BEECHJET 390 PREMIER 1

OVERVIEW :

390 Premier 1

Corporate Jet

The Beechcraft 390 Premier I is a twin-engined light corporate jet aircraft produced by the US-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 44,5 ft
Wing Area 22,3 m² 240 ft²
Length 14,02 m 46,0 ft
Height 4,67 m 15,3 ft
First Flight 22.12.1998
Production Status in production
ICAO Code PRM1
FAA TCDS A00010WI
EASA TCDS A.073
Data for (Version) Beechcraft 390 Premier 1A
Variants Premier I, Premier IA

 

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