PRM1

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
RAYTHEON Premier 1
RAYTHEON 390 Premier 1
HAWKER BEECHCRAFT Premier 1
HAWKER BEECHCRAFT 390 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 (metric)
13.56 m
Length (metric)
14.02 m
Height (metric)
4.67 m
Powerplant

2 x Williams / Rolls-Royce FJ44-2A

Engine Model(s)
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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