# N511FE: 1965 Boeing 727-25, registration cancelled 2013-08-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 22, 2013 - Status when cancelled: Sale reported, canceled - 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: 18283 - Year built: 1965 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 14, 1989 - Last registry action: November 13, 2003 - Mode S code: A665A8 - Location: [Everett, WA](https://openairdocs.org/faa-place/WA/Everett) - Owner type: Individual - Owner's area on the map: 47.9027° N, 122.2559° W: Placed by OpenAirDocs at the center of ZIP code 98204, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N511FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=511FE - Page: https://openairdocs.org/deregistered/N511FE-2013-08-22 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 727-25: 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 99FDEA00245](https://openairdocs.org/sdr/99FDEA00245), Jun 25, 1999: WEB. CORRODED. WHILE WORKING NR 0795 FOUND CORROSION NOSE WHEEL WELL HORIZONTAL WEB AND BONDED DOUBLERS AT BS 294 TO BS 309, RBL 13 TO LBL 13, WL 181. - [SDR 99FDEA00221](https://openairdocs.org/sdr/99FDEA00221), Jun 15, 1999: CHORD. CORRODED. CORROSION (C53-224-03) PREVIOUS BLEND ON RT MID NOSE, BS 304-314, RBL 20, WL 170. - [SDR 99FDEA00220](https://openairdocs.org/sdr/99FDEA00220), Jun 15, 1999: FLOORBEAM. CORRODED. NR 639 - WHILE WORK NR 284 FOUND CORROSION ON FLOORBEAM, BS 560, RBL 10-12, WL 208. REPAIRED FLOORBEAM IAW FEDEX SRM 53-10-8 AND 51-30-2. - [SDR 99FDEA00219](https://openairdocs.org/sdr/99FDEA00219), Jun 15, 1999: WEB. GOUGED. FOUND CORROSION (C53-224-03) AND GOUGE ON VERTICAL WEB NEAR RT TRUNNION BOLT HOLE BS 309, RBL 14, WL 169. - [SDR 99FDEA00218](https://openairdocs.org/sdr/99FDEA00218), Jun 15, 1999: FRAME. CRACKED. CRACK INDICATION AT BS 970 FRAME, BOTTOM HOLE OF FRAME TO STRINGER 9L. - [SDR 99FDEA00216](https://openairdocs.org/sdr/99FDEA00216), Jun 11, 1999: CHORD. CORRODED. NR 799 WHILE WORKING NR 246 FOUND WING CTR SECTION LWR CHORD AT BS 870, RBL 16 TO RBL 55 TO BE CORRODED. - [SDR 99FDEA00215](https://openairdocs.org/sdr/99FDEA00215), Jun 11, 1999: WEB. CORRODED. NR 634 WHILE WORKING NR 246 FOUND BS 870 WING CTR SECTION AFT VERTICAL WEB TO BE CORRODED BEYOND LIMITS. - [SDR 99FDEA00214](https://openairdocs.org/sdr/99FDEA00214), Jun 11, 1999: CHORD. CORRODED. NR 246 CORROSION (C53-132-02(1)) BETWEEN BS 870 UPPER CHORD AND 870 WEB AT LBL 41. - [SDR 96FDEA01615](https://openairdocs.org/sdr/96FDEA01615), Oct 26, 1996: BULKHEAD. CRACKED. NR 0509 024, CRACK ON THE AFT SIDE OF THE 870 BULKHEAD AT RBL 9.5 AND WL 157. - [SDR 96FDEA01614](https://openairdocs.org/sdr/96FDEA01614), Oct 25, 1996: BULKHEAD. CRACKED. NR 0507 023, POSSIBLE CRACK ON AFT SIDE OF BS 950 BULKHEAD AT LBL 4 WL 176 AND AT LBL 11, WL 181 TO 184. - [SDR 96FDEA01583](https://openairdocs.org/sdr/96FDEA01583), Oct 15, 1996: FLOORBEAM. CORRODED. NR 0437 AND 022, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY AT BS 1148 LBL 11 TO 23 WL 199 ON FLOORBEAM AT NUTPLATE HOLES. *S/D* CORROSION FOUND TO BE OUT - [SDR 96FDEA01582](https://openairdocs.org/sdr/96FDEA01582), Oct 14, 1996: FLOORBEAM. CORRODED. NR 0609 AND 021, CORROSION (C53-224-01, -3) ON STA 1110 RBL 23 WL 208 UNDER TOP FLANGE OF FLOORBEAM. *S/D* FOUND CORROSION TO BE OUT OF LIMITS. CUT OUT DAMAGED - [SDR 96FDEA01577](https://openairdocs.org/sdr/96FDEA01577), Oct 14, 1996: S-DUCT SKIN. CORRODED. NR0496 AND 019, CORROSION (C54-451-02) ON INTERIOR SKIN OF S-DUCT AT BS 1201 AT CENTER LINE, MIDDLE OF S-DUCT. *S/D* REMOVED DAMAGED SKIN OF INTERIOR OF S-DUCT - [SDR 96FDEA01571](https://openairdocs.org/sdr/96FDEA01571), Oct 8, 1996: SKIN. CREASED. NR0145 AND 018, CREASE ON SKIN AT BS 254 STR 20 TO 21R. *S/D* REMOVED DAMAGE FROM SKIN AT BS 254 BETWEEN STR 20 TO 21R, FABRICATED AND INSTALLED REPAIR PER FEDE - [SDR 96FDEA01567](https://openairdocs.org/sdr/96FDEA01567), Oct 8, 1996: STIFFENER. CRACKED. NR0510 AND 017, TOP OF THE VERTICAL STIFFENER IS CRACKED IN THE WING CENTER SECTION AT BS 740 RBL 45. *S/D* REMOVED AND REPLACED VERTICAL STIFFENER IN THE WING - [SDR 96FDEA01566](https://openairdocs.org/sdr/96FDEA01566), Oct 7, 1996: FLOOR BEAM. CORRODED. NR0438 AND 016, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY AT BS 1130 LBL 11 TO 13 WL 199 ON FLOORBEAM AT NUTPLATE HOLES. *S/D* CORROSION FOUND TO BE OUT O - [SDR 96FDEA01563](https://openairdocs.org/sdr/96FDEA01563), Oct 4, 1996: FLOOR BEAM. CORROSION. NR0594 AND 015, CORROSION (C53-224-01, -3) AT BS 1110 RBL 43 WL 207 EMITTING FROM UNDER SIDE OF TOP FLANGE OF FLOOR BEAM AT FASTENER HOLE. *S/D* REPAIRED CORROS - [SDR 96FDEA01557](https://openairdocs.org/sdr/96FDEA01557), Sep 30, 1996: FLOORBEAM. CORRODED. NR0440 AND 012, CORROSION (C53-111-01,-3) IN AFT CARGO BAY AT BS1050 LBL TO RBL 20 WL 199 ON FLOOR BEAM AT NUTPLATE HOLES. *S/D* REMOVED CORRODED SECTION OF BS - [SDR 96FDEA01553](https://openairdocs.org/sdr/96FDEA01553), Sep 30, 1996: BONDING JUMPER. CORRODED. NR0589 AND 010, WHILE WORKING NR0218 FOUND NR 2 K-FLAP I/B BULLNOSE BONDING JUMPER UPPER ATTACH POINT CORRODED. *S/D* REPAIRED PER FEDEX SRM 57-50-3. - [SDR 96FDEA01552](https://openairdocs.org/sdr/96FDEA01552), Sep 28, 1996: FLOORBEAM. CORROSION. NR0434 AND 009, CORROSION (C53-224-01, -1, -100) AT STA 620 RBL 3 WL 208 ON FRAME FILLER. *S/D* REPAIRED FLOORBEAM AT BS 620 WL 208 RBL 35 TO LBL 24 IAW FEDEX S - [SDR 96FDEA01551](https://openairdocs.org/sdr/96FDEA01551), Sep 28, 1996: SKIN. DELAMINATION. NR0579 AND 008, WHILE WORKING NR0576 FOUND THREE AREAS OF DELAMINATION ON LOWER SURFACE. *S/D* REPAIRED DAMAGED SKIN TO RIGHT I/B FORE FLAP LOWER SURFACE PER FE - [SDR 96FDEA01556](https://openairdocs.org/sdr/96FDEA01556), Sep 27, 1996: FRAME. CORRODED. NR0541 AND 011, FOUND CORROSION (C53-221-01) ON FRAME WEB AND TWO STIFFENERS AFT SIDE OF BS 251.6 RBL 51 WL 215 TO 221. *S/D* REMOVED CORRODED WEB AND STIFFENER - [SDR 96FDEA01584](https://openairdocs.org/sdr/96FDEA01584), Sep 25, 1996: SKIN. CRACKED. NR 0580 AND 020, CRACK IN L/W O/B AILERON I/B AFT TRAILING EDGE CHORD. *S/D* STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER FEDEX SRM 51-40-3. - [SDR 96FDEA01535](https://openairdocs.org/sdr/96FDEA01535), Sep 25, 1996: SKIN. DELAMINATED. NR0576 AND 007, RT WING I/B FORE FLAP IS DELAMINATED AT I/B END UPPER SURFACE. *S/D* REPAIRED DAMAGED AREA TO RT WING I/B FORE FLAP PER SRM 51-40-6. - [SDR 96FDEA01534](https://openairdocs.org/sdr/96FDEA01534), Sep 25, 1996: ACT MOUNT. CRACKED. NR 0219 AND 006. NR 3 SLAT ACTUATOR ROD END MOUNT I/B AND O/B RIBS ARE CRACKED. ***S/D***** REMOVED AND REPLACED NR 3 SLAT ACTUATOR ROD AND MOUNT I/B AND O/B RI - [SDR 96FDEA01519](https://openairdocs.org/sdr/96FDEA01519), Sep 21, 1996: DOOR FRAME. CRACKED. NR0055, 004, AFT ENTRY DOOR LT SIDE FRAME IS CRACKED AT 41 INCHES FROM BOTTOM OF DOOR. - [SDR 96FDEA01587](https://openairdocs.org/sdr/96FDEA01587), Sep 20, 1996: FLOORBEAM. CORRODED. CORROSION (C53-111-01, -3) IN AFT CARGO BAY AT BS 1050 LBL 20 TO RBL 20 WL 199 ON FLOORBEAM AT NUTPLATES HOLES. REMOVED CORRODED SECTION OF BS 1050 FLOORBEAM FR - [SDR 96FDEA01562](https://openairdocs.org/sdr/96FDEA01562), Sep 20, 1996: FLOORBEAM. CORRODED. NR0435 AND 014, CORROSION (C53-224-01, -3, C53-224-04) STR 9L STA 1130 RBL 25 TO 45 WL 208 UPPER FLANGE. *S/D* FOUND CORROSION TO BE OUT OF LIMITS. REPAIRED FLO - [SDR 96FDEA01561](https://openairdocs.org/sdr/96FDEA01561), Sep 20, 1996: FLOORBEAM. CORRODED. NR0439 AND 013, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY AT BS 1110 LBL 16 TO 30 WL 199 ON FLOORBEAM AT NUTPLATE HOLES. *S/D* CORROSION FOUND TO BE OUT O - [SDR 96FDEA01512](https://openairdocs.org/sdr/96FDEA01512), Sep 20, 1996: DOORWAY FRAME. CORRODED. NR0324 AND 003, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY ON THE FWD SIDE OF THE AFT CARGO DOOR FRAME BS 1110 STR 19R. *S/D* REMOVED DAMAGED AREA ON FRAME - [SDR 96FDEA01511](https://openairdocs.org/sdr/96FDEA01511), Sep 20, 1996: BONDING JUMPER. CORRODED. NR 0214 AND 002. NR 1 K-FLAP TO BULLNOSE INBOARD BONDING JUMPER UPPER AND LOWER ATTACH POINTS ARE CORRODED. REMOVED CORRODED AREAS, BLENDED, AND TREATED UPPER A - [SDR 96FDEA01513](https://openairdocs.org/sdr/96FDEA01513), Sep 18, 1996: FLOORBEAM. CORRODED. NR0250 AND 001, CORROSION (C53-111-01-2) ON FLOORBEAM LOWER FLANGE AROUND NUTPLATE HOLE AT BS 520 WL 200 RBL 4. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. 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