N607FE
Service difficulty reports · 454
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N607FE' AND registry_match = 'registration' 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 n_number = 'N607FE' AND registry_match = 'registration' 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 04FDEA02304Skin · crackedLT WING, THRU FUEL TANK ACCESS PANEL CUTOUT 535BT, UPPER STRINGER NR 12, STRINGER END FOUND WITH CRACK OF ABOUT 10 INCHES IN LENGTH. REPAIR CARRIED OUT AT LT WING FUEL TANK ACCESS PANEL CUT-OUT 535BT, UPPER STRINGER NR 12 AS PER SRM 57-20-00 FIG 10, VOL I. FSDR 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 04FDEA02292Skin · delaminatedLEFT HAND ELEVATOR LOWER SURFACE AT STA XE 356 TO XE 370 FOUND WITH DELAMINATION APPROXIMATELY 14 INCHES IN DIAMETER. REMOVED AND REPLACED AS PER MM 27-30-30. ELEVATOR OPERATIONAL CHECK CARRIED OUT AS PER MM 27-30-00, FOUND SATISFACTORY.SDR 04FDEA02291Skin · delaminatedRT OUTBOARD ELEVATOR LOWER SURFACE STA XE 353 TO XE 372 FOUND WITH DELAMINATION APPROXIMATELY 18 INCHES IN DIAMETER. REMOVED AND REPLACED AS PER MM 27-30-30. ELEVATOR OPERATIONAL CHECK CARRIED OUT AS PER MM 27-30-00, FOUND SATISFACTORY.SDR 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 04FDEA02222Seat Track · crackedMAIN DECK CARGO COMPARTMENT - AT STA 755 AXIS X = 47.58 SEAT TRACK LOWER SURFACE FOUND CRACKED. DAMAGED SEAT TRACK AT MAIN DECK CARGO COMPARTMENT, STA 755 AXIS X = 47.58 REMOVED AS PER SRM 51-31-01, VOLUME 2. REPAIR TRACK FABRICATED, REWORKED AND INSTALLED ASDR 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: WINGSDR 04FDEA02224Hinge · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) HOLE NR 3 PIVOT INBOARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093, FINAL DIAMTER= 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT OUTBOASDR 04FDEA02223Fitting · corrodedRT WING INBOARD 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= 0.878. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80312, TITLE: WINSDR 04FDEA02221Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 3 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.187 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD SDR 04FDEA02220Floorbeam · crackedRIGHT HAND CAC COMPARTMENT AT STA 6-90 AT APPROX 64 INCHES FROM CENTER FOUND CRACK AT FLOORBEAM LOWER CHORD. CRACK AT CAC, RT COMPARTMENT AT STA 6-90 AT APPROX. 64 INCHES FROM CENTER AT FLOORBEAM LOWER CHORD CARRIED OUT REPAIR AS PER FEDEX EA NR 1-5310-79813,SDR 04FDEA02219Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.497, MATERIAL REMOVED = 0.026, REMAINING THICKNESS = 0.471 AND REPAIRED AS PER FEDEX EA 1-575SDR 04FDEA02218Longeron · crackedFORWARD CARGO COMPARTMENT AT STA 1119 TO 6-10 LONGERON 51R FOUND CRACKED AT SPLICE JOINT AREA. REPAIRED AS PER SRM 53-10-00 FIG 2 VOL I. NDT INSPECTION CARRIED OUT, FOUND NO CRACK EVIDENT.SDR 04FDEA02217Hinge · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) HOLE NR 2 ACTUATOR OUTBOARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER= 1.062, FINAL DIAMTER= 1.221 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT O
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