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| Delivered from the Diamond II, deliveries of the Beechjet 400 began in June 1986, with low rate production continuing until that model was replaced by the Model 400A, which was delivered from November 1990. The new 400A incorporated a number of improvements over its predecessor. A higher max takeoff weight and greater operating ceiling improved performance, while repositioning the rear fuselage fuel tank increased cabin volume. The flightdeck features Collins Pro Line 4 EFIS with three colour displays - two primary flight displays (PFDs) and a multifunction display (MFD) with a second MFD optional. A new luxury standard interior for the Beechjet which was introduced in 1996. |
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| Seating (normal) |
7 |
Max Takeoff (lbs) |
16,300 |
| Seating (maximum) |
- |
Certified Ceiling (ft) |
45,000 |
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| Engines |
2 P&WC JT15D-5 |
To (Sealevel, ISA Temp) (ft) |
3,906 |
| Output lbs ea. Flat Rating |
2,965/ISA+12 |
Landing Distance (ft) |
2,960 |
| Maximum Mach No. |
0.78 |
Max Range (fuel) (nm) |
1,428 |
| High Speed Cruise (Kts) |
450 |
Max Range (payload) (nm) |
748 |
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| Flight Time 300nm |
0 + 46 |
Flight Time 1000nm |
2 + 24 |
| Flight Time 600nm |
1 + 27 |
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| External |
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Internal |
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| Length (ft) |
48.40 |
Length (ft) |
15.50 |
| Height (ft) |
13.90 |
Height (ft) |
4.80 |
| Span (ft) |
43.50 |
Width: Max floor (ft) |
4.90 |
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