- Registered owner
- Marc Inc
- Location
- Bolton, MS
- Owner type
- Corporation
- Serial number
- 310P0200
- Year built
- 1969
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- August 2, 1969
- Certificate issued
- September 1, 2016
- Expires
- September 30, 2029
- Mode S code
- A0317E
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 36
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1975 | 1 |
|---|---|
| 1979 | 1 |
| 1981 | 1 |
| 1983 | 1 |
| 1986 | 1 |
| 1987 | 1 |
| 1988 | 2 |
| 1989 | 1 |
| 1991 | 1 |
| 1993 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 2 |
| 2004 | 1 |
| 2005 | 3 |
| 2007 | 1 |
| 2010 | 1 |
| 2012 | 1 |
| 2016 | 3 |
| 2020 | 1 |
| 2022 | 2 |
| 2023 | 5 |
See all 43 ADs
Information bulletins that may apply · 9
Advisory, not mandatory.
Airframe · Cessna T-310P
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-09-16Landing Gear: Main Landing Gear Torque TubeSAIB ACE-99-06Engine · Continental GTSIO-520-C
SAIB NE-18-16POWERPLANT Alternator Drive CouplingSAIB 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-09-08Reciprocating Engine Cylinder SectionNTSB investigations
No NTSB investigations matched to N111SDMatched 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 T-310P aircraft
FAA incident reports
No FAA accident or incident reports matched to N111SDMatched 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 T-310P aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2022FA0000457Cylinder · leakingOVERHAULED RH ENGINE WAS INSTALLED ON THE AIRCRAFT. AFTER TEST FLIGHT, AN OIL LEAK WAS NOTED FROM THE #6 CYLINDER BASE. THE CRS THAT OVERHAULED THE ENGINE INSTRUCTED US TO REMOVE THE #6 CYLINDER TO CHECK FOR ISSUES. DURING THE REMOVAL OF THE CYLINDER, IT WASSDR 2022FA0000455Crankshaft · brokenDURING CLIMB AFTER TAKEOFF FROM KZPH, AROUND 5000 FT, THE RH ENGINE BEGAN RUNNING ROUGH, THE RH MAGNETO WAS TURNED OFF IN AN ATTEMPT TO DIAGNOSE THE ROUGHNESS. THE ENGINE RAN EVEN MORE ROUGHLY WITH THE RH MAGNETO OFF, THE RH MAGNETO WAS TURNED BACK ON, AND AP
STCs that may be installed · 305
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna T-310P
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