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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 04FDEA01557Flap Track · corrodedLEFT I/B FLAP TRACK MOUNT HOLES CORRODED. REMOVED AND REPLACED FLAP TRACK IAW CMM 57-52-01 AT MAE.SDR 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.SDR 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.SDR 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 SDR 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.SDR 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.SDR 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.SDR 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 - SDR 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 -SDR 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 1-5750-76718SDR 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 - SDR SWAA041507Structure · delaminatedDURING SCHEDULED A1 CHECK, FOUND RIGHT WING T/E OUTBOARD AFT FLAP, DELAMINATED. REMOVED AND REPLACED RIGHT OUTBOARD AFT FLAP PER MM.SDR 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.SDR 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.SDR 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.SDR 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)SDR 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)SDR 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 51-1SDR 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.SDR 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 FSDR 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 SDR 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 OUSDR 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 SDR 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 EDSDR 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 1-57SDR 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 TRAILSDR 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 1SDR 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 - SDR 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 EDGESDR 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 - TRAILSDR 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 EDGSDR 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, WSDR 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 EDSDR 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 - TRAILINGSDR 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/HSDR 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 DEVICSDR 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 - TRAILINSDR 04FDEA01472Vane · corrodedCOMPLY WITH EA 8-5750-77429 WINGS ARC1455-510 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-77429.SDR 04FDEA01471Support · corrodedCOMPLY WITH EA 8-5750-77428, WINGS - ARC1455 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-77428.SDR 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 SDR 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, WISDR 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 EDGESDR 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, WISDR 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 EDGSDR 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, WINSDR 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 DEVSDR 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 PSDR 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 TRAILSDR 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 CARRIEDSDR 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
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