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.

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 INCHESApr 19, 2016 · N613FE · Doug MD11FSDR 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 IApr 19, 2016 · N613FE · Doug MD11FSDR 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.Apr 19, 2016 · N613FE · Doug MD11FSDR 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 BUSHINGMar 29, 2016 · N612FE · Doug MD11FSDR 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 Mar 29, 2016 · N612FE · Doug MD11FSDR 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 FABRMar 29, 2016 · N612FE · Doug MD11FSDR 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 FABMar 29, 2016 · N612FE · Doug MD11FSDR 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 FABRIMar 29, 2016 · N612FE · Doug MD11FSDR 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 BUMar 29, 2016 · N612FE · Doug MD11FSDR 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 1.220Mar 29, 2016 · N612FE · Doug MD11FSDR 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".Mar 29, 2016 · N612FE · Doug MD11FSDR 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".Mar 29, 2016 · N612FE · Doug MD11FSDR 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 1.220Mar 29, 2016 · N612FE · Doug MD11FSDR 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 1.220Mar 29, 2016 · N612FE · Doug MD11FSDR 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".Mar 28, 2016 · N612FE · Doug MD11FSDR 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".Mar 28, 2016 · N612FE · Doug MD11FSDR 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". NEMar 28, 2016 · N612FE · Doug MD11FSDR 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". NMar 28, 2016 · N612FE · Doug MD11FSDR 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 0.7Mar 28, 2016 · N612FE · Doug MD11FSDR 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 RMar 27, 2016 · N612FE · Doug MD11FSDR 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.Mar 22, 2016 · N805HC · Aerosp ATR42500SDR 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.Feb 18, 2016 · N493AA · Doug DC982SDR 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.Jan 29, 2016 · N593FE · Doug MD11FSDR 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 Jan 29, 2016 · N593FE · Doug MD11FSDR 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 Jan 29, 2016 · N593FE · Doug MD11FSDR 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.Jan 29, 2016 · N593FE · Doug MD11FSDR 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.Jan 29, 2016 · N593FE · Doug MD11FSDR 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.Jan 29, 2016 · N593FE · Doug MD11FSDR 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.Jan 29, 2016 · N593FE · Doug MD11FSDR 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.Jan 27, 2016 · N996DL · Doug MD88SDR 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.Jan 27, 2016 · N593FE · Doug MD11FSDR 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.Jan 27, 2016 · N593FE · Doug MD11FSDR 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.Jan 27, 2016 · N593FE · Doug MD11FSDR 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.Jan 16, 2016 · N696AE · Emb EMB145LRSDR 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.Dec 23, 2015 · N672AW · Airbus A320232SDR ABXR201511172Linkage · wornFOUND LOOSE BUSHINGS IN FLAP SUPPORT LINKAGE 9 - 10 BEAM. BUSHINGS WERE REMOVED, HOLES IN LINKAGE OVERSIZED & OVERSIZED BUSHINGS WERE INSTALLED.Nov 17, 2015 · N673BF · Boeing 767238SDR 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.Nov 17, 2015 · N673BF · Boeing 767238SDR 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.Nov 10, 2015 · N965TW · Doug DC983SDR 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.Nov 9, 2015 · N907DL · Doug MD88SDR DALA2015102606425Trunnion · corrodedWEAR ON TRUNNION INBD FLAP FOUND OUT LIMITS LT WING. REPLACED TRUNNION IAW CMM 57-21-21-400-806-C01.Oct 25, 2015 · N359NW · Airbus A320212SDR DALA2015102606424Trunnion · corrodedWEAR ON TRUNNION INBD FLAP FOUND OUT LIMITS. REPLACED TRUNNION OF INBD. FLAP RT IAW CMM 57-21-21-400-806-C01.Oct 25, 2015 · N359NW · Airbus A320212SDR AALA20151015006Support Fitting · crackedRIGHT WING, GND SPOILER ACTUATOR SUPPORT FITTING CRACKED AT FWD INBD CHAMFER. REPLACED RT WING GND SPOILER SUPPORT FITTING WITH NEW FITTING.Oct 14, 2015 · N984TW · Doug DC983SDR 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.Oct 14, 2015 · N344NB · Airbus A319114SDR 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.Oct 2, 2015 · N624FE · Doug MD11FSDR 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.Oct 2, 2015 · N624FE · Doug MD11FSDR FDEA201510023041Hinge · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION.Oct 2, 2015 · N624FE · Doug MD11FSDR FDEA201510023040Hinge · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION.Oct 2, 2015 · N624FE · Doug MD11FSDR FDEA201510013028Hinge · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION.Oct 1, 2015 · N624FE · Doug MD11FSDR FDEA201510013027Hinge · corrodedRIGHT WING OTBD FLAP FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION.Oct 1, 2015 · N624FE · Doug MD11FSDR FDEA201510013026Hinge · corrodedRIGHT WING OTBD FLAP FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION.Oct 1, 2015 · N624FE · Doug MD11F
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