JASC 5744
Service difficulty reports · 2,721
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 FDEA201604191264Hinge Bracket · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, FWD ATTACH INBD LUG BORE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.254 INCHES, FINAL HOLE DIAMETER 1.260 INCHES & MAXIMUM ALLOWABLE DIAMETER 1.254 INCHESSDR FDEA201604191263Hinge Bracket · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.217 INCHES, FINAL HOLE DIAMETER 1.223 INCHES & MAXIMUM ALLOWABLE DIAMETER 1.220 ISDR FDEA201604191262Hinge Bracket · corrodedLEFT WING OTBD FLAP OUTBOARD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.217 INCHES, FINAL HOLE DIAMETER 1.223 INCHES & MAXIMUM ALLOWABLE DIAMETER 1.SDR FDEA201603291112Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORRODED. REWORKED FOUND EXCEEDED LIMITS IAW CMM 57-52-04. EXISTING HOLE DIAMETER 1.193", FINAL HOLE DIAMETER 1.196, MAXIMUM ALLOWABLE HOLE DIAMETER 1.15". NEW REPAIR BUSHINGSDR FDEA201603291111Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.190", FINAL HOLE DIAMETER 1.225" & MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR SDR FDEA201603291110Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.215", FINAL HOLE DIAMETER 1.250", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRSDR FDEA201603291109Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.255", FINAL HOLE DIAMETER 1.285", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABSDR FDEA201603291108Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.257", FINAL HOLE DIAMETER 1.283", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRISDR FDEA201603291107Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE, FOUND CORRODED. CORROSION REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.248", FINAL HOLE DIAMETER 1.283", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSDR FDEA201603291106Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.216", FINAL HOLE DIAMETER 1.226 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220SDR FDEA201603291104Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.704", FINAL HOLE DIAMETER 0.737 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.709".SDR FDEA201603291103Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, UPPER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.957", FINAL HOLE DIAMETER 0.961 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.944".SDR FDEA201603291102Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.222", FINAL HOLE DIAMETER 1.228 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220SDR FDEA201603291101Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.284", FINAL HOLE DIAMETER 1.289 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220SDR FDEA201603281090Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.588", FINAL HOLE DIAMETER 0.596 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584".SDR FDEA201603281089Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.588", FINAL HOLE DIAMETER 0.596 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584".SDR FDEA201603281088Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SURFACES, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS: 0.412", MATERIAL REMOVED 0.002" & MINIMUM ALLOWABLE THICKNESS 0.423". NESDR FDEA201603281087Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD. STUD ATTACH SURFACES FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0.420", MATERIAL REMOVED: 0.010" & MINIMUM ALLOWABLE THICKNESS 0.423". NSDR FDEA201603281086Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44- 08. EXISTING HOLE DIAMETER 0.720", FINAL HOLE DIAMETER 0.737 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.7SDR FDEA201603271077Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE, FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.220", FINAL HOLE DIAMETER 1.223 & MAX ALLOWABLE HOLE DIAMETER 1.220". NEW RSDR COEA2016032222805Hinge · corrodedHEAVY CHECK COE & MINOR REPAIR. RT WING LOWER TE DROP DOWN PANEL 632AB HAS LEVEL 2 CORROSION ON OTBD HINGE. REPLACED HINGE WITH OEM PART.SDR AALA20160218007Former · crackedLEFT WING LE NR 4 SLAT TRACK, INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD HINGE ATTACH FITTING. ACFT IN BASE MX.SDR FDEA201601290389Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE WING SIDE, PIVOT HOLE BORE CORROSION. REWORKED & FOUND EXCEEDS LIMITS IAW CMM 57-44-08. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323078 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201601290388Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMITS IAW CMM 57-44-08. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323078 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM SDR FDEA201601290387Hinge · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMITS IAW CMM 57-44-08. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323078 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM SDR FDEA201601290374Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323026 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201601290373Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323026 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201601290372Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORRODED. FOUND OUT OF LIMIT IAW CMM 57-44-09. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323026 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201601290371Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. A NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323026 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR DALA2016012800690Support · crackedCRACKED AFT INBD FOLLOWER BEARING SUPPORT OF SLAT TRACK NR 5 AT LT WING. BEARING SUPPORT OF SLAT TRACK NR 5 AT LT WING WAS REPLACED IAW AMM 27-80-01.SDR FDEA201601270325Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORRODED. FOUND OUT OF LIMIT IAW CMM 57-44-09. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0322999 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201601270324Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORRODED. FOUND OUT OF LIMIT IAW CMM 57-44-09. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0322999 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201601270323Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORRODED. FOUND OUT OF LIMIT IAW CMM 57-44-09. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0322999 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR SIMA20160116004Hinge Fitting · corrodedLEFT SPOILER CTR HINGE FITTING ON WING IS CORRODED. R & R LT SPOILER CTR HINGE FITTING ON WING IAW AMM 57-51-02.SDR AALA201601209002Hinge Fitting · wornAIRCRAFT WAS IN BASE MX. RT WING SPOILER NR 2 HINGE CTR FITTING HAS AN AREA OF WEAR. REPAIRED FITTING IAW SRM 57-70-00 PARAGRAPH 4C FIG 201 SHEET 2.SDR ABXR201511172Linkage · wornFOUND LOOSE BUSHINGS IN FLAP SUPPORT LINKAGE 9 - 10 BEAM. BUSHINGS WERE REMOVED, HOLES IN LINKAGE OVERSIZED & OVERSIZED BUSHINGS WERE INSTALLED.SDR ABXR201511171Support · gougedDEFECTS BEYOND SRM LIMITS FOUND IN FLAP SUPPORT HOLES FOR FLAP SUPPORTS 1, 7 & 8 WHILE ACCOMPLISHING SB 767-57A0131. HOLES WERE OVERSIZED, OVERSIZE BOLTS INSTALLED.SDR AALA20151110011Fitting · crackedRIGHT WING GND SPOILER ACTUATOR CASTING, WING SIDE, IS CRACKED IN RADIUS AT FWD OTBD SIDE. R & R SPOILER ACTUATOR FITTING IAW SRM 51-30-02 & SRM 51-30-05.SDR DALA2015111006843Hinge · wornLEFT WING OTBD FLAP HINGE AT BS XW= 333 HAS PLAY AT HINGE POINT, LW. AFT FLAP HINGE, BOLT OF HINGE POINT, AND BUSHINGS OF LT WING OTBD FLAP HINGE AT BS XW=333.147 WERE REPLACED IAW CMM 27-50-5 AND AMM 27-51-01.SDR DALA2015102606425Trunnion · corrodedWEAR ON TRUNNION INBD FLAP FOUND OUT LIMITS LT WING. REPLACED TRUNNION IAW CMM 57-21-21-400-806-C01.SDR DALA2015102606424Trunnion · corrodedWEAR ON TRUNNION INBD FLAP FOUND OUT LIMITS. REPLACED TRUNNION OF INBD. FLAP RT IAW CMM 57-21-21-400-806-C01.SDR AALA20151015006Support Fitting · crackedRIGHT WING, GND SPOILER ACTUATOR SUPPORT FITTING CRACKED AT FWD INBD CHAMFER. REPLACED RT WING GND SPOILER SUPPORT FITTING WITH NEW FITTING.SDR DALA2015101506157Attach Bracket · crackedRIGHT WING AILERON INBD ACTUATOR ATTACH BRACKET OTBD LUG IS CRACKED, MEASURED AT .610". REPLACED RT WING INBD AILERON ACTUATOR ATTACH BRACKET IAW SRM 51-42-11.SDR FDEA201510023043Hinge · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE, FWD MOUNT INBD HOLE SURFACE CORRODED. REPAIRED IAW EA 1-5750-T0320588 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201510023042Hinge · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE, FWD MOUNT INBD HOLE BORE CORRODED. A REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0320588 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201510023041Hinge · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION.SDR FDEA201510023040Hinge · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION.SDR FDEA201510013028Hinge · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION.SDR FDEA201510013027Hinge · corrodedRIGHT WING OTBD FLAP FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION.SDR FDEA201510013026Hinge · corrodedRIGHT WING OTBD FLAP FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION.
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