# N510FE: 1965 Boeing 727-25, registration cancelled 2006-11-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 20, 2006
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-25](https://openairdocs.org/model/boeing-727-25) (registry code 1384006)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Serial number: 18282
- Year built: 1965
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: March 14, 1989
- Certificate issued: January 25, 1989
- Last registry action: April 20, 2004
- Mode S code: A661F1
- Owner when cancelled: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%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/N510FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=510FE
- Page: https://openairdocs.org/deregistered/N510FE-2006-11-20

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 (43)

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

- [SDR 97FDEA00721](https://openairdocs.org/sdr/97FDEA00721), Oct 9, 1997: DUCT. CRACKED. 97-0199 ENGINE NR 2 FIRE LIFHT ILLUMINATED ON CLIMB-OUT WHILE IN CLIMB POWER. LIGHT WENT OUT WHEN THROTTLE WAS RETARDED TO IDLE. FIRE CIRCUIT TESTED GOOD. FOUND
- [SDR 96FDEA01538](https://openairdocs.org/sdr/96FDEA01538), Sep 26, 1996: CHORD. CORRODED. NR0705 AND 041, WHILE WORKING NR0689 FOUND LOWER LT NOSE CHORD AT 320 LBL 19 TO BE CORRODED OUT OF LIMITS. *S/D* REMOVED CORRODED LOWER LT LOWER NOSE CHORD, NEW
- [SDR 96FDEA01537](https://openairdocs.org/sdr/96FDEA01537), Sep 26, 1996: CHORD. CRACKED. NR0702 AND 040, WHILE WORKING NR0689 FOUND RT LOWER NOSE CHORD CRACKED AT BS 293 RBL 15 WL 140. *S/D* REMOVED CRACKED RT LOWER NOSE CHORD. NEW RT LOWER NOSE CHO
- [SDR 96FDEA01536](https://openairdocs.org/sdr/96FDEA01536), Sep 25, 1996: SKIN. CORRODED. NR0039 AND 039, BULGE IN SKIN ABOVE AFT LT SERVICE DOOR STA 1170 TO 118 STR 18L. *S/D* REPLACED SECTION OF SKIN AND REPAIRED REF FEDEX EA 7-5330-31176.
- [SDR 96FDEA01525](https://openairdocs.org/sdr/96FDEA01525), Sep 24, 1996: STRINGER. CORRODED. NR0673 AND 038, WHILE WORKING ON NR0039 FOUND CORROSION ON STRINGER 20L AT BS 1163.
- [SDR 96FDEA01524](https://openairdocs.org/sdr/96FDEA01524), Sep 23, 1996: BEAM. CORRODED. NR0697 AND 037, WHILE WORKING NR0642 FOUND CORROSION UNDER INTERCOSTAL ON TOP FLANGE OF TRACK BEAM STA 266 WL 208 LBL 10 TO 8. *S/D* REMOVED AND REPLACED WL 208
- [SDR 96FDEA01515](https://openairdocs.org/sdr/96FDEA01515), Sep 19, 1996: WEB. CORROSION. NR0686 AND 036, UPON REMOVAL OF WEB FOR ACCESS OF 870 UPPER CHORD. FOUND 870 WEB TO BE CORRODED BS 870 RBL TO LBL 50 WL 161. *S/D* REMOVED AND REPLACED 870 WEB 
- [SDR 96FDEA01492](https://openairdocs.org/sdr/96FDEA01492), Sep 17, 1996: CHORD. CORRODED. NR 0674 AND 035, CORROSION (C53-224-05) ON BS 740 LOWER CHORD FOR CENTER WING SECTION FROM LBL 7 TO LBL 27. *S/D* REMOVED DAMAGED LOWER CHORD AT BS 740 AND INST
- [SDR 96FDEA01588](https://openairdocs.org/sdr/96FDEA01588), Sep 16, 1996: SHELF. CRACKED. NR 0689 - 042, WHILE WORKING NR0669 FOUND NOSE GEAR DRAG BRACE SUPPORT BEAM TO BE CRACKED BS 336 WL 153 LBL 13 TO LBL 20. *S/D* REMOVED DRAG BRACE SHELF, INSTAL
- [SDR 96FDEA01488](https://openairdocs.org/sdr/96FDEA01488), Sep 16, 1996: SPAR CHORD. CORROSION. NR 0685 AND 034, UPON REMOVAL OF REAR SPAR WEB FOUND CORROSION ON LOWER 870 SPAR CHORD BS 870 LBL 50 TO RBL 50 WL 161. *S/D* REMOVED CORROSION ON BS 870 SPAR CH
- [SDR 96FDEA01487](https://openairdocs.org/sdr/96FDEA01487), Sep 16, 1996: FLOORBEAM. CORRODED. NR 0623 AND 033, WHILE WORKING NR 0248 FOUND A CORRODED NUTPLATE HOLE AT BS 1166 LBL 12 WL 200 AFT LOWER FLANGE. *S/D* REPAIRED BS 1166 FLOORBEAM LOWER CHORD IA
- [SDR 96FDEA01486](https://openairdocs.org/sdr/96FDEA01486), Sep 16, 1996: CHORD. CORRODED. NR 0542 AND 032, CORROSION (C53-224-05) BS 740 RBL 68 ON UPPER CHORD OF CENTER FUEL CELL. *S/D* REMOVED DAMAGED UPPER CHORD AT BS 740 AND INSTALLED NEW CHORD IA
- [SDR 96FDEA01485](https://openairdocs.org/sdr/96FDEA01485), Sep 16, 1996: CHORD. CORRODED. NR 0431 AND 031, CORROSION (C53-224-05) BS 740 LBL 12 ON LOWER CHORD OF CENTER FUEL CELL. *S/D* REMOVED DAMAGED LOWER CHORD AT BS 740 AND INSTALLED NEW CHORD PE
- [SDR 96FDEA01484](https://openairdocs.org/sdr/96FDEA01484), Sep 16, 1996: STIFFENER. CORRODED. NR 0425 AND 030, CORROSION (C53-111-01-1) ON HORIZONTAL STIFFENER AT BS 314 BL 0 TO LBL 12 WL 183.
- [SDR 96FDEA01483](https://openairdocs.org/sdr/96FDEA01483), Sep 16, 1996: SKIN. CORRODED. NR 0271 AND 029, BS 328 PLUS 7 WL 142 LBL 20 SKIN IS BULGING. *S/D* REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL DOUBLER AT BS 330 TO 356 WL 148 T0 152 LBL 20 IA
- [SDR 96FDEA01482](https://openairdocs.org/sdr/96FDEA01482), Sep 16, 1996: SKIN. CRACKED. NR 0300 AND 028, BS 1060 STR 24R WL 155 THERE IS A CRACK IN SKIN. *S/D* REMOVED DAMAGED SKIN AT BS 1060 STR 24R WL 155 AND REPAIRED PER FEDEX SRM 53-30-3 FIG 3A
- [SDR 96FDEA01479](https://openairdocs.org/sdr/96FDEA01479), Sep 13, 1996: CHORD. CORRODED. NR 0288 AND 027, CORROSION (C53-224-01, -3) ON FWD FLANGE OF BS 1176 CHORD RBL 15 TO LBL 15 WL 208. *S/D* REPAIRED BS 1176.9 CHORD PER SB 727-53-0184 PART II OP
- [SDR 96FDEA01478](https://openairdocs.org/sdr/96FDEA01478), Sep 13, 1996: FLOORBEAM. CORRODED. NR 0656 AND 026, WHILE WORKING NR 0571, UPON REMOVAL OF HAT CHANNEL FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 328 RBL 12 TO 15 WL 208. *S/D* UPPER CHORD OF
- [SDR 96FDEA01477](https://openairdocs.org/sdr/96FDEA01477), Sep 13, 1996: SPAR CHORD. CORRODED. NR 0661 AND 025, CORROSION AT BS 870 RBL 40 TO RBL 55, WL 190 UPPER CHORD. CORROSION IS OUT OF LIMITS AS PER FEDEX SRM. *S/D* REMOVED CORROSION ON UPPER STA 870
- [SDR 96FDEA01472](https://openairdocs.org/sdr/96FDEA01472), Sep 12, 1996: DOORWAY FRAME. CORRODED. NR0558 AND 024, CORROSION (C53-111-01-1) ON DOOR CUTOUT SIDE FRAME AT BS 215 RBL 16 WL 167. *S/D* REMOVED DAMAGED SIDE FRAME WEB AND INSTALLED NEW SIDE FRAME WE
- [SDR 96FDEA01471](https://openairdocs.org/sdr/96FDEA01471), Sep 12, 1996: FLOOR BEAM. CORRODED. NR0369 AND 023, CORROSION (C53-224-01) AROUND FASTENER HOLE ON UNDERSIDE OF FLOOR BEAM TOP CHORD BS 380 LBL 25 WL 208, OUT OF LIMITS. *S/D* REMOVED DAMAGED AREA
- [SDR 96FDEA01470](https://openairdocs.org/sdr/96FDEA01470), Sep 12, 1996: FLOOR BEAM. CORRODED. NR0365 AND 022, CORROSION (C53-224-02, -1) AROUND FASTENER HOLES ON FLOOR BEAM TOP CHORD AT BS 660 RBL 11 AND 35 WL 208.
- [SDR 96FDEA01463](https://openairdocs.org/sdr/96FDEA01463), Sep 10, 1996: INTERCOSTAL. CORRODED. NR 0624 AND 021, CORROSION (C53-221-01) ON TOP OF INTERCOSTAL STA 266 WL 208 LBL 6. *S/D* REMOVED AND REPLACED TOP CHORD OF INTERCOSTAL AT BS 259 TO 277 LBL 6 W
- [SDR 96FDEA01462](https://openairdocs.org/sdr/96FDEA01462), Sep 10, 1996: BEAR STRAP. CORRODED. NR 0499 AND 020, CORROSION (C53-111-01, -3) ON BEAR STRAP AT BS 1105 RBL 28 WL 151. *S/D* REPAIRED BEAR STRAP PER FEDEX EA 7-5310-31169.
- [SDR 96FDEA01459](https://openairdocs.org/sdr/96FDEA01459), Sep 10, 1996: FLOORBEAM. CORRODED. NR 0375 AND 018, CORROSION (C53-224-01, -1) AROUND FASTENER HOLES ON UNDERSIDE OF FLOORBEAM AT BS 620 LBL TO 44 WL 208. *S/D* REPAIRED FLOORBEAM AT BS 620 LBL 1
- [SDR 96FDEA01458](https://openairdocs.org/sdr/96FDEA01458), Sep 10, 1996: WEB. CORRODED. NR 0290 AND 017, CORROSION (C53-224-01, -3) EMANATING FROM UNDER NUTPLATES ON BOTTOM SIDE OF SHEAR WEB AT BS 1174 RBL 22 LBL 16 WL 208. *S/D* REPAIRED AREA AT R
- [SDR 96FDEA01455](https://openairdocs.org/sdr/96FDEA01455), Sep 9, 1996: BULKHEAD WEB. CRACKED. NR 0506 AND 016, CRACKS IN BS 950 BULKHEAD LBL 4.5 AND RBL 4 WL 175. *S/D* REPAIRED CRACKS IN BS 950 BULKHEAD LBL 4.5 AND RBL 4, WL 175 PER FEDEX SRM 53-10-9, P
- [SDR 96FDEA01454](https://openairdocs.org/sdr/96FDEA01454), Sep 9, 1996: ANGLE. CRACKED. NR 0296 AND 015, FORWARD CARGO DOOR NR 5 L-ANGLE FROM TOP IS CRACKED. *S/D* REMOVED AND REPLACED FWD CARGO DOOR NR 5 LT, ANGLE PER FEDEX SRM 51-10-1, 53-30-2.
- [SDR 96FDEA01453](https://openairdocs.org/sdr/96FDEA01453), Sep 9, 1996: ANGLE. CRACKED. NR 0295 AND 014, FORWARD CARGO DOOR NR 3 L-ANGLE FROM TOP IS CRACKED.
- [SDR 96FDEA01452](https://openairdocs.org/sdr/96FDEA01452), Sep 9, 1996: BEAM. CRACKED. NR 0294 AND 013, FORWARD CARGO DOOR NR 2 FROM TOP TRANSVERSE BEAM IS CRACKED. *S/D* REMOVED AND REPLACED FWD CARGO DOOR NR 2 FROM TOP TRANSVERSE BEAM PER FEDEX 
- [SDR 96FDEA01451](https://openairdocs.org/sdr/96FDEA01451), Sep 9, 1996: BEAM. CRACKED. NR 0275 AND 012, AFT CARGO DOOR BEAM NR 2 FROM TOP IS CRACKED IN RADIUS. *S/D* REMOVED AND REPLACED AFT CARGO DOOR BEAM NR 2 FROM TOP PER FEDEX SRM 51-10-1.
- [SDR 96FDEA01450](https://openairdocs.org/sdr/96FDEA01450), Sep 9, 1996: FLOORBEAM. CORRODED. NR 0372 AND 011, CORROSION (C53-224-01, -1) AROUND FASTENER HOLES ON UNDER SIDE OF FLOORBEAM AT BS 560 RBL 56 TO LBL 56 WL 208. *S/D* REPAIRED TOP CHORD OF BS 5
- [SDR 96FDEA01449](https://openairdocs.org/sdr/96FDEA01449), Sep 9, 1996: INTERCOSTAL. CRACKED. NR 0345 AND 010, AFT CARGO DOOR AFT HINGE INTERCOSTAL IS BENT AND CRACKED. *S/D* REMOVED AND REPLACED AFT CARGO DOOR AFT HINGE INTERCOSTAL.
- [SDR 96FDEA01446](https://openairdocs.org/sdr/96FDEA01446), Sep 8, 1996: CHORD. CORROSION. NR 0422 AND 009, CORROSION (C53-111-01-1) ON LT MID NOSE CHORD AT BS 350 LBL 13 WL 169. *S/D* REMOVED AND REPLACED MID NOSE CHORD AT BS 350 LBL 13 WL 169 IAW DR
- [SDR 96FDEA01445](https://openairdocs.org/sdr/96FDEA01445), Sep 8, 1996: FLOOR BEAM. CORRODED. NR 0370 AND 008, CORROSION (C53-224-01, -1) AND BARE METAL 480 RBL 60 LBL 44 WL 208.
- [SDR 96FDEA01444](https://openairdocs.org/sdr/96FDEA01444), Sep 8, 1996: FLOOR BEAM. CORRODED. NR 0378 AND 007, CORROSION (C53-224-01, -1) AROUND FASTENER HOLE ON FLOOR BEAM TOP CHORD AT BS 580 LBL 36 WL 208.
- [SDR 96FDEA01443](https://openairdocs.org/sdr/96FDEA01443), Sep 8, 1996: FLOOR BEAM. CORRODED. NR 0248 AND 006, CORROSION (C53-111-01, -3) ON LOWER CHORD OF FLOOR BEAM AT BS 1166 WL 200 RBL 27 AT NUTPLATE. *S/D* MECHANICALLY REMOVED CORROSION IN AN AREA O
- [SDR 96FDEA01442](https://openairdocs.org/sdr/96FDEA01442), Sep 6, 1996: FLOORBEAM. CORRODED. NR 0446 AND 005, CORROSION (C53-111-01, -2) ON LOWER CHORD OF FLOORBEAM AT BS 600 LBL 15 WL 200. *S/D* REMOVED AND REPLACED FLOORBEAM LOWER CHORD STA 600 LBL TO
- [SDR 96FDEA01438](https://openairdocs.org/sdr/96FDEA01438), Sep 6, 1996: FLOORBEAM. CORRODED. NR 0285 AND 004, CORROSION (C53-224-02) ON 344 FLOORBEAM RBL 18 TO LBL 65 WL 208, OUT OF LIMITS. *S/D* REMOVED CORROSION ON BS 344 FLOORBEAM RBL 18 TO LBL 65 WL
- [SDR 96FDEA01437](https://openairdocs.org/sdr/96FDEA01437), Sep 6, 1996: FLOOR BEAM. CORROSION. NR 0292 AND 003, CORROSION (C53-224-01, -3) AROUND NUTPLATE HOLES ON BS 1030 UPPER CHORD RBL 21 TO LBL 21 WL 208. *S/D* REPAIRED OUT OF LIMITS UPPER CHORD IAW F
- [SDR 96FDEA01436](https://openairdocs.org/sdr/96FDEA01436), Sep 6, 1996: SKIN. DELAMINATED. NR 0196 AND 002, LT WING I/B FORE FLAP HAS A LARGE CREASED DENT MID SPAN UPPER SURFACE WBL 203.0. *S/D* LT WING I/B FORE FLAP REPAIRED PER FDEA SRM 51-40-6.
- [SDR 96FDEA01433](https://openairdocs.org/sdr/96FDEA01433), Sep 5, 1996: WEDGE. DELAMINATION. NR 0175 AND 001, RT WING O/B MID FLAP T/E WEDGE DELAMINATED MARKED. *S/D* REMOVED AND REPLACED DAMAGED SKIN ON RT WING O/B MID FLAP T/E WEDGE IAW FDEA SRM 51-40
- [SDR 96FDEA00850](https://openairdocs.org/sdr/96FDEA00850), Apr 25, 1996: EXTEND SWITCH. MALFUNCTIONED. DURING FLAP RETRACTION THE NR 7 SLAT FAILED TO RETRACT. AMBER LIGHT REMAINED ON AT PILOT'S PANEL AND GREEN LIGHT REMAINED ON AT THE SLAT/FLAP INDICATOR PANEL. R

## 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 19980127017169I](https://openairdocs.org/incident/19980127017169I), Jan 27, 1998: Boeing 72725 (N510FE), Richmond, VA. Contained compressor failure at cruise possibly disk. Landed number two engine out with no further incident.

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