N104FE, cancelled Oct 15, 2002

Service difficulty reports · 19

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 = 'N104FE' AND deregistration_id = 'N104FE-2002-10-15'
  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 01FDEA00829Acm · failed01-305 IN CLIMB CREW NOTICED ODOR IN COCKPIT. R&R LT ACM PER MM 21-51-001-4.Sep 11, 2001 · N104FE · Boeing 72722C · Humidity Control SystemSDR 99FDEA00491Overheat Loop · inopNR 1 ENG STRUT FLICKERED ON T/O ROLL MOMENTARILY AND THEN EXTINGUISH AT 4,000' ALT, LIGHT ILLUM STEADY. *S/D* REMOVED AND REPLACED OVERHEAT LOOP PER MM 26-14-1, LEAK CK NORMAL. LIGHT OPER CK NORM. OK FOR SERVICE.Nov 30, 1999 · N104FE · Boeing 72722C · Overheat DetectionSDR 97FDEA00748Spar Chord · corrodedNR 0323 005, CORROSION (C53-224-05) WING CENTER SECTION UPPER FWD SPAR CHORD, BS 740, LBL 38-44 AND 53-57, WL 202.Oct 16, 1997 · N104FE · Boeing 72722C · Wing SparSDR 97FDEA00747Spar Chord · corrodedCORROSION (C53-132-02-1/2) WING CENTER SECTION LWR SPAR CHORD BS 740, LBL 32 TO 42, WL 169. *S/D* ACCESSED AREA REMOVED LOWER BS 740 CENTER TANK SPAR CHORD RBL 70.5 TO LBL 70.5, WL 169. INSPECTED FASTENER HOLES, COLD WORKED FASTENER HOLES, FLAP PEENED SKIN,Oct 16, 1997 · N104FE · Boeing 72722C · Wing SparSDR 97FDEA00746Chord · corrodedNR 0385 007, WHILE WORKING NR 0245 FOUND CORROSION ON OUTBOARD FLANGE OF THE LONGITUDINAL BEAM LOWER CHORD FROM BS 863-870, LBL 45, WL 188.Oct 16, 1997 · N104FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 97FDEA00745Rib · corrodedNR 0391 006, WHILE WORKING NR 0375, FOUND CORROSION ON WING PLUS CHORD ON BOTTOM PORTION BS 870, LBL 67 AT INBOARD, AFT FASTENER HOLES AND OUTBOARD AFT FASTENER HOLE.Oct 16, 1997 · N104FE · Boeing 72722C · Wing, Rib/BulkheadSDR 97FDEA00743Bulkhead Web · crackedNR 0392 004, WHILE WORKING (NR 0246) FOUND CRACK IN 740 BULKHEAD WEB AT BLO, WL 168 AND CORROSION AT LBL 6, WL 170 AND AT RBL 1 AND 2 WL 170.Oct 15, 1997 · N104FE · Boeing 72722C · Fuselage Main, BulkheadSDR 97FDEA00678Stringer · corrodedCORROSION (C53-224-03) FOUND ON STRINGER 22R AT BS 448. *S/D* REPAIRED STRINGER 22R AT BS 448 IAW FED-EX SRM 53-10-3.Sep 23, 1997 · N104FE · Boeing 72722C · Fuselage Main, Longeron/StringerSDR 97FDEA00677Web · corrodedCORROSION (C53-224-06) ON WEB AT BS 351 TO 360, LBL 65, WL 208.Sep 22, 1997 · N104FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 97FDEA00668Spar Chord · corrodedNR 0245 001 CORROSION (C53-132-02-1/2) WING CENTER SECTION UPPER REAR SPAR CHORD BS 870, RBL 70-LBL 70, WL 188. REMOVED AND REPLACED DAMAGED 870 UPPER CHORD PER FED-EX EA 7-5710-36196.Sep 19, 1997 · N104FE · Boeing 72722C · Wing SparSDR 97FDEA00469Oil Press Sw · failed97-0136 NR 1 LOW OIL BYPASS LIGHT CAME ON AFTER TAKEOFF. NR 1 THRUST LEVER TO IDLE LIGHT OUT .30 SECONDS LATER LIGHT CAME ON AND STAYED ON. OIL PRESS 48 PSI OIL TEMPERATURE NORMAL. ENGINE SHUT DOWN AFTER 2 MINUTE WIND MILLING. REMOVED AND INSPECTED MAIN OIJul 24, 1997 · N104FE · Boeing 72722C · Engine Oil Indicating SystemSDR 96FDEA00367Web · crackedCRACK IN WEB AT BS 520 WL 198 RBL 58. REMOVED, FABRICATED NEW WEB AND INSTALLED THE WEB AT BS 500 TO 560 RBL 58 WL 198, AS PER BOEING DRAWING 65-19309.Mar 1, 1996 · N104FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEAOO740Frame · damaged(NRO 783) MECHANICAL DAMAGE TO FRAME AT BS 380, STR 7 L/H WL 280 CORRECTIVE ACTION FOUND DAMAGE TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED FRAME AT STATION 380 STR 7 L/H WL 280 PER FEDEX SRM 53-10-4 .Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage Main, FrameSDR 95FDEAOO739Seat Track · corrodedNRO-781, CORROSION ON SEAT TRACK FLANGE AT BS 360 LBL 60 WL 208.1. REMOVED CORROSION ON SEAT TRACK FLANGE AT BS 360 LBL 60 WL 208.1, IAW FEDEX SRM 53-10-01.Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEAOO738Seat Track · corrodedNRO-780, CORROSION ON SEAT TRACK FLANGE AT BS 344 TO BS 349 LBL 58 WL 208.1. REMOVED CORROSION ON SEAT TRACK FLANGE AT BS 344 TO BS 349 LBL 58 WL 208.1, FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-01. INSTALLED NEW ONE.Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEAOO737Angle · corrodedNRO-777, CORROSION AROUND NUTPLATES ON FORWARD ENTRY DOOR AT BS 310 TO 343 LBL 62 WL 309. REMOVED CORRODED SUPPORT AT BS 310 TO 343 LBL 62 WL 309, IAW FEDEX SRM 51-IC-1.Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 95FDEAOO736Floorbeam · corrodedNRO-777, CORROSION ON TOP CHORD OF FLOORBEAM AT BS 344 RBL 20 TO LBL 60 WL 208 STR 8. REMOVED TOP CHORD FLOORBEAM AT BS 344 RBL 70 TO LBL 70 WL 208 STR 8, IAW FEDEX REPAIR DRAWING NR SR27-53-007, DUE TO TOP CHORDS OF FLOORBEAM OUT OF LIMITS.Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 95FDEAOO735Shear Tie · crackedCRACKED AND DAMAGED SHEAR TIE AT BS 640, LT STR 8. REPAIRED DAMAGED SHEAR TIE IAW FEDEX EA 7-5310-24654.Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 95FDEAOO734Frame · dentedDENTED FRAME AT BS 560, STR 6 RT. REPAIRED DENTED FRAME IAW FEDEX SRM 53-10-4.Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage Main, Frame
Back to N104FE, cancelled Oct 15, 2002