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 FDEA201611234215Hinge Fitting · corrodedRIGHT WING, FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE FOUND CORRODED.Nov 23, 2016 · N603FE · Doug MD11SDR 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.Nov 23, 2016 · N603FE · Doug MD11FSDR 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.Nov 23, 2016 · N603FE · Doug MD11FSDR 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.Nov 23, 2016 · N603FE · Doug MD11FSDR 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.Nov 23, 2016 · N603FE · Doug MD11FSDR 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.Nov 23, 2016 · N603FE · Doug MD11FSDR 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.Nov 23, 2016 · N603FE · Doug MD11FSDR 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.Nov 23, 2016 · N603FE · Doug MD11FSDR 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.Nov 11, 2016 · N105UW · Airbus A320214SDR AALA201611159027Bolt · corrodedCORROSION ON RIGHT WING SLAT TRACK 10 LOWER MIDDLE BOLT BETWEEN RIBS 20-22. REPLACED LOWER MIDDLE BOLT IAW AMM 27-84-66.Nov 8, 2016 · N105UW · Airbus A320214SDR 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.Sep 18, 2016 · N617FE · Doug MD11FSDR 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.Sep 18, 2016 · N617FE · Doug MD11FSDR 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.Sep 18, 2016 · N617FE · Doug MD11FSDR 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.Sep 18, 2016 · N617FE · Doug MD11FSDR 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.Sep 18, 2016 · N617FE · Doug MD11FSDR 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.Sep 18, 2016 · N617FE · Doug MD11FSDR 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.Sep 18, 2016 · N617FE · Doug MD11FSDR 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.Sep 16, 2016 · N945UW · Emb ERJ190100IGWSDR 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.Sep 16, 2016 · N617FE · Doug MD11FSDR 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.Sep 16, 2016 · N617FE · Doug MD11FSDR 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.Sep 16, 2016 · N617FE · Doug MD11FSDR 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.Sep 16, 2016 · N617FE · Doug MD11FSDR 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 ANDSep 16, 2016 · N617FE · Doug MD11FSDR 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 ASep 16, 2016 · N617FE · Doug MD11FSDR 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 ANSep 16, 2016 · N617FE · Doug MD11FSDR 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 ISep 16, 2016 · N617FE · Doug MD11FSDR 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 ISep 16, 2016 · N617FE · Doug MD11FSDR 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 ANSep 16, 2016 · N617FE · Doug MD11FSDR 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 FABRICATESep 16, 2016 · N617FE · Doug MD11FSDR 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 FABRICATEDSep 16, 2016 · N617FE · Doug MD11FSDR 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.Aug 27, 2016 · N963UW · Emb ERJ190100IGWSDR 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.Aug 27, 2016 · N963UW · Emb ERJ190100IGWSDR 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.Aug 27, 2016 · N963UW · Emb ERJ190100IGWSDR 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.Aug 27, 2016 · N963UW · Emb ERJ190100IGWSDR 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.Aug 14, 2016 · N102UW · Airbus A320214SDR 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.Aug 13, 2016 · N102UW · Airbus A320214SDR 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.Aug 13, 2016 · N102UW · Airbus A320214SDR 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.Aug 13, 2016 · N102UW · Airbus A320214SDR 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.Aug 13, 2016 · N102UW · Airbus A320214SDR 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.Aug 12, 2016 · N102UW · Airbus A320214SDR 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.Aug 12, 2016 · N102UW · Airbus A320214SDR 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.Aug 12, 2016 · N102UW · Airbus A320214SDR 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.Aug 12, 2016 · N102UW · Airbus A320214SDR 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-AAug 12, 2016 · N102UW · Airbus A320214SDR 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 INSJul 13, 2016 · N582FE · Doug MD11FSDR 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 FABRICATEDJul 13, 2016 · N582FE · Doug MD11FSDR 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 AJul 13, 2016 · N582FE · Doug MD11FSDR 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 1-5Jul 13, 2016 · N582FE · Doug MD11FSDR 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 1-575Jul 13, 2016 · N582FE · Doug MD11FSDR 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". REPAJul 13, 2016 · N582FE · Doug MD11F
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