N6632J1980 Beechcraft 76
Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply3 service difficulty reports
Registration
FAA Aircraft Registry · Oct 19, 2026- Registered owner
- So Cal Leasing LLC
- Owner type
- LLC
- City, state
- El Cajon, CA
- Certificate issued
- May 5, 2007
- Expires
- Sep 30, 2027
- Airworthiness
- Standard · Normal
- Airworthiness date
- Mar 10, 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
- Beechcraft
- Model
- 76
- Year
- 1980
- Serial number
- ME-337
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 4
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A8C205
Engine
- Make and model
- Lycoming O-360-A1g6d
- Type
- Reciprocating
- Power
- 180 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2007 – nowSo Cal Leasing LLCEl Cajon, CA · current
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 (5)
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 |
|---|---|---|---|
| 2021-08-06 | Textron Aviation Inc. Airplanes | May 25, 2021 | Airframe (76)Certain serial numbers: 76 ME-1–ME-437. Only with: Excludes airplanes with MLG "A" frame assemblies P/N 105-810023-0083 (left) and P/N 105-810023-0084 (right) installed. |
| 2006-10-21 | Engine Components Incorporated (ECi) Reciprocating Engine Connecting Rods | Jun 22, 2006 | Engine (O-360-A1G6D)Only with: ECi connecting rods P/N AEL11750 (forging P/N AEL11488) installed, rod serial numbers 54/6 and below, produced between January 2002 and January 2004. |
| 2006-06-16 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, and… | Apr 27, 2006 | Engine (O-360-A1G6D)Only with: Engines manufactured new or rebuilt, overhauled, or that had a crankshaft installed after March 1, 1999. |
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (O-360-A1G6D)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999. |
| 99-05-13 | Raytheon Aircraft Company 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55… | Apr 19, 1999 | Airframe (76)Certain serial numbers: F33A CE-290–CE-1791; E33C CJ-26–CJ-179; F33C CJ-26–CJ-179; A36 E-185–E-3046; B36TC EA-242–EA-591; 58 TH-1–TH-1798 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (3)
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 · a frame · crackedFeb 3, 1997
WHEN INSTALLING LANDING GEAR 'A' FRAMES PER AD 91-14-14 AND SB 2361 REV 3, THE RIGHT AND LEFT 'A' FRAMES WERE REMOVED FROM THE AIRCRAFT FOR FURTHER INSPECTION. A MAGNAFLUX INSPECTION OF THESE PARTS WAS PERFORMED AND THE 'A' FRAMES WERE FOUND CRACKED. THE MAGNAFLUX INSPECTION IS NOT CALLED OUT FOR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · a frame · crackedFeb 3, 1997
WHEN INSTALLING LANDING GEAR 'A' FRAMES PER AD 91-14-14 AND SB 2361 REV 3, THE RIGHT AND LEFT 'A' FRAMES WERE REMOVED FROM THE AIRCRAFT FOR FURTHER INSPECTION. A MAGNAFLUX INSPECTION OF THESE PARTS WAS PERFORMED AND THE 'A' FRAMES WERE FOUND CRACKED. THE MAGNAFLUX INSPECTION IS NOT CALLED OUT FOR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · actuator tube · disconnectedFeb 29, 1996
PILOT REPORTED FLAPS WOULD NOT EXTEND IN-FLIGHT. EXAMINED FLAP SYSTEM AND FOUND TUBE ACTUATOR DISCONNECTED FROM ACTUATOR ASSEMBLY. RECONNECTED TUBE AND FUNCTIONAL CHECK OF FLAPS SATISFACTORY. SUBMITTER SUGGESTS A METHOD BE DEVELOPED BY BEECH TO SAFETY TUBE ACTUATOR TO ACTUATOR ASSEMBLY.
From FAA Service Difficulty Reports; matched by N-number and serial number.
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