# Service difficulty reports: N105FE, cancelled Feb 18, 2003

A list on [N105FE, cancelled Feb 18, 2003](https://openairdocs.org/deregistered/N105FE-2003-02-18.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR 1FDEA00798](https://openairdocs.org/sdr/1FDEA00798.md): Plug · faulty · Aug 31, 2001 · N105FE · Boeing 72722C · Extinguishing System
  > 01-298 MOD TYPE F NR 7-26-020 REV NO PS FIRE PROTECTION. COMPLIED WITH FLEET CAMPAIGN DIRECTIVE 7-26-020. REMOVED AND REPLACED PLUG FROM LINE AT COUPLING.
- [SDR 01FDEA00798](https://openairdocs.org/sdr/01FDEA00798.md): Coupling · defective · Aug 31, 2001 · N105FE · Boeing 72722C · Extinguishing System
  > FIRE PROTECTION ENG STRUT FIRE X NOZZLE INSP COMPLY WITH FLEET CAMPAIGN DIRECTIVE 7-26-020. REMOVED AND REPLACED LINE A COUPLING.
- [SDR 99FDEA00022](https://openairdocs.org/sdr/99FDEA00022.md): Mechanism · iced up · Jan 20, 1999 · N105FE · Boeing 72722C · Trailing Edge Flap Control System
  > DURING FLAP RETRACT ON T/O, FLAPS DID NOT MOVE TO SELECT POSITION. INSPECTED FLAPS, NO FAULTS FOUND. SUSPECT PROBLEM DUE TO COLD WEATHER ICING CONDITION. HEAT LT AND RT WHEEL WELLS. CYCLED FLAPS FOUND TO BE WITHIN LIMITS AS PER M/M 27-52-12 & 27-52-1.
- [SDR 98FDEA00592](https://openairdocs.org/sdr/98FDEA00592.md): Compressor · bird strike · Sep 24, 1998 · N105FE · Boeing 72722 · Turbine Engine Compressor Section
  > 98-235 - ON T/O, SUSPECT BIRD STRIKE AT NOSE WHEEL WELL AREA, FOLLOW BY SEVERE VIBRATION IN NR 3 ENG. ENG SHUTDOWN IAW FOM AND EMERG LAND MADE (MEM RETURN). REMOVED AND REPLACED NR 3 ENG COMPRESSOR BLADES DAMAGED IAW WORK CARD 70T0503 AND 70T0301. OPS CHECK
- [SDR 98FDEA00295](https://openairdocs.org/sdr/98FDEA00295.md): Keel Beam · corroded · Apr 25, 1998 · N105FE · Boeing 72722C · Fuselage Main, Keel
  > CORROSION ON KEEL BEAM BS 1063 TO 1068, RBL 7, WL 150. *S/D* ACCOMPLISHED KEEL BEAM REPAIR PER FED-EX EA NR 7-5310-38660, BS 1063 TO 1068, RBL 7, WL 150.
- [SDR 98FDEA00220](https://openairdocs.org/sdr/98FDEA00220.md): Beam · corroded · Mar 26, 1998 · N105FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > NR 0170 007 - CORROSION ON LONGITUDINAL BEAM UNDER NUTPLATES AT BS 765, RBL 25, WL 208. REPAIRED LONGITUDINAL BEAM AT BS 765, RBL 25, WL 208 IAW FED-EX EA 7-5310-37471B.
- [SDR 98FDEA00219](https://openairdocs.org/sdr/98FDEA00219.md): Channel · cracked · Mar 26, 1998 · N105FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > NR 0449 006 - WHILE WORKING NR 0227 FOUND CHANNEL CRACKED AT BS 555.05, WL 187 AS MARKED NR 65-18620-14. REMOVED AND REPLACED CHANNEL (NR 1 TRANSVERSE BEAM) WL 187 IN FWD CARGO DOOR IAW FED-EX SRM 51-30-2.
- [SDR 98FDEA00158](https://openairdocs.org/sdr/98FDEA00158.md): Spar Chord · corroded · Mar 5, 1998 · N105FE · Boeing 72722C · Wing Spar
  > CORROSION (C53-132-02-1/2) ON UPPER REAR SPAR CHORD BS 870, LBL 65 - RBL 65, WL 178. *S/D* REMOVED AND REPLACED UPPER REAR SPAR CHORD BS 870 LBL 65 - RBL 65 WL 178 PER FEDEX EA 7-5710-38738.
- [SDR 98FDEA00157](https://openairdocs.org/sdr/98FDEA00157.md): Spar Chord · corroded · Mar 5, 1998 · N105FE · Boeing 72722C · Wing Spar
  > CORROSION (C53-132-02-1/2) ON LOWER REAR SPAR CHORD BS 870, LBL 65 TO RBL 65, WL 148. *S/D* REMOVED AND REPLACED LWR SPAR CHORD BS 870 LBL 65 - RBL 65 WL 148 PER FEDEX EA 7-5710-38738.
- [SDR 98FDEA00156](https://openairdocs.org/sdr/98FDEA00156.md): Web · corroded · Mar 5, 1998 · N105FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > CORROSION (C53-132-02-1/2) ON WEB BS 870, RBL 65 LBL 65, WL 178 TO 148. *S/D* REMOVED AND REPLACED 870 CENTER TANK WEB PER FED-EX EA 7-5710-38738.
- [SDR 98FDEA00155](https://openairdocs.org/sdr/98FDEA00155.md): Chord · corroded · Mar 5, 1998 · N105FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > CORROSION (C53-224-03, 1, 2) ON UNDERSIDE OF TOP CHORD BS 344, RBL 16, WL 207 AROUND HI-LOCK, AND AT RBL 31, WL 208. *S/D* REMOVED CORROSION ON UNDERSIDE OF TOP CHORD BS 344, RBL 16, WL 207. CORROSION FOUND TO BE WITHIN LIMITS PER FED-EX SRM 53-10-1. REMOV
- [SDR 98FDEA00145](https://openairdocs.org/sdr/98FDEA00145.md): Stiffener · corroded · Mar 2, 1998 · N105FE · Boeing 72722C · Fuselage Miscellaneous Structure
  > NR 0272 001 CORROSION (C53-100-01(1)) ON NOSE WHEEL WELL BOX STIFFENER BS 346, WL 182, LBL 14. REMOVED AND REPLACED STIFFENER BS 346, WL 182, LBL 14 PER FED-EX DRAWING 65-18415 AND FED-EX SRM 51-30-2.
- [SDR 97FDEA00876](https://openairdocs.org/sdr/97FDEA00876.md): Switch · malfunctioned · Dec 4, 1997 · N105FE · Boeing 72722C · Engine Oil Indicating System
  > AFTER DEPARTURE, THE NR 1 LOW OIL/BYPASS LIGHT ILLUMINATED. OIL PRESS APPROX 47 PSI AND TEMP WITHIN LIMITS. PER CHECK LIST SECURED NR 1 ENG AND RETURNED TO ORD. REMOVED AND REPLACED OIL FILTER, NO CONTAMINATION FOUND. RAN ENGINE PER JET RUN HANDBOOK. NO L
- [SDR 97FDEA00178](https://openairdocs.org/sdr/97FDEA00178.md): Panel · missing · Mar 17, 1997 · N105FE · Boeing 72722 · Nacelle/Pylon, Plate/Skin
  > ON TAKEOFF, A PYLON PANEL FELL OFF THE AIRCRAFT. MAINTENANCE RETRIEVED THE PANEL, NO OTHER ASSOCIATED PROBLEMS WITH AIRCRAFT. VERTICAL STABILIZER, FUSELAGE AND ENGINE COWLING INSPECTED, NO DAMAGE FOUND. MISSING PANEL INSTALLED ON UPPER SIDE OF NR 1 PYLON.
- [SDR 95FDEA01283](https://openairdocs.org/sdr/95FDEA01283.md): Frame · bent · Sep 7, 1995 · N105FE · Boeing 72722C · Fuselage Main, Frame
  > CORROSION LOWER SIDE OF FWD FLANGE STA 480 FLOOR FRAME RBL 3 TO 6. REMOVED CORROSION INSTALLED REPAIR PER 53-10-8 FIG 5 PG 31.
- [SDR 95FDEA01275](https://openairdocs.org/sdr/95FDEA01275.md): Floorbeam · corroded · Sep 6, 1995 · N105FE · Boeing 72722C · Fuselage Main, Floor Beam
  > CORROSION ON TOP OF FLOOR BEAM C/L TO LBL 24 STA 560, MAIN CARGO LOBE. REMOVED CORROSION AND REPAIRED FLOORBEAM PER SRM 53-10-5 PG 31 TO 48.
- [SDR 95FDEA01282](https://openairdocs.org/sdr/95FDEA01282.md): Frame · bent · Sep 1, 1995 · N105FE · Boeing 72722C · Fuselage Main, Frame
  > NR 0413 UPPER LOBE FRAME BENT 3 INCHES ABOVE RT FLOOR LINE STA 500. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER 51-40-3 PG 3.
- [SDR 95FDEA01253](https://openairdocs.org/sdr/95FDEA01253.md): Stringer · cracked · Sep 1, 1995 · N105FE · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > MAIN CARGO, NR 7L STR AT STA 460 CRACKED. CUTOUT CRACKED STR SECTION. REPAIRED PER SRM 53-10-3 PAGE 7, FUSELAGE STR REPAIR.
- [SDR 95FDEA01249](https://openairdocs.org/sdr/95FDEA01249.md): Frame · bent · Sep 1, 1995 · N105FE · Boeing 72722C · Fuselage Main, Frame
  > UPPER LOBE FRAME BENT 3 INCHES ABOVE RT FLOOR LINE STA 500. REMOVED DAMAGED AREA INSTALLED DOUBLER PER 51-40-3 PG 3.
- [SDR 95FDEA01248](https://openairdocs.org/sdr/95FDEA01248.md): Frame · bent · Sep 1, 1995 · N105FE · Boeing 72722C · Fuselage Main, Frame
  > UPPER LOBE FRAME BENT 3 INCHES ABOVE RT FLOOR LINE STA 520. REMOVED DAMAGED AREA OF FRAME AND INSTALLED REPAIR PER SRM 51-40-3 PG 1 TO 4.
- [SDR 95FDEA01247](https://openairdocs.org/sdr/95FDEA01247.md): Frame · cracked · Sep 1, 1995 · N105FE · Boeing 72722C · Fuselage Main, Frame
  > FRAME BENT AND CRACKED STA 540 AT STR 7 TO 6R. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER SRM 51-10-4 PG 3 AND 4.
- [SDR 95FDEA01220](https://openairdocs.org/sdr/95FDEA01220.md): Rib · cracked · Aug 28, 1995 · N105FE · Boeing 72722C · Wing, Rib/Bulkhead
  > LT WING AT STA 738.5 INSIDE SURGE TANK, RIB CRACKED IN RADIUS AT AFT STR LOWER ATTACHMENT, NR 1023. INSTALLED DOUBLER ON RIB STA 738.5 L/LT WING, REF SRM 57-10-5.
- [SDR 95FDEA01219](https://openairdocs.org/sdr/95FDEA01219.md): Floorbeam · corroded · Aug 23, 1995 · N105FE · Boeing 72722C · Fuselage Main, Floor Beam
  > BS 560 LBL 29 TO 32 MAIN CARGO, FOUND CORROSION ON TOP LEG OF FLOORBEAM BETWEEN LT INBD AND LT CENTER CARGO TIE-DOWN TRACKS. REMOVED CORROSION INSTALLED REPAIR PER 53-10-8 PG 31 TO 48.
- [SDR 95FDEA01218](https://openairdocs.org/sdr/95FDEA01218.md): Floorbeam · corroded · Aug 22, 1995 · N105FE · Boeing 72722C · Fuselage Main, Floor Beam
  > CORROSION TOP AFT FLANGE ON STA 1110 FLOORBEAM, LOWER SIDE AT FASTENER HOLES RBL 35 TO 40 AFT CARGO CEILING, NR 0994.
- [SDR 95FDEA01217](https://openairdocs.org/sdr/95FDEA01217.md): Floorbeam · corroded · Aug 22, 1995 · N105FE · Boeing 72722C · Fuselage Main, Floor Beam
  > CORROSION IN UPPER LOBE FLOORBEAM, UPPER FWD FLANGE STA 1110 RBL 48 TO 60, NR 0996.
- [SDR 95FDEA01216](https://openairdocs.org/sdr/95FDEA01216.md): Floorbeam · corroded · Aug 22, 1995 · N105FE · Boeing 72722C · Fuselage Main, Floor Beam
  > HEAVY CORROSION LOWER FLANGE OF UPPER LOBE FLOORBEAM STA 1110 RBL 28 TO 30 IN AFT CARGO COMPT CEILING, NR 0993.

## 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 = 'N105FE' AND deregistration_id = 'N105FE-2003-02-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N105FE-2003-02-18/reports

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