- Registered owners
- Elliott Frank FElliott Cecilia R
- Location
- Mojave, CA
- Owner type
- Partnership
- Serial number
- T210-0436
- Year built
- 1969
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- May 1, 1969
- Certificate issued
- April 16, 2011
- Expires
- April 30, 2027
- Mode S code
- A18E36
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 60
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1969 | 1 |
|---|---|
| 1974 | 1 |
| 1975 | 1 |
| 1977 | 1 |
| 1978 | 1 |
| 1979 | 5 |
| 1980 | 1 |
| 1981 | 1 |
| 1984 | 1 |
| 1985 | 3 |
| 1986 | 2 |
| 1987 | 2 |
| 1988 | 5 |
| 1990 | 1 |
| 1991 | 1 |
| 1993 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 2 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 3 |
| 2016 | 1 |
| 2020 | 2 |
| 2022 | 2 |
| 2023 | 5 |
| 2024 | 1 |
See all 67 ADs
Information bulletins that may apply · 14
Advisory, not mandatory.
Airframe · Cessna T210J
SAIB AIR-20-10AD 2020-03-16 Alternative Methods of Compliance and FAQSAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-17-16Main Landing Gear Actuator InspectionSAIB 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 SeatsSAIB CE-05-27R1StabilizersEngine · 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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB DEN04CA096Accident · Minor injuriesData collectionFinal reportCheyenne, WYthe detachment of the nut and bolt that attaches the throttle control cable to the fuel induction due to improper maintenance. Contributing factors were the fiber optics wire, fence, and ditch, and the unavailability of suitable terrain on which to make a…NTSB DEN90LA078Accident · Minor injuriesLimited investigationFinal reportEnglewood, COThe pilot's loss of directional control during an aborted takeoff.
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20040703012549AFinal Approach · Cheyenne, WY(-23) While making an approach to the airport for landing, the pilot added power with no engine response. The throttle cable disconnected from the engine control arm due to the throttle attaching bolt missing along with the washer, nut and cotter pin.…Accident 19900325005259ATo Aborted (Fixed Wing) · Denver, COUnable to rotate for liftoff, aborted late. Ran off end runway into culvert. Had near full down trim.Incident 19790823023219IStarting Engines · North Platte, NEPilot set brakes started engine and rolled into parked aircraft.
Service difficulty reports · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
STCs that may be installed · 334
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna T210J
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA2598NMInstallation of an air to air intercooler in the engine induction system downstream of the turbocharger. (See specific serial numbers) H S/N T210-308 THRU T210-0392)STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.