N1361G1980 Cessna 402C
This N-number isn't registered right now. Below is its last known registration, canceled May 22, 2020.
Safety record in brief:No NTSB accidents or incidents since 19829 ADs may apply20 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 19, 2026- Last registered owner
- Hyannis Air Service INC
- Owner type
- Corporation
- City, state
- Hyannis, MA
- Certificate issued
- Jan 5, 1996
- Canceled
- May 22, 2020
- Airworthiness
- Standard · Normal
- Airworthiness date
- Mar 12, 1980
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
- 402C0270
- 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
- A093FD
Engine
- Make and model
- Cont Motor Tsio-520 Ser
- Type
- Reciprocating
- Power
- 300 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 1996 – 2020Hyannis Air Service INCHyannis, MA
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (9)
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. |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (TSIO-520 SER)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
Show all 9 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 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. |
| 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 (20)
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.
- Wings · spar cap · corrodedJun 1, 2018
CORROSION WAS DISCOVERED ON THE LT AFT LOWER OUTBOARD SPAR CAP WS 221.71 ON THE FORWARD SIDE OF THE CAP, INSIDE THE FUEL TANK, NEAR THE RADIUS. THE CORRODED AREA MEASURED .075 TALL, .243 IN WIDTH, AND .063 IN DEPTH. OUT OF LIMITS IAW MEB 95-11, R1, SECTION 3, THE SPAR CAP WAS REPLACED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · fitting · corrodedNov 2, 2017
DURING A ROUTINE VISUAL INSPECTION OF THE WING ATTACH FITTINGS, CORROSION WAS DISCOVERED ON THE LEFT OUTBOARD FORWARD, AFT SIDE WING ATTACH FITTING. THE FITTING WAS REMOVED AND REPLACED WITH FACTORY NEW PARTS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · exhaust valve · damagedNov 7, 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 · damagedJul 4, 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. - Nacelles and pylons · beam · crackedMar 21, 2015
THE LT NACELLE INBD ENG BEAM WAS FOUND TO BE CRACKED JUST FWD OF AFT ENG MOUNT, TRANSVERSE TO LENGTH OF BEAM, ACROSS UPPER FACE OF BEAM, DURING NDT PRESCRIBED WITHIN MEL-54-01. REMOVE BEAM ASSEMBLY FROM NACELLE, PERFORM DETAILED VISUAL INSPECTION OF SURROUNDING STRUCTURE & INSTALL NEW BEAM…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Nacelles and pylons · beam · crackedMar 21, 2015
THE LT NACELLE OTBD ENG BEAM WAS FOUND TO BE CRACKED JUST FWD OF AFT ENG MOUNT, TRANSVERSE TO LENGTH OF BEAM, ACROSS UPPER FACE OF BEAM, DURING NDT PRESCRIBED WITHIN MEL-54-01. REMOVE BEAM ASSEMBLY FROM NACELLE, PERFORM DETAILED VISUAL INSPECTION OF SURROUNDING STRUCTURE & INSTALL NEW BEAM…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · door · unsecureDec 16, 2014
RIGHT SIDE EMER DOOR OPENED AT 1000 FT AFTER DEPARTURE. INSPECTED THE EMER EXIT DOOR SYS, SECURED THE EMER EXIT DOOR, SEALED & SEATED PROPERLY IN THE DOOR FRAME. NO FURTHER DEFECTS FOUND.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · bolt · failedMay 27, 2013
CREW REPORTED LOSING RT ENGINE MAP AT 9000 FEET AND NOTICED OIL LEAKING FROM RT ENGINE COWL. THE RT PROP WAS FEATHERED AND RT ENGINE SHUTDOWN AND THE ACFT RETURNED TO DEPARTURE AIRFIELD. MX INSPECTED AND FOUND THE CRANKSHAFT GEAR WAS SEPARATED FROM THE CRANKSHAFT. A REPLACEMENT ENGINE WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · drag brace · crackedDec 19, 2012
AT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMENT DRAG BRACE HAS BEEN INSTALLED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Nacelles and pylons · beam · crackedDec 1, 2012
DURING A SCHEDULED MX EVENT, THE RT ENGINE ASSY WAS REMOVED FOR A SCHEDULED TIME CHANGE. UPON REMOVAL, A CRACK WAS DISCOVERED AT THE RT NACELLE CROSSOVER BEAM IN THE AREA OF TURBOCHARGER BRACKET HOLE LOCATIONS. LOCATION OF CRACK RELATIVE TO RT NACELLE CROSSOVER BEAM 5654104-12. C/A WILL BE TO…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 20 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026