- Registered owner
- A2g International LLC
- Location
- San Juan Capo, CA
- Owner type
- LLC
- Serial number
- 33701851
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- March 20, 1978
- Certificate issued
- November 4, 2022
- Expires
- November 30, 2029
- Mode S code
- AD2383
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 13
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 |
| 1988 | 1 |
| 1990 | 1 |
| 1997 | 1 |
| 2000 | 1 |
| 2005 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 1 |
| 2022 | 1 |
| 2023 | 2 |
Airframe · Cessna T337H
AD 2023-09-09Exhaust Turbine System (Recip)AD 2023-10-02Indicating/Recording System, NavigationAD 2022-03-15Fuel Quantity IndicatorAD 2011-10-09Seat Rails and Roller Housing InspectionsAD 2010-21-18WingsAD 2008-26-10Alternate static air source selector valveAD 2005-01-19Mode S transpondersAD 2000-06-01Fuel Strainer AssemblyAD 97-01-13Fuel, Oil and Hydraulic HosesAD 79-10-14 R1Fuel Tank VentingAD 78-20-12Aircraft TiresAD 78-09-05Wing Spar Caps and Web DoublersAD 77-08-05Single Engine TakeoffsSuperseded and historical ADs · 1
Information bulletins that may apply · 6
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 SeatsNTSB investigations
No NTSB investigations matched to N946ASMatched 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 N946ASMatched 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 N946ASGeneral 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 N946AS not matched to an aircraft · 21
They name N946AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR ASMF200503006Skin · damagedDURING TRANSIT CHECK WAS DETECTED HIT IN LT AILERON. DURING REVISION WAS DETECTED DAMAGED THE AILERON FITTING PN 44938931-507. THE LT AILERON WAS REPLACED AND TESTED IAW MM 27-10-0 AND MM 27-10-00. TEST FLIGHT WAS PERFORMED IAW GMM CHAPTER 4-10-6, NOTE 2 AND SDR ASMF200407010Engine · failedAIRCRAFT RETURNED, RT ENGINE FAILED. CAPTAIN REPORTED DURING TAKE OFF AT 111 KNOTS, RT ENGINE EXPERIMENTED AN EXPLOSION WITH DROPPED OF PARAMETERS AND LOW FUEL FLOW, REACHED 770 DEGREES (F). DURING MAINTENANCE REVISION, RT ENGINE WAS DETECTED WITH FAN JAMMEDSDR ASMF200407003Engine · overtempCAPTAIN REPORTED THAT DURING TAKE OFF AT HMO, LT ENGINE EGT INDICATION REACHED 610 DEGREES (C) DURING 40 SECONDS AND DURING CLIMB (TAIL COMP HIGH) LIGHT TURNED ON. HIGH TEMPERATURE PROCEDURE WAS PERFORMED IAW MM 72-00-00 AND (TAIL COMP HIGH) LIGHT TURNED OFF.
See all 21 unmatched reportsSTCs that may be installed · 188
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