Light Business Jets
Hawker 750
ICAO: H25B
Overview
The Hawker 400XP was introduced in the early 2000s as an updated variant of the Hawker 400. Designed for corporate and charter use, it emphasized reliable performance and cabin comfort. The aircraft competed in the light jet segment.
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Specifications
Units
- Engine
- 2 × Pratt and Whitney JT15D-5
- Engine type
- Turbofan
- Thrust
- 2 × 2,965 lbf · 13 kN
- Avionics
- Collins Pro Line 4, Collins DBU-5000 Data Base Unit, Honeywell Mark V TAWS
- Wing tips
- No winglets
- Seats
- 8
- Crew
- —
- Cabin width
- 4 ft 11 in · 1.50 m
- Cabin height
- 4 ft 10 in · 1.47 m
- Cabin length
- 15 ft 8 in · 4.78 m
- Exterior length
- 48 ft 5 in · 14.76 m
- Tail height
- 13 ft 5 in · 4.10 m
- Fuselage diameter
- 5 ft 7 in · 1.70 m
- Wing span
- 43 ft 5 in · 13.23 m
- Baggage volume
- 35 ft³ · 1.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 16,300 lb · 7,400 kg
- Max landing weight
- 15,700 lb · 7,100 kg
- Max payload
- 2,000 lb · 900 kg
- Fuel capacity
- 730 gal · 2,800 L · 2,200 kg (Jet A)
- Max cruise speed
- 450 kt · 518 mph · 833 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 119 kt · 137 mph · 220 km/h
- Range
- 1,565 nm · 1,800 mi · 2,900 km
- Fuel burn
- 2.14 nm/gal · 1.05 km/L
- Ceiling
- 45,000 ft · 13,700 m
- Rate of climb
- 4,020 ft/min · 20 m/s
- Takeoff distance
- 4,700 ft · 1,430 m
- Landing distance
- 3,000 ft · 920 m
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