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 AALA201712059004Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE. RIGHT AILERON FAILED BACKLASH FUNCTIONAL TEST. REPLACED AILERON HINGE FITTING NR 2 PER AMM 57-61-00-000-81.SDR AALA201712059003Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE. RIGHT AILERON FAILED BACKLASH FUNCTIONAL TEST. REPLACED AILERON HINGE FITTING NR 1 PER AMM 57-61-00-000-801.SDR FDEA201711083191Hinge · corrodedRT WING I/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0331058A P1 STEP F(1) AND STEP F (3). RT WING INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201711083190Hinge · corrodedLT WING INBD FLAP OUTBD FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0331052A P1 STEP F(1) AND STEP F (3). LT WING INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100SDR FDEA201710233025Hinge Bracket · wornLEFT FWD WING SIDE INBD FLAP FWD OTBD HINGE PIVOT BORE WORN. FOUND THE INDB & OTBD FACE OUT OF LIMITS IAW CMM 57-44-07. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-87635F, P2, STEP 1F (1) AND STEP 1F (3). THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMMSDR V0XD20171009006Attach Bracket · crackedRIGHT SLAT TRACK CANISTER 1 - 3 HAS A CRACKED ATTACH BRACKET. FABRICATED AND INSTALLED THE ATTACH BRACKET IAW REO 67057-42-577.SDR FDEA201710052859Hinge Bracket · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. REWORKED IAW CMM 57-44-09. OUT OF LIMITS, A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335621, PART 1, STEP 2.SDR FDEA201709282772Hinge · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. RH WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08 EXISTING HOLE: 1.224", FINAL HOLE: 1.229SDR FDEA201709282771Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 1.2235", FINAL HOLE 1.229", MAXIMUM ALLOWABLE HOLE 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-SDR FDEA201709282770Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE 0.708", FINAL HOLE 0.712", MAXIMUM ALLOWABLE HOLE 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750-T0SDR FDEA201709282769Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.709", FINAL HOLE: 0.712", MAXIMUM ALLOWABLE HOLE: 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750SDR FDEA201709282768Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING THICKNESS: 760", MATERIAL REMOVED: 0.050", REMAINING THICKNESS: 0.710", MINIMUM ALLOWABLE THICKNESS: 0.720", REPAIR SDR FDEA201709282767Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT I/B BORE SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING THICKNESS: 0.729", MATERIAL REMOVED: 0.026" REMAINING THICKNESS: 0.703". REPAIR SHIM FABRICATED AND INSTALLED AS PERSDR FDEA201709282766Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.948", FINAL HOLE: 0.951", MAXIMUM ALLOWABLE HOLE: 0.944". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-575SDR FDEA201709282765Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.9535", FINAL HOLE: 0.957", MAXIMUM ALLOWABLE HOLE: 0.944". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-57SDR FDEA201709282764Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 2.317", FINAL HOLE: 2.321", MAXIMUM ALLOWABLE HOLE: 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750-T033562SDR FDEA201709282763Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT, OTBD BORE SURFACE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PT 1, STEP 1.SDR FDEA201709282762Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) FWD MOUNT, OTBD LUG SURFACE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA 1-5750-T0335603, PART 1, STEP 1.SDR FDEA201709282761Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR ATTACH OTBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1E.SDR FDEA201709282760Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR ATTACH INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1E.SDR FDEA201709282759Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) BARREL NUT HOLE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1F.SDR FDEA201709282758Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1B, AND STEP 1.SDR FDEA201709282757Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) LOWER MOUNT INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1B, AND STEP 1.SDR FDEA201709282756Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) UPPER MOUNT INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1A.SDR FDEA201709272750Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) UPPER MOUNT OTBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1A.SDR FDEA201709272749Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1C.SDR FDEA201709272748Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE: DIA: 1.222", FINAL HOLE: DIA: 1.228", MAXIMUM ALLOWABLE HOLE: DIA: 1.220". OVERSIZED BUSHING FABRICATED AND INSTASDR FDEA201709272747Hinge Arm · corrodedLT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE: DIA: 1.224", FINAL HOLE: DIA: 1.228", MAXIMUM ALLOWABLE HOLE: DIA: 1.220". OVERSIZED BUSHING FABRICATED AND INSTASDR FDEA201709272746Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD BORE CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1B, AND STEP 1.SDR FDEA201709272745Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) LOWER MOUNT INBD BORE CORRODED. THE BORE CORROSION WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. FABRICATED AND INSTALLED A REPAIR IAW 1-5750-T0335583, PART 1, STEP 1B, AND STEP 1.SDR FDEA201709272744Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. CORROSION WAS WORKED IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1.SDR FDEA201709272743Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. CORROSION FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1A.SDR FDEA201709272742Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 1.253", FINAL HOLE: 1.259", MAXIMUM ALLOWABLE HOLE; 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1SDR FDEA201709272741Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 1.252", FINAL HOLE: 1.259", MAXIMUM ALLOWABLE HOLE: 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1SDR FDEA201709272740Hinge Arm · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.692", FINAL HOLE: 0.702", MAXIMUM ALLOWABLE HOLE: 0.667". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T03SDR FDEA201709272739Hinge · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT LOWER BOLT HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.3255", FINAL HOLE: 0.408", MAXIMUM ALLOWABLE HOLE: 0.391". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER ESDR FDEA201709272738Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.390", FINAL HOLE: 0.408", MAXIMUM ALLOWABLE HOLE: 0.391". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EASDR FDEA201709272737Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.586", FINAL HOLE: 0.597", MAXIMUM ALLOWABLE HOLE: 0.584". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750SDR FDEA201709272736Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.586", FINAL HOLE: 0.597", MAXIMUM ALLOWABLE HOLE: 0.584". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750SDR FDEA201709272735Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 2.3165", FINAL HOLE: 2.322", MAXIMUM ALLOWABLE HOLE: 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T03356SDR AALA20170926006Hinge Fitting · corrodedCORROSION ON LEFT WING OUBOARD FLAP LOWER INBD SIDE OF CENTER HINGE FITTING AT STUD. REMOVED AND REPLACED THE HINGE FITTING IAW AMM 57-40-01-201.SDR FDEA201709252710Hinge Bracket · corrodedRIGHT WING INBD FLAP OTBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T033099 A, PART 1, STEP 1F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709252709Hinge Bracket · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE) PIVOT OTBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533C-PT5, STEP 2B, AND 2A. . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2SDR FDEA201709252705Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR ATTACH OTBD BORE CORRDED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330993 A, PART 1, STEP 1F. REPAIR CLASSIFEID AS MAJOR IAW SDR FDEA201709252704Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD HINGE (WING SIDE) ACTUATOR ATTACH INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330993, PART 1, STEP 1F. REPAIR CLASSIFEID AS MAJOR IAW GMSDR FDEA201709122508Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR OTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122507Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122506Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED, AND FOUND OUT OF LIMIT IAW CMM 57-44-08. THE OTBD FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122505Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122503Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE RIGHT WING OTBD FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.
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