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.

SDR SWAA041921Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FORE FLAP DELAMINATED. R & R LT OUTBOARD FORE FLAP PER MM.Jul 7, 2004 · N619SW · Boeing 7373H4SDR 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.Jul 7, 2004 · N619SW · Boeing 7373H4SDR 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, Jul 6, 2004 · N745DH · Boeing 727224SDR 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 - OUTBOJul 6, 2004 · N606FE · Doug MD11SDR 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 - OUTBOAJul 6, 2004 · N606FE · Doug MD11SDR 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-Jul 6, 2004 · N606FE · Doug MD11SDR 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 EAJul 6, 2004 · N606FE · Doug MD11SDR 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 1-5750-7Jul 6, 2004 · N606FE · Doug MD11SDR 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 FEDJul 6, 2004 · N606FE · Doug MD11SDR 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 REJul 6, 2004 · N606FE · Doug MD11FSDR 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 Jul 6, 2004 · N606FE · Doug MD11FSDR 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; MATERIALJul 6, 2004 · N606FE · Doug MD11FSDR 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; MATERIJul 6, 2004 · N606FE · Doug MD11FSDR 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 REMOJul 6, 2004 · N606FE · Doug MD11FSDR 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 REJul 6, 2004 · N606FE · Doug MD11FSDR 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 REPAIRJul 6, 2004 · N606FE · Doug MD11FSDR 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 CJul 6, 2004 · N606FE · Doug MD11FSDR 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. COJul 6, 2004 · N606FE · Doug MD11FSDR 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. COMPLJul 6, 2004 · N606FE · Doug MD11FSDR 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, MATEJul 6, 2004 · N606FE · Doug MD11FSDR 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 Jul 6, 2004 · N606FE · Doug MD11FSDR 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, Jul 6, 2004 · N606FE · Doug MD11FSDR 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, MATEJul 6, 2004 · N606FE · Doug MD11FSDR 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 INCHJul 6, 2004 · N606FE · Doug MD11FSDR 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. Jul 6, 2004 · N606FE · Doug MD11FSDR 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 REJul 6, 2004 · N606FE · Doug MD11FSDR 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 INCHJul 6, 2004 · N606FE · Doug MD11SDR 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, ANJul 6, 2004 · N606FE · Doug MD11FSDR 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, MATERJul 6, 2004 · N606FE · Doug MD11FSDR 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 DIAMETERJul 6, 2004 · N606FE · Doug MD11FSDR 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= Jul 6, 2004 · N606FE · Doug MD11FSDR 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.Jul 6, 2004 · N606FE · Doug MD11FSDR 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= 1Jul 6, 2004 · N606FE · Doug MD11FSDR 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 RJul 6, 2004 · N606FE · Doug MD11FSDR 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 REMOVJul 6, 2004 · N606FE · Doug MD11FSDR 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= 1.22Jul 6, 2004 · N606FE · Doug MD11FSDR 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 REPAIREDJul 6, 2004 · N606FE · Doug MD11FSDR 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 DIAMEJul 6, 2004 · N606FE · Doug MD11FSDR 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 DIAMETJul 6, 2004 · N606FE · Doug MD11FSDR 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=Jul 6, 2004 · N606FE · Doug MD11FSDR 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.Jul 6, 2004 · N606FE · Doug MD11FSDR 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 REMJul 6, 2004 · N606FE · Doug MD11FSDR 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.Jul 6, 2004 · N606FE · Doug MD11FSDR 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 REMOJul 6, 2004 · N606FE · Doug MD11FSDR 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 REMJul 6, 2004 · N606FE · Doug MD11FSDR 04FDEA01966Hinge · corrodedRIGHT WING - OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED.Jul 6, 2004 · N606FE · Doug MD11SDR IXXA060446SFitting · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF97. REPAIRED PER ALL APPLICABLE DATAJul 5, 2004 · N41CX · Doug DC862FSDR IXXA060413SSkin · debondedDURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP SKIN DEBONDED AT STATION XW115. REPAIRED PER ALL APPLICABLE DATA.Jul 5, 2004 · N41CX · Doug DC862FSDR IXXA060412SFitting · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF219. REPAIRED PER ALL APPLICABLE DATA.Jul 5, 2004 · N41CX · Doug DC862FSDR IXXA060411SFitting · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XT340. REPAIRED PER ALL APPLICABLE DATA.Jul 5, 2004 · N41CX · Doug DC862F
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