N694ES - 2004 Raytheon Aircraft Company Hawker 800XP Aircraft Registration
H25B2004 RAYTHEON AIRCRAFT COMPANY HAWKER 800XP
Aircraft Description
N694ES is a 2004 Raytheon Aircraft Company HAWKER 800XP, a twin-engine turbo-fan aircraft registered to Monfort Aviation LLC in Eaton, CO. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on December 9, 2004. The registration certificate was issued on September 21, 2015. The registration is set to expire on September 30, 2028. Powered by a Honeywell TFE731-5BR engine producing 4750 pounds of thrust, N694ES is. The aircraft's Mode S transponder code is A93A07 (hex), used for ADS-B identification and flight tracking. N694ES was last tracked by AviatorDB near Ogden Hinckley Airport (KOGD) on June 24, 2026. The FAA registry record for N694ES was last updated on June 10, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Hawker 850XP, the final and most advanced variant of the world's longest-running corporate jet production program, represented the culmination of a lineage stretching back to 1962. First flown in 2006, it was a mid-size twinjet business aircraft featuring Hawker's innovative blended winglets that could carry up to 13 passengers. With a range of 2,642 nautical miles and cruising at 463 knots, the aircraft stretched the performance envelope of its predecessors. Manufactured by Raytheon Aircraft Company, only 100 examples were built during its brief three-year production run. AviatorDB tracks 2,152 Raytheon Aircraft Company aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is H25B.
AviatorDB has found no NTSB accident or incident reports involving N694ES. 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 15, 2014 | CEN15IA014 | MINR | None | The failure of the main landing gear tire, which resulted in separation of the servo block and subsequent total loss of all hydraulic system pressure and prevented the landing gear from extending before landing. |
Additional Details
Last Known Position
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-06-15 01:32:20 UTC