Aircraft Description
N644SR is a 2006 Cirrus Design Corp SR22, a single-engine reciprocating (piston) aircraft registered to Bas Part Sales LLC in Greeley, CO. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on August 2, 2006. Powered by a Cont Motor IO-550-N engine producing 310 horsepower, N644SR is. The aircraft's Mode S transponder code is A875B7 (hex), used for ADS-B identification and flight tracking. The FAA registry record for N644SR was last updated on January 14, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Cirrus SR22, the world's best-selling general aviation aircraft since 2002, revolutionized single-engine aviation with its innovative safety systems and modern design. First delivered in 2001, it is a low-wing single-engine aircraft powered by a 310-horsepower Continental piston engine, seating four passengers plus pilot. With a 38.3-foot wingspan and composite construction, the SR22 introduced the first FAA-certified ballistic parachute system as standard equipment. Nearly 8,000 examples have been manufactured by Cirrus Aircraft Corporation. AviatorDB tracks 9,011 Cirrus Design Corp aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is SR22.
AviatorDB has found no NTSB accident or incident reports involving N644SR. 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 (1)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Mar 28, 2021 | WPR21LA145 | Substantial | None | A total loss of engine power resulting from a catastrophic engine failure caused by a shift of the No. 2 main bearing and bearing seal, which resulted in oil starvation to the crankshaft; the reason for the bearing and bearing seal shift could not be determined due to the extent of the engine damage. Contributing to the accident was the failure of the airframe parachute system to deploy due to undetermined inconsistencies within ignition material in the rocket igniter assembly/squib. |
Additional Details
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC