Aircraft Description
N470ZW is a 2004 Bombardier INC CL-600-2B19, a twin-engine turbo-fan aircraft registered to Csi Aviation INC in Killeen, TX. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on May 3, 2004. The registration certificate was issued on March 1, 2026. The registration is set to expire on March 31, 2033. Powered by a Ge CF34 SERIES engine producing 9140 pounds of thrust, N470ZW is. The aircraft's Mode S transponder code is A5C36E (hex), used for ADS-B identification and flight tracking. N470ZW was last tracked by AviatorDB at coordinates 44.2585, -88.5190 on April 4, 2025. The FAA registry record for N470ZW was last updated on March 1, 2026. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Learjet 60, a high-performance mid-size business jet that marked Bombardier's successful revival of the struggling Learjet marque, first flew on October 10, 1990. A low-wing twin-turbofan aircraft seating 6-8 passengers, it featured a fuselage stretched 43 inches over its predecessor and delivered class-leading climb performance to 41,000 feet in 18.5 minutes at maximum weight. Spanning 264.5 square feet of wing area with a maximum takeoff weight of 23,500 pounds, the aircraft was manufactured by Learjet Inc. under Bombardier Aerospace in Wichita, Kansas. AviatorDB tracks 2,968 Bombardier INC aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is LJ60.
AviatorDB has found no NTSB accident or incident reports involving N470ZW. 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
Operator / Airline
Powerplant & Avionics
NTSB Accident History (1)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Dec 16, 2007 | DCA08FA018 | Substantial | None | the captain’s attempt to salvage the landing from an instrument approach which exceeded stabilized approach criteria, resulting in a high sink rate, likely stall, and hard landing which exceeded the structural limitations of the airplane. Contributing to the accident was the first officer’s poor execution of the instrument approach, and the lack of effective intra-cockpit communication between the crew. Additional contributing factors to the accident are the lack of effective oversight by AWAC and the FAA to ensure adequate training and an adequate experience level of first officers for line operations. |
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