# N186FE: 1966 Boeing 727-22, registration cancelled 2007-06-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 27, 2007 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-22](https://openairdocs.org/model/boeing-727-22) (registry code 1384002) - Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 18872 - Year built: 1966 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: April 28, 1966 - Certificate issued: August 31, 1989 - Last registry action: March 15, 2005 - Mode S code: A15778 - 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/N186FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=186FE - Page: https://openairdocs.org/deregistered/N186FE-2007-06-27 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 (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 04FDEA03234](https://openairdocs.org/sdr/04FDEA03234), Nov 26, 2004: ATTACH FITTING. DAMAGED. MAIN FRAME MLG FWD TRUNNION ATTACH FITTING OVERSIZE HOLE REWORK C/W EA 7-5710-55408 ENT BY: 497236 RPT BY: 497236 FACT 26NOV04 15:03 COMPLIED WITH EA 7-5710-554 - [SDR 04FDEA03170](https://openairdocs.org/sdr/04FDEA03170), Nov 19, 2004: HINGE. GOUGED. DOOR MAIN CARGO DOOR UPPER HINGE LOBE GOUGE REPAIR P/N B27-53-070-19. ENT BY: 497207 RPT BY: 497207 FACT 20 NOV 04 00:49 BFM U COMPLIED WITH EA NR 7-5210-82074 - [SDR 04FDEA03103](https://openairdocs.org/sdr/04FDEA03103), Nov 12, 2004: SEAT TRACK. GOUGED. FWD CARGO SEAT TRACK RT SIDE AT PFM BOX HAS A GOUGED/WORN LOBE. REMOVED FWD CARGO SEAT TRACK RT SIDE AT PFM BOX IAW SRM 51-30-02. CHECKED LIMITS IAW SRM 53-10-0 - [SDR 04FDEA03087](https://openairdocs.org/sdr/04FDEA03087), Nov 11, 2004: SEAT TRACK. CORRODED. RT UPPER LOBE BS480, RBL40, SEAT TRACK CORRODED AROUND RIVET. FABRICATED SEAT TRACK IAW SRM 53-10-5 PG 4, WITH MAT ID AND MPN 60-6549/7075-T6511. LOCATED AND DR - [SDR 02FDEA00416](https://openairdocs.org/sdr/02FDEA00416), Jun 16, 2002: SKIN. DENTED. SKIN DENTED AT BS 720, STR 16R. - [SDR 02FDEA00418](https://openairdocs.org/sdr/02FDEA00418), Jun 15, 2002: SKIN. CORRODED. CORROSION STR 19L TO 23L, BS 350-360 SKIN BULGING AROUND FASTENERS. REMOVED AND REPLACED SKIN PER EA 7-5330-64974 & SRM 53-30-3. - [SDR 02FDEA00447](https://openairdocs.org/sdr/02FDEA00447), Jun 12, 2002: FITTING. CORRODED. LEFT WING O/B AILERON FITTING CORRODED ON TOPSIDE OF FITTING. REMOVED AND REPLACED FITTING PER MM 27-10-131-4. - [SDR 01FDEA00012](https://openairdocs.org/sdr/01FDEA00012), Jan 6, 2001: ACTUATOR. FAILED. 01-002 DURING CLIMBOUT, LANDING GEAR SELECTOR IN OFF POSITION. RED DOORS LIGHT ILLUMINATED, WITH AMBER RT MLG DOOR LIGHT. REPLACED DOOR ACTUATOR PER B727 MM 32- - [SDR 00FDEA00208](https://openairdocs.org/sdr/00FDEA00208), Apr 3, 2000: SKIN. CRACKED. DURING ROUTINE INSP, EXT FUSELAGE SKIN FOUND CRACK IN THE A ROW AT 9/32 FASTENER HOLE AT BS 440, STR 4L. - [SDR 00FDEA00183](https://openairdocs.org/sdr/00FDEA00183), Mar 27, 2000: CHANNEL. CORRODED. AFT BAG BIN FLOOR SUPPORT CHANNEL CORRODED BEYOND ALLOWED LIMITS, ON LWR SURFACE, AT FASTENER HOLES BENEATH RT FLOOR TRACK BS 960. *S/D* REMOVED ANGLE, FAB AND - [SDR 00FDEA00174](https://openairdocs.org/sdr/00FDEA00174), Mar 27, 2000: ATTACH FITTING. CORRODED. DURING ROUTINE INSP, THE LEFT O/B AILERON, I/B ATTACH FITTING WAS FOUND TO HAVE INTERGRANULAR CORROSION. REMOVED AND REPLACED PER IAW MM 27-10-031-2. - [SDR 00FDEA00173](https://openairdocs.org/sdr/00FDEA00173), Mar 27, 2000: ATTACH FITTING. CORRODED. DURING ROUTINE INSP, RIGHT O/B AILERON, I/B ATTACH FITTING WAS FOUND TO HAVE INTERGRANULAR CORROSION. REMOVED AND REPLACED PER IAW MM 27-10-031-2. - [SDR 00FDEA00172](https://openairdocs.org/sdr/00FDEA00172), Mar 27, 2000: WEB. CRACKED. DURING ROUTINE INSP, WEB INSIDE VERTICAL STABILIZER AT FIN STA 110.4 FOUND CRACKED. REPAIRED IAW SRM 53-10-9 FIG 4. - [SDR 00FDEA00182](https://openairdocs.org/sdr/00FDEA00182), Mar 27, 2000: SKIN. CRACKED. DURING ROUTINE INSP, FUSELAGE SKIN FOUND CRACKED AT LAP JOINT, STR 20L, BS 1185. *S/D* FAB FILLER, DOUBLER AND INSTALLED IAW SRM 53-30-3 FIG 3A. - [SDR 97FDEA00866](https://openairdocs.org/sdr/97FDEA00866), Nov 26, 1997: SKIN. CORRODED. CORROSION (C53-100-01) ON EXTERIOR SKIN FROM BS 1149 TO BS 1153, RBL 2, WL 148. *S/D* REMOVED SECTION OF SKIN (9.7 X 7.5) AT BS 1149 TO 1159, RBL 2 LBL 2, WL 14 - [SDR 97FDEA00863](https://openairdocs.org/sdr/97FDEA00863), Nov 24, 1997: SKIN. DENTED. DENTED EXTERIOR SKIN AT BS 1135 BETWEEN STRINGERS 18L AND 19L, LBL 65, WL 192. *S/D* ACCESSED DAMAGED AREA AND INSTALLED COUNTERSINK WASHERS, FABRICATED PARTS A - [SDR 97FDEA00862](https://openairdocs.org/sdr/97FDEA00862), Nov 24, 1997: FRAME. CRACKED. BS 500 FRAME IS CRACKED UNDER FLOOR SUPPORT AT RBL 9, WL 156. *S/D* REPAIRED FRAME AT BS 500, RBL 9, WL 156 UNDER FLOOR SUPPORT IAW FEDEX SRM 51-40-3. - [SDR 97FDEA00857](https://openairdocs.org/sdr/97FDEA00857), Nov 24, 1997: CREASE BEAM. CORRODED. NR 0125 003 CORROSION (C53-224-06) ON CREASE BEAM VERTICAL FLANGE BS 310-346, LBL 62, WL 209. REMOVED OLD CORRODED CREASE BEAM AND DRILLED AND INSTALLED FASTENE - [SDR 97FDEA00856](https://openairdocs.org/sdr/97FDEA00856), Nov 24, 1997: STRINGER. CORRODED. WHILE WORKING CUSTOMER CARD NR NR0154, FOUND CORROSION ON STR 30, BS 1148, WL 142. *S/D* REMOVED DAMAGED STRINGER AT BS 1138 TO BS 1158, STR 30, WL 142 AND REPA - [SDR 97FDEA00851](https://openairdocs.org/sdr/97FDEA00851), Nov 21, 1997: SKIN. CORRODED. CORROSION (C53-100-01) ON EXTERIOR SKIN AT BS 1080 BETWEEN STR 27L AND 28L, WL 144, LBL 12 TO LBL 24. *S/D* REPAIRED SKIN AT BS 1080 BETWEEN STR 27L AND 28L, LB - [SDR 97FDEA00850](https://openairdocs.org/sdr/97FDEA00850), Nov 21, 1997: FRAME. CRACKED. BS 680 FRAME HAS CRACK EMANATING FROM RADIUS IN CUTOUT FOR STR 26 RT. *S/D* STOP DRILLED CRACK AT BS 680, STR 26 RT PER FEDEX SRM 51-10-1 AND REPAIRED CRACK PER ## Other aircraft with N186FE - [Registered now](https://openairdocs.org/aircraft/N186FE): Boeing 767-300F, S/N 63117, built 2020 --- 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.