# Service difficulty reports: N104FE, cancelled Oct 15, 2002 A list on [N104FE, cancelled Oct 15, 2002](https://openairdocs.org/deregistered/N104FE-2002-10-15.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 01FDEA00829](https://openairdocs.org/sdr/01FDEA00829.md): Acm · failed · Sep 11, 2001 · N104FE · Boeing 72722C · Humidity Control System > 01-305 IN CLIMB CREW NOTICED ODOR IN COCKPIT. R&R LT ACM PER MM 21-51-001-4. - [SDR 99FDEA00491](https://openairdocs.org/sdr/99FDEA00491.md): Overheat Loop · inop · Nov 30, 1999 · N104FE · Boeing 72722C · Overheat Detection > NR 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. - [SDR 97FDEA00748](https://openairdocs.org/sdr/97FDEA00748.md): Spar Chord · corroded · Oct 16, 1997 · N104FE · Boeing 72722C · Wing Spar > NR 0323 005, CORROSION (C53-224-05) WING CENTER SECTION UPPER FWD SPAR CHORD, BS 740, LBL 38-44 AND 53-57, WL 202. - [SDR 97FDEA00747](https://openairdocs.org/sdr/97FDEA00747.md): Spar Chord · corroded · Oct 16, 1997 · N104FE · Boeing 72722C · Wing Spar > CORROSION (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, - [SDR 97FDEA00746](https://openairdocs.org/sdr/97FDEA00746.md): Chord · corroded · Oct 16, 1997 · N104FE · Boeing 72722C · Fuselage Miscellaneous Structure > NR 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. - [SDR 97FDEA00745](https://openairdocs.org/sdr/97FDEA00745.md): Rib · corroded · Oct 16, 1997 · N104FE · Boeing 72722C · Wing, Rib/Bulkhead > NR 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. - [SDR 97FDEA00743](https://openairdocs.org/sdr/97FDEA00743.md): Bulkhead Web · cracked · Oct 15, 1997 · N104FE · Boeing 72722C · Fuselage Main, Bulkhead > NR 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. - [SDR 97FDEA00678](https://openairdocs.org/sdr/97FDEA00678.md): Stringer · corroded · Sep 23, 1997 · N104FE · Boeing 72722C · Fuselage Main, Longeron/Stringer > CORROSION (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. - [SDR 97FDEA00677](https://openairdocs.org/sdr/97FDEA00677.md): Web · corroded · Sep 22, 1997 · N104FE · Boeing 72722C · Fuselage Miscellaneous Structure > CORROSION (C53-224-06) ON WEB AT BS 351 TO 360, LBL 65, WL 208. - [SDR 97FDEA00668](https://openairdocs.org/sdr/97FDEA00668.md): Spar Chord · corroded · Sep 19, 1997 · N104FE · Boeing 72722C · Wing Spar > NR 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. - [SDR 97FDEA00469](https://openairdocs.org/sdr/97FDEA00469.md): Oil Press Sw · failed · Jul 24, 1997 · N104FE · Boeing 72722C · Engine Oil Indicating System > 97-0136 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 OI - [SDR 96FDEA00367](https://openairdocs.org/sdr/96FDEA00367.md): Web · cracked · Mar 1, 1996 · N104FE · Boeing 72722 · Fuselage Miscellaneous Structure > CRACK 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. - [SDR 95FDEAOO740](https://openairdocs.org/sdr/95FDEAOO740.md): Frame · damaged · Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage Main, Frame > (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. - [SDR 95FDEAOO739](https://openairdocs.org/sdr/95FDEAOO739.md): Seat Track · corroded · Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage, Seat/Cargo Attach Fittings > NRO-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. - [SDR 95FDEAOO738](https://openairdocs.org/sdr/95FDEAOO738.md): Seat Track · corroded · Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage, Seat/Cargo Attach Fittings > NRO-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. - [SDR 95FDEAOO737](https://openairdocs.org/sdr/95FDEAOO737.md): Angle · corroded · Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage Miscellaneous Structure > NRO-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. - [SDR 95FDEAOO736](https://openairdocs.org/sdr/95FDEAOO736.md): Floorbeam · corroded · Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage Main, Floor Beam > NRO-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. - [SDR 95FDEAOO735](https://openairdocs.org/sdr/95FDEAOO735.md): Shear Tie · cracked · Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage Miscellaneous Structure > CRACKED AND DAMAGED SHEAR TIE AT BS 640, LT STR 8. REPAIRED DAMAGED SHEAR TIE IAW FEDEX EA 7-5310-24654. - [SDR 95FDEAOO734](https://openairdocs.org/sdr/95FDEAOO734.md): Frame · dented · Jun 16, 1995 · N104FE · Boeing 72722C · Fuselage Main, Frame > DENTED FRAME AT BS 560, STR 6 RT. REPAIRED DENTED FRAME IAW FEDEX SRM 53-10-4. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N104FE-2002-10-15/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.