Aircraft Description
N25HW is a 2006 Cirrus Design Corp SR22, a single-engine reciprocating (piston) aircraft registered to Skimait Cirrus LLC in Kalispell, MT. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on June 22, 2006. The registration certificate was issued on November 22, 2025. The registration is set to expire on November 30, 2032. Powered by a Cont Motor IO-550-N engine producing 310 horsepower, N25HW is. The aircraft's Mode S transponder code is A255E9 (hex), used for ADS-B identification and flight tracking. N25HW was last tracked by AviatorDB at coordinates 47.7791, -116.8075 on March 3, 2026. The FAA registry record for N25HW was last updated on November 22, 2025. 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 N25HW. 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 |
|---|---|---|---|---|
| Oct 23, 2022 | CEN23LA017 | Substantial | None | The pilot’s loss of control after encountering windshear while landing in a strong, gusting crosswind. Contributing was pilot’s decision to continue the landing with a 90-degree crosswind at 30 knots. |
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