# N286SC: 1980 Boeing 727-2A1, registration cancelled 2018-01-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 3, 2018
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-2A1](https://openairdocs.org/model/boeing-727-2a1) (registry code 138407F)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Serial number: 21601
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 19, 1989
- Certificate issued: January 4, 2012
- Last registry action: December 15, 2014
- Mode S code: A2E5D8
- Owner when cancelled: [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC)
- Location: [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.4607° N, 83.8443° W: Placed by OpenAirDocs at the center of ZIP code 45177, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N286SC
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=286SC
- Page: https://openairdocs.org/deregistered/N286SC-2018-01-03

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 727-2A1: https://openairdocs.org/model/boeing-727-2a1.md

## Service difficulty reports (198, newest 50)

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

- [SDR C8GA2011000001](https://openairdocs.org/sdr/C8GA2011000001), Mar 23, 2011: CONTROL CABLE. OUT OF ADJUST. DURING APPROACH, WITH THE GEAR LEVER PLACED IN THE DOWN POSITION, THE GREEN LANDING GEAR INDICATION LIGHTS WERE ILLUMINATED AS WELL AS THE RED INDICATION LIGHTS
- [SDR FOTR20006NR2095](https://openairdocs.org/sdr/FOTR20006NR2095), Feb 24, 2010: SKIN. DENTED. (FOTR) DENT ON LT FUSELAGE SKIN BS 1319 STR 9L. REPAIRED ON FASI WO 20006. N/R 02095- R & R PREVIOUS REPAIR TO LT FUSELAGE SKIN AT STA 1319 STR 9L IAW SRM 53-30
- [SDR FOTR20006NR2059](https://openairdocs.org/sdr/FOTR20006NR2059), Feb 13, 2010: SKIN. DEBONDED. RT WING INBD AILERON TAB LOWER SURFACE DISBONDED 22 INCHES FROM OTBD END. REPAIRED ON FASI WO 20006, N/R 02059. REPAIRED RT WING INBD AILERON TAB AT WBL 280 BY 
- [SDR FOTR20006NR2054](https://openairdocs.org/sdr/FOTR20006NR2054), Feb 12, 2010: STRUCTURE. CRACKED. RT WING INBD MID FLAP LOWER T/E CHORD CRACKED WBL 100. REPAIRED ON FASI WO 20006, N/R 02054. REMOVED AND REPLACED RT WING INBD MID-FLAP LOWER T/E CHORD SECTION 
- [SDR FOTR20006NR2033](https://openairdocs.org/sdr/FOTR20006NR2033), Feb 10, 2010: SKIN. DEBONDED. RT WING NR 9 SPOILER LOWER SURFACE HAS DISBONDED DOUBLER JUST AFT OF ACTUATOR ATTACH FITTING. REPAIRED ON FASI WO 20006, N/R 02033. REPAIRED RT WING NR 9 SPOILE
- [SDR FOTR20006NR2031](https://openairdocs.org/sdr/FOTR20006NR2031), Feb 10, 2010: SKIN. DEBONDED. LT INBD AFT FLAP LOWER SURFACE HAS DISBONDED AREA AT WBL 135. REPAIRED ON ASI WO 20006, N/R 02031. INSTALLED HOT BONDED REPAIR TO LEFT INBD AFT FLAP LOWER SURFA
- [SDR FOTR20006NR2028](https://openairdocs.org/sdr/FOTR20006NR2028), Feb 10, 2010: SKIN. PUNCTURED. RT ELEVATOR LOWER SKIN WORN THRU AT ELEV STA 78 NEAR CENTER OF ELEVATOR. REPAIRED ON FASI WO 20006, N/R 02028. INSTALLED REPAIR DOUBLER ON RIGHT ELEVATOR LOWER 
- [SDR FOTR20006NR2027](https://openairdocs.org/sdr/FOTR20006NR2027), Feb 9, 2010: FRAME. DAMAGED. UPPER CABIN FRAME DAMAGED AT BS 380 STR 5L. REPAIRED ON FASI WO 20006. N/R 02027. INSTALLED REPAIR ANGLE TO FUSELAGE FRAME AT BS 380, STR 5L IAW B727 SRM 53-10-
- [SDR FOTR20006NR2023](https://openairdocs.org/sdr/FOTR20006NR2023), Feb 8, 2010: SKIN. DEBONDED. RT OTBD AILERON TAB, UPPER SURFACE INBD END HAS AREA OF DISBOND. REPAIRED ON FASI WO 20006. N/R 02023, INSTALLED HOT BONDED REPAIR TO RT OTBD AILERON TAB UPPER 
- [SDR FOTR20006NR2021](https://openairdocs.org/sdr/FOTR20006NR2021), Feb 8, 2010: SKIN. PUNCTURED. RT WING OTBD FORE FLAP HAS SEVERAL GOUGES. REPAIRED ON FASI W/0 NR 20006, N/R 02021" INSTALLED REPAIR DOUBLER TO RT WING OTBD FORE FLAP AT WS 465 IAW SRM 57-50-
- [SDR FOTR20006NR2020](https://openairdocs.org/sdr/FOTR20006NR2020), Feb 8, 2010: STRINGER CLIP. PUNCTURED. FRAME TO STR. BRACKET HAS HOLE IN RADIUS AT STA. 672 STR. 13L. REPAIRED ON FASI W/O NR 20006, N/R 02020- R & R SUPPORT ANGLE AT STA 672 STR 13L IAW SRM 51-30-2,
- [SDR FOTR20006NR2016](https://openairdocs.org/sdr/FOTR20006NR2016), Feb 8, 2010: SKIN. GOUGED. LT WING NR 4 SLAT OTBD END GOUGED. REPAIRED ON W/O NR 20006, N/R 02016- R & R LT WING NR4 SLAT OTBD RIB IAW SRM 51-30-2, REV 102 WITH PN 65-17286-13.
- [SDR FOTR20006NR2013](https://openairdocs.org/sdr/FOTR20006NR2013), Feb 8, 2010: WEDGE. DELAMINATED. RT AILERON OTBD T/E WEDGE HAS AREA OF DISBOND ON UPPER INBD END. REPAIRED ON FASI W/O NR 20006, N/R 02013. INSTALLED HOT BONDED REPAIR TO RIGHT WING OTBD AILERO
- [SDR FOTR20006NR2012](https://openairdocs.org/sdr/FOTR20006NR2012), Feb 8, 2010: SKIN. DELAMINATED. RT OTBD AILERON T/E WEDGE HAS AREA OF DISBOND ON UPPER SURFACE. REPAIRED ON FASI W/O NR 20006, NR 02012 - INSTALLED HOT BONDED REPAIR TO RT WING OTBD AILERON T/
- [SDR FOTR20006NR2011](https://openairdocs.org/sdr/FOTR20006NR2011), Feb 8, 2010: SKIN. DELAMINATED. RT WING OTBD AFT FLAP IS DELAMINATED AT STA WBL 338. REPAIRED ON FASI W/O NR 20006, N/R 2011 INSTALLED HOT BONDED REPAIR TO RT WING OTBD AFT FLAP AT WBL 228 IAW
- [SDR FOTR20006NR1992](https://openairdocs.org/sdr/FOTR20006NR1992), Feb 6, 2010: SKIN. DENTED. RT WING INBD FLAP LOWER SURFACE IS DENTED AT WS 135. REPAIRED ON FASI W/O 20006, N/R 01992, INSTALLED HOT BONDED REPAIR TO LOWER SURFACE OF RT INBD AFT FLAP AT 
- [SDR FOTR20006NR1984](https://openairdocs.org/sdr/FOTR20006NR1984), Feb 5, 2010: STRINGER. CORRODED. AFT AIRSTAIR AT BS 1323 CENTER STRINGER AT LOWER END CORRODED. REPAIRED ON FSAI W/O NR 20006, N/R 01984. REPAIRED STRINGER AT AFT STAIRS STA 1323 IAW B727 SRM 5
- [SDR FOTR20006NR1976](https://openairdocs.org/sdr/FOTR20006NR1976), Feb 5, 2010: WEB. CRACKED. LT SIDE OF FUSELAGE INTERIOR WEB CRACKED JUST ABOVE NR 2 ENG "S" DUCT AT BS 1303. REPAIRED ON FASI W/O NR 20006, N/R 01976. INSTALLED REPAIR DOUBLER TO CRACKED 
- [SDR FOTR20006NR1972](https://openairdocs.org/sdr/FOTR20006NR1972), Feb 5, 2010: DOUBLER. CRACKED. L1 DOOR UPPER HINGE SKIN DOUBLER CRACKED LOWER CORNER. REPAIRED ON FASI W/O NR 20006, N/R 01972. REPLACED EXTERNAL DOUBLER AT LEFT FORWARD ENTRY DOOR UPPER HING
- [SDR FOTR20006NR1971](https://openairdocs.org/sdr/FOTR20006NR1971), Feb 5, 2010: SHEAR TIE. CRACKED. STA 600 STR 16L SHEAR TIE CRACKED. REPAIRED ON FASI W/O NR 20006, NR 01971, REPLACED CRACKED SHEAR TIE AND DOUBLER AT BS 680, STR 16L IAW B727 SRM 53-20-2 FIG 3
- [SDR FOTR20006NR1969](https://openairdocs.org/sdr/FOTR20006NR1969), Feb 5, 2010: STRINGER CLIP. CRACKED. STA 700 STR. 16L STR CLIP CRACKED. REPAIRED ON FASI W/O NR 20006,NR 01969. REPLACED CRACKED STRINGER CLIPS AT BS 700 STR 16L IAW DRAWING NR 66-11809 REV B AND B
- [SDR FOTR20006NR1965](https://openairdocs.org/sdr/FOTR20006NR1965), Feb 5, 2010: FRAME. DENTED. STA 720A STR 16R FRAME IS DENTED. REPAIRED ON FASI W/O NR 20006, NR 01965. INSTALLED REPAIR DOUBLER TO FRAME AT BS 720A, STR 16R, DUE TO DENT, IAW B727 SRM 53-1
- [SDR FOTR20006NR1962](https://openairdocs.org/sdr/FOTR20006NR1962), Feb 5, 2010: FRAME. GOUGED. LEFT UPPER CABIN FRAME GOUGED AT BS 670 BETWEEN STR 5L AND 6L. REPAIRED ON FASI W/O 20006, N/R 01962. REMOVED AND REPLACED FUSELAGE FRAME AT BS 670 BETWEEN STR 
- [SDR FOTR20006NR1862](https://openairdocs.org/sdr/FOTR20006NR1862), Feb 4, 2010: FRAME. BENT. STA 420 FRAME BENT AT STR 7R. REPAIRED ON FASI W/O NR 20006, NR 01862. INSTALLED REPAIR DOUBLER TO FRAME AT BS 420, STR 7R, DUE TO DENT, IAW B727 SRM 53-10-2 FI
- [SDR FOTR20006NR1850](https://openairdocs.org/sdr/FOTR20006NR1850), Feb 4, 2010: STRUCTURE. PUNCTURED. RT INBD AFT FLAP LOWER SURFACE IS PUNCTURED NEAR INBD END. REPAIRED ON FASI W/O NR 20006, NR 01850. INSTALLED HOT BONDED REPAIR TO RIGHT INBD AFT FLAP LOWER SUR
- [SDR FOTR20006NR5780](https://openairdocs.org/sdr/FOTR20006NR5780), Feb 3, 2010: WEB. CORRODED. LT MOP SILL CORRODED UNDERSIDE STA 1130 BELOW FLOOR. REPAIRED ON FASI WO 20006, N/R 05780. REMOVED AND REPLACED WEB BETWEEN STA 1110 TO 1130 IAW B727 SRM 53-10-
- [SDR FOTR20006NR5718](https://openairdocs.org/sdr/FOTR20006NR5718), Feb 3, 2010: FLOORBEAM. CRACKED. MAIN CABIN OVERWING FLOORBEAM T-CHORD CRACKED AT BS 760 RBL.45.5. REPAIRED ON FASI W/O NR 20006, N/R 05718. REMOVED AND REPLACED MAIN CABIN FLOORBEAM T-CHORD AT
- [SDR FOTR20006NR5753](https://openairdocs.org/sdr/FOTR20006NR5753), Feb 3, 2010: ANGLE. CORRODED. STA 1166 AT STR 17 WEB AREA CORRODED. REPAIRED ON FASI W/O NR 20006, N/R 005753. REMOVED AND REPLACED UPPER ANGLE AND LOWER CHANNEL SUPPORT AT STA 1166, STR 17R
- [SDR FOTR20006NR 5760](https://openairdocs.org/sdr/FOTR20006NR%205760), Feb 3, 2010: FLOORBEAM. DAMAGED. STA 1070 FLOORBEAM DOUBLE DRILLED HOLE RBL.50. REPAIRED ON FASI W/O NR 20006, N/R 04858. REMOVED AND REPLACED UPPER SUPPORT FITTING AT RT LOWER TORQUE BOX WEB A
- [SDR FOTR20006NR1842](https://openairdocs.org/sdr/FOTR20006NR1842), Feb 3, 2010: FRAME. DENTED. MAIN CABIN FRAME BS 280 FLANGE IS DENTED AT STR 6R. REPAIRED ON FASI W/ONR 20006, NR 01842. INTALLED REPAIR DOUBLER TO FRAME AT BS 380, STR 6R, DUE TO DENT, IAW
- [SDR FOTR20006NR1841](https://openairdocs.org/sdr/FOTR20006NR1841), Feb 3, 2010: FRAME. DENTED. MAIN CABIN FRAME BS.400 FLANGE IS DENTED AT STR 6R. REPAIRED ON FASI W/O 20006,NR 01841 INSTALLED REPAIR DOUBLER TO FRAME AT BS 400, STR 6R, DUE TO DENT, IAW SR
- [SDR FOTR20006NR1798](https://openairdocs.org/sdr/FOTR20006NR1798), Feb 3, 2010: INTERCOSTAL. CRACKED. AFT PIT HAS A CRACK AT INTERCOSTAL STR 23L BETWEEN BS 950D TO 950E. REPAIRED ON FASI W/O NR20006, NR01798. R & R CRACKED INTERCOSTAL BETWEEN BS 950D TO BS 950E,
- [SDR FOTR20006NR1795](https://openairdocs.org/sdr/FOTR20006NR1795), Feb 3, 2010: SKIN. CRACKED. LT OTBD FOREFLAP WBL 348 CRACK ON SKIN FWD OF FITTING. REPAIRED ON FASI W/O NR 20006,NR 01795 - INSTALLED REPAIR DOUBLER TO LT OTBD FOREFLAP AT WS 348 IAW SRM 5
- [SDR FOTR20006NR1794](https://openairdocs.org/sdr/FOTR20006NR1794), Feb 3, 2010: SKIN. CRACKED. RT OTBD FORE FLAP WBL 348 CRACK ON SKIN FWD OF FITTING. REPAIRED ON FASI W/O 20006, NR 01794. INSTALLED REPAIR DOUBLER TO RT OTBD FOREFLAP AT WS 348 IAW SRM 57-
- [SDR FOTR20006NR1778](https://openairdocs.org/sdr/FOTR20006NR1778), Feb 3, 2010: SKIN. DELAMINATED. RT OTBD AILERON T/E WEDGE PUNCTURED ON LOWER SURFACE. REPAIRED ON FASI W/O NR 20006, NR 01778 - INSTALLED HOT BONDED REPAIR DOUBLER TO RT OTBD AILERON TAB IAW S
- [SDR FOTR20006NR5683](https://openairdocs.org/sdr/FOTR20006NR5683), Feb 2, 2010: PANEL. DELAMINATED. NR 6 SPOILER PANEL LOWER SKIN DOUBLER BELOW ACTUATOR ATTACH FITTING IS DISBONDED. REPAIRED ON FASI WO 20006, N/R 05683. INSTALLED BONDED REPAIR TO NR 6 SPOILER 
- [SDR FOTR20006NR5666](https://openairdocs.org/sdr/FOTR20006NR5666), Feb 2, 2010: SKIN. DELAMINATED. LT INBD AILERON TAB HAS DELAMINATION LOWER SURFACE CENTER. REPAIRED ON FASI WO 20006, N/R 05666. INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB LOWER S
- [SDR FOTR20006NR5665](https://openairdocs.org/sdr/FOTR20006NR5665), Feb 2, 2010: SKIN. DELAMINATED. LT IB AILERON TAB LOWER SURFACE OTBD HAS DELAMINATION AREA-MARKED. REPAIRED ON FASI WO 20006. N/R 05665- INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB
- [SDR FOTR20006NR5664](https://openairdocs.org/sdr/FOTR20006NR5664), Feb 2, 2010: SKIN. DELAMINATED. LT INBD AILERON TAB LOWER SURFACE INBD HAS DELAMINATION. REPAIRED ON FASI WO 20006, N/R 05664. INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB LOWER SUR
- [SDR FOTR20006NR5661](https://openairdocs.org/sdr/FOTR20006NR5661), Feb 2, 2010: SKIN. CRACKED. FUSELAGE STA 1096 AT STRINGER 1 FIRST FAIRING FASTENER RT SKIN HAS CRACKS. REPAIRED ON FASI WO 20006, N/R 05661. REPAIRED FUSELAGE SKIN AT STA 1096, STR 1 IAW B
- [SDR FOTR20006NR5649](https://openairdocs.org/sdr/FOTR20006NR5649), Feb 2, 2010: STRINGER CLIP. GOUGED. STR TIE CLIP GOUGED STA 440 STR 4R. REPAIRED ON FASI WO 20006, N/R 05649. REMOVED AND REPLACED STRINGER TO FRAME CLIP AT STR 4R, STA 440 IAW BOEING DWG 65-45313
- [SDR FOTR20006NR5647](https://openairdocs.org/sdr/FOTR20006NR5647), Feb 2, 2010: STRINGER CLIP. CRACKED. STR TIE CLIP CRACK STA 460 STR 2R. REPAIRED ON FASI WO 20006 N/R 05647. REMOVED AND REPLACED STRINGER TO FRAME CLIP AT STR 2R, STA 460 IAW BOEING DWG 65-45313 R
- [SDR FOTR20006NR5633](https://openairdocs.org/sdr/FOTR20006NR5633), Feb 2, 2010: STRINGER CLIP. CRACKED. CABIN AREA STA 700, STRINGER 7L FRAME TO STRINGER BRACKET IS CRACKED. REPAIRED ON FASI WO 20006. N/R 05633- R & R STRINGER TO FRAME CLIP AT STR 7L, STA 700 IAW 
- [SDR FOTR20006NR5630](https://openairdocs.org/sdr/FOTR20006NR5630), Feb 2, 2010: STRINGER. CRACKED. CABIN AREA STA 720B FWD OF LIGHT HOUSING, STRINGER 15L IS CRACKED. REPAIRED ON FASI WO 20006. N/R 05630- REPAIRED STR 15L AT STA 720B IAW SRM 53-10-3 FIG 5 AND 
- [SDR FOTR20006NR5629](https://openairdocs.org/sdr/FOTR20006NR5629), Feb 2, 2010: STRINGER. CRACKED. CABIN AREA STA 720C AFT OF LIGHT HSG, STRINGER 15L IS CRACKED. REPAIRED ON FASI WO20006. N/R 05629- REPAIRED STR 15L AT STA 720C IAW SRM 53-10-3 FIG 5 AND 51-30
- [SDR FOTR20006NR5443](https://openairdocs.org/sdr/FOTR20006NR5443), Feb 1, 2010: FRAME. PUNCTURED. AFT PIT FRAME PUNCTURED STR 27L BS 1130. REPAIRED ON FASI WO 20006, N/R 05443. REPAIRED AFT CARGO COMPARTMENT FRAME AT STR 27L, STA 1130 IAW B727 SRM 53-10-2 FI
- [SDR FOTR20006NR5442](https://openairdocs.org/sdr/FOTR20006NR5442), Feb 1, 2010: SHEAR TIE. CORRODED. AFT PIT FRAME SHEAR TIE HAS SURFACE CORROSION BETWEEN STR 30 AND 28R. REPAIRED ON FASI WO 20006, N/R 05442. REMOVED AND REPLACED AFT CARGO COMPARTMENT FRAME SHE
- [SDR FOTR20006NR5604](https://openairdocs.org/sdr/FOTR20006NR5604), Feb 1, 2010: FRAME. DENTED. FWD CARGO COPT FRAME 720A HAS 2 DENTS IN THE UPPER FLANGE BETWEEN STR 24L-25L. REPAIRED ON FASI WO20006. N/R 05604- REPAIRED FRAME AT STA 720A BETWEEN STR 24L A
- [SDR FOTR20006NR5600](https://openairdocs.org/sdr/FOTR20006NR5600), Feb 1, 2010: FRAME. DENTED. FWD CARGO COMPT FRAME BS 680 UPPER FLANGE IS DENTED AND WEB IS BENT BETWEEN STR 23L-24L. REPAIRED ON FASI WO20006. N/R 05600- REPAIRED FRAME AT STA 680 BETWEEN 
- [SDR FOTR20006NR5599](https://openairdocs.org/sdr/FOTR20006NR5599), Feb 1, 2010: FRAME. DENTED. FWD CARGO COMPT FRAME BS 680 HAS 4 DENTS IN THE UPPER FLANGE BETWEEN STR 23R-25R, WEB IS BENT. REPAIRED ON FASI WO20006, N/R 05599. REPAIRED FRAME AT STA 680 BE

All 198: https://openairdocs.org/deregistered/N286SC-2018-01-03/reports.md

## 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 20010406012429I](https://openairdocs.org/incident/20010406012429I), Apr 6, 2001: Boeing 7272A1 (N286SC), Toledo, OH. (-23)Crew declared emergency during taxi for takeoff due to smoke in the cockpit. Aircraft taxied back to ramp without incident. Maintenance found the smoke…

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