N120FE

Cancelled 2003

Deregistered aircraft · 1966 Boeing 727-25C · Pratt & Whitney JT8D-1

Cancelled
January 15, 2003
Status when cancelled
Second triennial mailing, no response
Serial number
19356
Year built
1966
Type
Fixed wing multi engine
Engine
Turbo-jet
Airworthiness
Standard, transport
Airworthiness date
February 10, 1967
Certificate issued
November 21, 1995
Last registry action
December 22, 1998
Mode S code
A05434
Owner when cancelled
Rfc N120fe/9 Inc
Location
Cheyenne, WY
Owner type
Corporation

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.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N120FE and the event date: up to this one’s cancellation.

Service difficulty reports · 11

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

SDR 02FDEA00314Turbine · damagedNR 2 ENGINE COMPRESSOR STALLED EXCESSIVE VIBRATION. INTAKE HAD NO APPARENT DAMAGE, EXHAUST SHOWED THE TURBINE BLADES HAD DAMAGE AND POOLS OF OIL. REMOVED AND REPLACED NR 2 ENGINE. OK FOR SERVICE.May 7, 2002 · N120FE · Boeing 727100 · Turbine SectionSDR 02FDEA00090O-Ring · damagedLOST HYDRAULIC SYS-A QT & PRESS INSTANTLY. REMOVED AND REPLACED O-RING, SERVICED HYD SYS.Feb 6, 2002 · N120FE · Boeing 72725C · Hydraulic System, MainSDR 99FDEA00308By Pass Switch · inop99-188 - AFT T/O ENG NR 3 LOW OIL PRESSURE OR FILTER BYPASS LIGHT ILLUM AT 500 FT ABOVE GROUND LEVEL. OIL PRESS AND TEMP WERE NORM. SHUTDOWN ENG PER RED TAB. OIL QUANTITY NORM. REMOVED AND REPLACED OIL FILTER BYPASS SW MM 79-33-002, INSP MAIL OIL STRAINER Aug 3, 1999 · N120FE · Boeing 72725C · Engine Oil Indicating SystemSDR 99FDEA00042Fan · failedFUME IN THE COCKPIT, MASK UP AND RETURN TO MCI FOR INVESTIGATION. FOUND GASPER FAN C/B POPPED. REMOVED FAN IAW 727 M/M 20-23-0. *S/D* INSTALLED GASPER FAN PER MM 20-23-0, RAN OPER NORMAL.Feb 3, 1999 · N120FE · Boeing 72725C · Air Distribution FanSDR 98FDEA00755Fitting · corrodedFOUND ON VISUAL INSP WITH LATCHING PINS. REMOVED AT C-001 CHECK, CARGO DOOR LATCH FITTING NR 2 THROUGH NR 8 CORRODED INSIDE BORE. REMOVED AND REPLACED LATCH FITTING.Dec 18, 1998 · N120FE · Boeing 72725C · Cargo/Baggage DoorsSDR 98FDEA00754Rib · crackedBS 760 AT RBL 70.5 RIB UPPER CHORD IS CRACKED. FOUND AT COOL CHECK BY VISUAL INSP. LARGE REPAIR INSTALL IAW SB 727-57-0112.Dec 18, 1998 · N120FE · Boeing 72725C · Wing, Rib/BulkheadSDR 98FDEA00753Mount · crackedNR 1 ENG AFT FITTING MOUNT CRACKED. FOUND BY VISUAL INSP AT C-001 CHECK/FITTING. REMOVED AND REPLACED IAW SB 727-54-0017.Dec 18, 1998 · N120FE · Boeing 72725C · Engine Mount SectionSDR 96FDEA01707Fire Light · illuminatedWHEEL WELL FIRE LIGHT CAME ON INTERMITTENTLY DURING TAKEOFF. GROUND RACK HOLD DOWN BROKEN. REMOVED AND REPLACED HOLD DOWN. OPERATIONAL CHECK GOOD.Dec 24, 1996 · N120FE · Boeing 72725 · Fire DetectionSDR 96FDEA01090Bellframe · crackedSTR 9L IS CRACKED AT BELLFRAME 440L LWR RIVET. STR FLANGE CRACKED, VIEWED FROM UNDERSIDE AT RIVET BULKTAIL. REMOVED DAMAGED SECTION OF STR 9L FROM STA 430 TO 450. INSTALLED NEW SECTION OF STR 9L STA 430 TO 450 PER SRM 53-10-3 PGS 5, 6, 7 AND 8.Jun 11, 1996 · N120FE · Boeing 72725C · Fuselage Main, FrameSDR 96FDEA01046Stringer · corrosionCORROSION STA 6L STA 848 TO 870 UPPER LOBE. CUT CORROSION OUT, INSTALLED STR DOUBLER PER SRM 53-10-3 PG 5 TO 8.Apr 30, 1996 · N120FE · Boeing 72725C · Fuselage Main, Longeron/StringerSDR 96FDEA01045Spar · crackedLT WING FRONT SPAR UPPER CHORD CRACKED ABOVE AND O/B OF NR 2 LE FLAP ACTUATOR. REMOVED CRACK, VOID IN CORROSION AND CORROSION ABOVE AND O/B OF NR 2 LE FLAP ACTUATOR. INSTALLED REPAIR DOUBLER PER FEDEX EA 7-5710-28691 DATE 5-22-96.Apr 29, 1996 · N120FE · Boeing 72725C · Wing Spar

Other aircraft with N120FE · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N120FE is registered now to the first aircraft listed.