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 FDEA201611234215Hinge Fitting · corrodedRIGHT WING, FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE FOUND CORRODED.SDR FDEA201611234214Hinge Bracket · corrodedRIGHT WING - OUTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE FOUND WITH CORROSION. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-70329763 PART 1 STEP 1B.SDR FDEA201611234213Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD FWD HINGE (WING SIDE) BARREL NUTS HOLE BORE CORROSION. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1D.SDR FDEA201611234212Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD FWD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE FOUND WITH CORROSION. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0329763. PART 1 STEP 1B.SDR FDEA201611234211Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FOUND WITH SURFACE CORROSION. REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1.SDR FDEA201611234210Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE SURFACE CORROSION. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1.SDR FDEA201611234209Hinge Bracket · corrodedRIGHT WING, OUTBD FLAP OTBD FWD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750- T0329763 PART 1 STEP 1A AND STEP 1.SDR FDEA201611234208Hinge Bracket · corrodedRIGHT HAND WING - OUTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750- T0329763 PART 1 STEP 1A AND STEP 1.SDR AALA201611169004Pivot · corrodedCORROSION ON LEFT WING OUTBOARD FLAP TRACK NR 3 PIVOT BOLT. REPLACED PIVOT BOLT IAW AMM 27-54-62-000-001-A AND AMM 27-54-62-400-001-A.SDR AALA201611159027Bolt · corrodedCORROSION ON RIGHT WING SLAT TRACK 10 LOWER MIDDLE BOLT BETWEEN RIBS 20-22. REPLACED LOWER MIDDLE BOLT IAW AMM 27-84-66.SDR FDEA201609183299Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1A.SDR FDEA201609183298Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE. LOWER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1B.SDR FDEA201609183297Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1B AND STEP 1.SDR FDEA201609183296Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED EA 1-5750-T0328351 PART 1 STEP 1C.SDR FDEA201609183295Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1C.SDR FDEA201609183294Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1 STEP 1A AND STEP 1.SDR FDEA201609183293Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1A AND STEP 1.SDR AALA201609289020Hinge · corrodedAIRCRAFT IN BASE MAINTENANCE. RUSTED LEFT REAR SPAR AILERON NR 3 HINGE BEARING AT -Y13751L. REPLACED AILERON NR 3 HINGE PER SRM 57-61-01.SDR FDEA201609163283Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1C.SDR FDEA201609163282Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1C.SDR FDEA201609163281Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, FWD MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR WAS BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1B.SDR FDEA201609163280Hinge · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE, WING SIDE LOWER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. FABRICATED A REPAIR BUSHING AND INSTALLED IAW EA 1-5750-T0328311 PART 1 STEP 1.SDR FDEA201609163279Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE LOWER MOUNT OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE: DIA 0.707", FINAL HOLE: DIA 0.729", MAXIMUM ALLOWABLE HOLE: DIA 0.709". REPAIR BUSHING FABRICATED ANDSDR FDEA201609163278Hinge · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE, WING SIDE ACTUATOR INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE: DIA 1.246", FINAL HOLE: DIA 1.250", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED ASDR FDEA201609163277Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE ACTUATOR OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 1.220", FINAL HOLE: DIA 1.224", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED ANSDR FDEA201609163276Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE ACTUATOR INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE: DIA 1.249", FINAL HOLE: DIA 1.252", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND ISDR FDEA201609163275Hinge · corrodedRT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER BARREL NUT HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE: DIA 0.406", FINAL HOLE: DIA 0.421", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED AND ISDR FDEA201609163274Hinge Bracket · corrodedRT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE UPPER BARREL NUT HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 0.406", FINAL HOLE: DIA 0.421", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED ANSDR FDEA201609163273Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT, OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 0.582", FINAL HOLE: DIA 0.598", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATESDR FDEA201609163272Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 0.582", FINAL HOLE: DIA 0.598", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATEDSDR AALA201609059014Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT AILERON NR 4 HINGE FITTING FAILED BACKLASH CHECK. REPLACED HINGE FITTING IAW AMM 57-61-00-000-801.SDR AALA201609059013Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT AILERON NR 3 HINGE FITTING FAILED BACKLASH CHECK. REPLACED HINGE FITTING IAW AMM 57-61-00-000-801.SDR AALA201609059012Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT AILERON NR 2 HINGE FITTING FAILED BACKLASH CHECK. REPLACED HINGE FITTING IAW AMM 57-61-00-000-801.SDR AALA201609059011Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LT AILERON NR 1 HINGE FITTING FAILED BACKLASH CHECK. REPLACED HINGE FITTING IAW AMM 57-61-00-000-801.SDR AALA201609099007Bolt · corrodedCORROSION ON LEFT WING FORWARD BOLT AT THE NR 1 SLAT, TRACK NR 4 BETWEEN RIB 5 - 6. REPLACED FORWARD BOLT IAW AMM 27-84-63-400-002-A.SDR AALA201609099006Bolt · corrodedCORROSION ON LEFT WING UPPER FORWARD SLAT BOLT AT SLAT NR 5, TRACK NR 12 BETWEEN RIB 25 - 26. REPLACED THE SLAT BOLT IAW AMM 27-84-67-400-002-A.SDR AALA201609089006Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LT WING UPPER SLAT BOLT AT SLAT NR 5, TRACK NR 11 BETWEEN RIB 23-24. REPLACED SLAT BOLT IAW AMM 27-84-67-400-002-A STEP 4C, 2, A, B, F, H, M AND 4D, 13.SDR AALA201609089005Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE, CORROSION ON LT WING UPPER FORWARD SLAT BOLT AT SLAT NR 2, TRACK NR 6 BETWEEN RIB 11-12. REPLACED SLAT BOLT IAW AMM 27-84-64-000-001-A AND AMM 27-84-64-400-002-A.SDR AALA201609089004Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE, CORROSION ON LT WING UPPER AFT SLAT BOLT AT SLAT NR 5, TRACK NR 12 BETWEEN RIB 25-27. REPLACED SLAT BOLT IAW AMM 27-84-67-400-002-A, STEP 4C, 2, A, B, F, H, M AND 4D 13.SDR AALA201609149004Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LT WING SPOILER NR 2 INBD HINGE PIN BETWEEN RIB 11-12. REPLACED HINGE PIN IAW AMM 27-64-42-400-001-A.SDR AALA201609089002Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE, CORROSION ON RT WING LOWER SLAT BOLT AT SLAT NR 3, TRACK NR 8, RIB 16-17. REPLACED LOWER SLAT BOLT IAW AMM 27-84-65-400-002-A.SDR AALA201609079017Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON RT WING SPOILER NR 5 INBD INNER HINGE PIN BETWEEN RIB 20-21. REPLACED INNER HINGE PIN IAW AMM 27-64-45-400-001-A.SDR AALA201609079013Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE, CORROSION ON RT WING SPOILER NR 4 INBD INNER HINGE PIN BETWEEN RIB 17-18. REPLACED INNER HINGE PIN IAW AMM 27-64-44-400-001-A.SDR AALA201609069013Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RT WING TRACK NR 4 PIVOT BOLT BETWEEN RIB 19-20. REPLACED PIVOT BOLT IAW AMM 27-54-62-000-001-A AND AMM 27-54-62-400-001-ASDR FDEA201607132433Hinge · corrodedRIGHT WING, INBD FLAP OTBD FWD HINGE, WING SIDE, PIVOT BORE FOUND, CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-07. EXISTING HOLE DIA: 2.531", FINAL HOLE DIA: 2.536" AND MAXIMUM ALLOWABLE HOLE DIA: 2.531". NEW REPAIR BUSHING FABRICATED AND INSSDR FDEA201607132430Hinge · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR ATTACH OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.221", FINAL HOLE DIA: 1.225", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATEDSDR FDEA201607132429Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR ATTACH INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.221", FINAL HOLE DIA: 1.225", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED ASDR FDEA201607132428Hinge · corrodedRT WING, OTBD FLAP, OTBD FWD HINGE UPPER MOUNT INBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.880", FINAL HOLE: DIA 0.953", MAXIMUM ALLOWABLE HOLE: DIA 0.944". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5SDR FDEA201607132427Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE UPPER MOUNT OTBD BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT CMM 57-44-09. EXISTING HOLE: DIA 0.880". FINAL HOLE: DIA 0.953". MAXIMUM ALLOWABLE HOLE: DIA 0.944", REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-575SDR FDEA201607132426Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE UPPER MOUNT, INBD BORE SURFACE AREA CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.715", MATERIAL REMOVED: 0.003", REMAINING THICK: 0.712". MINIMUM ALLOWABLE THICKNESS: 0.720". REPA
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