• Mykonos, Greece
  • From €4.000 / TRIP
  • 34°, Clear

Hawker Beechcraft Premier 1A

Beechraft Premier 1 is a light jet aircraft manufactured by the Beechcraft Division of Hawker Beechcraft. The aircraft was designed to compete with the Cessna Citation Jet series of aircraft.

Design of the Premier I began early in 1994 under the designation PD 374, and development was authorized to continue early the following year. Design of the Premier I began early in 1994 under the designation PD 374 and development was authorized to continue early the following year. The aircraft was officially launched at the annual National Business Aviation Association Convention in September 1995 and construction of the first prototype commenced late in 1996.

The Premier I prototype was rolled out on 19 August 1998 and its first flight was on 22 December 1998, four prototypes were used in the flight test program and its FAA Type Certificate was issued on 23 March 2001.

On 22 September 2005, the upgraded Premier 1A was certified which featured a new cabin interior and imporved systems.

Hawker Beechcraft Premier 1A

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It is powered by two FJ44-2A Pratt & Williams International engines offering 7,200 libres of thrust.

The Maximum range of the Hawker Beechcraft Premier 1A is 1,430 nm operating with available fuel.

The cabin volume is 285 cubic feet. Typical configuration features 7 Guests and 2 Pilots.

Maximum Take-Off Weight (MTOW) is 12,500 Libres (5,670 Kg) with a maximum range of 1,430 nm.

 

Maximum Cruise

Speed:

454 kts 841 Km/h
Long-range

Speed:

370 kts 685 Km/h