# N507FE: Boeing 727-25, registration cancelled 2001-08-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 17, 2001
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-25](https://openairdocs.org/model/boeing-727-25) (registry code 1384006)
- Serial number: 18278
- Type of aircraft: Fixed wing multi engine
- Certificate issued: June 27, 1989
- Last registry action: November 20, 1998
- Mode S code: A65473
- Owner when cancelled: [Ferderal Express Corporation](https://openairdocs.org/faa-owner/FERDERAL%20EXPRESS%20CORPORATION)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N507FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=507FE
- Page: https://openairdocs.org/deregistered/N507FE-2001-08-17

From the FAA registry file of October 29, 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 727-25: https://openairdocs.org/model/boeing-727-25.md

## Service difficulty reports (32)

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

- [SDR 97FDEA00343](https://openairdocs.org/sdr/97FDEA00343), Jun 11, 1997: CHORD. CORRODED. NR 0123 003, CORROSION BETWEEN AND ON WEB AND CHORD AT BS 1176, RBL 12, WL 208. *S/D* REMOVED 1176 CHORD FROM RBL 32.75 TO LBL 65. FOUND CORROSION ON WEB UNDER 
- [SDR 97FDEA00342](https://openairdocs.org/sdr/97FDEA00342), Jun 11, 1997: SKIN. CORRODED. NR 0325 004, LIGHTNING STRIKE ON EXTERIOR SKIN BS 1075, WL 205, BETWEEN 16 RT AND 17 RT. *S/D* REMOVED LIGHTNING STRIKE ON EXTERIOR SKIN 1075, WL 205 BETWEEN ST
- [SDR 97FDEA00326](https://openairdocs.org/sdr/97FDEA00326), Jun 6, 1997: FRAME. CRACKED. NR 0320 001 WHILE WORKING 7-5300-7-2304 M1, FOUND BS 930 FRAME TO BE CRACKED AT BS 930, WL 188-194, LBL 62. REPAIRED CRACK AT BS 930 FRAME W/L 188-194, LBL 62 P
- [SDR 95FDEA01698](https://openairdocs.org/sdr/95FDEA01698), Nov 7, 1995: MECHANISM. WORN. FL 31.0, MACH .84 NOTICED 10 TO 12 DEG R/YOKE DISPLACEMENT. ATTEMPTED TO TRIM RUDDER AND GOT A MOD-SEVERE BUFFET, CONTINUED AFTER SLOWING TO .80 MACH. BUFFET ST
- [SDR 95FDEA00174](https://openairdocs.org/sdr/95FDEA00174), Feb 17, 1995: FRAME. DOUBLE DRILLED. DOUBLE HOLE IN FRAME BS 600, STR 4R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 51-40-3.
- [SDR 95FDEA00177](https://openairdocs.org/sdr/95FDEA00177), Feb 16, 1995: FLOORBEAM. CORRODED. CORROSION FOUND ON TOP CHORD OF FLOORBEAM BS 276, RBL 12, WL 208. REPAIRED TOP CHORD FLOORBEAM IAW 727 SRM 51-40-04, 51-20-01.
- [SDR 95FDEA00176](https://openairdocs.org/sdr/95FDEA00176), Feb 16, 1995: FLOORBEAM. CORROSION. CORROSION ON TOP AND BOTTOM OF FLOORBEAM AT BS 312, LBL 45, WL 208. REPAIRED TOP AND BOTTOM OF FLOORBEAM AT BS 312, LBL 45, WL 208 IAW EA 7-5310-23790.
- [SDR 95FDEA00175](https://openairdocs.org/sdr/95FDEA00175), Feb 16, 1995: FLOORBEAM. CORROSION. FOUND CORROSION ON FLOORBEAM STA 560, RBL 16, WL 198. REMOVED CORROSION AND REPAIRED FLOORBEAM AT BS 560, RBL 16, WL 198 PER FEDEX EA 7-5310-23795.
- [SDR 95FDEA00173](https://openairdocs.org/sdr/95FDEA00173), Feb 16, 1995: FLOORBEAM. CORROSION. CORROSION (72C237-02) UNDER TOP CHORD OF FLOORBEAM AT NUTPLATES HOLES BS 1110, RBL 10-50, WL 208. REPAIRED FLOORBEAM BS 1110, RBL 10-50, WL 208 PER FEDEX EA 7-5
- [SDR 95FDEA00149](https://openairdocs.org/sdr/95FDEA00149), Feb 15, 1995: FLOOR BEAM. CORRODED. CORROSION ON TOP AND BOTTOM OF TOP CHORD OF FLOORBEAM AT BS 344 RBL 17 - LBL 61 WL 208. REPLACED TOP CHORD FROM LBL 707 - RBL 70. IAW FEDEX DRAWING NUMBER SR 27
- [SDR 95FDEA00150](https://openairdocs.org/sdr/95FDEA00150), Feb 13, 1995: SHEAR TIE. CRACKED. FOUND SHEAR TIE CRACKED AT AFT SIDE STA 441 RT BETWEEN STR 18 AND 19, RBL 65. REMOVED CRACKED SHEAR TIE STA 441 RT STR 18 AND 19 (AFT SIDE) RBL 65 AND REPLACED 
- [SDR 95FDEA00148](https://openairdocs.org/sdr/95FDEA00148), Feb 13, 1995: FLOOR BEAM. CORRODED. CORROSION FLOOR BEAM UPPER CHORD BS 680 LBL 36 WL 208. REMOVED CORRODED CHORD, FABRICATED AND INSTALLED REPLACEMENT CHORD AT BS 680 LBL 36 TO RBL 14 WL 208 PER 
- [SDR 95FDEA00142](https://openairdocs.org/sdr/95FDEA00142), Feb 12, 1995: FRAME. CRACKED. WHILE ACCESSING FOR FUSELAGE 00124, FOUND FRAME CRACKED AT STA 500 RBL 24 WL 158. CUT OUT DAMAGE FRAME AREA. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3.
- [SDR 95FDEA00140](https://openairdocs.org/sdr/95FDEA00140), Feb 11, 1995: BEAM. CRACKED. CRACK FOUND ON LONGITUDINAL BEAM AT BS 758 RBL 45 WL 208. REMOVED AND REPLACED LONGITUDINAL BEAM AT STA 758 RBL 45 WL 208.
- [SDR 95FDEA00138](https://openairdocs.org/sdr/95FDEA00138), Feb 11, 1995: FRAME. CORRODED. FOUND CORROSION UNDER NUTPLATE ON FRAME STA 500 LBL 53 WL 175. CUT OUT DAMAGED AREA ON FRAME BS 500 LBL 53 WL 175 AREA OF 1 INCH BY .75 INCH FABRICATED FILLER-D
- [SDR 95FDEA00141](https://openairdocs.org/sdr/95FDEA00141), Feb 10, 1995: HINGE FITTING. CORRODED. RIGHT O/B AILERON 2ND HINGE FITTING FROM I/B END HAS CORROSION. REMOVED AND REPLACED NEW AILERON HINGE FITTING.
- [SDR 95FDEA00139](https://openairdocs.org/sdr/95FDEA00139), Feb 10, 1995: FRAME. CORRODED. FOUND CORROSION UNDERNEATH NUTPLATE ON FRAME STA 560 LBL 48 WL 170. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED 
- [SDR 95FDEA00128](https://openairdocs.org/sdr/95FDEA00128), Feb 9, 1995: SKIN. GOUGED. FIXED L/E GOUGED ON LOWER SURFACE AT NR 4 SLAT I/B TRACK. REMOVED EXISTING REPAIR AND FABRICATED AND INSTALLED NEW REPAIR PER FEDEX SRM 5730-2.
- [SDR 95FDEA00127](https://openairdocs.org/sdr/95FDEA00127), Feb 9, 1995: BEAM. CORRODED. CORROSION FOUND ON TOP AND BOTTOM SIDE OF LONGITUDINAL BEAM IS SEVERAL AREAS FROM BS 760-840 WL 208 LBL 25. REMOVED AND REPLACED LONGITUDINAL BEAM IAW 53-10-2.
- [SDR 95FDEA00125](https://openairdocs.org/sdr/95FDEA00125), Feb 9, 1995: FRAME. CORRODED. CORROSION IS FWD CARGO BAY ON FRAME AT BS 520 STR 26 LBL 25. REMOVED CORROSION FROM FRAME OUT OF LIMITS PER SRM REPAIRED PER FEDEX SRM 51-40-3.
- [SDR 95FDEA00123](https://openairdocs.org/sdr/95FDEA00123), Feb 9, 1995: BLKHD WEB. CRACK. POSSIBLE CRACK AT BS 950 BULKHEAD LBL 40 WL 185. REPAIRED CRACK IS 950 BULKHEAD AT LBL 40 WL 185 PER FEDEX SRM 53-10-9 FIG 2.
- [SDR 95FDEA00129](https://openairdocs.org/sdr/95FDEA00129), Feb 8, 1995: DOUBLER. CORRODED. BS 451-457 BETWEEN STR 18-19R RBL 65 INTERNAL DOUBLER ON E-BAY EXHAUST HAS SIGNS OF CORROSION. REMOVED OLD DOUBLER BS 451-457 STR 18 AND 19R RBL 65 AND INSTALLE
- [SDR 95FDEA00124](https://openairdocs.org/sdr/95FDEA00124), Feb 8, 1995: SKIN. OIL CANNING. SKIN IS OIL CANNING BS 367 BETWEEN STR 22 AND 23R. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW FEDEX SRM 53-30-3.
- [SDR 95FDEA00122](https://openairdocs.org/sdr/95FDEA00122), Feb 7, 1995: SKIN. CORRODED. CORROSION (76C002-00) NR 6 K-FLAP DATAPLATE. REMOVED DAMAGE AROUND DATAPLATE, REPAIRED K-FLAP WEB AND RELOCATED DATAPLATE IAW SRM 5250-3, DWG SR 27-57-010 REV B
- [SDR 95FDEA00121](https://openairdocs.org/sdr/95FDEA00121), Feb 7, 1995: SEAT TRACK. CORROSION. CORROSION ON SEAT TRACK FLANGE AT BS 344-347, LBL 42, WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 344-400, LBL 45, WL 208.
- [SDR 95FDEA00120](https://openairdocs.org/sdr/95FDEA00120), Feb 7, 1995: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FLANGE BS 480-483 LBL 46 WL 208.5. REMOVED AND REPLACED SEAT TRACK AT BS 480-590 LBL 46 WL 208.5 PER FEDEX SRM 53-10-5.
- [SDR 95FDEA00119](https://openairdocs.org/sdr/95FDEA00119), Feb 7, 1995: SEAT TRACK. CORROSION. CORROSION ON SEAT TRACK FLANGE BS 620-627, LBL 45, WL 208.5 IS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK AT BS 590 - 650, LBL 45, WL 208.
- [SDR 95FDEA00118](https://openairdocs.org/sdr/95FDEA00118), Feb 7, 1995: BEAM. CRACKED. FWD ENTRY DOOR LOWER GATE BEAM HAS A 1.5 INCHES CRACK ON FWD SIDE. REMOVED AND REPLACED FWD ENTRY DOOR LWR GATE BEAM.
- [SDR 95FDEA00114](https://openairdocs.org/sdr/95FDEA00114), Feb 6, 1995: STRINGER. CORROSION. CORROSION (NRO246) FOUND ON STR 19R FROM BS 435-440 RBL 65. REMOVED AND REPLACED STR 19R FROM BS 410.5 - 441 IAW FEDEX SRM 53-10-3 FIG 1 DETAIL II.
- [SDR 95FDEA00117](https://openairdocs.org/sdr/95FDEA00117), Feb 5, 1995: SEAT TRACK. DAMAGED. MECHANICAL DAMAGE ON SEAT TRACK AT BS 600 PLUS 16 INCHES - 620 PLUS 3, BL 0, WL 208.5 IS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK FROM BS 600 - 720, BL 0,
- [SDR 95FDEA00126](https://openairdocs.org/sdr/95FDEA00126), Feb 4, 1995: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FLANGE BS 490-540, 570 AND 640, RBL 25, WL 208.5. REMOVED AND REPLACED TRACK FROM BS 480-740 IAW FEDEX SRM 53-10-1.
- [SDR 95FDEA00116](https://openairdocs.org/sdr/95FDEA00116), Feb 4, 1995: CLIP. DAMAGED. MECHANICAL DAMAGE FOUND ON STR CLIP AT BS 400 STR 6L. REMOVED AND REPLACED STR CLIP AT BS 400 STR 6L.

## FAA accident and incident reports (1)

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 19951107039689I](https://openairdocs.org/incident/19951107039689I), Nov 7, 1995: Boeing 72725 (N507FE), Wichita, KS. Buffet vibrations en route. Right yoke not level. Te flaps loose. Replaced carriage plates and bushings.

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