N810BW1980 Cessna 402C
Safety record in brief:No NTSB accidents or incidents since 19829 ADs may apply7 service difficulty reports
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Hyannis Air Service INC
- Owner type
- Corporation
- City, state
- Hyannis, MA
- Certificate issued
- Jul 25, 2011
- Expires
- Jul 31, 2027
- Airworthiness
- Standard · Normal
- Airworthiness date
- Apr 1, 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
- 402C0279
- 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
- AB098A
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- 2011 – nowHyannis Air Service INCHyannis, MA · current
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 (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 (7)
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.
- Nacelles and pylons · beam · crackedAug 4, 2026
DURING SCHEDULED INSPECTION A CRACK WAS VISUALLY IDENTIFIED ON THE LEFT HAND CROSSOVER BEAM (OEM: 5654104-11) FORWARD FACE. THIS CRACK MEASURES APPROXIMATELY 1.375 INCHES LONG AND IS CONSISTENT WITH OTHER CRACKS VISUALLY IDENTIFIED ON THESE BEAMS IN THE PAST. THIS BEAM HAS BEEN CHANGED USING NEW…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · spar cap · corrodedSep 11, 2020
DURING MAINTENANCE CORROSION DAMAGE WAS IDENTIFIED ON BOTTOM FACE OF THE HORIZONTAL LEG OF THE LEFT HAND LOWER OUTBOARD SPAR CAP (P/N: 5122041-23). THIS DAMAGE IS LOCATED BETWEEN LWS 203.21 AND 212.46. AT IT'S DEEPEST THIS DAMAGE MEASURES .027 INCHES DEEP. THIS MEASUREMENT EXCEEDS THE MAXIMUM…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Nacelles and pylons · fitting · crackedMay 19, 2017
DURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED ON THE LT OUTBOARD FITTING. THE CRACK AS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .102 IN LENGTH.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reportsShow fewer reports
- Starting · relay · failedJul 27, 2015
PILOT REPORTED LEFT ENGINE STARTER LIGHT ILLUMINATED. THE FLIGHT DIVERTED FROM ITS ORIGINAL DESTINATION. INSPECTED & FOUND LEFT STARTER RELAY INTERMITTENT. R & R LEFT STARTER RELAY, THE STARTER REMAINED INOPERATIVE. R & R THE LEFT ENGINE STARTER & OPERATIONALLY CHECKED WITH NO FURTHER DEFECTS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · unknown · odorJan 15, 2015
INTERMITTENT SMELL OF ELEC OR PLASTIC CHEMICAL BURNING COMING FROM THE SWITCH BREAKER PANEL. INSPECTED PILOT SWITCH & BREAKER AREA. NO DEFECTS NOTED AT THIS TIME. R & R AVIONICS MASTER SWITCH IAW MM CHAPTER 39-40-00. OPERATIONS CHECKED GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · fitting · corrodedOct 17, 2012
DURING NEW ACFT CONFORMITY INSPECTION, IT WAS NOTED THAT THE LT UPPER FORWARD FUSELAGE FITTING WAS CORRODED. THE DETERMINED CORRECTIVE ACTION WAS TO REMOVE AND REPLACE WITH NEW PART. REPAIRS ARE ONGOING.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · drag brace · crackedApr 20, 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…
From FAA Service Difficulty Reports; matched by N-number and serial number.
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