Aircraft Description
N115CD is a 2007 Cirrus Design Corp SR22, a single-engine reciprocating (piston) aircraft registered to High Flying Investments LLC in Texarkana, AR. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on December 13, 2007. The registration certificate was issued on June 28, 2017. The registration is set to expire on June 30, 2027. Powered by a Cont Motor IO-550-N engine producing 310 horsepower, N115CD is. The aircraft's Mode S transponder code is A03EFC (hex), used for ADS-B identification and flight tracking. N115CD was last tracked by AviatorDB at coordinates 34.2204, -94.3126 on March 2, 2026. The FAA registry record for N115CD was last updated on January 22, 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 N115CD. 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 23, 1999 | CHI99FA112 | Destroyed | Fatal | the lack of sufficient aileron-to-wing gap clearance design. Contributing factors were the inadequate oversight of the Federal Aviation Administration of the design and manufacturing and flight test process of Cirrus Design Corporation, the location of the control yoke, the inadequate surveillance of the test flight and the test flight procedures by the Cirrus Design Corporation. The destabilizing crosswind condition that existed on the landing runway was an additional factor. |
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