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 FDEA201910102565Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP, INBOARD FORWARD HINGE, WING SIDE LOWER MOUNT INBOARD HOLE SURFACE CORRODED. HOLE SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113SDR FDEA201910102562Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE WAS CORRODED. THE CORROSION WAS REWORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-575SDR FDEA201910102560Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), INBOARD ACTUATOR HOLE BORE FOUND CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, SDR FDEA201910102559Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE), OUTBOARD FWD MOUNT HOLE BORE FOUND CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-57SDR FDEA201910102556Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), INBOARD FWD MOUNT BORE WAS CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0SDR FDEA201910102555Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), UPPER MOUNT, OUTBOARD HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-TSDR FDEA201910102554Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER MOUNT OUTBOARD HOLE SURFACE CORRODED. SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1,SDR FDEA201910102553Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER MOUNT INBOARD HOLE SURFACE CORRODED. SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, SDR FDEA201910102552Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER MOUNT OUTBOARD HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, SDR FDEA201910102551Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1.SDR FDEA201910102550Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT HOLE BORE WAS CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T035001SDR FDEA201910102549Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1SDR FDEA201910102548Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), UPPER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP SDR FDEA201910102547Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED, AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750-T0350013 PART 1 STEP 1 . REPAIR SDR FDEA201910102546Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1. THE RSDR SWAA2022040585000Former · crackedFAIRING FORMER IS CRACKED AT BS 663 RBL 27 WL 142 / REPAIRED PER: EA 1-757-16635 REV IR AND ATS ER 19-05139 REV IRSDR FDEA2019100752450Hinge Bracket · corrodedRIGHT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07, AND EA 1-5750-T0330908 A, PART 1, STEP 1SDR FDEA2019100752449Hinge Bracket · corrodedLEFT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. CORROSION REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07, AND EA 1-5750-T0330906 A, PART 1, STEP 1, F(1), ANSDR FDEA2019100752447Hinge Bracket · corrodedLEFT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE SURFACE FOUND CORRODED. CORROSION REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-04 , REPAIR EVALUATED AND FOUND THE LEFT OUTBOARD FLAP AFT INBOARD HINGE PIVOT INBOARD LUG SURFACE REMSDR FDEA2019100752446Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORRODED. CORROSION WORKED AND IAW CMM 57-44-08 FOUND TO EXCEED LIMITS. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-08 AND EA 1-5750-T0349923, PART 1, STEP 3. THESDR FDEA201910032430Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TOE EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PARSDR FDEA201910032429Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, SDR FDEA201910032428Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, SDR FDEA201910032427Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349923, PART 1, STEP 3B, AND INSTALLED IAW CSDR FDEA201910032426Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349923, PART 1, STEP 3B, AND INSTALLED IAW CMM SDR FDEA201910032425Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT BORE FOUND CORRODED. WORKED THE CORROSION AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, PART 1, STEP 3A, AND SDR FDEA201910032424Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG BORE WAS FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T034988SDR FDEA201910032423Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PARTSDR FDEA201910032422Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT, OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349887, PART 1, STEP 3B, AND INSTALLED SDR FDEA201910032421Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT, INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349887, PART 1, STEP 3B, AND INSTALLED IAW CMSDR FDEA201910032420Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT, INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PARTSDR FDEA2019100322399Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750- T0349884, PART 1, STEP 3A, AND INSTALLED IAW CMM 57SDR FDEA2019100312389Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE LOWER MOUNT, OUTBOARD BORE WAS FOUND CORRODED. THE CORROSION WAS WORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349884, PART 1, STEP 3A, AND INSTALLSDR FDEA2019100312388Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE LOWER MOUNT, INBOARD BORE SURFACE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PARSDR FDEA201910012387Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE BRACKET, INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PSDR FDEA2019100312386Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE BRACKET, OUTBOARD LUG BORE WAS FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PSDR FDEA2019100312385Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE FITTING OTBD LUG BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PART 1, STEP 3C, SDR FDEA2019100312384Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE ACTUATOR, INBOARD LUG BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PART 1, STEPSDR FDEA2019100312383Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750- T0349824, PART 1, STEP 3,SDR FDEA2019100312382Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW CMM 57- 44-09 AND EA 1-5750-T0349824, PART 1, STSDR FDEA2019100312381Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. WORKED THE CORROSION AND FOUND EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750-T0349824, PART 1, STEP 3B, AND SSDR FDEA201909192286Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. RESDR FDEA201909192285Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPASDR FDEA201909192284Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPASDR FDEA201909192283Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAISDR FDEA201909102195Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT SURFACE REWORKED AS PER CMM 57-44-09 AND FOUND LOWER BARREL NUT FACE EXCEED LIMIT BASE THE DIFFESDR FDEA201909082156Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-07. OVERSIZED BUSHING FABRICATED BY MSDR FDEA201909052108Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-07. OVERSIZED BUSHING FABRICATED BY MACSDR FDEA201909032079Hinge Fitting · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVESDR FDEA201909032078Hinge Fitting · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERS
Back to JASC 5744