Aircraft Description
N468CM is a 2000 Cessna 172R, a single-engine reciprocating (piston) aircraft registered to University of Central Missouri in Warrensburg, MO. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on February 15, 2000. The registration certificate was issued on May 18, 2000. The registration is set to expire on July 31, 2027. Powered by a Lycoming I0360 SER engine producing 180 horsepower, N468CM is. The aircraft's Mode S transponder code is A5B791 (hex), used for ADS-B identification and flight tracking. N468CM was last tracked by AviatorDB at coordinates 39.2321, -94.0058 on March 21, 2026. The FAA registry record for N468CM was last updated on March 4, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Cessna 172RG Cutlass RG served as general aviation's affordable solution for complex aircraft training, bridging the gap between basic flight instruction and commercial pilot requirements. First flown before its 1980 introduction, it was a high-wing single-engine monoplane that could seat up to four occupants with retractable landing gear and a constant-speed propeller. With a cruise speed of 140 knots and a range of 710 nautical miles, the aircraft was manufactured by Cessna Aircraft Company. AviatorDB tracks 80,556 Cessna aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is C72R.
AviatorDB has found no NTSB accident or incident reports involving N468CM. AviatorDB cross-references all FAA registration data with NTSB accident and incident reports, providing a comprehensive safety overview for every registered aircraft in the United States.
Registered Owner
Powerplant & Avionics
NTSB Accident History (2)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Jul 1, 2014 | CEN14LA333 | Substantial | None | The partial loss of engine power for reasons that could not be determined because an operational test run of the engine did not reveal any anomalies that would have precluded normal operation. |
| Nov 20, 1988 | NYC89LA034 | Destroyed | Serious | COLLISION WITH TREES AND TERRAIN DUE TO THE PILOT EXCEEDING APPROACH MINIMUM ALTITUDE DURING AN ILS APPROACH. |
The partial loss of engine power for reasons that could not be determined because an operational test run of the engine did not reveal any anomalies that would have precluded normal operation.
COLLISION WITH TREES AND TERRAIN DUE TO THE PILOT EXCEEDING APPROACH MINIMUM ALTITUDE DURING AN ILS APPROACH.
Additional Details
Last Known Position
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC