# N180FE: 1966 Boeing 727-22, registration cancelled 2006-09-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 29, 2006 - Status when cancelled: Valid registration - Airframe: [Boeing 727-22](https://openairdocs.org/model/boeing-727-22) (registry code 1384002) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Serial number: 18867 - Year built: 1966 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 19, 2004 - Certificate issued: March 4, 2004 - Last registry action: March 4, 2004 - Mode S code: A1412E - Owner when cancelled: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP) - 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/N180FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=180FE - Page: https://openairdocs.org/deregistered/N180FE-2006-09-29 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 727-22: https://openairdocs.org/model/boeing-727-22.md ## Service difficulty reports (30) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 06FDEA0016](https://openairdocs.org/sdr/06FDEA0016), Jan 4, 2006: O-RING. LEAKING. JUST AFTER LEVEL OFF AT 16000 EXPERIENCED COMPLETE SYS-A HYD FAILURE. QTY AND PRESSURE BOTH WENT IMMEDIATELY TO ZERO. RAN QRH CHECKLIST, TIMED SYS-A FLUID SHUTO - [SDR 05FDEA02219](https://openairdocs.org/sdr/05FDEA02219), Aug 3, 2005: INDICATOR. SPINNING. NR 3 EPR GAUGE ERRATIC SPINNING RAPIDLY WHEN T/O POWER SET. AFTER RTO, OPERATELY NORMALLY ON SECOND ATTEMPT. INFO NOTED PER CREW, OPS CHECK GOOD ON GROUND, NO D - [SDR 05FDEA01745](https://openairdocs.org/sdr/05FDEA01745), Jun 29, 2005: HYDRAULIC SYSTEM. LEAKING. AT ROTATION A-SYS HYD FLUID WENT TO ZERO, RAN QRH, KEPT GEAR DOWN AND FLAPS 15, HAD A-SYS FLUID SHUT OFF SWITCHED OFF 23 MIN. DECLARED EMERGENCY. R & R INBOARD - [SDR 97FDEA00395](https://openairdocs.org/sdr/97FDEA00395), Jul 8, 1997: FRAME. CRACKED. NR 0646 013 WHILE WORKING CUSTOMER CARD NR 0607, FOUND FRAME CRACKED BS 1110, WL 153, RBL 25. REPAIRED CRACKED FRAME AT BS 1110, WL 153, RBL 25. ALL WORK DONE P - [SDR 97FDEA00365](https://openairdocs.org/sdr/97FDEA00365), Jun 24, 1997: FRAME. CRACKED. CRACK IN FRAME BS 680, STR 22L IN FORWARD CARGO BAY. *S/D* REMOVED DAMAGED FRAME AREA 2.75 DIAMETER AREA. HFEC NOTED NO CRACKS FOUND. FABRICATED REPAIR PARTS FR - [SDR 97FDEA00362](https://openairdocs.org/sdr/97FDEA00362), Jun 20, 1997: SKIN. DISBONDED. SKIN IS DISBONDED AT BS 1143 TO 1166 BETWEEN STR 24R TO 25R. *S/D* ACCESSED AREA, REMOVED EXISTING DOUBLERS, REMOVED SKIN BS 1080 TO 1183, STR 20 TO 26R. DRILLE - [SDR 97FDEA00361](https://openairdocs.org/sdr/97FDEA00361), Jun 19, 1997: CHORD. CRACKED. RIGHT MAIN GEAR WELL, BS 950, RBL 3, WL 180, - 75 CRACK TOP OF AFT VERTICAL CHORD. *S/D* REMOVED DAMAGED VERTICAL CHORD, FABRICATED AND INSTALLED NEW VERTICAL C - [SDR 97FDEA00357](https://openairdocs.org/sdr/97FDEA00357), Jun 19, 1997: SKIN. DISBONDED. NR 0577 007, SKIN IS DISBONDED AT BS 1143 TO 1183 RT BETWEEN STR 18, 19 AND 20. *S/D* REPAIRED DISBONDED SKIN AT BS 1143 TO 1183 RT BETWEEN STR 18, 19 AND 20 RT - [SDR 97FDEA00356](https://openairdocs.org/sdr/97FDEA00356), Jun 19, 1997: STRINGER. CORRODED. NR 0124 008 CORROSION (C53-224-01(3)) ON STRINGER 2 RT AT BS 967. REPAIRED CORRODED STRINGER NR 2 RT AT BS 967. ALL WORK DONE PER FED-EX SRM 51-40 AND 53-10-3. - [SDR 97FDEA00350](https://openairdocs.org/sdr/97FDEA00350), Jun 17, 1997: FLOORBEAM. CORRODED. NR 0573 006 WHILE WORKING NR 0172 FOUND CORROSION EMANATING FROM UNDER CEILING SUPPORT STRAP BS 540, RBL 25, WL 200. REPAIRED FLOORBEAM AT BS 540, RBL 25, WL 20 - [SDR 97FDEA00346](https://openairdocs.org/sdr/97FDEA00346), Jun 13, 1997: CHORD. CORRODED. NR 0571 004, CORROSION (C53-100-01,1) ON UPPER CHORD OF FRAME AT BS 220, RBL 21, WL 148. *S/D* REMOVED DAMAGED UPPER CHORD. FABRICATED AND INSTALLED NEW UPPER C - [SDR 97FDEA00338](https://openairdocs.org/sdr/97FDEA00338), Jun 11, 1997: FLOORBEAM. CORRODED. NR 0215 002 CORROSION EMANATING FROM UNDER NUT PLATE BS 600 FLOORBEAM UPPER CHORD AT RBL 17, WL 208. REMOVED DAMAGED FLOORBEAM UPPER FLANGE REPAIRED PER FED-EX - [SDR 97FDEA00347](https://openairdocs.org/sdr/97FDEA00347), Jun 5, 1997: FRAME. CRACKED. NR 0558 005, FRAME CRACKED AT BS 680, STR 26R FWD CARGO BAY. *S/D* STOP DRILLED CRACK, FABRICATED DOUBLER AND INSTALLED AT BS 680, STR 26R AS PER FED-EX SRM 51- - [SDR 97FDEA00345](https://openairdocs.org/sdr/97FDEA00345), Jun 5, 1997: ANGLE. CORRODED. NR 0504 003, CORROSION ON SHEAR TIE AFT SIDE OF BS 660, STR 27 TO 28 RT. *S/D* REMOVED CORRODED SHEAR TIE ANGLE FROM BS 660 FRAME, AFT SIDE BETWEEN STR 27 TO 28 - [SDR 97FDEA00329](https://openairdocs.org/sdr/97FDEA00329), Jun 5, 1997: FRAME. DENTED. NR 0502 001, BS 660 FRAME DENTED BETWEEN STR 24 TO 23 LT. *S/D* REPAIRED DENTED FRAME BS 660 BETWEEN STR 24 AND 23L PER FED-EX SRM 51-40-3. - [SDR 97FDEA00360](https://openairdocs.org/sdr/97FDEA00360), Jun 1, 1997: BEAM. CRACKED. NR 0214 FORWARD ENTRY DOOR LOWER GATE BEAM IS CRACKED IN RADIUS ON AFT SIDE. REMOVED AND INSTALLED NEW FORWARD ENTRY DOOR LOWER GATE BEAM IAW FED-EX SRM 51-30-2 - [SDR 95FDEA00849](https://openairdocs.org/sdr/95FDEA00849), Jun 28, 1995: POST. CRACKED. RIGHT NR 2 WINDOW CUT OUT DOUBLER IS CRACKED IN THE UPPER AFT RADIUS. REPAIRED CRACK IN DOUBLER IAW EO 7-5330-7-3354 PART 5. - [SDR 95FDEA00848](https://openairdocs.org/sdr/95FDEA00848), Jun 28, 1995: SPAR. CORRODED. CORROSION FOUND ON UPPER REAR SPAR CHORD BS 870 AT RBL 20 AND LBL 10. REMOVED AND REPLACED UPPER REAR SPAR CHORD AT BS 870 PER EA NR 95-2684 AND DWG NR 65C21531 - [SDR 95FDEA00847](https://openairdocs.org/sdr/95FDEA00847), Jun 28, 1995: KEEL BEAM. CORRODED. RIGHT KEEL BEAM CORRODED, BS 953, RBL 6, WL 156. CUT ACCESS HOLE IN SKIN, REMOVED AND REPLACED KEEL BEAM THEN REPAIRED HOLE IN SKIN. REF: TCO EWO NR 95-2710 AND - [SDR 95FDEA00846](https://openairdocs.org/sdr/95FDEA00846), Jun 28, 1995: FRAME. CRACKED. AFT CARGO BAY BS 1130 STR 27L, FRAME IS CRACKED. CUT OUT DAMAGE AND REPAIR PER SRM 51-40-3. - [SDR 95FDEA00845](https://openairdocs.org/sdr/95FDEA00845), Jun 28, 1995: FITTING. CORRODED. STA 351, CORROSION ON STR 26R DOG BONE FITTING. REMOVED AND REPLACED STR 26R STA 351. FITTING IAW FEDEX SRM 51-30-2. - [SDR 95FDEA00844](https://openairdocs.org/sdr/95FDEA00844), Jun 28, 1995: FRAME. DAMAGED. FOUND FIGURE EIGHT HOLE IN FRAME FLANGE AT STA 1030 STR 27R. TRIMMED OUT DAMAGED PORTION OF FRAME, FABRICATED REPAIR PART AND INSTALLED WET WITH SEAL AS PER SRM - [SDR 95FDEA00843](https://openairdocs.org/sdr/95FDEA00843), Jun 28, 1995: FRAME. CRACKED. CRACKED FRAME AT BS 1070 STR 27L. REMOVED AND REPLACED FRAME AT BS 1070 STR 24-27L AND TREATED IAW FEDEX SRM 51-40-03, FEDEX MM 51-20-31 AND 51-20-21. - [SDR 95FDEA00842](https://openairdocs.org/sdr/95FDEA00842), Jun 28, 1995: FRAME. CRACKED. CRACKED FRAME AT BS 1090 STR 27L. REMOVED AND REPLACED FRAME BS 1090 STR 24-27L AND TREATED IAW FEDEX SRM 57-40-03, FEDEX MM 51-20-31 AND 51-20-21. - [SDR 95FDEA00841](https://openairdocs.org/sdr/95FDEA00841), Jun 28, 1995: STRINGER. CRACKED. STR 23L IS CRACKED AT STA 380. REMOVED AND REPLACED STR 23L STA 360-384 IAW FEDEX SRM 53-10-3. - [SDR 95FDEA00840](https://openairdocs.org/sdr/95FDEA00840), Jun 28, 1995: STRINGER. CRACKED. POSSIBLE CRACKS ON STR 24L BS 380. REMOVED DAMAGED STR, FABRICATED REPAIR PARTS AND INSTALLED IAW FEDEX SRM 53-10-3. - [SDR 95FDEA00839](https://openairdocs.org/sdr/95FDEA00839), Jun 28, 1995: SKIN. GOUGED. FORWARD CARGO BAY DOORWAY CUT OUT BS 523 BETWEEN STR 22 AND 23R, 2 EACH GOUGES MAXIMUM DEPTH OF .030 INCH. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR - [SDR 95FDEA00838](https://openairdocs.org/sdr/95FDEA00838), Jun 28, 1995: SKIN. DENTED. DENT APPROXIMATELY .100 INCH DEEP IN SKIN AT BS 461 WL 210 RT SIDE. CUT OUT DENT AT BS 461 WL 210 AND FABRICATED A REPAIR DOUBLER AND INSTALLED AS PER FEDEX SRM - [SDR 95FDEA00837](https://openairdocs.org/sdr/95FDEA00837), Jun 28, 1995: TIE. CRACKED. WEB TO FRAME TIE FOUND TO BE CRACKED AT STA 823 RBL 67 WL 208. REMOVED FRAME TIE AT STA 823 RBL 67 WL 208 FABRICATED NEW TIE ALODINED AND PRIMED, INSTALLED PER - [SDR 95FDEA00836](https://openairdocs.org/sdr/95FDEA00836), Jun 28, 1995: SKIN. GOUGED. GOUGE LESS THAN .004 INCH DEEP IN SKIN AT BS 410 WL 156 LT SIDE. FOUND GOUGE TO BE OUT OF LIMITS, REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AT BS 410 WL 156 L ## Other aircraft with N180FE - [Registered now](https://openairdocs.org/aircraft/N180FE): Boeing 767-300F, S/N 63111, built 2019 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.