N836EA Engine Log - Power Section
SOCATA TBM 700 · Maintenance Manual
Overview
This document is a maintenance logbook for the Socata TBM 700 aircraft, specifically detailing the engine maintenance records. It includes entries for various inspections, repairs, and compliance with maintenance manuals and service bulletins.
- Engine manufacturer: Pratt & Whitney Canada Corp.
- Engine model: PT6A-66D
- Maintenance performed in accordance with TBM850 Maintenance Manual.
- Regular inspections include 100-hour and annual checks.
- No defects noted during inspections.
- Engine is certified airworthy after each inspection.
- Maintenance performed by Cutter Aviation, FAA Repair Station No. U7TR491Y.
- Work orders are filed for all maintenance activities.
Document
Source
Originally published by fluxconsole.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Maintenance Manual
- Year ·
- 2013
- File size ·
- 14 MB
- Publisher ·
- fluxconsole.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Engine model ·
- PT6A-66D
- Registration ·
- N836EA
- Serial number ·
- 657
Performance
- Total time ·
- 863.1
- Time since new ·
- 863.1
- Time since overhaul ·
- 416
What is the N836EA Engine Log - Power Section?
The N836EA Engine Log - Power Section is a maintenance manual for the SOCATA TBM 700, dated 2013.
Where does the N836EA Engine Log - Power Section come from?
This copy of the N836EA Engine Log - Power Section was originally published by fluxconsole.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the N836EA Engine Log - Power Section published?
The N836EA Engine Log - Power Section — the SOCATA TBM 700 maintenance manual on file — is dated 2013.
Most owners only have the POH. Here's the essential set for the SOCATA TBM 700.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Engine Details
The engine is a Pratt & Whitney PT6A-66D, with specific serial numbers and maintenance records.
Record of Engine Maintenance
Details of maintenance tasks performed, including inspections and repairs, are recorded with dates and times since new and overhaul.
Inspection Compliance
Maintenance activities comply with the TBM850 Maintenance Manual, including various inspection checklists.
Maintenance Run-Ups
Pre and post-inspection maintenance run-ups are performed, with no defects noted.
Authorized Signatures
Each maintenance entry is certified by an authorized individual, ensuring compliance and airworthiness.
Work Orders
Pertinent details of repairs and inspections are filed under specific work orders at the repair station.
Safety notes
- Engine must be inspected in accordance with the TBM850 Maintenance Manual.
- All disrupted systems must be restored and functionally tested.
- No defects noted during inspections must be documented.
- Airworthiness certification is required after maintenance.
Full document text
Transport Canada Transports Canada TP 14182 (Revised 05/2005) Engine Logbook "POWER SECTION MODULE LOG BOOK TC-1001185 oG o06 Canadä Volume#: Opened on: 15 FEB2013 ENGINE DETAILS 1. Manufacturer Pratt & WhitneyCanadaCorp: 2. Type/Model/Series E.T.C.E- 21 PT6A-66DB/S:/3 PS- vo 320 3. Serial Number Section 1: Record of enginemaintenance and elementary work Date --/--ļ-- 15 FEB2013 Time since new O Time since overhaul Total cycles Details of task New engine final acceptancetest completed satisfactorily and isin condition for safeoperation, JGAvntes3|245 23Asz 2o335s 2SAni 2ol3 5Ao BOAt oi3|6" So 2 2 Artt présetlArtà la SOCATA tisa ttrbépAtement Qualité oner Signature AME ACA/AMO SCA/AMO This Power Section module is combined with Gas Generator. SIN:PCE- RVO320 NGNO 34550 RPM,at ITT Trim: 850_SHP /5Ve 24.0 Co TS Trim resistance: 70•6 Ohms KPVIDOR 1401) (E) RDAHER-SOCTA sOCATA Agrément de Prodution FR- 2tG-0027| TC. 4-58 NO024 SOCATA -DEPARTENENTQUALITE VERIEICATIONatENTRETIENSTOGKAGE DAHER-SOCATA Registration Model No. Serial No. EngineMIN Engine S/N 1. 2. 3 4. N836EA TBM 700 657 PT6A-66D PCE-RVO320 CUIE>Leading the Business of Aviation Cutter Aviation San Antonio, Inc. 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 POWER SECTION RECORD ENTRY Hour Meter Total Time TSN LCSN 101.8 101.8 101.8 Page 1 of 1 COMPLIED WITH SOCATA TBM850 FIRST 100 HOUR INSPECTION AS PER SOCATA TBM850 MAINTENANCE MANUAL CHAPTER 05-20-02 INSPECTION CHECKLIST. BLENDED MINOR EROSION AND NICKS FROM FIRST STAGE COMPRESSOR BLADES AW PT6A-66D MM CHAPTER 72-30-00. COMPLIED WITH 100 HOUR INSPECTION/CHECK OF RGB CHIP DETECTOR. NO DEFECTS NOTED. PRE AND POST INSPECTION MAINTENANCE RUN-UPS WERE PERFORMED. NO DEFECTS NOTED. I CERTIFY THISENGINE HAS BEENINSPECTEDINACCORDANCEWITH THEINSTRUCTIONSAND PROCEDURES OF A FIRST 100 HOUR INSPECTION IN ACCORDANCE WITH THE TBM850 MAINTENANCE MANUAL CHAPTER 5-20-01 AND IS CONSIDERED TO BE IN AIRWORTHY CONDITION AND APPROVED FOR RETURN TO SERVICE. Pertinent details of the repair are onfile at thisrepairstationunder Work Order:11M-2494. Date: 7/29/2013 Authorized Signature: Tom Bierschwale Page 1 Section 1: Record of engine maintenance and elementary work Date --/- - /-- Time since new Time since overhaul >CUIE>Leading the Business of Aviation Cutter Aviation San Antonio, Inc. 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 Total cycles Details of task DAHER-SOCATA Registration Model No. Serial No. Engine MIN Engine SIN N836EA TBM 700 657 PT6A-66D PCE-RVO320 POWER SECTION RECORD ENTRY Hour Meter Total Time TSN CSN 195.1 195..1 195.1 Page 1of 1 COMPLIED WITH SOCATA TBM850 "A" INSPECTION AS PER SOCATA TBM850 MAINTENANCE MANUAL CHAPTER 1. 2. 05-20-02 INSPECTION CHECKLIST. COMPLIED WITH 100 HOUR RECOMMENDED COMPRESSOR AND TURBINE WASHES IAW P&W PT6A-66D MM CHAPTER 71-00-00. 3. PRE AND POST INSPECTION MAINTENANCE RUN-UPS WERE PERFORMED. NO DEFECTS NOTED. ICERTIFYTHISENGINEHASBEENINSPECTEDINACCORDANCEWITH THEINSTRUCTIONSANDPROCEDURESOF AN "A" INSPECTION IN ACCORDANCE WITH THE TBM850 MAINTENANCE MANUAL CHAPTER 5-20-01 AND IS CONSIDERED TO BE IN AIRWORTHY CONDITION AND APPROVED FOR RETURN TO SERVICE. Pertinent details of the repair are on file at this repair station under Work Order: 11M-2584. Date: 10/16/2013 Authorized Signature: Tom Bierschwale DAHER-SOCATA Registration Model No. Serial No. Engine M/N Engine S/N 1. 2 3 N836EA TBM 700 657 PT6A-66D PCE-RVO320 »CUIER>Leading the Business of Aviation Cutter Aviation San Antonio, Inc. POWER SECTION RECORD ENTRY Hour Meter 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone(210)340-6780Fax(210)384-3394 SN Total Time TSN 337.2 337.2 337.2 Page 1 of 1 COMPLIED WITH SOCATA TBM850 "B+" ANNUAL INSPECTION AS PER SOCATA TBM850 MAINTENANCE MANUAL CHAPTER 05-20-02 INSPECTION CHECKLIST. COMPLIED WITH 12 MONTHI100 HOUR INSPECTION OF MAGNETIC CHIP DETECTORS IAW PT6A-66D MM 72-00-00. NO DISCREPANCIES NOTED AT THIS TIME. COMPLIED WITH 100 HOUR RECOMMENDED COMPRESSOR AND TURBINE WASHES IAW P&W PT6A-66D MM 71-00-00. COMPLIED WITH 400 HOUR BORESCOPE INSPECTION IAW PT6A-66D MM 72-00-00. NO DISCREPANCIES NOTED AT THIS TIME. 4 5 COMPLIED WITH 400 HOUR FUEL NOZZLE CLEANING AND FLOW CHECK. PERFORMED BY VECTOR AEROSPACE (CRS-U8TR793Y). REFERENCE 8130-3 DATED 04-22-2014 UNDER VWO# 34-00719. INSTALLATION PERFORMED IAW PRATT & WHITNEY PT6A-66D MM 73-11-05. OPS/LEAK CHECK GOOD. COMPLIED WITH 200 HOUR INSPECTION OF SECOND STAGE POWER TURBINE BLADES IAW PRATT &WHITNEY 6 PT6A-66D MM 72-00-00. NO DEFECTS NOTED AT THIS TIME. INSTALLED ONE NEW FUEL NOZZLE TRANFER TUBE P/N 3011155 DURING INSTALLATION OF FUEL NOZZLES FOR CLEAN AND FLOW CHECK. PRE AND POST INSPECTION MAINTENANCE RUN-UPS WERE PERFORMED. NO DEFECTS NOTED. 7 8 I CERTIFY THIS ENGINE HAS BEEN INSPECTED IN ACCORDANCE WITH THE INSTRUCTIONS AND PROCEDURES OF AN "B+" ANNUAL INSPECTION IN ACCORDANCE WITH THE TBM850 MAINTENANCE MANUAL CHAPTER 5-20-01 AND IS CONSIDERED TO BE IN AIRWORTHY CONDITION AND APPROVED FOR RETURN TO SERVICE. Pertinent details ofthe repair are on file at this repair station under Work Order: 11M-2844. Date: 04/28/2014 Authorized Signature: Richard Kurland Signature AME ACA/AMO SCA/AMO DAHER-SOCATA Registration Model No. Serial No. Engine M/N Engine S/N N836EA TBM 7O0 657 PT6A-66D PCE-RVO320 >CUIIE>Leading the Business of Aviation Cutter Aviation San Antonio, Inc. 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 POWER SECTION RECORD ENTRY Hour Meter Total Time TSN CSN 432.1 432.1 479.3 326 Page 1of 1 1. COMPLIED WITH PRATT & WHITNEY SB 72-14474R1 ISSUED DEC. 13, 2013 INSPECTION OF THE ENGINE OIL DISCOLORATION FOR CARBON PARTICLES. FOUND TO BE WITHIN ACCEPTABLE LIMITS AND ASSESSED COLOR
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TO BE BETWEEN SAMPLE 2 AND SAMPLE 3 ON FIGURE1. NO FURTHER ACTION REQUIRED. The aircraft/component identified above was maintained or altered in accordance with current regulations of the Federal Aviation Adninistration and is approved for return to service for the work performed. All disrupted systems were restored and functionally tested in accordance with mfg's instructions. Pertinent details of the repair are on file at this repair station under Work Order: 11M-2956 Date: 07/15/2014 Authorized Signature: Richard Kurland DAHER-SOCATA Registration Model No. Serial No. Engine M/N Engine S/N 1 2 3 N836EA TBM 700 657 PT6A-66D PCE-RVO320 »CUIE>Leading the Business of Aviation Cutter Aviation San Antonio, Inc. 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 POWER SECTION RECORD ENTRY Hour Meter Total Time CSN TSOH 557.9 557.9 416 Page 1 of 1 COMPLIED WITH 100 HOUR CONTINUITY AND COCKPIT INDICATOR CHECKS OF MAGNETIC CHIP DETECTORS IAW PT6A-66D MM 72-10-00. NO DISCREPANCIES NOTED AT THIS TIME. COMPLIED WITH 100 HOUR RECOMMENDED COMPRESSOR AND TURBINE WASHES IAW P&W PT6A66D MM 71-00-00. COMPLIED WITH 200 HOUR INSPECTION OF SECOND STAGE POWER TURBINE BLADES IAW PRATT &WHITNEY PT6A-66D MM 72-50-04. NO DEFECTS NOTED AT THIS TIME. The aircraf/component identified above was maintained or altered in accordance with current regulations of the Federal Aviation Administration and is approved for return to service for the work performed. All disrupted systems were restored and functionally tested in accordance with mfg's instructions. Pertinent details of the repair are on file at this repair station under Work Order: 11M-3086 Date: 12/19/2014 Authorized Signature: Tom Bierschwale ction 1: Record of engine maintenance and elementary work Date --/--/-- Time since new DAHER Registration Model No. Serial No. Engine M/N Engine S/N N836EA TBM 700 657 PT6A-66D PCE-RV0320 Time since overhaul Total cycles Details of task >CUIILEB> Leading the Business of Aviation Cutter Aviation San Antonio, Inc. 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 POWER SECTION RECORD ENTRY Hour Meter Total Time CSN TSOH 644.2 644.2 465 Page 1 of 1 1. COMPLIED WITH SOCATA TBM850 "A+" ANNUAL INSPECTION AS PER SOCATA TBM850 MAINTENANCE MANUAL CHAPTER 05-20-02 INSPECTION CHECKLIST 2 COMPLIED WITH 12 MONTH/600 HOUR BRIDGE AND CONTINUITY CHECKS OF MAGNETIC CHIP DETECTORS IAW PT6A-66D MM CHAPTER 72-10-00. NO DEFECTS NOTED. LEAK CHECKED GOOD. COMPLIED WITH 6 MONTH/600 HOUR (HIGH HUMIDITY) CHECK OF AGB OIL PUMP INLET SCREEN IAW P&W PT6A- 66D MM CHAPTER 72-60-00. NO DEFECTS NOTED. LEAK CHECKED GOOD. COMPLIED WITH 600 HOUR FUEL INLET SCREEN INSPECTION AND CLEANING IAW P&W PT6A-66D MM CHAPTER 3 4 5 73-10-00. NO DEFECTS NOTED. LEAK CHECKED GOOD. COMPLIED WITH 600 HOUR REPLACEMENT OF FUEL PUMP OUTLET FILTER. NEW FILTER PIN AN6235-3A INSTALLED. LEAK CHECKED GOOD. PRE AND POST INSPECTION MAINTENANCE RUN-UPS WERE PERFORMED. NO DEFECTS NOTED. 6 I CERTIFY THIS ENGINE HAS BEEN INSPECTED IN ACCORDANCE WITH THE INSTRUCTIONS AND PROCEDURES OF AN "A+" ANNUAL INSPECTION IN ACCORDANCE WITH THE TBM850 MAINTENANCE MANUAL CHAPTER 5-20-02 AND IS CONSIDERED TO BE IN AIRWORTHY CONDITION AND APPROVED FOR RETURN TO SERVICE. Pertinent details of the repair are on file at this repair station under Work Order: 11M-3286. Date: 04/10/2015 Authorized Signature: Tom Bierschwale - - - Signature AM ACA/E SCA/A |DAHER |Registration Model No. Serial No. Engine MIN Engine S/N N836EA TBM 700 657 PT6A-66D PCE-RVO320 »CUIIER>Leading the Business of Aviation Cutter Aviation San Antonio, Inc. 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 POWER SECTION RECORD ENTRY Hour Meter Total Time TSN. CSN 863.1 863.1 863.1 Page 1 of 1 COMPLIED WITH SOCATA TBM850 "C" INSPECTION AS PER SOCATA TBM850 MAINTENANCE MANUAL CHAPTER 1. 05-20-02 INSPECTION CHECKLIST. COMPLIED WITH 6 MONTHI600 HOUR AGB INTERNAL OIL PUMP SCAVENGE SCREEN CHECK PER PRATT & WHITNEY PT6A-66D MM 72-60-00. NO DEFECTS NOTED. 2. COMPLIED WITH 100 HOUR RECOMMENDED COMPRESSOR WASHIRINSE AND TURBINE RINSE PER PRATT & 3. WHITNEY PT6A-66D MM 71-00-00. COMPLIED WITH 100 HOUR12 MONTH RGB AND AGB CHIP DETECTOR CHECKS/OPERATIONAL CHECKS PER PRATT & WHITNEY PT6A-66D MM 72-10-00. COMPLIED WITH 400 HOUR ENGINE FUEL NOZZLE CLEANING AND FLOW CHECK. REINSTALLED REPAIRED ONE INLET FUEL ADAPTER PIN 3119856-01, THIRTEEN REPAIRED FUEL ADAPTERS PIN 3119855-01 AND FOURTEEN 5. INSPECTED SHEATHS P/N 3119920-01 PER PRATT & WHITNEY PT6A-66D 73-11-05. OPSILEAK CHECK GOOD. REFERENCE DALLAS AIRMOTIVE, INC. (CRS-YRR4491L) 8130-3'S DATED 09-30-2015 UNDER# RPR40571. COMPLIED WITH 400 HOUR BOROSCOPE INSPECTION PER PRATT & WHITNEY PT6A-66D MM 72-00-00. CT BLADES HAVE MINOR IMPACT DAMAGE WHICH WAS FOUND TO BE WITHIN LIMITS. NO OTHER DEFECTS NOTED. 6. INSTALLED NEW LEFT AND RIGHT IGNITORS PIN CH34055 PER PRATT & WHITNEY PT6A-66D MM 74-20-00. OPS CHECK GOOD. PRE AND POST INSPECTION MAINTENANCE RUN-UPS WERE PERFORMED. NO DEFECTS NOTED. 8. 7. I CERTIFY THIS ENGINE HAS BEEN INSPECTED IN ACCORDANCE WITH THE INSTRUCTIONS AND PROCEDURES OFA "C" INSPECTION IN ACCORDANCE WITH THE TBM850 MAINTENANCE MANUAL CHAPTER 5-20-01 AND IS CONSIDERED TO BE IN AIRWORTHY CONDITION AND APPROVED FOR RETURN TO SERVICE. Pertinent details of the repair areonfile at thisrepairstation underWork Order:11M-3488. Date: 10/09/2015 Authorized Signature: Richard Kurand Sec DAHER Registration Model No. |Serial No. Engine M/N Engine S/N 1 N836EA TBM 700 657 PT6A-66D PCE-RV0320 »CIIFR>Leading the Business of Aviation Cutter Aviation San Antonio, Inc. 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 POWER SECTION RECORD ENTRY Hour Meter Total Time CSN TSOH. 994.9 994.9 715 Page 1 of 1 INSPECTED THIS ENGINE USING DAHER TBM700 MM CHAPTER 5-20-02 (STANDARD PROGRAM A INSP), 05-20- 05 (12 MONTH SPECIAL CHECKS) AND PRATT & WHITNEY PT6A-66D MM CHAPTER 72-00-00, TABLE 601 INSPECTION CHECK LISTS AS A GUIDE. INSTALLED NEW PROPELLER GOVERNOR SOLENOID VALVE PIN 3032083, SIN ARK1386T. OPS CHECKED AND 2. LEAK CHECKED GOOD. REFERENCE PT6A-66D MM CHAPTER 73-10-08. COMPLIED WITH 12 MONTHI200 HOUR ROUTINE AND MINOR INSPECTIONS AND MAINTENANCE PER PRATT& 3 WHITNEY PT6A-66D MM CHAPTER 72-00-00 TABLE 601. COMPLIED WITH 100 HOUR (SALT LADEN) COMPRESSOR AND TURBINE WASHES. REFERENCE PT6A-66D MM CHAPTER 72-00-00. COMPLIED WITH 12 MONTHI600 HOUR BRIDGE AND CONTINUITY CHECKS OF MAGNETIC CHIP DETECTOR IAW PT6A-66D MM CHAPTER 72-10-00. NO DEFECTS NOTED. LEAK CHECKED GOOD. 5 6 COMPLIED WITH 12 MONTH OPERATIONAL CHECK OF CHIP DETECTOR COCKPIT INDICATION SYSTEM. NO DEFECTS NOTED. COMPLIED WITH 12 MONTH ENGINE OIL CHANGE. SERVICED ENGINE WITH BP2380. LEAK CHECK GOOD. REFERENCED PT6A-66D MM TR 72-7 AND PRATT & WHITNEY SB 14001 R18. CONVERSION TO AEROSHELL 560 7. HTS OIL PENDING OUTCOME OF OIL AND FILTER ANALYSIS. COMPLIED WITH PRATT AND WHITNEY SB14293R3 REPLACEMENT OF EXHAUST DUCT DRAIN NIPPLE AND CAP BY INSTALLATION OF NEW PLUG P/N MS9902-04 AND GASKET PIN 3023431. 8. 9. COMPLIED WITH PRATT AND WHITNEY SB14473R3 BY INSPECTION OF TORQUE LIMITER PER SB INSTRUCTIONS. NO DEFECTS NOTED. COMPLIED WITH PRATT AND WHITNEY SB14509R1 BY INSTALLATION OF CORRECT OVERSPEED GOVERNOR MOUNT WASHERS PIN 3103007-01 PER SB INSTRUCTIONS. 11. PRE AND POST INSPECTION MAINTENANCE RUN-UPS WERE PERFORMED. NO DEFECTS NOTED. 10. The aircraft/component identified above was maintained or altered in accordance with current regulations of the Federal Aviation Administration and is approved for return to service for the work performed. All disrupted systems were restored and functionaly tested in accordance with mfg's instructions. Pertinent details of the repair are on file at this repair station under Work Order: 11M-3679. Date: 03/21/2016 Authorized Signature: Tom Berschwale DAHER Registration ModelNo. Serial No. Engine MIN Engine SIN N836EA TBM 700 657 PT6A-66D PCE-RVO320 >CUITER> Leading the Business of Aviation Cutter Aviation San Antonio, Inc. 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 POWER SECTION RECORD ENTRY Hour Meter Total Time TSN CSN 1220.9 1220.9 1220.9 Page 1 of 1 1. 2 COMPLIED WITH SOCATA TBM850 "B" INSPECTION AS PER SOCATA TBM850 MAINTENANCE MANUAL CHAPTER 05-20-03 INSPECTION CHECKLIST. COMPLIED WITH ROUTINE AND MINOR INSPECTIONS AND MAINTENANCE. REFERENCED PRATT & WHITNEY 3 PT6A-66D MM CHAPTER 72-00-00 TABLE 601. COMPLIED WITH 6 MONTH/600 HOUR AGB INTERNAL OIL PUMP SCAVENGE SCREEN CHECK. REFERENCED 4 PRATT & WHITNEY PT6A-66D MM 72-60-00. NO DEFECTS NOTED. COMPLIED WITH 100 HOUR RECOMMENDED COMPRESSOR WASH/RINSE AND TURBINE RINSE. REFERENCED PRATT & WHITNEY PT6A-66D MM 71-00-00. COMPLIED WITH 100 HOUR RGB AND AGB CHIP DETECTOR CONTINUITY CHECK AND COCKPIT INDICATION CHECK. REFERENCED PRATT & WHITNEY PT6A-66D MM 72-00-00. 5 6 COMPLIED WITH 200 HOUR CLEANING AND INSPECTION OF P3 FILTER DRAIN VALVE. REFERENCED PT6A-66D MM 73-10-07. NO DEFECTS NOTED. 7 COMPLIED WITH 400 HOUR ENGINE FUEL NOZZLE CLEANING AND FLOW CHECK. REINSTALLED INSPECTED INLET FUEL ADAPTER (1) PIN 3119856-01, INSPECTED FUEL ADAPTERS (13) PIN 3119855-01 AND INSPECTED SHEATHS (14) P/N 3119920-01 REFERENCED PRATT & VWHITNEY PT6A-66D 73-11-05. OPS/LEAK CHECK GOOD. REFERENCE VECTOR AEROSPACE (CRS-U8TR793Y) 8130-3 DATED 1 1/01/2016 UNDER WO# 36-02263. COMPLIED WITH 400 HOUR BOROSCOPE INSPECTION REFERNCED PRATT & WHITNEY PT6A-66D MM 72-00-00. HSI PERFORMED DUE TO FOD FOUND DURING BORESCOPE. COMPLIED WITH 600 HOUR INSPECTION OF FUEL PUMP INLET SCREEN FOR FOREIGN MATTER OR 8 9 DISTORTION. REFERENCED PRATT & WHITNEY PT6A-66D MM 73-10-02. NO DEFECTS NOTED. COMPLIED WITH 600 HOUR INSPECTION OF FUEL PUMP OUTLET FILTER FOR FOREIGN MATTER OR DISTORTION. REFERENCED PRATT & WHITNEY PT6A-66D MM 73-10-02. 10. 11. COMPLIED WITH 1750 HOUR HOT SECTION INSPECTION. INSTALLED "NEW OUTER COMBUSTION LINER PIN 3055663-01, SIN FTA663A0368, "REPAIRED" IE DUCT P/IN 3123302-01, SIN RWA98D809, "REPAIRED" CT DISK PIN 3053740-01, S/N YUAA012A581, "INSPECTED" INNER COMBUSTION LINER PIN 3116790-01, S/N RWA96D374 AND NEW ITT PROBE P/N 3116132-01. REFERENCED PRATT & WHITNEY PT6A-66D MM 72-00-00 TABLE 603, 72-40-01, 72-50-01 AND 72-50-02. PERFORMED GROUND PERFORMANCE RUN, OPS CHECKS AND LEAK CHECKS WITH SATISFACTORY RESULTS. PERORMANCE RUN RESULTS ON FILE UNDER THISWNO#. COMPLIED WITH PRATT & WHITNEY SB 14489 REPLACEMENT OF SAFETY CABLE. FOUND PREVIOUSLY COMPLIED WITH. 12. 13. PRATT & WHITNEY SB14357 R4 INSPECTION OF FUEL NOZZLE ASSEMBLY AND SB14495R3 INSPECTION OF FUEL NOZZLE TIPS COMPLIED WITH BY VECTOR AEROSPACE DURING 400 HOUR CLEANING AND FLOW CHECK. REFERENCE THEIR 8130-3 DATED 11/01/2016 UNDER WO# 36-02263. 14. PRE AND POST INSPECTION MAINTENANCE RUN-UPS WERE PERFORMED. NO DEFECTS NOTED. I CERTIFY THIS ENGINE HAS BEEN INSPECTED IN ACCORDANCE WITH THE INSTRUCTIONS AND PROCEDURES OF A "B" INSPECTION IN ACCORDANCE WTH THE TBM850 MAINTENANCE MANUAL CHAPTER 5-20-01 AND IS CONSIDERED TO BE IN AIRWORTHY CONDITION AND APPROVED FOR RETURN TO SERVICE. Pertinent details of the repair are on file at this repair station under Work Order: 11M-3942. Date: 12/06/2016 Authorized Signature: Richard Kurland AME AVAMO WAMO Sectic |AHERRegistration Model No. Serial No. Engine M/N Engine S/N 1 N836EA TBM.700 657 PT6A-66D PCE-RVO320 CIIER>Leading the Business of Aviation Cutter Aviation San Antonio, Inc. 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 POWER SECTION RECORD ENTRY Hour Meter Total Time CSN TSOH 1311.8 1311.8 969 Page 1 of 1 INSPECTED THIS ENGINE USING DAHER TBM700 MM CHAPTER 5-20-02 (STANDARD PROGRAM A INSP), 05-20- 05 (12 MONTH SPECIAL CHECKS) AND PRATT & WHITNEY PT6A-66D MM CHAPTER 72-00-00, TABLE 601 INSPECTION CHECK LISTS AS A GUIDE. COMPLIED WITH 12 MONTHI200 HOUR ROUTINE AND MINOR INSPECTIONS AND MAINTENANCE PER PRATT & WHITNEY PT6A-66D MM CHAPTER 72-00-00 TABLE 601. COMPLIED WITH 12 MONTHI600 HOUR BRIDGE AND CONTINUITY CHECKS OF MAGNETIC CHIP DETECTOR IAW PT6A-66D MM CHAPTER 72-10-00. NO DEFECTS NOTED. LEAK CHECKED GOOD. COMPLIED WITH 100 HOUR OPERATIONAL CHECK OF CHIP DETECTOR COCKPIT INDICATION SYSTEM. NO DEFECTS NOTED. PRE AND POST INSPECTION MAINTENANCE RUN-UPS WERE PERFORMED. NO DEFECTS NoTED. 2 3 4 5 The aircraft/component identified above was maintained or altered in accordance with current regulations of the Federal Aviation Administration and is approved for return to service for the work performed. All disrupted systems were restored and functionally tested in accordance with mfg's instructions. Pertinent details of the repair are on file at this repair station under Work Order: 11M4117. Date: 04/07/2017 Authorized Signature: Tom Bierschwale FDAHER Registration Model No. Serial No. Engine MIN Engine S/N 1 N836EA TBM 700 6577 PT6A-66D PCE-RVO320 >IIIER>Leading the Business of Aviation Cutter Aviation San Antonio, Inc. 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 POWER SECTION RECORD ENTRY Hour Meter Total Time CSN TSOH 1357.3 1357.3 Page 1 of 1 PERFORMED COMPRESSOR AND TURBINE WASHES. PERFORMED GRPOND RUN-UP. NO DEFECTS NOTED. REFERENCE PT6A-66D MM CHAPTER 71-00-00. The aircraft/component identified above was maintained or altered in accordance with current regulations of the Federal Aviation Administration and is approved for return to service for the work performed. All disrupted systems were restored and functionally tested in accordance with mfg's instructions. Pertinent details of the repair are on file at this repair station under Work Order: 11M-4189. Date. 06/05/2017 Authorized Signature: Tom Bierschwale Signature AME ACA/AMO SCA/AMO DAHERRegistration Model No. Serial No. EngineMIN Engine S/N N836EA TBM 700 657 PT6A-66D PCE-RVO320 >CUIER>Leading the Business of Aviation Cutter Aviation San Antonio, Inc. 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 POWER SECTION RECORD ENTRY Hour Meter Total Time CSN TSOH 1524.6 1524.6 Page 1. of 1 INSPECTED THIS ENGINE USING DAHER TBM70O MM CHAPTER 5-20-04 (STANDARD PROGRAM C INSP), 05-20- 05 (12 MONTH SPECIAL CHECKS) AND PRATT & WHITNEY PT6A-66D MM CHAPTER 72-00-00, TABLE 601 1. INSPECTION CHECK LISTS AS A GUIDE. COMPLIED WITH 12 MONTH ROUTINE AND MINOR INSPECTIONS AND MAINTENANCE PER PRATT & WHITNEY 2. PT6A-66D MM CHAPTER 72-00-00 TABLE 601. COMPLIED WITH 12 MONTH BRIDGE AND CONTINUITY CHECKS OF MAGNETIC CHIP DETECTOR IAW PT6A-66D MM CHAPTER 72-10-00, 72-60-00. NO DEFECTS NOTED. 3. COMPLIED WITH MAGNETIC CHIP DETECTOR COCKPIT INDICATION SYSTEM CHECK. REF PRATT & WHITNEY PT6A-66D MM 72-00-00, PAGE 612. NO DEFECTS NOTED. COMPLIED WITH 200 HOUR MAGNETIC CHIP DETECTOR COCKPIT INDICATION SYSTEM CHECK IAW PRATT & WHITNEY PT6A-66D MM 72-00-00, PAGE 612. NO DEFECTS NOTED. 5. 6. 7. INSTALLED NEW UH IGNITION LEAD PART NUMBER 3119836-01. REF P&W MM CH. 74-20-00. PRE AND POST INSPECTION MAINTENANCE RUN-UPS WERE PERFORMED. NO DEFECTS NOTED. The aircraft/component identified above was maintained or altered in accordance with current regulations of the Federal Aviation Administration and is approved for return to service for the work performed. All disrupted systems were restored and functionally tested in accordance with mfg's instructions. Petinent details of the repair are on file at this repair station under Work Order: 11M4483. Date: 04-13-2018 Authorized Signature. S.HOLLIDAY DAHERRegistration Model No. Serial No. Engine M/N: Engine S/N N836EA TBM 700 657 PT6A-66D PCE-RVO320 >CIHEB>Leading the Business of Aviation Cutter Aviation San Antonio, Inc. 367 Sandau R. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 POWER SECTION RECORD ENTRY Hour Meter Eng. Total Time CSN: TSOH 1668.0 1668.0 1054 Page 1of 1 INSPECTED THIS ENGINE USING DAHER TBM700 MM CHAPTER 5-20-02 (STANDARD PROGRAM A INSP), 05-20-05 (12 MONTH SPECIAL CHECKS) AND PRATT & WHITNEY PT6A-66D MM CHAPTER 72-00-00, TABLE 601 INSPECTION CHECK LISTS AS A GUIDE. COMPLIED WITH 400 HOUR ENGINE FUEL NOZZLE CLEANING AND FLOW CHECK. REMOVED AND REINSTALLED 13 FUEL NOZZLES PIN 3119855-01 AND ONE PIN 3119856-01 AFTER CLEANING AND INSPECTION WAS DONE BY STANDARD 2 1 3. AERO CRS# U8TR793Y UNDER THEIR Wo# 39-00807. TORQUED MOUNT BOLTS TO 36 IN LBS AND SAFTIED. REF P&W MIM #3070902 CHAP. 73-11-05. COMPLIED WITH 400 HOUR BORESCOPE INSPECTION IN CONJUNCTION WITH FUEL NOZZLE INSPECTION. NO IMPACT DAMAGE, TIP EROSION, SULFADATION ON CT BLADES. NOTED A FEW BLISTERS ON COMPRESSOR TURBINE BLADES, NONE WERE POPPED. NO CRACKS ON COMPRESSOR TURBINE GUIDE VANE ASSY, NO CRACKS ON INNER OR OUTER RINGS, NO BURNED OR CRACKED VANES, SEGMENTS ARE NOT ERODED OR CURLED. NOTED A SMALL AMOUNT OF TRANSFER AT ON SEGMENTS NEAR A SEGMENT SEAM WITH NO BLADE DEFORMATION. NO FRETTING WEAR AT PT DISK FACE ALL WORK ACCOMPLISHED IAW PRATT & VWHITNEY PTSA-66D MM 72-00-00, PAGE 616. COMPLIED WITH 12 MONTHI200 HOUR ROUTINE AND MINOR INSPECTIONS AND MAINTENANCE PER PRATT & WHITNEY 4 PT6A-66D MM CHAPTER 72-00-00 TABLE 601. COMPLIED WITH 12 MONTHI600 HOUR AGB/RGB BRIDGE AND CONTINUITY CHECKS OF MAGNETIC CHIP DETECTOR IAW PT6A-66D MM CHAPTER 72-10-00. NO DEFECTS NOTED. LEAK CHECKED GOOD. COMPLIED WITH 12 MONTH/200 HOUR OPERATIONAL CHECK OF CHIP DETECTOR COCKPIT INDICATION SYSTEM. NO 5 6 DEFECTS NOTED. COMPLIED WITH 200 HOUR P3 FILTER DRAIN VALVE CLEANING AND INSPECTION. NO DEFECTS NOTED. REF P&W MIM 7 #3070902. CHAP. 73-10-07. PERFORMED ENG!NE COMPRESSOR WASH/RINSE AND TURBINE RINSE FOR AIRCRAFT OPERATING IN A SALT LADEN ENVIRONMENT IAW MM CH. 71-00-00. COMPLIED WITH PRATT & WHITNEY RECOMMENDED ANT-CORROSION APPLICATION TO COMPRESSOR INLET. 8 9 10 PRE AND POST INSPECTION MAINTENANCE RUN-UPS WERE PERFORMED. NO DEFECTS NOTED. The aircraf'component identified above was maintained or altered in accordance with current regulations of the Federal Aviation Administraton and is approved for return to service for the work performed. All disrupted systems were restored and functionaly tested in accordancewithmfg'sinstructions.Pertinentdetails ofthe repairareon file atthisyepair station under Work Order:11M-4896. Date: 05-09-2019 Authorized Signature: S HOLLIDAY |DAHERRegistration Model No. Serial No. Engine MIN Engine S/N N836EA TBM700 657 PT6A-66D PCE-RVO320 »CUIER>Leading the Business of Aviation Cutter Aiation San Antonio, Inc. 367 Sandau Rd. San Antonio, Texas 78216 FAA Repair Station No. U7TR491Y Phone (210) 340-6780 Fax (210) 384-3394 POWER SECTION RECORD ENTRY Hour Meter |Total Time CYCLES Page1 of 1 1693.1 1693.1 1210 INSPECTED STAGE 1 COMPRESSOR BLADES FOR FOD. FOUND NO REFERENCE PRATT & WHITNEY M/M CHAPTER 70-00-00 PAGE 606. INSPECTED ENGINE INLET HOUSING FOR CORROSION. FOUND NO DISCREPENCIES AT THIS TIME REFERENCE PRATT & WHITNEY MM CHAPTER 72-00-00 PAGE 602. 1 2. 3. REMOVED DAMAGED REVERSE LINKAGE SWIVEL JOINT AND INSTALLED OVERHAULED SWIVEL JOINT, PIN 3019266 REFERENCE PRATT & WHITNEY PT6A-66D EMM 76-10-00, PARAGRAPH H. The aircraf/component identified above was maintained or altered in accordance with current requlations of the Federal Aviaton Administration and is approved for return to service for the work performed. All disrupted systems were restored and functionallytestedin accordance with mfg.'s instructions. Pertinent details of the repair are on file at this repair station under Work Order: 11M-5081. Date: 10-24-2019 Authorized Signature: S.HOLLIDAY DISCREPENCIES AT THIS TIME, Signature AME ACA/AMO SCA/AMO StandardAero CRS# U8TR793Y; EASA# 145.5299 PT6A-66D PCE-RV0320 TSO: Work Order: Order/Task: CSO: StandardAero 600 E. Dallas Road, Suite 400, Grapevine, TX 76051 Manufacturer: Description: TSN: Pratt & Whitney Canada Engine Assembly,Complete 1693.1 Part Deseription CSN: Model No: Serial No: 1074 LCF PARTS ACCESSED THIS VISIT 39-01856 232/316 NJA N/A CSN PN InstalledSN Installed TSN CSN PN RemovedS/NRemoved TSN 1074 3053740-01 YUAAO12A581 1693.1 YUAA012A581| 1693.1 Compressor Turbine Disk Details of work performed: Split engine at "C" Flange, removed hot section components asnecessary and complied with Hot Section Inspection. Installed inspected and repaired hot section components with a final CT Blade tip clearance of 0.018". Re-mated the engine at 1074 3053740-01 C" Flange and completed Hot SectionInspection. All work performed inaccordance with the Pratt & Whitney Canada PT6A-66D Maintenance Manual P/N: 307O902 Revision No. 18.1, dated July 6, 2017 and the Daher Aerospace TBM 850 Maintenance Manual P/N: Z00.DMAMMPXEEOR47. StandardAero serviced the engine with 3 quarts of Aeroshell 560. Primary Parts installed new this visit: (10) new Shroud Segments P/N: 3039465CL15 and (1) new PT Seal Ring P/N: 3057818-01. NOTE: StandardAero witnessed satisfactory ground performance runs and leak check performed by Cutter Aviation of San Antonio. Pertinent details of this repair are on file at this repair station under work order:39-01856. The aircraft, aircraft engine, appliance identified abovewas repaired and inspected inaccordance with current maintenance rules of the Federal Aviation Regulations and is approved for return to service with respect to the work performed. DATE: AUTHORIZED BY (PRINT): Daniel Fray TXO03R1 SIGATIRE: 16-0ct-19 AVEX SAFETY-DATA -DETAILS C.RS. X1ID595Y N836EA/ Engine 1. MFR: Pratt & Whitney HOBBS: 2,180.00 Page 1 of 1 11804 CorporateWay Broomfield, co 80021 Phone: (720)399-8008 | Fax: (720) 541-9001 October 13, 2022 SN:657 w Work Order No: MXCO1130 Model: PT6A-66D CSN: TSN: 2,180.00 TSO: CSO: Performed pre-maintenance borescope of engine first stage compressor blades L.A.W. Pratt and Whitney PT6A-66D MM Chapter 72 Performed post-maintenance borescope of engine first stage compressor blades L.A.W. Pratt and Whitney PT6A-66D MM Chapter 72. No changes noted between pre and post maintenance. 2. This aircraft, airframe, aircraft engine, propeller or appliance was repaired/inspected in accordançe with the current Federal Aviation Regulations and has been found to be in an airworthy condition for scope of work performed. Pertinent details of the repairinspection are on file at this Repair Station under Work Order No. MXCO1130. V jor|3/22 Date For: FAA Approved Repair Station C.R.S. X1ID595Y Page 6 Make: Model: Serial No.: AFTT: TSNEW: 2516.8 P&W PT6A-66D PCE-RVO320 2516.8 Reg. No Date: w/O No.: Hobbs: CSHSI: 502 N836EA 9/27/2024 2451 2516.8 HANCOCKAVIATIO NSALES|SERVICE ENGINE MAINTENANCE ENTRY TSHSI: 825.5 TC: 1712 Description of Work Accomplished. InspectionsCompleted: * Completed an Annual Inspection IAW 14 CFR Part 43 Appendix D using the TBM850 MM Chapter 5-20-02 (Standard Program A Insp) and 5-20-05 (12 Month Special Checks) Inspection Check Lists as a guide. Engine Run and Ground Operational Checks were satisfactory * Completed an A Inspection using the TBM700 MM Chapter 5-20-02 (Standard Program A Insp) Check List as a guide. *C/WCT disc desalination & compressor power recovery wash IAW P&W PT6A-66DChapter 71 *C/W 12 Month/ 200 Hour Routine & Minor and maintenance per P&W PT6A-66D MM 72- 00-00 Table 601 Approval for Return to Service The article identified above was repaired and inspected in accordance with current FAA regulations and was found to be airworthy and is approved for return to service. Pertinent details of the work performed are on file at this agency under this work order. Authorized Signature Hancock Aviation LLC 4409 Chuck Yeager Avenue Baton Rouge, LA 70807 Joseph B Averett 2740243 IA/AP Phone: (225) 800-2359 Fax: (225) 224-6211 Email: info@hancockaviation.com Web: www.hancockaviation.com