N502FE

Cancelled 2001

Deregistered aircraft · Boeing 727-25

Cancelled
July 28, 2001
Status when cancelled
Triennial form not returned
Serial number
18271
Type
Fixed wing multi engine
Certificate issued
February 13, 1989
Last registry action
January 16, 2001
Mode S code
A641E0
Owner when cancelled
Federal Express Corporation
Location
Memphis, TN
Owner type
Corporation

From the FAA registry file of October 27, 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 N502FE and the event date: up to this one’s cancellation.

Service difficulty reports · 12

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

SDR 98FDEA00682Coalescer Bag · contaminated98-261 ACRID, RANCID BURN SMELL FROM LH PACK. ISOLATE LH PK & ODOR SUBSIDED. 2 PKS REQ THIS A/C. ODOR BEGAN T/O ROLL. ODOR CEASE F/L 180. RET AT DES USING #1 BLD. R&R WATER SEP BAG, SEALS ON N1 TACH & FRONT ACCY DRIVE SUPPORT ON AML 01041373. R&R BLD AIR Oct 28, 1998 · N502FE · Boeing 72725 · Humidity Control SystemSDR 97FDEA00810Switch · malfunctionMAIN CARGO DOOR LIGHT CAME ON SHORTLY AFTER TAKEOFF. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL: 52-4A, MCD VERIFIED CLOSED. REMOVED AND REPLACED CONTROL SWITCH ARM/DISARM SWITCH. REMOVED AND REPLACED DOOR UNLOCK LT ON MANUAL HAND PUMP PANEL. C/B CARGO DOORNov 9, 1997 · N502FE · Boeing 72725 · Door Warning SystemSDR 97FDEA00097Stringer · corrodedNR 0190 009 CORROSION (C53-224-03) ON STR 19 RT BS 313. *S/D* FABRICATED AND INSTALLED FASTENERS TO LOWER FLANGE DOUBLER AT STR 19 RT BS 313. ALODINED AND PRIMED, SEALED PER FED-EX SRM 53-10-3 FIG NR 1.Feb 10, 1997 · N502FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 97FDEA00087Bulkhead · crackedNR 0172 005. BS 950 BULKHEAD IS CRACKED LBL 31, WL 183. REPAIRED CRACK AT LBL 31, WL 183 ON BS 950 BULKHEAD I.A.W. FED-EX SRM 53-10-9.Feb 3, 1997 · N502FE · Boeing 72725 · Fuselage Main, BulkheadSDR 97FDEA00086Frame · corrodedNR 0405 006. CORROSION (C53-224-03) ON FRAME STA 423, BL ZERO, WL 152. REMOVED FRAME AT STA 423, BL ZERO, WL 152 (E-BAY) ORDERED AND INSTALLED NEW FRAME PER FED-EX SRM 51-30-2.Feb 3, 1997 · N502FE · Boeing 72725 · Fuselage Main, FrameSDR 97FDEA00084Stiffener · corrodedNR 0401 08. CORROSION (C53-224-03) ON VERTICAL STIFFENER STA 344, LBL 13, WL 180. REMOVED CORROSION ON STIFFENER. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. DRILLED UP AND INSTALLED NEW STIFFENER PER FED-EX SRM 51-30-2.Feb 2, 1997 · N502FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00078Bulkhead · crackedNR 0170 04. 950 BULKHEAD IS CRACKED AT RBL 4.5 AND LBL 4.5 WL 176. REPAIRED CRACKS AT 950 BULKHEAD, RBL 4.5 AND LBL 4.5, WL 176 PER FED-EX SRM 53-10-9.Jan 29, 1997 · N502FE · Boeing 72725 · Fuselage Main, BulkheadSDR 97FDEA00085Stiffener · corrodedNR 0402 07. CORROSION (C53-224-03) ON HORIZONTAL STIFFENER STA 344, LBL 8, WL 180. REMOVED AND REPLACED STIFFENER PER FED-EX SRM 51-30-2.Jan 27, 1997 · N502FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00076Nose Chord · corrodedNR 0406 002. CORROSION (C53-224-03-1/2) ON RT MID-NOSE CHORD BS 312-344, RBL 13, WL 167. REMOVED AND REPLACED RT MID-CHORD AT BS 294 TO 351, WL 169, RBL 13 I.A.W. BAC DRW. 65-18415.Jan 27, 1997 · N502FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00075Web · corrodedNR 0337 003. CORROSION (C53-100-01(1) ON WEB OF FRAME AND BONDED DOUBLER AT BS 211.8, LBL 19, WL 152. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED WEB AND REPLACED BONDED DOUBLER I.A.W. FED-EX SRM 53-10-01, 51-40-2.Jan 27, 1997 · N502FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00071Floorbeam · corrodedNR 0140 001. CORROSION (C53-224-06) AROUND FASTENER HOLE ON FLOORBEAM AT BS 344, LBL 34 TO LBL 57, WL 208. REMOVED CORRODED UPPER CHORD AT BS 344, RBL 62 - LBL 62, WL 208. INSTALLED NEW UPPER CHORD I.A.W. FED-EX REPAIR DWG SR 27-53-007.Jan 25, 1997 · N502FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA01343Line · leakingNR 2 ENGINE WOULD NOT RUN HIGHER THAN EPR 1.02, N1 63.0, EGT 260 DEGREES, N2 74.0, AND FUEL FLOW 2950 POUNDS PER HOUR. POSSIBLE FUEL LEAK. ENGINE SHUT DOWN AS A PRECAUTION. FOUND LEAK ON SECONDARY MANIFOLD TUBE. REMOVED AND REPLACED PACKING FOR SECONDARYAug 10, 1996 · N502FE · Boeing 72725 · Engine Fuel Distribution