N414X1962 Cessna 310G
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply1 service difficulty report
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Individual owner
- City, state
- Caldwell, ID
- Certificate issued
- Jun 23, 2011
- Expires
- Jun 30, 2027
- Airworthiness
- Standard
- Airworthiness date
- Apr 19, 1962
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
- 310G
- Year
- 1962
- Serial number
- 310G0091
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 6
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A4E509
Engine
- Make and model
- Cont Motor I0-470 Series
- Type
- Reciprocating
- Power
- 260 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 – nowIndividual ownerCaldwell, ID · 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 (1)
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 |
|---|---|---|---|
| 2016-17-08 | Elevator Tab Control System | Sep 12, 2016 | Airframe (310G) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
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.
- Fuselage · attach angle · damagedApr 1, 2005
AT ANNUAL INSPECTION, FOUND 3 RIVETS AND 1 BOLT SHEARED AT RT FWD MLG TRUNNION ATTACH ANGLE. RIVETS WERE UPPER 2 ROWS OF 4 ROWS. REMAINING RIVETS SHOWED SIGNS OF (SMILE) FROM INSTALLATION. SHEARED BOLT WAS IN UPPER FWD POSITION OF FWD ANGLE. SHEARED FASTENERS WERE VISIBLE THROUGH INSPECTION PANEL…
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