N613FE
Service difficulty reports · 422
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 = 'N613FE' 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 = 'N613FE' 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 04FDEA02270Skin Panel · corrodedLEFT HAND WING UPPER SURFACE TRAILING EDGE PANEL FORWARD EDGE FOUND BULGING AT OUTBOARD OF NR 5 SPOILER XORS 827. REMOVED AS PER SRM 51-21-01, VOLUME II, MATERIAL THICKNESS=0.270, MATERIAL REMAINED=0.231, MATERIAL REMOVED=0.039 FOUND WITHIN LIMIT (0.054) ASSDR 04FDEA02269Barrel Nut · corrodedLEFT HAND NR 27 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79810, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 27L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX ESDR 04FDEA02268Barrel Nut · corrodedLEFT HAND NR 29 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79809, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 29L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX ESDR 04FDEA02267Barrel Nut · corrodedLEFT HAND NR 1 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79820, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 1L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO SDR 04FDEA02208Structure · corrodedLEFT HAND HORIZONTAL STABILIZER NR 28L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-80302, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 28L - CORROSION RSDR 04FDEA02207Structure · corrodedLEFT HAND HORIZONTAL STABILIZER NR 24L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-80303, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 24L - CORROSION RSDR 04FDEA02206Structure · corrodedRIGHT HAND NR 1 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79824, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 1R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX ESDR 04FDEA02205Structure · corrodedLEFT HAND NR 20 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79833, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 20L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX SDR 04FDEA02204Structure · corrodedLEFT HAND NR 18 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79803, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 18L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX SDR 04FDEA02203Structure · corrodedLEFT HAND NR 16 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79823, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 16L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDESDR 04FDEA02202Structure · corrodedLEFT HAND NR 6 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79827, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 6L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EOSDR 04FDEA02201Structure · corrodedLEFT HAND NR 2 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000.SDR 04FDEA02200Structure · corrodedRIGHT HAND HORIZONTAL STABILIZER NR 5R BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7- 5000.SDR 04FDEA02199Structure · corrodedRT HORIZONTAL STABILIZER NR 13R BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-79830, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 13R - CORROSION REPAIR SDR 04FDEA02195Structure · corrodedLEFT HAND HORIZONTAL STABILIZER NR 14L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II.SDR 04FDEA02194Structure · corrodedLEFT HAND HORIZONTAL STABILIZER 26L BARREL NUT BORE FOUND WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II.SDR 04FDEA02160Fitting · crackedAFT FUSELAGE COMPT STA 2007 RIGHT HAND X=-10 VERTICAL SUPPORT FITTING MOST END SUSPECT CRACKED. CUT AND REMOVED AS PER SRM 53-00-01, FIGURE 8, VOLUME I. REPAIR ANGLES FABRICATED AS PER SRM 53-00-01, FIGURE 8, VOLUME I, T-SECTION MACHINED AS PER FEDEX E.SDR 04FDEA02146Seat Track · corrodedMAIN DECK, RIGHT HAND MOST OUTBOARD SEAT TRACK CORRODED AT R1 DOORWAY. REMOVED LAVATORY ON MAIN DECK AS PER AMM 25-41-06-4. REMOVED AND REPLACED RIGHT HAND MOST OUTBOARD SEAT TRACK AT R1 DOORWAY AS PER SRM 51-35-01, VOLUME II. REINSTALLED LAVATORY MODULE ASSDR 04FDEA02147Seat Track · corrodedMAIN DECK, LEFT HAND MOST OUTBOARD SEAT TRACK CORRODED AT L1 DOORWAY. CORRODED SEAT TRACK AT MAIN DECK, LEFT HAND MOST OUTBOARD AT L1 DOORWAY REMOVED AS PER SRM 51-31-01, VOLUME II AND REPLACED AS PER SRM 51-31-01, VOLUME II.SDR 04FDEA02145Seat Track · wornMAIN DECK, SEAT TRACK LBL 47 FOUND WITH DEEP SCRATCHES AT STA 1100. NEW TRACK AND SPLICE REWORKED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I.SDR 04FDEA02140Stringer · crackedRIGHT HAND UPPER NR 9 STRINGER END FOUND CRACK AT INSIDE ACCESS PANEL 638AB. REPAIR ANGLES FABRICATED AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED AS PER SRM 57-20-00, FIGURE 10, SHEET 6, VOLUME I.SDR 04FDEA02139Stringer · crackedLEFT HAND UPPER NR 9 STRINGER END FOUND CRACK AT INSIDE ACCESS PANEL 538AB. REPAIR SPLICE ANGLE FABRICATED AS PER SRM 57-20-00, VOLUME I; NEW STRINGER AND SPLICE ANGLES INSTALLED AS PER SRM 57-20-00, VOLUME I.SDR 04FDEA02137Stop Fitting · corrodedLEFT HAND WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II.SDR 04FDEA02136Stop Fitting · crackedRIGHT HAND WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II.SDR 04FDEA02135Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.403, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.398 AND REPAIRED AS PER FEDEXSDR 04FDEA02134Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.400, MATERIAL REMOVED=0.006, REMAINING THICKNESS=0.394 AND REPAIRED AS PER FEDEX EASDR 04FDEA02133Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NR 1-5750-77942. TITLE: WINGS - TSDR 04FDEA02132Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02131Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.002, REMAINING THICKNESS=0.504, AND REPAIRED AS PER FEDEX EA NR 1-5SDR 04FDEA02130Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.503, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.499 AND REPAIRED AS PER FEDEX EA NSDR 04FDEA02129Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02128Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.095 AND REPAIRED AS PER EA NR 1-5750-77942. TITLE: WINGS - TRAILING SDR 04FDEA02127Hinge · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER FEDEX EA NR 1-5750-77940. TITLE: WINSDR 04FDEA02126Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.405", MATERIAL REMOVED = 0.005, REMAINING THICKNESS=0.400, AND REPAIRED AS SDR 04FDEA02125Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED ASPER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER 1.062, FINAL DIAMETER 1.207, AND REPAIRED AS PER FEDEX EA NR 1-5750-77940. TITLE: SDR 04FDEA02124Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02123Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED.SDR 04FDEA02122Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.505, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.501, AND REPAIRED AS PER FEDEX EASDR 04FDEA02121Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02120Hinge · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.510, MATERIAL REMOVED=0.003, REMAINING THICKNESS=0.507, AND REPAIRED AS PER FEDEX EA NR 1-SDR 04FDEA02119Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NO. 1-5750-77941. TITLE: WINGS - SDR 04FDEA02118Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.406, MATERIAL REMOVED=0.008, REMAINING THICKNESS=0.398 AND REPAIRED AS PER FEDEX ESDR 04FDEA02117Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WINGS - SDR 04FDEA02116Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.404, MATERIAL REMOVED=0.007, REMAINING THICKNESS=0.397 AND REPAIRED AS PER FEDEX ESDR 04FDEA02115Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.196 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE ANSDR 04FDEA02114Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.501 AND REPAIRED AS PER FEDEX EA NR 1-5SDR 04FDEA02113Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.193 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDSDR 04FDEA02112Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.502 AND REPAIRED AS PER FEDEX EA NR 1-5SDR 04FDEA02111Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIA.=1.062, FINAL DIAMETER = 1.218 AND REPAIRED AS PER EA NR 1-5750-77943. TRAILING EDGE DEVICES -SDR 04FDEA02110Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
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