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 SWAA041921Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FORE FLAP DELAMINATED. R & R LT OUTBOARD FORE FLAP PER MM.SDR SWAA041920Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT WING INBOARD AFT T/E FLAP PER MM.SDR DHL2004745518Skin · delaminatedC-CHECK, LT OTBD AFT FLAP LOWER SURF WBL 400 HAS 2 AREAS OF DELAMINATION. CUT OUT DELAM AREA. FABBBED ONE FILLER AND ONE DOUBLER. CLEARED, PREPED, APPLIED ADHESHIVE PRIMER & ADHESIVE TO ALL MATING SURFACES. BONDED, CURED, SANDED, CLEANED, TREATED, PRIMED, SDR 04FDEA01985Hinge Bracket · corrodedOUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.195. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOSDR 04FDEA01984Hinge Bracket · corrodedOUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.196. COMPLIED WITH FEDEX EA# 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOASDR 04FDEA01983Hinge Bracket · corrodedOUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.399; MATERIAL REMOVED 0.004; REMAINING THICKNESS: 0.395 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-SDR 04FDEA01981Hinge Bracket · corrodedLEFT WING - OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.506; MATERIAL REMOVED 0.002"; REMAINING THICKNESS: 0.504 AND REPAIR CARRIED OUT AS PER FEDEX EASDR 04FDEA01982Hinge Bracket · corrodedOUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.407; MATERIAL REMOVED 0.002; REMAINING THICKNESS: 0.405 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-7SDR 04FDEA01980Hinge Bracket · corrodedLEFT WING - OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.495; MATERIAL REMOVED 0.032"; REMAINING THICKNESS: 0.463 AND REPAIR CARRIED OUT AS PER FEDSDR 04FDEA01961Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1.218 INCH AND RESDR 04FDEA01960Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1.217 INCH AND SDR 04FDEA01959Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.414 INCH; MATERIALSDR 04FDEA01958Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.415 INCH; MATERISDR 04FDEA01957Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.482 INCH; MATERIAL REMOSDR 04FDEA01956Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.514 INCH; MATERIAL RESDR 04FDEA01955Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1.126 INCH AND REPAIRSDR 04FDEA01954Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.093 INCH; FINAL DIAMETER: 1.147 INCH AND REPAIR CSDR 04FDEA01953Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.130 INCH. COSDR 04FDEA01952Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 INCH, FINAL DIAMETER = 1.127 INCH. COMPLSDR 04FDEA01951Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.505 INCH, MATESDR 04FDEA01950Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.497 INCH, MATERIAL SDR 04FDEA01949Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.405 INCH, SDR 04FDEA01948Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.404 INCH, MATESDR 04FDEA01947Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.223 INCHSDR 04FDEA01946Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.223 INCH. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. SDR 04FDEA01988Hinge Bracket · corrodedRT WING, INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.254 INCH, AND RESDR 04FDEA01987Hinge Bracket · corrodedLEFT WING - INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. LEFT WING - INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.326 INCHSDR 04FDEA01986Hinge Bracket · corrodedLEFT WING, INBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. LEFT WING, INBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.248 INCH, ANSDR 04FDEA01977Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.470 INCH, MATERSDR 04FDEA01975Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETERSDR 04FDEA01974Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= SDR 04FDEA01970Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.SDR 04FDEA01969Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1SDR 04FDEA01968Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.470 INCH, MATERIAL RSDR 04FDEA01967Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.380 INCH, MATERIAL REMOVSDR 04FDEA01965Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.22SDR 04FDEA01963Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, PIVOT HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 2.256 INCH, FINAL DIAMETER=2.329 INCH, AND REPAIREDSDR 04FDEA01962Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD LOWER MOUNT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD LOWER MOUNT HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 0.516 INCH, FINAL DIAMESDR 04FDEA01945Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETSDR 04FDEA01944Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=SDR 04FDEA01943Hinge Bracket · corrodedLT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. LT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.SDR 04FDEA01942Hinge Bracket · corrodedLT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.495 INCH, MATERIAL REMSDR 04FDEA01941Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, UPPER SIDE LINK HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, UPPER SIDE LINK HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 0.323 INCH, FINAL DIAMETER= 0.SDR 04FDEA01964Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.460 INCH, MATERIAL REMOSDR 04FDEA01976Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.410 INCH, MATERIAL REMSDR 04FDEA01966Hinge · corrodedRIGHT WING - OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED.SDR IXXA060446SFitting · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF97. REPAIRED PER ALL APPLICABLE DATASDR IXXA060413SSkin · debondedDURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP SKIN DEBONDED AT STATION XW115. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060412SFitting · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF219. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060411SFitting · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XT340. REPAIRED PER ALL APPLICABLE DATA.
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