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 FDEA201702120526Hinge Bracket · corrodedRIGHT WING, INBD FLAP, FWD (WING SIDE) OTBD HINGE PIVOT HOLE BORE CORRODED. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07 AND EA 1-5750-73360 D, PART 3, STEP 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201702020338Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE, WING SIDE, ACTUATOR INBD HOLE SURFACE CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1.SDR FDEA201702020337Hinge · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE, WING SIDE, ACTUATOR OUTBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1C.SDR FDEA201702020336Hinge · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1C.SDR FDEA201702020335Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE SURFACE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1.SDR FDEA201702020334Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE SURFACE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1.SDR FDEA201702020333Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE CORRODED. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1, AND STEP 1B.SDR FDEA201702020332Hinge Bracket · corrodedRIGHT HAND WING OUTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE CORRODED. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1, AND STEP 1B.SDR FDEA201702020331Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1A.SDR FDEA201702020330Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD FWD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133 PART 1, STEP 1A.SDR FDEA201702020329Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1B.SDR FDEA201702020328Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1B.SDR FDEA201702020327Hinge · corrodedRIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1, AND STEP 1A.SDR FDEA201702020326Hinge · corrodedRIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1, AND STEP 1A.SDR FDEA201702020325Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1B.SDR FDEA201702020324Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1B.SDR FDEA201702020323Hinge Bracket · corrodedLEFT WING OTBD FLAP FWD INBD HINGE (WING SIDE) UPPER MOUNT OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1A.SDR FDEA201702020322Hinge Bracket · corrodedLEFT WING OTBD FLAP FWD INBD HINGE (WING SIDE) UPPER MOUNT INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1A.SDR FDEA201702020321Hinge Bracket · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331076, PART 1, STEP 1B.SDR FDEA201702020320Hinge · corrodedLEFT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44- 09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331076, PART 1, STEP 1B.SDR FDEA201702020319Hinge · corrodedLEFT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE SURFACE CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. TWO SHOULDER BUSHINGS AND REPAIR SHIMS FABRICATED AND INSTALLED IAW EA 1-5750-T0331076, PART 1, STEP SDR AALA20170129008Hinge Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND WING OUTBOARD FLAP CENTER HINGE FITTING. REPLACED HINGE FITTING PER CMM 27-50-02.SDR FDEA201701250248Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD FORWARD HINGE BRACKET PIVOT BORE FOUND CORRODED. CORROSION REWORKED AND FOUND WITHIN LIMITS IAW 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW 57-44-07 AND EA 1-5750-T0330596A, PART 1, STEP 1F. THE REPAIR WAS SDR FDEA201701250247Hinge Bracket · corrodedLEFT WING- INBD FLAP OTBD FWD HINGE BRACKET PIVOT BORE FOUND CORRODED. CORROSION REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-07 AND EA 1-5750-T0330593 A, PART 1, STEP 1. REPAIR CLASSIFIED AS MAJSDR FDEA201701150172Hinge Bracket · corrodedRT HAND WING OUTBD FLAP OUTBD FWD HINGE BRACKET UPPER INBOARD MOUNT BORE FOUND CORROSION. CORROSION AT RT WING O/B FLAP O/B FWD HINGE BRACKET UPPER INBD MOUNT BORE NR 2 HOLE. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA. 0.943", FINALSDR FDEA201701150171Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE BRACKET UPPER OUTBOARD MOUNT BORE FOUND CORROSION. HINGE BRACKET REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.943", FINAL HOLE DIA 0.952" MAXIMUM ALLOWABLE HOLE DIA 0.944 OVERSIZE BUSHINGSDR FDEA201701150170Hinge Bracket · corrodedRT WING OUTBD FLAP OUTBD FWD HINGE BRACKET SIDE ATTACH UPPER BORE FOUND CORROSION. CORROSION AT RT WING O/B FLAP O/B FWD HINGE BRACKET UPPER O/B MOUNT BORE. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZE BUSHING WAS FABRICATED AND INSTALLED ISDR FDEA201701150169Hinge Bracket · corrodedRT WING OUTBD FLAP OUTBD FWD HINGE BRACKET SIDE ATTACH LOWER BORE FOUND CORROSION. CORROSION AT RT WING O/B FLAP O/B FWD HINGE BRACKET UPPER O/B MOUNT BORE. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA. 0.389", FINAL HOLE DIA. 0.409" SDR FDEA201701150168Hinge Bracket · corrodedRT WING OUTBD FLAP OUTBD FWD HINGE BRACKET ACTUATOR OUTBD LUG BORE FOUND CORROSION. CORROSION AT RT WING O/B FLAP O/B FWD HINGE BRACKET UPPER O/B MOUNT BORE. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA. 1.248", FINAL HOLE DIA 1.256" SDR FDEA201701130147Hinge Bracket · corrodedLEFT WING, INBD FLAP FWD HINGE BRACKET PIVOT SPOT FACE FOUND CORRODED. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. REPAIRED IAW EA 1-5750-T0330593 A, PART 1, STEP 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201701130146Hinge Bracket · corrodedLEFT WING, INBD FLAP AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE FOUND CORRODED. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-74282 C, PART 5, STEP 2A & 2B. REPAIR CLASSIFIED AS MAJSDR FDEA201701130143Bracket · corrodedRIGHT WING INBD FLAP INBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZE BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-74277, D, PART 5, STEP 2A & 2B. REPAIR CLASSIFIED ASSDR DALA2016120509536Hinge Fitting · crackedRIGHT WING REAR SPAR LOWER CAP INBD HINGE FITTING AT XRS 164 SHOWS A CRACK INDICATION. REPAIRED IAW DRAWING J060271-510 AND ER/A 552142-14AD, REV. ORIG.SDR FDEA201611284261Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329456A P1, STEP 1F.SDR FDEA201611264246Hinge Fitting · corrodedLEFT WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. A WASREPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-72644C PART 2 STEP 1.F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611234230Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE SURFACE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1.SDR FDEA201611234229Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1C.SDR FDEA201611234228Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1C.SDR FDEA201611234227Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) UPPER MOUNT INBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1A.SDR FDEA201611234226Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1B.SDR FDEA201611234221Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1C.SDR FDEA201611234220Hinge Bracket · corrodedLEFT WING OTBD, FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09, A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1C.SDR FDEA201611234219Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1A AND DTEP 1.SDR FDEA201611234218Hinge Bracket · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1A AND 1.SDR FDEA201611234217Hinge Bracket · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1B.SDR FDEA201611234225Hinge Bracket · corrodedRIGHT WING OUTBD FLAP, INBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO329708 PART 1STEP 1A AND STEP 1.SDR FDEA201611234224Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-7-TO329708 PART 1 STEP 1A AND STEP 1.SDR FDEA201611234223Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR OTBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO329708 PART 1 STEP 1A AND STEP 1.SDR FDEA201611234222Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO329708 PART 1STEP 1B AND STEP 1.SDR FDEA201611234216Hinge Bracket · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE FOUND WITH CORROSION. FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1C.
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