l enl vement Accumulated This Installation du mat riel Observations Installation d entretien de r vision bon de travail et timbre du v rificateur R f rence Cycles depuis neuf l installation du N de s rie du mat riel moteur module Temps depuis neuf l installation du mat riel Cumul at present Mod le Total Accumulated To Date Model Engine Module Engine Module When erial
39. UR MINOR INSPECTION INSTALLED PT6 O RING KIT SERVICED ENGINE GAS GENERAT Ea WITH BP 2380 II TURBINE OIL SECURITY LEAK AND FUNCTION CHECKS PERFORMED WITH NO FAULTS WITH 150 MINOR amp 600 BORESCOPE HOUR ENGINE INSPECTIONS R R ENG FUEL AT BUND me RING KIT GINE Ee 13 ea REF P amp w DIR 08 23 06 W O 14 siad on nied FAULTS FOUND MAINTENANCE DONE I A W PRATT amp WHITNEY PT6A 66 M M NORAUVLIDI TM aI NAN ONE AWF ERAT A WHITNEY MM AND THE AVANTAIR 180 AAIP SECTION 2 EE ENGINE APPROVED FOR SERVICE MAINTENANCE 2 COMPLIED WITH ENGINE HOT SECTION INSPECTION ENGINE APPROVED FOR SERVICE lt r AUTHORIZED SIGNATURE SHOE PY pz 2 z AUTHORIZED SIGNATURE AP m lt 24 d 10 07 06 ENG P N PT6A 66 DATE 12 21 06 SN PCE RK 0125 x ENG P N PT6A 66 ENG TT 1883 0 S N PCE RK0125 e ENG TC 1470 ENG TSN 2174 1 ENG CSN 1687 GAS GENERATOR 1025141092 POSITION 2 co N109SL 1092 MPLIED WITH 150 HOUR MINOR I AI w NSPECTION INSTALI 2174 WITH BP 2380 II TURBIN TALLED A PT6 O RING KIT E OIL SECURITY LEAK AND FUNCTION CHE 1682 PERFORMED WITH NO AULTS MAINTENANCE DONE VA W PRATT amp WHITNEY PT6A 66 M M GAS GENERATOR ENGINE APPROVED FOR SERVICE COMPLIED WITH 150 HOUR MINOR INSPECTION INSTALLED A PT6 O RING KIT SERVICE
40. a o ames mu ee Ga m a em ES a w I e w w i ca w 2008 OCT 31 TEST CELL 0502 TESTED AS PER OH MANUAL REV 45 APPLICABLE SB FINAL VANE FLOW AREAS FIRST STAGE 7 08 SECOND STAGE 252 24 07 ERFORMANCE DATA TAKE OFF PART POWEE mm SPEC ACTUA SPEC ACTUAL ROP SPEED 2000 2000 2000 L S STD DAY POWER 850 850 650 T T T5A TRIMMED DEG R 1681 1651 1617 5D DERIVED DEG R 1740 1640 1605 AS GEN SPEED RPM 35150 34700 34300 FC 18400 BTU LB LB SHP HR 0 683 0 663 0 770 RESSURE RATIO 34500 RPM 7 91 7 95 FUEL TYPE CBW 204 TEST LHV 14534 BTU LB S G 817 46 DEG F OIL TYPES PWA 521 TYPE II OIL CONSUMPTION 0 0 LB HR T O OIL PRESSURE 118 9 PSI OIL TEMPERATPRE 153 DEG F I T T TRIM DELTA T UNTRIMMED TRIMMED 0 0 DEG F I T T TRIM DELTA T UNTRIMMED TR MMED 0 0 DEG I T T TRIM CLASS 20 TRIM RESISTANCE Com OHMS COLD HARNESS RESISTANCE 0 00 OHMS B O V SEAT CLASSY AS TESTED 12 B O V SEAT CLASS AS SHIPPED 16 ANDLING AND CONTROL SETTINGS Oo I n TRIMMED MAX NG N A RPM NTRIMMED MAX NG 39000 RPM DATA PLATE SPEED 34700 RPM IDLE SPEED 20175 RPM ACCEL TZME F I TO MAX T1 2 27 SECS 41 DEGF ENGINE DRY WEIGHT N A UBS THE UNDERSIGNED CERTILI IES THAT T
41. ction 72 50 02 Disk O D 9 516 Concentricity 001 Trim Weights EQ6N G27N Installed Per Data Plate EEE A E Disassembled Cleaned and Inspected Small Exit Duct Assembly Reassembled Using 10 Each New Shroud Segments P N 30394650115 1 Each New Intemal Seal Ring P N 3123386 01 and 1 Each New Power Output Seal Ring P N 3057808 01 Pre ground Shroud Segments to an Average Tip Clearance of 018 All work Performed I A W Pratt amp Whitney Canada Maintenance Manual P N 3036122 Rev 30 Dated Dec 08 2006 section 72 50 01 The aircraft and or component identified above was repaired and inspected in accordance with current federal air regulations This overhaul or repair does not include installation on an aircraft Pertinent details of the repair are on file at this agency on the above work order DATE COMPLETED MAY 21 2007 MCO QA 001 9 06 _ AIRCRAFTREG N109SL _ AIRCRAFT SIN 1092 ___ DISTRIBUTION 1 CUSTOMER 2 SHOP 3 FILE
42. er the manufactwf Authorized Inspector Pratt amp Whitney Canada Corp 7007 Chemin de la Savane St Hubert Quebec Canada J3Y 3X7 List of Service Bulletins Incorporated This Visit Customer Avantair Print Date 31 OCT 2008 Page 001 of 001 Description ROTOR COMPONENTS SERVICE LIFE INTERCONNECT ROD INSPECTION OF FUEL CONTROL UNIT REPLACEMENT OF BOLTS amp NUTS OF THE FCU CONNECTOR ROD CT ROTOR AIR SEAL REPLACEMENT OF BOLTS OF THE FCU CONNECTOR ROD REPL OF OPERATING TIME BETWEEN OVERHAUL amp HOT SPARK IGNITERS INSPECTION OF 6 3 6 6 7 S 3 3 CLAUDE MONGRAN 9 P amp WC SVCE CENTRE 14005 14027 14047 14075 14094 14106 14122 14159 14182 14218 14253 14277 14314 14353 ENGINE SERIAL NO ENGINE MODEL BUILD SPEC SERVICE BULLETINS 14013 14032 14048 14077 14096 14107 14124 14163 14189 14219 14258 14280 14317 14361 APPROVED BY PCE RK0125 PT6A 66 676 14014 14017 14019 14034 14036 14037 14051 14052 14055 14078 14080 14086 14097 14098 14100 14108 14110 14111 14125 14127 14129 14164 14165 14167 14198 14202 14207 14222 14223 14225 14259 14260 14266 14283 14289 14294 14329 14332 14333 14362 R MEUNIER PRATT amp WHITNEY CANADA ENGINE BUILD RECORD STATUS THE FOLLOWING SERVICE BULLETINS ARE BASIC TO 14021 14038 14061 14087 14101 14112 14144 14168 14213 14233 14269 14295 14337 14022 14039 14067 14089 14103 14115 14145 14169
43. ggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with current Federal Aviation Regulations and is approved to retum to service Pertinent details are on file with Avantair Inc s Quality Assurance Department i 4 oy L Authorized Signature d 4 License Number d 5 bis CARRIED FORWARD ae SS oO 4 TOTAL THIS pace MAXIMUM HOURS BETWEEN OVERHAULS TOTAL FROM PREVIOUS SUMMARY u TOTAL SINCE MFG acu Wc Tho HOURS LICENCE NUMBER TOTAL THIS PAGE TOTAL FROM PREVIOUS SUMMARY Performed the following Maintenance ll NIO09SL DATE 8 4 07 Pratt amp Whimey PIGA 66 ACCSN 2211_ SS k i POSITION 2 Performed 600 HOUR INSPECTION in accordance with Pratt amp Whitney PT6A 66 M M 3036122 Complied with the following Scheduled Inspection items Complied with the following AD s and SB s EN ENGINE SERVICE AND MAINTENANCE RECORD TIME RUN TIME SINCE OVERHAUL INSTALLATIONS INSPECTIONS REPAIRS ADJUSTMENTS MODIFICATIONS m OT c d COMPLETE win E ETE NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR 5 p ENTRIES DRAW A DIAGONAL LINE THROUGH ANY UNUSED LIMES IN
44. ota 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 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 2 Pratt amp Whitney Canada Pratt amp Whitney Canada Corp Une soci t de United Technologies A United Technologies Company 1000 Marie Victorin Historique des pi ce dur e de vie limit e 1000 Mare Victor Life Limited Parts History Record J4G 1 1 450 677 9411 Centre de revision P amp WC JR3_6904_E 2007 05 Service Center N de bulletin de vente Sales Order No Service D signation de la pi ce Part Name mis le A M J Issue Date Y M D 2008 10 31 Temps depuis neuf Cycles depuis neuf Time Since New Cycles Since New Code de traitement thermique Heat Code 155100 Overhaul Manuel amp R vision Manual amp Revision SB14002 REV 19 EPADA N de s rie du mati forg Forging Mat Serial ROTOR COMPRESSOR Num ro du mat riel Material Number Material Serial No 3040944 TXA1A5399 Donn es sur le moteur module Engine Module Data Cycles de
45. puis Temps depuis N de s rie du mat riel Timbre du v rificat 2d Tre 3995 Inspection Stamp Donn es sur le mat riel Material Data Observations Temps depuis neuf g NEURO Tm neuf Cumul de cette installation Cumul jusqu pr sent Installation d entretien de Finstallation du N de s rie du l enl vement i i r vision bon de travail et timbre du installation du mat riel module Mod le Ju malene Accumulated This Installation Total Accumulated To Date v riicateur R f rence Engine Module Engine Module Model Remarks Eng Module T SN When When erial No N When Maintenance Overhaul Facility Material Installed Material Material Work Order amp Inspection Stamp Installed Removed Reference 3 058 RK0125 PT6A 66 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 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 Pratt amp Whitney Canada Pratt amp Whitney Canada Corp Une soci t de United
46. r Service Bulletin as applicable 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 T S em Z Pratt amp Whitney Canada Pratt amp Whitney Canada Coro Historique des piece a duree de VIe limit e Une saci t da United Technologies A United Technologies Company Pp haben Life Limited Parts History Record door 3481 Centre de revision P amp WC JR3 6904 2007 05 Service Center N de bulletin de vente Sales Order No Service 155100 Overhaul Manuel amp R vision Manual amp Revision SB14002 REV 19 D signation de la pi ce Code de traitement thermique mis le A M J Part Name Heat Code Issue Date Y M D IMPELLER CENTRIFUGAL PZBLH 2008 10 31 Temps depuis neuf Cycles depuis neuf Time Since New Cycles Since New 094 4 073 2 3 059 N de s rie du mat forg Forging Matl Serial N de s rie du mat riel Material Serial No EAAA000H272 Num ro du mat riel Material Number 3036898 Timbre du v rificateur Inspection Stamp Donn es sur le moteur module Engine Module Data Donn es sur mat riel Material Data G Temps depuis ss Temps depuis instal Obren aige neuf s e 2 Cumul de cette installation Cumul jusqu pr sent Installation d entretien de
47. wing AD s and SB s e None complied with at this time Performed the following Maintenance Installed A PT6 O Ring kit Serviced Engine with BP 2380 Turbine oil Security leak and functional checks performed with no faults found R R Fuel Nozzles P N 3119855 01 WO 2875 p d The above maintenance was performed in accordance with Piaggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with Current Federal Aviation Regulations and is approved to return to service Pertinent details are on file with Avantair Inc s Quality Assurance Department Authorized Signature Certificate Number 77 PLEH T LLL LLL LL aa TOTAL THIS PAGE x i Py MAXIMUM HOURS BETWEEN OVERHAULS HOURS TOTAL FROM PREVIOUS SUMMARY TOTAL SINCE MFG 13 LICENCE NUMBER ENGINE SERVICE AND MAINTENANCE RECORD TIME SINCE FICA S TIME RUN OVE RH AUL INSTALLATIONS INSPECTIONS REPAIRS ACJUSTMENTS MODIFICATION INE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS MATE T 1 L NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE E zr ENTRIES DRAW DIAGONAL LINE ay F am i min nas mins LS quem SIGNATURE BROUt FORW 1
48. y 1 3059046 0 1 SEAL PL 9375 SFT DIAX1 4375X 312 1 3059258 01 FILTER ELEMENT OPTION IC 1 OVERHAUL 3070389 01 RING SEALING CPRSR TURBINE SHROUD 1 3024286 SPACER ASSY SCAVENGE PUMP 3070391 01 RING SEAL COMPRESSOR TURBINE VANE 1 3037278 BEARING OPTION IC 3100936 01 SPRING HELIGAL COM PR 734X 1 22X16 1 J 2008 10 31 13 52 58 31 10 2008 13 52 34 PR1 400 PW23015 fopt unig queue tmp tmfd57821031135257B 3102409 01 SPRING HELICAL COMPRESSION 1 3102685 01 ELBOW TUBE TO BOSS 4375 20 X 5625 18 1 3107549 01 TIE ROD COMPRESSOR ROTOR 375 24UNJF 1 3108085 02 SEAL AIR COMPRESSOR ROTOR 1 3109287 01 STRAINER ELEMENT OIL NOZZLE ASSY OF 1 3109686 01 SEAL TUBE RETAINING 2 3112606 01 WASHER CUP 1 467 DIA NOM 1 3112608 01 SPACER OIL SLINGER 1 3113607 01 SPRING EXPANDER 1 3118591 01 BLADE TURBINE 43 ENGINE SERVICE AMD TIME SINCE OVERHAUL INSTALLATIONS INSPECTIONS CARTE NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE TIME RUN DATE lt BROUGHT FORWAF D de SSeS rr Removed POSITION 2 S ENG CSN 3059 CSO oo M F EN l Ll BEEN TOTAL THIS PAGE s TOTAL FROM PREVIOUS SUMMARY TOTAL SINCE MFG LLL ED lt u s go D C z m CL p m
Download Pdf Manuals
Related Search