RAYTHEON 390 Premier 1

Aircraft
Name: 
390 Premier 1
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
Low wing
Tail: 
T-tail
WTC
L
APC
B
Type Code: 
L2J
Engine: 
Jet
Engine Count: 
Multi
Position: 
Both sides of rear fuselage
Landing gear: 
Tailwheel retractable
Manufacturered as
HAWKER BEECHCRAFT 390 Premier 1
HAWKER BEECHCRAFT Premier 1
RAYTHEON 390 Premier 1
RAYTHEON Premier 1

PRM1

The Beechcraft Premier I is a light jet aircraft made by the Beechcraft division of Hawker Beechcraft. The aircraft was designed to compete with the Cessna CitationJet series of aircraft.

Technical Data
Wing span: 
13.56 m
Length: 
14.02 m
Height: 
4.67 m
Powerplant: 

2 x Williams / Rolls-Royce FJ44-2A

Engine Model: 
Williams FJ44
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
915 m
MTOW: 
5670 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL150)
IAS: 
320 kts
ROC: 
n/a
Initial Climb (to FL240)
IAS: 
320 kts
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
450 kts
MACH: 
0.83
Ceiling: 
410
Range: 
1500 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
750 m

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