N615FE
Service difficulty reports · 469
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 = 'N615FE' 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 = 'N615FE' 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 04FDEA02704Structure · corrodedCORROSION REMOVED ON NR 33 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 33L, REPAIRED AS PER EA 1-5510-81550.SDR 04FDEA02703Structure · corrodedCORROSION REMOVED ON NR 35 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 35L, REPAIRED AS PER EA 1-5510-81556.SDR 04FDEA02702Structure · corrodedCORROSION REMOVED ON NR 36 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. REPAIRED AS PER EA 1-5510-81553, HORIZONTAL STABILIZER-BARREL NUT BORE 36L - REWORKED BEYOND S/B MD11-55-023 REV. 2 LIMITS.SDR 04FDEA02701Structure · corrodedCORROSION REMOVED ON NR 33 RT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 33R, REPAIRED AS PER EA 1-5510-81547.SDR 04FDEA02700Structure · corrodedCORROSION REMOVED ON 31R BARREL NUT BORE FOUND EXCEEDED LIMIT IAW EO 1-5510-7-5000 C3 PT1 FIG 03. RT HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 31R, REPAIRED AS PER EA 1-5510-81555.SDR 04FDEA02671Structure · corrodedCORROSION REMOVED ON NR 29 LEFT BARREL NUT BORE FOUND EXCEEDED LIMIT. SNRM N1061: CORROSION REPAIRED AS PER EA 1-5510-80355 HORIZONTAL STABILIZER. BARREL NUT BORE 29L. REWORKED BEYOND SB MD11-55-023 REV2 LIMIT.SDR 04FDEA02667Skin · corrodedCORROSION REMOVED ON NR 8 RIGHT HAND BARREL NUT BORE, FOUND EXCEEDED LIMIT. CORROSION REPAIRED AS PER EA 1-5510-80349 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 8R, CORROSION REPAIR SB MD11-55-023 REV2 AND EO 1-5510-7-5000.SDR 04FDEA02673Panel · corrodedCORROSION REMOVED ON NR 15 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 15L. REPAIRED AS PER EA NR 1-5510-81560, TITLE: HORIZONTAL STABILIZER-BARREL NUT BORE 15L. REWORKED BEYOND S/B MD11SDR 04FDEA02670Panel · corrodedCORROSION REMOVED ON NR 31 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 31L. REPAIRED AS PER EA NR 1-5510-80358, TITLE: HORIZONTAL STABILIZER BARREL NUT BORE 31L. REWORK BEYOND S/B MD11-5SDR 04FDEA02669Spar Cap · corrodedCORROSION REMOVED ON NR 36 RIGHT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 36R. REPAIRED AS PER EA NR 1-5510-81544, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 36R. REWORKED BEYOND S/BSDR 04FDEA02668Panel · corrodedCORROSION REMOVED ON NR 32 RIGHT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 32R. REPAIRED AS PER EA NR 1-5510-81559, TITLE: HORIZONTAL STABILIZER BARREL NUT BORE 32R. REWORKED BEYOND S/B SDR 04FDEA02672Structure · corrodedCORROSION REMOVED ON NR 13 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT.SDR 04FDEA02659Frame · dentedMAIN DECK, LT SIDEWALL STRUCTURE FRAME'S INNER CHORD DENT AT STA 1701, L-12L. FRAME AT STA 1701 L-12L DAMAGED DOUBLER REMOVED AND REPLACED AS PER SRM 53-00-00 VOL I FIG 1.SDR 04FDEA02660Frame · dentedMAIN DECK, RT SIDEWALL STRUCTURE FRAME'S INNER CHORD DENT AT STA 1721, L-12R. FRAME AT STA 1721 RT SIDEWALL L-12R DENTED AREA REPAIRED AS PER SRM 53-30-00 VOL I FIG 1. REPAIR IS CAT B INITIAL INSPECTION AT 14,500 AND REPETITIVE INSPECTION REQUIRED AT 9,500SDR 04FDEA02654Bracket · corrodedRT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 TO 443, ORIGINAL DIAMETER=1.1SDR 04FDEA02653Bracket · corrodedRT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 TO 443, ORIGINAL DIAMETER=1.1SDR 04FDEA02652Bracket · corrodedLEFT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION. REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442-443, ORIGINAL DIAMETER=1.SDR 04FDEA02633Fitting · crackedLT WING O/B FLAP STOP FITTING FOUND CRACKED. LEFT WING O/B FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33- 01 VOL II.SDR 04FDEA02632Panel · corrodedLEFT WING UPPER SURFACE XIS=247 FWD SIDE FOUND CORROSION. LEFT WING UPPER SURFACE XIS=247 FWD SIDE REPAIRED AS PER EA NR 1-5710- 81539, TITLE: WINGS LT WING UPPER SURFACE, CORROSION BLEND OUT AT XORS 144.25.SDR 04FDEA02623Bracket · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.125 INSDR 04FDEA02622Bracket · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION. REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.077 INSDR 04FDEA02621Bracket · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION. REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.096 ISDR 04FDEA02620Bracket · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. SNRM N0448: LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL THICKNESS=0.514 INSDR 04FDEA02619Bracket · corrodedLT WING , O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE FOUND CORRODED. LEFT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL THICKNESS=0.503 INCH, MATESDR 04FDEA02618Bracket · corrodedLEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOT FACE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOT FACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.39SDR 04FDEA02617Bracket · corrodedLEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.400 SDR 04FDEA02615Bracket · corrodedLEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.SDR 04FDEA02616Bracket · corrodedLEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=SDR 04FDEA02634Track · crackedENG NR 2, LEFT THRUST REVERSER TRANSLATING SLEEVE TOP SLIDE TRACK AFT EDGE FOUND WITH SUSPECTED CRACK AT AFT EDGE.SDR 04FDEA02630Hinge · corrodedRT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02629Hinge · corrodedRT WING-OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02628Hinge · corrodedSNRM N0456: RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02627Hinge · corrodedSNRM N0455: RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02626Hinge · corrodedSNRM N0454: RT WING- OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02625Hinge · corrodedSNRM N0453: RT WING- OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02624Hinge · corrodedRT WING-OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02614Hinge · corrodedSNRM N0442: LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02613Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02612Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02611Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02610Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02609Hinge · corrodedLT WING - OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02608Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02607Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA02604Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.094 INSDR 04FDEA02603Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.125 INSDR 04FDEA02602Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.502 INCH, MATERISDR 04FDEA02601Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.497 INCH, MATERISDR 04FDEA02600Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.408 INCH, MASDR 04FDEA02599Bracket · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.392 INCH
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