Aircraft Description
N305UP is a 1995 Boeing 767-34AF, a twin-engine turbo-fan aircraft registered to United Parcel Service Co in Louisville, KY. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on December 11, 1995. The registration certificate was issued on December 12, 1995. The registration is set to expire on February 28, 2029. Powered by a Ge CF6-80 SERIES engine producing 47600 pounds of thrust, N305UP is. The aircraft's Mode S transponder code is A333B5 (hex), used for ADS-B identification and flight tracking. N305UP was last tracked by AviatorDB near Portland International Airport (KPDX) on June 26, 2026. The FAA registry record for N305UP was last updated on July 18, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Boeing 767-200, aviation's first twin-engine wide-body airliner, revolutionized commercial aviation by proving that twin-engine aircraft could efficiently operate long-haul routes previously requiring four engines. First flown on September 26, 1981, it was a low-wing twin-engine wide-body that could accommodate 210 passengers in three-class configuration. Measuring 159 feet in length with a 156-foot wingspan, it achieved a maximum range of 3,900 nautical miles and cruising speed of Mach 0.86. The aircraft was manufactured by Boeing Commercial Airplanes at their Everett, Washington facility. AviatorDB tracks 6,895 Boeing aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is B762.
AviatorDB has found no NTSB accident or incident reports involving N305UP. 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 |
|---|---|---|---|---|
| Mar 5, 2016 | DCA16CA113 | Substantial | None | the pilot flying's failure to maintain airspeed and correct pitch attitude. Contributing to the accident was the pilot's failure to maintain appropriate thrust after disconnecting the autothrottles. Also contributing was the first officer's failure to monitor the decaying airspeed and increasing pitch. |
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