Beech / Beechcraft 390 Premier 1
Corporate Jet
The Beechcraft 390 Premier I is a twin-engined light corporate jet aircraft produced by the American manufacturer Hawker Beechcraft Corporation (earlier by Raytheon Aircraft).
Crew | 1-2 | |
Passengers | 6 |
Propulsion | 2 Turbofan Engines | |
Engine Model | Williams / Rolls-Royce FJ44-2A | |
Engine Power (each) | 10,2 kN | 2300 lbf |
max. Cruise Speed | 683 km/h | 369 kts 425 mph |
max. Speed (vne) | 835 km/h | 451 kts 519 mph |
Mmo (max. Mach) | Mach 0.80 | |
Service Ceiling | 12.497 m | 41.000 ft |
Range | 2.519 km | 1.360 NM 1.565 mi. |
Empty Weight | 3.719 kg | 8.200 lbs |
max. Takeoff Weight | 5.670 kg | 12.500 lbs |
max. Landing Weight | 5.262 kg | 11.600 lbs |
Wing Span | 13,56 m | 44 ft 6 in |
Wing Area | 22,3 m² | 240 ft² |
Length | 14,02 m | 45 ft 12 in |
Height | 4,67 m | 15 ft 4 in |
First Flight | 22.12.1998 | |
Production Status | out of production | |
Production Range | 1999-2013 | |
Total Production | 298 |
ICAO Code | PRM1 | |
FAA TCDS | A00010WI | |
EASA TCDS | A.073 | |
Data for (Version) | Beechcraft 390 Premier 1A | |
Variants | Premier I, Premier IA |
[Photo-ID: 1814] © Karsten Palt 2009-04-03 | |
Beech 390 Premier IA Hawker Beechcraft Reg.: N42LQ c/n: RB-263 | |
AERO Friedrichshafen 2009 [Friedrichshafen (EDNY / FDH)] |