- Registered owner
- A2g International LLC
- Location
- San Juan Capo, CA
- Owner type
- LLC
- Serial number
- 33701844
- Year built
- 1978
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- March 14, 1978
- Certificate issued
- November 4, 2022
- Expires
- November 30, 2029
- Mode S code
- AD1FCC
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 30
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1977 | 1 |
|---|---|
| 1978 | 2 |
| 1981 | 2 |
| 1988 | 2 |
| 1990 | 1 |
| 1991 | 1 |
| 1993 | 2 |
| 1995 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 2000 | 2 |
| 2002 | 1 |
| 2005 | 1 |
| 2009 | 1 |
| 2010 | 3 |
| 2011 | 2 |
| 2012 | 2 |
| 2022 | 1 |
| 2023 | 5 |
See all 37 ADs
Information bulletins that may apply · 11
Advisory, not mandatory.
Airframe · Cessna T337H
SAIB AIR-21-16FLIGHT COMPARTMENT EQUIPMENT, Cessna Seat Back Attachment Bolt InspectionSAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-12-41Flight Controls Loose Glide ScrewSAIB CE-12-14Three Alternative Methods of Compliance for AD 2011-10-09SAIB CE-10-40R1Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanesSAIB CE-09-10Availability of Secondary Seat Stops for Pilot and Copilot SeatsEngine · Continental TSIO-360-H
SAIB NE-16-13Powerplant - Prohibited use of sealantSAIB NE-13-15Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control LeversSAIB NE-13-04Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing InspectionSAIB NE-10-09Reciprocating Engine Power Section: Hydraulic Valve LiftersSAIB NE-09-04Fuel Control/Reciprocating EnginesNTSB investigations
No NTSB investigations matched to N945ASMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna T337H aircraft
FAA incident reports
No FAA accident or incident reports matched to N945ASMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna T337H aircraft
Service difficulty reports
No reports matched to N945ASGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Cessna T337H aircraft
Reports on N945AS not matched to an aircraft · 34
They name N945AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR WX0600001Unknown · unknownPIA - LAS - CREW REPORTED ON TAKEOFF ROLL AT 100 KNOTS, THE PACKS SHUT DOWN AND THE RIGHT EPR GAUGE WENT TO 1.0. TAKEOFF ABORTED AND AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE RAN AIRCRAFT AT TAKEOFF POWER. EPR SYSTEM OPERATIONALLY CHECKED NORMSDR ASMF200508006Computer · failedAIRCRAFT RETURNED OF FLIGHT, BOTH DFGC OUT OF SERVICE. THE DFGC RTC BITE WERE PERFORMED IAW MM 22-01-05, TESTED CORRECT. THE OVERWEIGHT LANDING CHECK WAS PERFORMED IAW MM 05-51-04, ALL CORRECT. DURING OVERNIGHT CHECK, BOTH DFGC TESTS WERE PERFORMED IAW MM 22-0SDR ASMF200506002Anti-Ice Valve · failedAIRCRAFT RETURNED TO PLATFORM, LT STARTER VALVE DID NOT OPEN AND ANTI-ICE BREAKER OF NOSE COWLING POPPED OUT. THE REPORT WAS DEFERRED BY MEL 80-2 AND THE ANTI ICE VALVE WAS REPLACED IAW MM 30-20-01, TESTED CORRECT. DEFERRED REPORT WAS CLOSED.
See all 34 unmatched reportsSTCs that may be installed · 211
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna T337H
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller