JASC 5744
Service difficulty reports · 2,731
Reports filed under 5744 · Wing, Control Surface Attach Fittings, 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 = '5744' 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 = '5744' 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 04FDEA02912Support · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUGS HAVE CORROSION. REMOVED CORROSION FROM LOCATION NR 1 MOUNTING SURFACE IAW DACCMM 57-44-07 AND FEDEX EA8-5750-81473. PRIMED LUGS IAW DC109 SRM 57-21-01 VOLUME II. BEGINNING BORESDR 2004UALA00817Fitting · crackedRT WING OUTBOARD AILERON 2ND FROM OUTBD HINGE FITTING CRACKED THRU LWR AFT FASTENER LOWER AREA. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FITTING.SDR 2004UALA00828Hinge · brokenLT WING, REAR SPAR, OUTBOARD FLAP OUTBOARD HINGE FITTING BROKEN IN HALF. FLAP TRANSMISSION OVER TORQUE LIMIT INDICATOR ALSO POPPED. SUPPLEMENTAL DATA UPDATE, REAR SPAR RIB POST PART NR 113T1369-1 REPLACED. FLAP TRANSMISSION OVERTORQUE LIMIT INDICATOR RESET.SDR UPS04842902Fitting · crackedINSPECTION TYPE: C1, LEFT WING FLAP HINGE STATION 3 FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM 51-1-20D.SDR 04FDEA02086Hinge · corrodedC/W EA 8-5740-80575 WINGS RT INBD FLAP OUTBD HINGE UPPER HOLE LUG CORROSION REPAIR P/N ARC0154-2. COMPLIED WITH EA 8-5740-80575.SDR 04FDEA02046Bracket · corrodedCOMPLY EA 1-5750-78010 OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR HAS BEEN COMPLIED.SDR 04FDEA01802Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PG 402-407 ORIGINAL THICKNESS 0.517 INCH, MATERIASDR 04FDEA01799Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND SDR 04FDEA01798Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOSDR 04FDEA01801Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK UPPER BOLT HOLE FOUND CORRODED.SDR 04FDEA01800Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT HOLE BORE FOUND CORRODED.SDR 04FDEA01797Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED.SDR 04FDEA01796Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER MOUNTING SPOTFACE FOUND CORRODED.SDR 04FDEA01795Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED.SDR 04FDEA01794Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED.SDR 04FDEA01790Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED.SDR 04FDEA01789Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER MOUNTING INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PG 402-407 ORIG THK 0.52 MATERIAL REMOVED 0.033 REMAINING THICKNESS 0.487 & FOUND WITHIN LIMITS AS PER DWG TOLERASDR 04FDEA01788Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER =1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FSDR 04FDEA01787Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FEDESDR 04FDEA01786Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED.SDR 04FDEA01785Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER MOUNTING OUTBOARD BOLT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=0.516, FINAL DIAMETER=0.596 AND REPAIRED AS PER SDR 04FDEA01784Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER MOUNTING INBOARD BOLT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=0.516, FINAL DIAMETER=0.596 AND REPAIRED AS PER FESDR 04FDEA01783Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FESDR 04FDEA01782Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.225 AND REPAIRED AS PER FEDSDR 04FDEA01740Hinge Bracket · corrodedLEFT FWD (WING SIDE) I/B FLAP O/B HINGE PIVOT BORE SPOTFACE CORRODED. LEFT FWD (WING SIDE) I/B FLAP O/B HINGE PIVOT BORE SPOTFACE CORROSION. REMOVED AND EXCEED LIMITS AS PER CMM 57-44-07 PAGES 403-404. ORIGINAL THICKNESS = 0.483 INCH, REMAINING THICKNESS = SDR 04FDEA01739Hinge Bracket · corrodedRT FWD (WING SIDE) I/B FLAP O/B HINGE, PIVOT BORE SPOTFACE CORRODED. RT FWD (WING SIDE) I/B FLAP O/B HINGE, PIVOT BORE SPOTFACE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-44-07 PAGES 403-404. ORIGINAL THICKNESS=0.493 INCH, REMAINING THICKNESS=0.442 SDR 04FDEA01745Bracket · crackedLEFT OUTBOARD FLAP MOUNTED HINGE FAIRING ATTACH BRACKET CRACKED AT NUT PLATE. REMOVED AND REPLACED BRACKET AT LEFT O/B FLAP MOUNTED HINGE FAIRING IAW SRM 51-31-01.SDR 04FDEA01729Hinge Bracket · corrodedRT FWD (WING SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE CORROSION. REMOVED AND EXCEED LIMITS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.22SDR 04FDEA01728Hinge Bracket · corrodedRT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE CORROSION REMOVED AND EXCEED LIMITS PER CMM 57-44-08, ORIGINAL THICKNESS = 0.500 INCH, MATERIAL REMOVED = 0.012 INCH, REMAININGSDR 04FDEA01727Hinge Bracket · corrodedRT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B LOWER MOUNT BORE HOLE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B LOWER MOUNT BORE HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER=0.641 INCH, FINAL DIAMETER SDR 04FDEA01726Hinge Bracket · corrodedRT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SPOTFACE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SPOTFACE CORROSION. REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.427 INCH, MATERIAL REMOVED = 0.006 INSDR 04FDEA01716Bracket · corrodedRIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09, PAGES 402 - 407. ORIGINAL THICKNESS = 0.452 INCH, MATERIAL REMOVED = 0.00SDR 04FDEA01713Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP I/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. LT FWD (WING SIDE) O/B FLAP I/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIASDR 04FDEA01712Bracket · corrodedLT FWD (WING SIDE) O/B FLAP I/B HINGE - I/B ACTUATOR LUG HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIASDR 04FDEA01711Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.495 INCH, MATERIAL REMOVED = 0SDR 04FDEA01710Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SURFACE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SURFACE CORROSION REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.405 INCH, MATERIAL REMOVED = 0.003 INSDR 04FDEA01709Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP I/B HINGE, PIVOT BORE HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE, PIVOT BORE HOLE CORROSION REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 2.252 INCH, FINAL DIAMETER = 2.323 INCH. COMPLIED WITH FESDR 04FDEA01715Hinge · corrodedRIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED.SDR 04FDEA01714Hinge · corrodedRIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORRODED.SDR 04FDEA01699Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED AND EXCEED LIMIT PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1SDR 04FDEA01698Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = SDR 04FDEA01697Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09, PAGES 402-407. ORIGINAL THICKNESS = 0.427 INCH, MATERIAL REMOVED = 0.002 INSDR 04FDEA01512Hinge · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, FINAL DIAMETER: 1.1221, MAX ALLOWABLE DIAMETER: 1.190, EXCEED ALLOWABLE LIMIT AS PERSDR 04FDEA01511Hinge · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, FINAL DIAMETER: 1.1221, MAX ALLOWABLE DIAMETER: 1.190, EXCEED ALLOWABLE LIMIT AS SDR 04FDEA01510Hinge · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE), UPPER I/B MOUNTING BOLT BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER: 0.879, FINAL DIAMETER: 0.952, MAX ALLOWABLE DIAMETER: 0.944, EXCEED ALLOWABLE LIMIT AS PERSDR 04FDEA01509Hinge · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE), LOWER MOUNTING SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL THICKNESS OF LUG: 0.481, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.479, MINIMUM ALLOWABLE THISDR 04FDEA01508Hinge · corrodedRT WING OB FLAP IB HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (WING SIDE), SIDE LINK SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 FIG 1, PAGES 402 TO 407. ORIGINAL THICKNESS OF LUG: 0.429, MATERIAL REMOVED: 0.002, RESDR 04FDEA01373Hinge · corrodedLEFT WING - O/B FLAP O/B HINGE (WING SIDE), SIDE LINK BARREL NUT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL DIAMETER: 0.593, MAX ALLOWABLE DIAMETER: 0.667, FINAL DIAMETER: 0.661 WITHIN LIMIT. REPAIRED AS PESDR 04FDEA01372Hinge · corrodedLEFT WING - O/B FLAP O/B HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL THICKNESS OF LUG: 0.452, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.450. REPAIRED AS PER EA 1-SDR 04FDEA01371Hinge · corrodedLEFT WING - O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. BORE CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL DIAMETER: 1.187, MAX DIAMETER: 1.190, FINAL DIAMETER: 1.250 EXCEEDED LIMIT. REPAIRED AS PER
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