N10551980 Cessna 402C
This N-number isn't registered right now. Below is its last known registration, canceled Jun 27, 2024.
Safety record in brief:No NTSB accidents or incidents since 19828 ADs may apply12 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Individual owner
- City, state
- West Barn Starle, MA
- Canceled
- Jun 27, 2024
- Airworthiness
- Standard · Normal
- Airworthiness date
- Nov 4, 2010
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Cessna
- Model
- 402C
- Year
- 1980
- Serial number
- 402C0249
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 10
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A01A4E
Engine
- Make and model
- Ama/Expr Unknown Eng
- Type
- Reciprocating
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- until 2024Individual ownerWest Barn Starle, MA
- until 1976Individual ownerOklahoma City, OK · different airframe: Piel Emeraude Cp-301 S/N 101718
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (8)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2017-10-09 | Textron Aviation Inc. Airplanes | Jun 7, 2017 | Airframe (402C)Certain serial numbers: 402C 402C0001–402C1020; 414A 414A0001–414A1212. Only with: Equipped with Cessna Multi-Engine Service Kit SK402-47 (Original Issue, Rev A, or Rev B) or nacelle fittings P/Ns 5292029-9, -10, -11, -12, -21, -22, -23, or -24. |
| 2016-17-08 | Elevator Tab Control System | Sep 12, 2016 | Airframe (402C) |
| 2015-07-03 | Nacelles/Pylons | Apr 24, 2015 | Airframe (402C)Certain serial numbers: 402C 402C0001–402C1020; 414A 414A0001–414A1212 |
| 2012-23-01 | Wings | Dec 26, 2012 | Airframe (402C)Only with: Model 402C modified by STC SA927NW; Model 414A modified by STC SA892NW. |
| 2005-20-25 | The Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411… | Nov 9, 2005 | Airframe (402C)Certain serial numbers: 401 655; 401 401-0001–401-0322; 401A 655; 401A 401A0001–401A0132; 401B 401B0001–401B0221; 402 402-0001–402-0322; …. Only with: Equipped with an avionics bus circuit breaker switch P/N CM3589-50, 593-250-101, 593-250-102, W31-X2M5A-50, or W31-X1000-50. |
Show all 8 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2005-12-13 | Cessna Aircraft Company Models 402C and 414A Airplanes | Jun 22, 2005 | Airframe (402C) |
| 2000-01-16 | Cessna Aircraft Company 300 and 400 Series Airplanes | Feb 15, 2000 | Airframe (402C) |
| 98-04-28 | Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414… | Mar 13, 1998 | Airframe (402C) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (12)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Landing gear · axle · brokenNov 3, 2022
RIGHT MAIN GEAR AXLE FAILED ON LANDING/TAXI TO GATE. MAINTENANCE IS REPLACING LOWER BARREL & AXLE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · exhaust valve · damagedOct 30, 2016
CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · exhaust valve · damagedOct 10, 2016
CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Reciprocating engine · exhaust valve · damagedSep 17, 2016
CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · exhaust valve · damagedAug 8, 2016
CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · engine · damagedSep 16, 2015
RIGHT ENG OIL PRESS DROPPED TO ZERO IN FLIGHT. DIVERTED & ON SHORT FINAL APPROACH RT ENG STOPPED RUNNING. PROPELLER DID NOT FEATHER. POST LANDING INSPECTION REVEALED OIL LEAKING FROM TOP & BOTTOM OF ENG COWLING. PRELIMINARY EXAMINATION REVEALS TOP OF CRANKCASE BREACHED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · engine · failedAug 14, 2015
PILOT REPORTED RT ENG FAILED INFLIGHT. R & R THE ENG, OPERATIONAL & LEAK CHECKED GOOD. ENG HAS BEEN SENT FOR TEAR DOWN ANALYSIS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · caliper · misinstalledDec 27, 2014
RIGHT MAIN TIRE & GEAR BRAKE CALIPER HAS COME LOOSE & MOVED TO JAM UP ON STRUT. R & R THE RT BRAKE CALIPER, PAD SET & TIRE ASSEMBLY IAW MM CH 32-10-00 WITH NO DEFECTS NOTED. FURTHER INVESTIGATION LEAD TO THE DISCOVERY THAT THE RT MAIN TIRE HAD BEEN CHANGED PREVIOUSLY & THE BRAKE CALIPER WAS NOT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · spar · damagedApr 12, 2013
DURING A SCHEDULED MX EVENT, DAMAGE WAS NOTED TO THE FORWARD CARRY THROUGH SPAR ASSY IN THE CENTER SECTION. DAMAGE INCLUDES DRILL STARTS TO UPPER CAP AND CORRESPONDING WEB FLANGE CRACKS. THESE DAMAGE POINTS WERE MAPPED AND SUBMITTED FOR ENGINEERING ASSISTANCE. REPAIRS WILL BE CONDUCTED IAW REPAIR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · spar · damagedApr 12, 2013
DURING A SCHEDULED MX EVENT, DAMAGE WAS NOTED TO THE AFT CARRY THROUGH SPAR ASSY CENTER SECTION. DAMAGE INCLUDES WEB FLANGE CRACKS. OPEN
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 12 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026