# N119FE: 1966 Boeing 727-25C, registration cancelled 2012-06-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 4, 2012
- Status when cancelled: Sale reported, canceled
- Airframe: [Boeing 727-25C](https://openairdocs.org/model/boeing-727-25c) (registry code 138400H)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 19301
- Year built: 1966
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: January 26, 1967
- Last registry action: November 26, 2003
- Mode S code: A04E24
- Location: [Kalamazoo, MI](https://openairdocs.org/faa-place/MI/Kalamazoo)
- Owner type: Individual
- Owner's area on the map: 42.1972° N, 85.5555° W: Placed by OpenAirDocs at the center of ZIP code 49002, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N119FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=119FE
- Page: https://openairdocs.org/deregistered/N119FE-2012-06-04

From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 727-25C: https://openairdocs.org/model/boeing-727-25c.md

## Service difficulty reports (60, newest 50)

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

- [SDR 03FDEA01396](https://openairdocs.org/sdr/03FDEA01396), Aug 28, 2003: SKIN. CORRODED. CORROSION AND WORKING FASTENERS ON FUSELAGE SKIN ABOVE MAIN CARGO DOOR CUTOUT APPROXIMATELY STA.500 TO 560 STR 1L TO 5L. AIRCRAFT REMOVED FROM SERVICE BY FEDEX.
- [SDR 01FDEA00168](https://openairdocs.org/sdr/01FDEA00168), Feb 27, 2001: SEAT TRACK. CORRODED. DURING ROUTINE INSP, NR 6 MAIN CABIN SEAT TRACK FOUND CORRODED FROM BS 850 - 870. REMOVED AND REPLACED SEAT TRACK PER IAW BAC 727 SRM 51-30-2.
- [SDR 01FDEA00148](https://openairdocs.org/sdr/01FDEA00148), Feb 17, 2001: SEAT TRACK. CORRODED. DURING ROUTINE INSP, NR 6 MAIN CABIN SEAT TRACK FOUND CORRODED AT BS 475. *S/D* REMOVED, REPLACED AND FAB SEAT TRACK PER IAW BAC 727 SRM 53-10-5.
- [SDR 01FDEA00154](https://openairdocs.org/sdr/01FDEA00154), Feb 16, 2001: SEAT TRACK. CORRODED. DURING ROUTINE INSP NR 3 MAIN CABIN SEAT TRACK FOUND CORRODED AT BS 837. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5.
- [SDR 01FDEA00151](https://openairdocs.org/sdr/01FDEA00151), Feb 16, 2001: SEAT TRACK. CORRODED. DUR ROUTINE INSP NR 3 MAIN CABIN SEAT TRACK FOUND CORRODED FROM BS 420 - 440. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5.
- [SDR 01FDEA00150](https://openairdocs.org/sdr/01FDEA00150), Feb 16, 2001: SEAT TRACK. CORRODED. DURING ROUTINE INSP, NR 2 MAIN CABIN SEAT TRACK FOUND CORRODED AT BS 783. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5.
- [SDR 01FDEA00149](https://openairdocs.org/sdr/01FDEA00149), Feb 16, 2001: SEAT TRACK. CORRODED. DURING ROUTINE INSP, NR 2 MAIN CABIN SEAT TRACK FOUND CORRODED AT BS 825. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5.
- [SDR 01FDEA00116](https://openairdocs.org/sdr/01FDEA00116), Feb 13, 2001: FLOORBEAM. CORRODED. DURING ROUTINE INSP THE AFT CARGO FLOORBEAM AT BS 1130, STR 17R FOUND CORRODED. *S/D* REMOVED, REPLACED AND FAB DAMAGED AREA PER IAW FEDEX EA 7-5310-56274.
- [SDR 01FDEA00117](https://openairdocs.org/sdr/01FDEA00117), Feb 13, 2001: CROSSBEAM. CORRODED. DURING ROUTINE INSP, UPPER CTR SECTION LWR CARGO COMPT LWR CHORD OF CTR CROSSBEAM BL 0 FROM BS 500 - 640 FOUND CORRODED. *S/D* REPLACED, REMOVED & FAB PER IAW B
- [SDR 01FDEA00118](https://openairdocs.org/sdr/01FDEA00118), Feb 13, 2001: FLOORBEAM. CORRODED. DURING ROUTINE INSP, MAIN CABIN FLOORBEAM AT BS 950, RBL 6 FOUND CORRODED. *S/D* REMOVED, REPLACED, AND FAB PER IAW BAC 727 SRM 53-10-8.
- [SDR 01FDEA00114](https://openairdocs.org/sdr/01FDEA00114), Feb 12, 2001: SHEAR TIE. CRACKED. DURING ROUTINE INSP, FUSELAGE SHEAR TIE AT BS 1070, STR 6L FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB CLIP PER IAW BAC 727 SRM 51-20-1, 51-10-2, 51-30-2.
- [SDR 01FDEA00113](https://openairdocs.org/sdr/01FDEA00113), Feb 12, 2001: FRAME. CRACKED. DURING ROUTINE INSP, MAIN CABIN FRAME AT BS 1130 FOUND CRACKED AT STR 11L. *S/D* HFEC IND NO CRACKS PER IAW BAC 727 NDT MANUAL PART 6. TREATED, PRIMED AND REINS
- [SDR 01FDEA00108](https://openairdocs.org/sdr/01FDEA00108), Feb 10, 2001: SHEAR TIE. CRACKED. DURING ROUTINE INSP THE FUSELAGE SHEAR TIE AT BS 1050, STR 5R & 6R FOUND CRACKED. *S/D* REMOVED, REPLACED, FAB, TREATED AND PRIMED PER IAW 727 SRM 51-20-1, 51-1
- [SDR 01FDEA00105](https://openairdocs.org/sdr/01FDEA00105), Feb 10, 2001: SHEAR TIE. CRACKED. DURING ROUTINE INSP FUSELAGE SHEAR TIE AT BS 1070, STR 5R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-10-2, 51-30-2.
- [SDR 01FDEA00109](https://openairdocs.org/sdr/01FDEA00109), Feb 10, 2001: SHEAR TIE. CRACKED. DURING ROUTINE INSP FUSELAGE SHEAR TIE AT BS 1030, STR 5R & 6R FOUND CRACKED. *S/D* REMOVED, REPLACED, FAB, TREATED AND PRIMED PER IAW BAC 727 SRM 51-20-1, 51-1
- [SDR 01FDEA00096](https://openairdocs.org/sdr/01FDEA00096), Feb 8, 2001: SKIN. CRACKED. DURING ROUTINE INSP, FUSELAGE SKIN FOUND CRACKED AT BS 1313 LEFT AND AFT OR THE AIRSTAIR FRAME CUTOUT. *S/D* REAM UP HOLE PER IAW BAC 727 SRM 53-30-1. REMOVED A
- [SDR 01FDEA00097](https://openairdocs.org/sdr/01FDEA00097), Feb 8, 2001: BRACKET. CRACKED. DURING ROUTINE INSP, ATTACH BRACKET BS 359, STR 8R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1 AND BAC 5602, 51-30-2.
- [SDR 01FDEA00095](https://openairdocs.org/sdr/01FDEA00095), Feb 8, 2001: SKIN. CRACKED. DURING ROUTINE INSP, RIGHT WING NR 5 SLAT OUTBOARD UP STOP PAD CUTOUT FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-40-2.
- [SDR 01FDEA00098](https://openairdocs.org/sdr/01FDEA00098), Feb 7, 2001: RIB. CRACKED. DURING ROUTINE INSP, UPPER RUDDER, UPPER THRUST HINGE RIB FOUND CRACKED BY HFEC IN LEFT FWD LWR RADIUS. *S/D* REMOVED AND REPLACED RIB PER IAW BAC 727 51-30-2 A
- [SDR 01FDEA00099](https://openairdocs.org/sdr/01FDEA00099), Feb 7, 2001: RIB. CRACKED. DURING ROUTINE INSP, LWR RUDDER, LWR THRUST HINGE RIB FLANGE FOUND CRACKED BY HFEC AT RIGHT AFT END. *S/D* REMOVED AND REPLACED RIB PER IAW BAC 727 SRM 51-30-2 
- [SDR 01FDEA00085](https://openairdocs.org/sdr/01FDEA00085), Feb 7, 2001: FITTING. CRACKED. DURING ROUTINE INSP, LT MLG DOOR ACTUATOR RIB FITTING FOUND CRACKED BY HFEC. *S/D* REMOVED AND REPLACED LT MLG DOOR PER IAW BAC 727 MM 32-12-001.
- [SDR 01FDEA00086](https://openairdocs.org/sdr/01FDEA00086), Feb 7, 2001: FITTING. CRACKED. DURING ROUTINE INSP, MAIN CARGO DOOR LATCH CAM SUPPORT FITTING AT FS 487.1 FOUND CRACKED. *S/D* REMOVED AND REPLACED FITTING PER IAW FEDEX EO 7-5230-7-2323F PAR
- [SDR 01FDEA00087](https://openairdocs.org/sdr/01FDEA00087), Feb 7, 2001: FITTING. CRACKED. DURING ROUTINE INSP, MAIN CARGO DOOR LATCH CAM SUPPORT FITTING AT FS 500 FOUND CRACKED. *S/D* REMOVED AND REPLACED FITTING PER IAW FEDEX EO 7-5230-7-2323F PART 
- [SDR 01FDEA00088](https://openairdocs.org/sdr/01FDEA00088), Feb 7, 2001: FITTING. CRACKED. DURING ROUTINE INSP, BS 870 TERMINAL FITTING WEB FOUND CRACKED NEAR STR 10R. *S/D* REMOVED AND REPLACED FITTING PER IAW SR DRW 27-53-026 AND EA 7-5310-56279.
- [SDR 01FDEA00093](https://openairdocs.org/sdr/01FDEA00093), Feb 7, 2001: CLIP. BENT. DURING ROUTINE INSP, FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE CONTAINER RELEASE SPRING CLIPS BENT. *S/D* REMOVED AND REPLACED PER IAW BAC 727 MM 25-60-013-4.
- [SDR 01FDEA00090](https://openairdocs.org/sdr/01FDEA00090), Feb 7, 2001: LIGHT. INOPERATIVE. DURING ROUTINE INSP, FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE LIGHT FOUND INOP. *S/D* REMOVED AND REPLACED BULB. OPS CK GOOD PER IAW BAC 727 MM 33-50-121-2.
- [SDR 01FDEA00100](https://openairdocs.org/sdr/01FDEA00100), Feb 7, 2001: FRAME. CRACKED. DURING ROUTINE INSP, BS 1070 FRAME FOUND CRACKED AT STR 28R. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-40-3, 51-30-2.
- [SDR 01FDEA00101](https://openairdocs.org/sdr/01FDEA00101), Feb 7, 2001: FRAME. CRACKED. DURING ROUTINE INSP, BS 1070 FRAME CRACKED AT STR 29R. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-40-3, 51-30-2.
- [SDR 01FDEA00091](https://openairdocs.org/sdr/01FDEA00091), Feb 7, 2001: FITTING. CRACKED. DURING ROUTINE INSP, FWD LWR CARGO COMPT DOOR CUTOUT, UPPER FWD DOOR STOP FITTING FOUND CRACKED. *S/D* REMOVED PAINT. HFEC IND NO CRACKS PER IAW BAC 727 NDT MAN
- [SDR 01FDEA00089](https://openairdocs.org/sdr/01FDEA00089), Feb 7, 2001: RIB. CRACKED. DURING ROUTINE INSP, NR 5 SLAT INBOARD ACTUATOR ATTACH RIB FOUND CRACKED. *S/D* BLENDED, TREATED AND PRIMED PER IAW BAC 727 SRM 57-50-1, 51-10-2.
- [SDR 01FDEA00092](https://openairdocs.org/sdr/01FDEA00092), Feb 7, 2001: FRAME. CRACKED. DURING ROUTINE INSP, FWD LWR CARGO COMP, DOOR CUTOUT, FRAME CRACKED AT BS 580 AT RBL 60 NEAR FWD STOP FITTING. *S/D* REMOVED PAIN, TREATED AND PRIMED AREA PER I
- [SDR 01FDEA00084](https://openairdocs.org/sdr/01FDEA00084), Feb 7, 2001: FITTING. CRACKED. DURING ROUTINE INSP, RIGHT BS 870 TERMINAL FITTING FOUND CRACKED AT FASTENER HOLE AT ROW 4 HOLE 3 & ROW 4 HOLE 3.
- [SDR 00FDEA00069](https://openairdocs.org/sdr/00FDEA00069), Feb 10, 2000: SWITCH. OUT OF ADJUST. AFT CARGO DOOR AND LIGHT CAME ON IN FLT WHILE CLIMBING. ADJUSTED LOWER AFT CARGO DOOR AND SLIDING FAIRING SWITCHES IAW MM 52-70-000-5. OPS CK GOOD.
- [SDR 99FDEA00154](https://openairdocs.org/sdr/99FDEA00154), Apr 21, 1999: PUMP. FAILED. 99-0093 - NR 2 ENG FLAMED OUT PASSING 4,000 FT, 240 KNOT IND. REMOVED AND REPLACED NR 2 FUEL PUMP AND CENTRAL IAW MM 73-21-000-4 AND MM 73-41-0001. OPS LEAK PWR
- [SDR 98FDEA00534](https://openairdocs.org/sdr/98FDEA00534), Aug 26, 1998: LIGHT. INOPERATIVE. NR 0468 ON TEST HOP FOUND MAIN CABIN DOOR EMER EXIT LIGHT BATTERY TO BE VERY LOW. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. OPS CK GOOD PER FED-EX M/M 33-
- [SDR 98FDEA00524](https://openairdocs.org/sdr/98FDEA00524), Aug 19, 1998: SWITCH. FAILED. AFTER T/O, THE LAND GEAR WOULD NOT RETRACT. APPROPRIATE RED TABS FOLLOW WITH NEG RESULT. FOUND THE LT MAIN LAND GEAR GROUND SAFETY SWITCH OVER CTR IN WRONG POSI
- [SDR 98FDEA00463](https://openairdocs.org/sdr/98FDEA00463), Jul 18, 1998: DOOR. NOT CLOSED. A/C WOULD NOT PRESSURIZE IN FLIGHT. FOUND E AND E COMPARTMENT DOOR CRACKED OPEN. EQUIPMENT ACCESS WARNING LIGHT INOPERATIVE. REPLACED SWITCH S114 AND GROUNDING 
- [SDR 96FDEA01289](https://openairdocs.org/sdr/96FDEA01289), Jul 27, 1996: WARNING HORN. SOUNDED. ON TAKEOFF, GEAR WARNING HORN SOUNDED WHEN GEAR RETRACTED WITH FLAPS IN 25 DEGREE POSITION. COULD NOT BE SILENCED WITHOUT LOWERING THE GEAR. PERFORMED LANDING G
- [SDR 96FDEA00655](https://openairdocs.org/sdr/96FDEA00655), Mar 18, 1996: SKIN. CORROSION. SKIN LAP UPPER PANEL, 65-18386-107, CORRODED, AND TRIMMED AWAY FUSE SKIN BETWEEN STR 21-22L FROM THE PRODUCTION SPLICE AT BS 1080.45 TO THE PRODUCTION SPLICE AT
- [SDR 96FDEA00654](https://openairdocs.org/sdr/96FDEA00654), Mar 18, 1996: SKIN. CORROSION. FUSELAGE PLATES CORRODED. REPAIR TO LT SKIN ASSY STA 1130 - STA 1183, STR 14 - STR 20L. REPETITIVE ULTRASONIC INSPECTION. SKIN REMOVED AND REPLACED PER EA 7-533
- [SDR 96FDEA00657](https://openairdocs.org/sdr/96FDEA00657), Mar 17, 1996: FLOOR BEAM. CORRODED. CABIN FLOOR BEAM AT STA 312, BL ZERO WAS FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVAL, BUT NO REPAIR WAS INSTALLED. REMOVED CORRODED AREA, FABRICATED FILLE
- [SDR 96FDEA00656](https://openairdocs.org/sdr/96FDEA00656), Mar 15, 1996: FLOOR BEAM. CORROSION. FLIGHT DECK FLOOR BEAM, STA 268, UPPER CHORD CORRODED AND PREVIOUS REPAIR NOT PER SRM LBL 2. REMOVED AND REPLACED FITTING IAW SRM 51-10-1.
- [SDR 96FDEA00653](https://openairdocs.org/sdr/96FDEA00653), Mar 15, 1996: FLOOR BEAM. CORROSION. STA 312 - STA 328, BL ZERO, LBL 22, FLOOR BEAM CORRODED ON UPPER SURFACE. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8.
- [SDR 96FDEA00652](https://openairdocs.org/sdr/96FDEA00652), Mar 14, 1996: FLOOR BEAM. CORROSION. UPPER LOBE CORROSION ON FLOOR BEAM STA 640, BL ZERO - RBL 65. REPAIRED IAW SRM 53-10-8.
- [SDR 96FDEA00643](https://openairdocs.org/sdr/96FDEA00643), Mar 14, 1996: FRAME. CRACKED. FRAME CRACKED AT STA 480, STR 9L. INSTALLED FUSELAGE CROWN FRAME REPAIR, STA 440, STR 9L, PER SRM 53-10-4, PG 18.
- [SDR 96FDEA00651](https://openairdocs.org/sdr/96FDEA00651), Mar 13, 1996: FLOOR BEAM. CORROSION. CABIN, FS 480, FLOOR BEAM HAS CORROSION AROUND FASTENER NUTPLATES, BOTTOM FLANGE BL 45 - BL 60R. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8.
- [SDR 96FDEA00650](https://openairdocs.org/sdr/96FDEA00650), Mar 11, 1996: FLOOR BEAM. CORROSION. CABIN, FS 740, FLOOR BEAM HAS CORROSION DEVELOPING IN SCREW HOLE AND NUTPLATES (BOTTOM SIDE) BETWEEN BL 8 RT TO BL 53 RT. INSTALLED FLOOR BEAM REPAIR PER ESO AN
- [SDR 96FDEA00649](https://openairdocs.org/sdr/96FDEA00649), Mar 11, 1996: FLOOR BEAM. CORROSION. CABIN, FS 740, FLOOR BEAM HAS HEAVY INTERGRANULAR CORROSION AT SCREW HOLE AND NUTPLATE 3.50 INCHES TO THE RT OF BL ZERO FLOOR TRACK, BOTTOM SIDE FLANGE. INSTALL
- [SDR 96FDEA00646](https://openairdocs.org/sdr/96FDEA00646), Mar 8, 1996: CASTING. CORRODED. RIGHT WING PIVOT BOLT HOLE FOR OUTBOARD AILERON QUAD CORRODED AT BOTTOM. REPLACED OUTBOARD AILERON LOCK-OUT SUPPORT CASTING PER 51-10-1.
- [SDR 96FDEA00642](https://openairdocs.org/sdr/96FDEA00642), Mar 8, 1996: SPAR CHORD. CRACKED. WS 304 RT WING 3RD STRINGER AFT OF FWD UPPER STAR CHORD CRACKED. REPAIRED STRINGER AT WS 304, 3RD FROM TOP FRONT SPAR CHORD. REPAIRED PER SRM 57-10-4.

All 60: https://openairdocs.org/deregistered/N119FE-2012-06-04/reports.md

## FAA accident and incident reports (3)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19941206047169I](https://openairdocs.org/incident/19941206047169I), Dec 6, 1994: Boeing 72725C (N119FE), Omaha, NE. NR3 engine lost oil pressure. Accessory gear housing bushing failed. Lost oil and pressure. Replaced engine.
- [Incident 19930125006519I](https://openairdocs.org/incident/19930125006519I), Jan 25, 1993: Boeing 72725C (N119FE), Portland, OR, Minor damage. Pilot diverted to Portland when pilots windshield cracked. Landed safely.
- [Incident 19890109005609I](https://openairdocs.org/incident/19890109005609I), Jan 9, 1989: Boeing 72725C (N119FE), Rochester, NY, Minor damage. Difficult to taxi. Returned to ramp. Smoke from right gear. Replaced wheel and brake assemblies and anti-skid valve

## Other aircraft with N119FE

- [Registered now](https://openairdocs.org/aircraft/N119FE): Boeing 767-300F, S/N 64057, built 2019

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