Aircraft Description
N444AM is a 2006 Cessna 525B, a twin-engine turbo-fan aircraft registered to Infinity & Beyond LLC in South Bend, IN. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on January 11, 2019. The registration certificate was issued on December 4, 2019. The registration is set to expire on December 31, 2029. Powered by a Williams FJ44-3A engine producing 2820 pounds of thrust, N444AM is. The aircraft's Mode S transponder code is A55985 (hex), used for ADS-B identification and flight tracking. N444AM was last tracked by AviatorDB near Teterboro Airport (KTEB) on June 26, 2026. The FAA registry record for N444AM was last updated on September 22, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Cessna 525 Citation CJ1 represented a significant evolution in light business aviation as an improved successor to the original CitationJet. First flown in 1999, it was a low-wing twin-engine business jet powered by Williams FJ44-1A turbofans that could accommodate 6-8 passengers in typical corporate configurations. Spanning 47 feet with a range of 887 nautical miles, the CJ1 was manufactured by Cessna Aircraft Company from 2000 to 2005. AviatorDB tracks 80,402 Cessna aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is C525.
AviatorDB has found no NTSB accident or incident reports involving N444AM. 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 29, 2003 | LAX04FA031 | Destroyed | Fatal | The pilot's continued VFR flight into instrument conditions between cloud layers and with reduced visibility due to smoke that resulted in an in-flight loss of control from spatial disorientation, and the structural overload of the airframe during the subsequent high speed descent. |
Additional Details
Last Known Position
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-07-01 01:32:20 UTC