JASC 5753

Service difficulty reports · 31,521

Reports filed under 5753 · Trailing Edge Flaps, newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE jasc_code = '5753'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 04FDEA01557Flap Track · corrodedLEFT I/B FLAP TRACK MOUNT HOLES CORRODED. REMOVED AND REPLACED FLAP TRACK IAW CMM 57-52-01 AT MAE.Jun 1, 2004 · N68051 · Doug DC1010SDR 04FDEA01552Fitting · damagedCOMPLY WITH EA 8-5750-78218 WINGS - RIGHT INBOARD FLAP, ROLLER FITTING REWORK. COMPLIED WITH EA 8-5750-78218 WINGS - RIGHT INBOARD FLAP, ROLLER FITTING REWORK AT MAE.Jun 1, 2004 · N68051 · Doug DC1010SDR 04FDEA01540Stop Fitting · corrodedCOMPLY WITH EA 8-5750-77430 WINGS - OUTBOARD FLAP INBOARD UP-STOP FITTING CORROSION REWORK, LEFT OUTBOARD FLAP. COMPLIED WITH EA 8-5750-77430.May 29, 2004 · N68051 · Doug DC1010SDR A6WA200460018Flap Track · wornLT NR 2 FLAP TRACK HAS WEAR BEYOND THE SRM LIMITS MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS REF AVMAX FAX 611-1908004. DAMAGED AREA MAPPED AND SUBMITTED TO BAE FOR REPAIR CRITERIA. NDT HFEC CARRIED OUT IAW BAE FAX BARA/AVR/6761/04-MK, NO CRACKS NOTED. DV May 28, 2004 · N611AW · Bac 146300ASDR A6WA200460017Flap Track · wornRT NR 2 FLAP TRACK HAS WEAR BEYOND THE SRM LIMITS. MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS REF AVMAX FAX 611-1908003. MAINTENANCE MAPPED AND SUBMITTED TO BE FOR REPAIR CRITERIA. NDT HFEC CARRIED OUT IAW BAE FAX BARA/AVR/6762/04-04-MK. NO CRACKS NOTED.May 28, 2004 · N611AW · Bac 146300ASDR 04FDEA01518Hinge Bracket · corrodedC/W 8-5710-77408, WINGS - RIGHT INBOARD FLAP - OUTBOARD HINGE BRACKET MOUNT HOLE REPAIR, P/N ARB3799-2. COMPLIED WITH EA 8-5710-77408 WINGS - RIGHT INBOARD FLAP - OUTBOARD HINGE BRACKET MOUNT HOLE REPAIR P/N 3799-2 AT MAE.May 28, 2004 · N68051 · Doug DC1010SDR 04FDEA01517Hinge Bracket · corrodedCOMPLY WITH EA 8-5740-77420 WING - RIGHT INBOARD FLAP - OUTBOARD HINGE BRACKET CORROSION REPAIR (P/N ARC0154-2). COMPLIED WITH EA 8-5740-77420 LEFT INBOARD FLAP - O/B HINGE BRACKET CORROSION REPAIR (P/N ARC 0154-2) FABRICATED BUSHING ON TRAV 432592 AT MAE.May 28, 2004 · N68051 · Doug DC1010SDR 04FDEA01507Hinge · corrodedLEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG. 402-407. ORIG. THK.: 0.415, MATERIAL REMOVED: 0.004, REMAINING THK.: 0.411. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76718 - May 28, 2004 · N594FE · Doug MD11SDR 04FDEA01506Hinge · corrodedLEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 PG. 402-407. ORIG. DIAM.: 1.187, FINAL DIAM.: 1.221, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76718 - WINGS -May 28, 2004 · N594FE · Doug MD11SDR 04FDEA01505Hinge · corrodedLEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND OUTBOARD ACTUATOR HOLE OUTBOARD CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 PG. 402-404. ORIG. DIAM.: 1.187, FINAL DIAM.: 1.222, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76718May 28, 2004 · N594FE · Doug MD11SDR 04FDEA01504Hinge · corrodedLEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND LOWER MOUNT MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG. 402-404. ORIG. THK.: 0.514, MATERIAL REMOVED: 0.008, REMAINING THK.: 0.506. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76718 - May 28, 2004 · N594FE · Doug MD11SDR SWAA041507Structure · delaminatedDURING SCHEDULED A1 CHECK, FOUND RIGHT WING T/E OUTBOARD AFT FLAP, DELAMINATED. REMOVED AND REPLACED RIGHT OUTBOARD AFT FLAP PER MM.May 27, 2004 · N303SW · Boeing 7373H4SDR 04FDEA01495Hinge Bracket · corrodedCOMPLY WITH EA 8-5740-77418 WINGS RT INBD FLAP, FWD HINGE ASSY PIVOT BORE CORROSION. COMPLIED WITH EA NR 8-5740-77418 WINGS-LT IB FLAP, FWD HINGE ASSY PIVOT BORE CORROSION, PART 1 ONLY. COMPLIED WITH AS STATED IN UPDATE.May 27, 2004 · N68051 · Doug DC1010SDR 04FDEA01494Hinge · corrodedCOMPLY WITH EA 8-5740-77431 WINGS-RT OB FLAP, OUTBD HINGE ASSY P/N ARC0503 PIVOT BORE REWORK. COMPLIED WITH EA 8-5740-77431 WINGS-RT OB FLAP, OB HINGE ASSY P/N ARC0503 PIVOT BORE REWORK AT MAE.May 27, 2004 · N68051 · Doug DC1010SDR 04FDEA01493Fitting · corrodedCOMPLY WITH EA 8-5750-77424 WINGS LT IB FLAP-OB HINGE BRACKET SIDE BRACE REPAIR (P/N ARC0182-1) COMPLIED WITH EA 8-5750-77424 (WINGS-LT IB FLAP- OB HINGE BRACKET SIDE BRACE REPAIR (PN ARC 018 2-1) AT MAE.May 27, 2004 · N68051 · Doug DC1010SDR USAA040292Skin · delaminatedPIT - FOUND SKIN AND CORE DELAMINATED 13 INCHES LONG BY 8 INCHES WIDE, LT OUTBOARD AFT FLAP, INBOARD T/E TOP SURFACE, HEAVY CORE CORROSION. INSTALLED NEW CORE, SKIN PANEL AND DOUBLER PER T/R 57-50-39A. (M)May 26, 2004 · N449US · Boeing 7374B7SDR USAA040300Skin · delaminatedFOUND SKIN DELAMINATED WITH CORROSION 13 INCHES LONG BY 8 INCHES WIDE, LT OUTBOARD AFT FLAP INBOARD T/E TOP SURFACE HEAVY CORE CORROSION. INSTALLED NEW CORE PER T/R 57-50-39A. LEVEL 1, TASK NR C57-306-01. (M)May 26, 2004 · N449US · Boeing 7374B7SDR IXXA0400092SSkin Panel · damagedDURING ROUTINE C CHECK INSPECTION, FOUND LT INBD FLAP HAS INTERIM REPAIR ON UPPER PLATING, STA XW 89.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIRS IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 PG 2 FIG 1. REMOVED UPPER PLATING IAW DC8 SRM 51-1May 26, 2004 · N830BX · Doug DC871FSDR 04FDEA01492Fitting · corrodedCOMPLY WITH EA 8-5750-77425 WINGS-LT IB FLAP, ROLLER FITTING ATTACH HOLES CORRODED AT MAE(PART 1 INTIAL IS COMPLIED WITH AND WILL REQUIRE A FOLLOW UP ACTION TO BE COMPLIED WITH. COMPLIED WITH AS STATED IN UPDATE.May 26, 2004 · N68051 · Doug DC1010SDR 04FDEA01491Hinge · corrodedLT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. DIA: 1.062, FINAL DIA: 1.191. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01490Hinge · corrodedLT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. THK. OF LUG: 0.402, MATERIAL REMOVED: 0.002, REMAINING THK.OF LUG: 0.400. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS May 26, 2004 · N594FE · Doug MD11SDR 04FDEA01489Hinge · corrodedLT WING OB FLAP AFT OB HINGE, FOUND OB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. DIAM.: 1.062, FINAL DIAM.: 1.196, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01488Hinge · corrodedLEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. THK. OF LUG: 0.397, MATERIAL REMOVED: 0.002, REMAINING THK. OF LUG: 0.395. REPAIR CARRIED-OUT AS PER FEDEX EA May 26, 2004 · N594FE · Doug MD11SDR 04FDEA01487Hinge · corrodedLEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. DIAM.: 1.093, FINAL DIAM.: 1.125, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01486Hinge · corrodedLEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG.THK. OF LUG: 0.504, MATERIAL REMOVED: 0.007, REMAINING THK.OF LUG: 0.497. REPAIR CARRIED - OUT AS PER FEDEX EA 1-57May 26, 2004 · N594FE · Doug MD11SDR 04FDEA01485Hinge · corrodedLEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. DIAM.: 1.062, FINAL DIAM.: 1.093, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - TITLE: WINGS - TRAILING EDGE AND TRAILMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01484Hinge · corrodedLEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. THK. OF LUG: 0.492, MATERIAL REMOVED: 0.002, REMAINING THK.OF LUG: 0.490. REPAIR CARRIED-OUT AS PER FEDEX EA 1May 26, 2004 · N594FE · Doug MD11SDR 04FDEA01483Hinge · corrodedLEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.512, MATERIAL REMOVED= 0.003, REMAINING THICKNESS= 0.409. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - May 26, 2004 · N594FE · Doug MD11SDR 04FDEA01482Hinge · corrodedLEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.091. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGEMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01481Hinge · corrodedLT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.507, MATERIAL REMOVED= 0.006, REMAINING THICKNESS= 0.501. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01480Hinge · corrodedLEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.093, FINAL DIAMETER =1.140. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01479Hinge · corrodedLEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.409, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.407. COMPLIED WITH FEDEX EA 1-5750-76716, WMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01478Hinge · corrodedLEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01477Hinge · corrodedLT WING OB FLAP AFT IB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.400, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.398. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILINGMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01476Hinge · corrodedLT WING - OB FLAP AFT IB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - L/HMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01475Hinge · corrodedRT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01474Hinge · corrodedRT WING - OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.400, MATERIAL REMOVED = 0.002, REMAINING THICKNESS= 0.398. COMPLIED WITH FEDEX EA 1-5750-76723, WINGS - TRAILINMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01472Vane · corrodedCOMPLY WITH EA 8-5750-77429 WINGS ARC1455-510 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-77429.May 26, 2004 · N68056 · Doug DC1010SDR 04FDEA01471Support · corrodedCOMPLY WITH EA 8-5750-77428, WINGS - ARC1455 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-77428.May 26, 2004 · N68056 · Doug DC1010SDR 04FDEA01463Hinge · corrodedRIGHT WING OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, TRAILING EDGE AND TRAILING May 26, 2004 · N594FE · Doug MD11SDR 04FDEA01462Hinge · corrodedRT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.403, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.401. COMPLIED WITH FEDEX EA 1-5750-76723, WIMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01461Hinge · corrodedRIGHT WING OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.093, FINAL DIAMETER =1.125. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, TRAILING EDGE AND TRAILING EDGEMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01460Hinge · corrodedRIGHT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.503, MATERIAL REMOVED= 0.005, REMAINING THICKNESS= 0.498. COMPLIED WITH FEDEX EA #1-5750-76723, WIMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01459Hinge · corrodedRIGHT WING OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.092. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, TRAILING EDGE AND TRAILING EDGMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01458Hinge · corrodedRIGHT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.508, MATERIAL REMOVED= 0.001, REMAINING THICKNESS= 0.507. COMPLIED WITH FEDEX EA 1-5750-76723, WINMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01457Hinge · corrodedRIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01456Hinge · corrodedRIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.410, MATERIAL REMOVED : 0.002, REMAINING THICKNESS OF LUG: 0.408. REPAIR CARRIED OUT AS PMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01455Hinge · corrodedRIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01454Hinge · corrodedRIGHT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD ACTUATOR. HOLE OUT SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.390, MATERIAL REMOVED : 0.002, REMAINING THICKNESS OF LUG: 0.388. REPAIR CARRIEDMay 26, 2004 · N594FE · Doug MD11SDR 04FDEA01453Hinge · corrodedRIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.093, FINAL DIAMETER =1.129. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE May 26, 2004 · N594FE · Doug MD11
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