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| The Model 390 Premier I is the first all new product of the Raytheon Aircraft Beech/Hawker combine to fly, and is an all new entry level corporate jet designed to compete head on with Cessna's highly successful CitationJet/CJ1 series. The Premier I was designed using CATIA computer aided design. Features include its composite carbonfibre/epoxy honeycomb fuselage, swept metal construction wings, T-tail and two WilliamsRolls FJ-44 turbofans. The composite fuselage is an important feature for a number of reasons. Firstly, advanced production techniques means a quicker construction and also allows greater (approx 13%) internal cabin space compared with a conventional construction fuselage of the same external dimensions. The Premier I is certificated for single pilot operations. The flightdeck features the new Collins Pro Line 21 EFIS avionics suite with two 20 x 25cm (8 x 10in) flat panel LCDs. |
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| Seating (normal) |
6 |
Max Takeoff (lbs) |
12,500 |
| Seating (maximum) |
- |
Certified Ceiling (ft) |
41,000 |
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| Engines |
2 Wms/RR FJ44-2A |
To (Sealevel, ISA Temp) (ft) |
3,792 |
| Output lbs ea. Flat Rating |
2,300/ISA+13 |
Landing Distance (ft) |
2,975 |
| Maximum Mach No. |
0.80 |
Max Range (fuel) (nm) |
1,360 |
| High Speed Cruise (Kts) |
451 |
Max Range (payload) (nm) |
787 |
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| Flight Time 300nm |
0 + 48 |
Flight Time 1000nm |
2 + 30 |
| Flight Time 600nm |
1 + 33 |
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| External |
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Internal |
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| Length (ft) |
46.00 |
Length (ft) |
13.50 |
| Height (ft) |
15.30 |
Height (ft) |
5.40 |
| Span (ft) |
44.50 |
Width: Max floor (ft) |
5.50 |
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