N609FE
Service difficulty reports · 475
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 = 'N609FE' 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 = 'N609FE' 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 04FDEA01369Hinge · corrodedRT WING O/B FLAP O/B HINGE (WING SIDE), FWD ATTACHMENT FORK, I/B HOLE SPOTFACE CORRODED. RT WING O/B FLAP O/B HINGE (WING SIDE), FWD ATTACHMENT FORK, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 FIG 401. ORIGINAL THICKNESS OF LUG:SDR 04FDEA01368Hinge · corrodedRT WING O/B FLAP O/B HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. SIDE LINK SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 FIG 401. ORIGINAL THICKNESS OF LUG: 0.450, MATERIAL REMOVED: 0.002, REMAINING THICKNES OF LUG: 0.448. REPAIRESDR 04FDEA01367Hinge · corrodedRT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER: 1.187, MAX ALLOWABLSDR 04FDEA01366Hinge · corrodedRT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER: 1.187, MAX ALLOWABLSDR 04FDEA01365Hinge · corrodedLT WING O/B FLAP I/B HINGE (WING SIDE), LOWER MOUNTING SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 1. ORIGINAL THICKNESS OF LUG: 0.459, MATERIAL REMOVED: 0.004, REMAINING THICKNESS OF LUG: 0.455 WITHIN LIMIT AS PER DRASDR 04FDEA01364Hinge · corrodedLEFT WING - O/B FLAP I/B HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. CORROSION REMOVED. ORIGINAL LUG THICKNESS: 0.393, MATERIAL REMOVED: 0.003, REMAINING THICKNESS OF LUG: 0.390 REWORKED AREA REPAIRED AS PER EA 1-5750-76674. LT O/B TRAILING EDGE FLASDR 04FDEA01363Hinge · corrodedLT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, MAX ALLOWABLE DIAMETR: 1.190, FINAL DIAMETER: 1.220, EXCEEDED LIMIT. REPAIRED AS PESDR 04FDEA01362Hinge · corrodedLT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, MAX ALLOWABLE DIAMETR: 1.190, FINAL DIAMETER: 1.220, EXCEEDED LIMIT. REPAIRED AS PESDR 04FDEA01361Splice · crackedCTR CARGO COMPT BILGE AREA SPLICE FITTING AT LONGERON 38 LEFT STA 1541. SUSPECT CRACK ORIGINATING FROM THE RIVET AREAS. CRACK SPLICE FITTING REMOVED AS PER SRM 51-33-01 VOL II. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-SDR 04FDEA01360Splice · crackedCTR CARGO COMPT BILGE AREA SPLICE FITTING AT LONGERON 46 LT STA 1541 CRACKED. SUSPECT CRACK ORIGINATING FROM THE RIVET AREAS. CRACK SPLICE FITTING REMOVED AT CENTER CARGO COMPARTMENT BILGE AREA SPLICE FITTING AT LONGERON 46 LT STA 1541 AS PER SRM 51-33-01 VOSDR 04FDEA01359Splice · crackedCTR CARGO COMPT BILGE AREA SPLICE FITTING AT LONGERON 44 RT STA 1541 FOUND CRACK. CRACK SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.SDR 04FDEA01358Hinge · corrodedRT WING I/B FLAP O/B HINGE (FLAP SIDE), I/B PIVOT PIN ATTACHMENT BORE FOUND CORRODED. RT WING I/B FLAP O/B HINGE (FLAP SIDE), I/B PIVOT PIN ATTACHMENT BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGE 446. ORIGINAL DIAMETER: 1.187, FINAL DIAMETER: 1.217, MAX ALSDR 04FDEA01357Hinge · corrodedRT WING I/B FLAP O/B HINGE (FLAP SIDE), O/B PIVOT PIN ATTACHMENT BORE FOUND CORRODED. RT WING I/B FLAP O/B HINGE (FLAP SIDE), O/B PIVOT PIN ATTACHMENT BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGE 446. ORIGINAL DIAMETER: 1.187, FINAL DIAMETER: 1.217, MAX SDR 04FDEA01328Skin · chafedFIXED LEADING EDGE SKIN BEHIND NR 3 SLAT CHAFED. REPAIRED AS PER SRM 57-10-00 FIG 15 VOL I.SDR 04FDEA01327Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.SDR 04FDEA01326Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.SDR 04FDEA01325Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNESS OF LUG: 0.403, MATSDR 04FDEA01324Hinge · corrodedRIGHT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNESS OF LUG: 0.404, MSDR 04FDEA01321Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNESS OF LUG: 0.504, MASDR 04FDEA01319Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNESS OF LUG: 0.477, MASDR 04FDEA01318Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER HOSDR 04FDEA01317Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.093, FINAL DIAMETER: SDR 04FDEA01315Hinge · corrodedRIGHT WING O/B FLAP I/B HINGE (FLAP SIDE), FOLLOW UP SYSTEM PUSH-PULL ROD ATTACHMENT HORN, MOUNTING BOLT HOLE CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), FOLLOW UP SYSTEM PUSH-PULL ROD ATTACHMENT HORN, MOUNTING BOLT HOLE CORROSION REMOVED AS PER CMM 20-SDR 04FDEA01312Hinge · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.SDR 04FDEA01311Hinge · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.21SDR 04FDEA01310Hinge · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT SPOTFACE FOUND CORRODED. ACTUATOR O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.402, MATERIAL REMOVED: 0.003, REMAINING THICKNESSSDR 04FDEA01309Hinge · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT SPOTFACE FOUND CORRODED. ACTUATOR I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.408, MATERIAL REMOVED: 0.007, REMAINING THICKNESS: SDR 04FDEA01308Hinge · corrodedRIGHT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.093. REPAIRED AS PER EA 1-5750-76672SDR 04FDEA01307Hinge · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.093, FINAL DIAMETER: 1.125. REPAIRED AS PER EA 1-5750-76672. RSDR 04FDEA01306Hinge · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.503, MATERIAL REMOVED: 0.002, REMAINING THICKNESDR 04FDEA01305Hinge · corrodedRIGHT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.492, MATERIAL REMOVED AT O/B FACE: 0.021, I/SDR 04FDEA01304Hinge · corrodedLEFT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.092. REPAIRED AS PER EA 1-5750-76671SDR 04FDEA01303Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.094, FINAL DIAMETER: 1.096. REPAIRED AS PER EA 1-5750-76671. SDR 04FDEA01302Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.498, MATERIAL REMOVED: 0.002, REMAINING THICKNESSDR 04FDEA01301Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.496, MATERIAL REMOVED AT O/B FACE: 0.004, I/B FACSDR 04FDEA01300Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. O/B ACTUATOR ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.395, MATERIAL REMOVED: 0.002, REMAINING THICKNESS:SDR 04FDEA01299Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. I/B ACTUATOR ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.392, MATERIAL REMOVED: 0.002, REMAINING THICKNESS: SDR 04FDEA01298Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. I/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.190. REPAIRED AS PER EA 1-5750-76671, LT OSDR 04FDEA01297Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. O/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.190. REPAIRED AS PER EA 1-5750-76671. LT SDR 04FDEA01295Hinge · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.494, MATERIAL REMOVED: 0.004, REMAINING THICKNESSDR 04FDEA01294Hinge · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.503, MATERIAL REMOVED: 0.002, REMAINING THICKNESSDR 04FDEA01293Hinge · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.095. REPAIRED AS PER EA 1-5750-76670. LTSDR 04FDEA01292Hinge · corrodedLEFT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.093, FINAL DIAMETER: 1.125. REPAIRED AS PER EA 1-5750-76670. LT O/B FLAP - I/B FLAP SIDE HSDR 04FDEA01291Hinge · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. O/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.1895. REPAIRED AS PER EA 1-5750-76670. LT SDR 04FDEA01290Hinge · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.1SDR 04FDEA01289Hinge · corrodedLEFT WING O/B FLAP I/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL LUG THICKNESS: 0.403, MATERIAL REMOVED: 0.005, REMAINING THICKNESS OF LUG: 0.398 REWORKED AREA REPAIRSDR 04FDEA01288Hinge · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. SPOTFACED, CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.405, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.403. REWORSDR 04FDEA01285Stringer · crackedLEFT WING NR 1 FUEL TANK - XORS 757 - ACCESS PANEL 536BB. SUSPECT CRACK ON NR 10 STRINGER. SLOTTED OUT CRACK AS PER SRM 51-31-01 VOL II. REPAIR ANGLES INSTALLED AS PER SRM 51-33-01 VOL II AND EA 1-5710-76680. UPPER WING STRINGERS 10 & 11 LEFT - CRACK REPAIR.SDR 04FDEA01284Stringer · crackedLEFT WING NR 1 FUEL TANK - XORS 717 - ACCESS PANEL 536AB. SUSPECT CRACK ON NR 11 STRINGER. SLOTTED OUT CRACK AS PER SRM 51-31-01 VOL II AND INSTALLED REPAIR ANGLES AS PER SRM 51-33-01 VOL II, & EA 1-5710-76680. UPPER WING STRINGERS 10 & 11 LT - CRACK REPAIR.SDR 04FDEA01282Stop Fitting · crackedRIGHT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED. RIGHT WING - OUTBOARD FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2 AND SRM 51-35-01 VOL 2.
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