JASC 5753
Service difficulty reports · 31,521
Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753' 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 = '5753' 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 USAA040390Roller · chafedPIT - FOUND SUPPORT FLAP ROLLER CHAFED .5 INCH BY 1 INCH AREA, FT AFT FLAP NR 1 OUTBOARD ROLLER ARM. REPLACED WITH AFT FLAP PER MM 27-51-39. (M)SDR P5CA0401166Fairing · delaminatedDELAMINATION SEVERAL AREA OF NR 4 FLAP TRACK AFT FAIRING L/W. REMOVED DAMAGE AREA PER SRM 51-40-15, BONDED REPAIR PER SRM 51-40-15.SDR P5CA0401165Flap Track · delaminatedDELAMINATION SEVERAL AREA O/B SIDE OF NR 2 FLAP TRACK AFT FAIRING R/W. REMOVED DAMAGED AREA PER SRM 51-40-15, BONDED REPAIRED PER SRM 51-40-12.SDR 04FDEA02313Roller · wornRT IB FLAP TRACK LOWER LOAD ROLLER WORN. REMOVED AND REPLACED LOWER LOAD ROLLER ON RT IB FLAP TRACK. INSTALLED AND TORQUED IAW EA 8-5750-80957 T.W. NR 8381H DUE 12-08-04. REF. N/R 00645SDR 04FDEA02312Roller · wornRT IB FLAP TRACK UPPER LOAD ROLLER WORN. REMOVED RT IB FLAP TRACK UPPER LOAD ROLLER AND REPLACED INSTALLED AND TORQUED IAW EA 8-5750-80957 T.W. NR 8381H, DUE 12-08-04. REF N/R N00646.SDR 04FDEA02311Roller · wornRIGHT HAND INBOARD FLAP MID TRACK ROLLER WORN. REMOVED AND REPLACED MID TRACK ROLLER ON RIGHT HAND INBOARD TRACK. INSTALLED AND TORQUED IAW FEDEX EA 8-5750-80957 TW 8381H DUE 12-08-04.SDR USAA040499Skin · delaminatedPIT - FOUND TOP SKIN DENTED WITH DELAMINATION, 1.5 INCH BY .025 INCH AREA, LEFT INBOARD FOREFLAP TOP CAMBER 58 INCHES FROM OUTBOARD END. INSTALLED TOP DOUBLER WITH FILLER MATERIAL PER BOEING SRM 51-70-10. (M)SDR 2004F00369Brace · crackedDURING FA02 A-CHECK ACCOMPLISHING ATLAS AIR ROUTINE WORK CARD 11FM15002, INSPECTION OF LEFT WING FOUND NR 4 FLAP CANOE FAIRING TO TRACK FORWARD OUTBOARD FITTING CRACKED IN HALF. (M) T64RSDR 2004FA0000693Brace · crackedDURING A-CHECK ACCOMPLISHING ATLAS AIR ROUTINE WORK CARD 11FM15002 INSPECTION OF LEFT WING FOUND NR 4 FLAP CANOE FAIRING TO TRACK FORWARD OUTBOARD FITTING CRACKED IN HALF. JETIIIB WORK ORDER 1063 NON-ROUTINE NR 132.SDR 04FDEA02293Hinge · corrodedLT WING, IB FLAP OB HINGE (FLAP SIDE) PIVOT HOLE NR 1, OB BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 PAGES 442 TO 443. ORIGINAL DIAMETER= 1.187, FINAL DIAMTER= 1.257" AND REPAIRED AS PER FEDEX EA 1-5750-80283, TITLE: WISDR 04FDEA02290Vane · corrodedRT WING INBOARD FLAP FLAP VANE NR 3 VANE TO TRACK SUPPORT ASSEMBLY HOLES FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. FINAL HOLE DIAMETER FORWARD=0.688, MIDDLE=0.688, AND AFT=0.748. BUSHINGS FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5SDR 04FDEA02289Vane · corrodedRT WING INBOARD FLAP FLAP VANE NR 1 VANE TO TRACK SUPPORT ASSEMBLY HOLES FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. FINAL HOLE DIAMETER FORWARD=0.748, MIDDLE=0.748, AND AFT=0.748. BUSHINGS FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-57SDR 04FDEA02288Vane · corrodedLT WING INBOARD FLAP FLAP VANE NR 3 VANE TO TRACK SUPPORT ASSEMBLY HOLES FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. FINAL HOLES DIAMETER FORWARD=0.688, MIDDLE=0.748, AND AFT=0.748. BUSHINGS FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-SDR 04FDEA02287Vane · corrodedLT WING INBOARD FLAP FLAP VANE NR 1 VANE TO TRACK SUPPORT ASSEMBLY HOLES FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. FINAL HOLES DIAMETER FORWARD=0.688, MIDDLE=0.748, AND AFT=0.748. BUSHINGS FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-SDR UIEA200400130Housing · corrodedDUIRNG SCHEDULED MAINTENANCE, FOUND CORROSION DAMAGE AT THE MAIN BEARING HOUSING BORE OF THE LEFT WING INBOARD TRAILING EDGE MID-FLAP CARRIAGE BEARING HOUSINGS ASSEMBY. REAMED BORE TO 6.100 INCHES DIAMETER AND REMOVED LOCAL SURFACE DAMAGE FROM AFFECTED AREA OFSDR SWAA042150Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD AFT T/E FLAP PER MM.SDR 04FDEA02258Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER= 1.075 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOASDR 04FDEA02257Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.500, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0.494 AND REPAIRED AS PER FEDEX EASDR 04FDEA02256Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.415, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.408 AND REPAIRED AS PER FEDEXSDR 04FDEA02255Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093, FINAL DIAMTER= 1.129 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARDSDR 04FDEA02254Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER= 1.074 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOSDR 04FDEA02253Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.504, MATERIAL REMOVED = 0.024, REMAINING THICKNESS = 0.480 AND REPAIRED AS PER FEDEX EASDR 04FDEA02252Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.510, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.505 AND REPAIRED AS PER FEDEX ESDR 04FDEA02251Hinge · corrodedRT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093, FINAL DIAMTER= 1.105 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBSDR 04FDEA02250Hinge · corrodedRT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER=1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RIGHTSDR 04FDEA02249Hinge · corrodedRT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.499, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.494 AND REPAIRED AS PER FEDEXSDR 04FDEA02248Hinge · corrodedRT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.408, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.401 AND REPAIRED AS PER FEDSDR 04FDEA02247Hinge · corrodedRT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER= 1.192 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OSDR 04FDEA02246Hinge · corrodedRT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 1 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER=1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBSDR 04FDEA02245Hinge · corrodedRT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.405, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.398 AND REPAIRED AS PER SDR 04FDEA02244Hinge · corrodedRT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAPSIDE) ACTUATOR HOLE NR 1 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER= 1.220 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTSDR 04FDEA02243Hinge · corrodedRT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.413, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0.407 AND REPAIRED AS PER FESDR 04FDEA02242Hinge · corrodedLT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER= 1.062, FINAL DIAMTER= 1.125 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT OUTSDR 04FDEA02241Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.510, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.505 AND REPAIRED AS PESDR 04FDEA02240Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.500, MATERIAL REMOVED = 0.009, REMAINING THICKNESS = 0.491 AND REPAIRED AS PERSDR 04FDEA02239Fitting · corrodedLEFT HAND WING - INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING AFT HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER=0.876, FINAL DIAMETER=0.8932. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-80310, TISDR 04FDEA02238Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.394, MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.390 AND REPAIRED ASDR 04FDEA02237Fitting · corrodedLEFT HAND WING - INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER=0.876, FINAL DIAMETER=0.8784. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-80310,SDR 04FDEA02236Fitting · corrodedLEFT HAND WING - INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING FORWARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8794. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-8SDR 04FDEA02235Vane · corrodedLEFT HAND WING - INBOARD FLAP - FLAP VANE INBOARD TEE FITTING AFT HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.882. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-80313,SDR 04FDEA02234Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.408, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0.402 AND REPAIRED ASSDR 04FDEA02233Vane · corrodedLEFT HAND WING - INBOARD FLAP - FLAP VANE INBOARD TEE FITTING MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8772. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-80313SDR 04FDEA02232Vane · corrodedLEFT HAND WING - INBOARD FLAP - FLAP VANE INBOARD TEE FITTING FORWARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER=0.876, FINAL DIAMETER=0.8806. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-80313,SDR 04FDEA02231Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 4 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.506, MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.502 AND REPAIRED AS PER FEDEXSDR 04FDEA02230Vane · corrodedRIGHT HAND WING INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING AFT HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8982. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80311SDR 04FDEA02229Vane · corrodedRIGHT HAND WING INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8794. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80SDR 04FDEA02228Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 4 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.124 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LEFT SDR 04FDEA02227Vane · corrodedRIGHT HAND WING - INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING FORWARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.877. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-SDR 04FDEA02226Vane · corrodedRIGHT HAND WING INBOARD FLAP. FLAP VANE INBOARD TEE FITTING AFT HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8784. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80312, SDR 04FDEA02225Fitting · corrodedRT WING INBOARD FLAP VANE INBOARD TEE FITTING MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER = 0.881. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80312, TITLE: WING
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