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Beech / Beechcraft 390 Premier 1

Beechcraft 390 Premier 1, Vibro Air, D-IATT, c/n RB-48 © Karsten Palt
Photo ©: Karsten Palt

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).
Crew1-2
Passengers6
 
Propulsion2 Turbofan Engines
Engine ModelWilliams / Rolls-Royce FJ44-2A
Engine Power (each)10,2 kN2300 lbf
 
max. Cruise Speed683 km/h369 kts
  425 mph
max. Speed (vne)835 km/h451 kts
  519 mph
Mmo (max. Mach)Mach 0.80
Service Ceiling12.497 m41.000 ft
Range2.519 km1.360 NM
1.565 mi.
 
Empty Weight3.719 kg8.200 lbs
max. Takeoff Weight5.670 kg12.500 lbs
max. Landing Weight5.262 kg11.600 lbs
 
Wing Span13,56 m44,5 ft
Wing Area22,3 m240 ft
Length14,02 m46,0 ft
Height4,67 m15,3 ft
 
First Flight22.12.1998
Production Statusin production
 
ICAO CodePRM1
FAA TCDSA00010WI
EASA TCDSA.073
 
Data for (Version)Beechcraft 390 Premier 1A
VariantsPremier I, Premier IA

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