September 12, 2017

Textron Hawker 400XP Overview (2004-2010)

Product Overview

The Hawker 400XP business jet is a small-cabin business jet produced by Textron Beechcraft in Wichita, Kansas, USA. It is ideal for short trips and strikes a good balance between comfort, performance, and operating costs.

As of June 2017, 61% of the Hawker 400XP were purchased pre-owned by their current owners, the other 39% new. 13% are for sale with the majority of those (76%) under an exclusive broker agreement. When for sale, the average time on the market is 337 days

Brief History

The Beechjet 400A was built from 1990 to 2003. In 2004 the Hawker 400XP replaced the Beechjet 400A starting with serial number RK-354. Upgrades from the 400A model included an increased gross weight, a longer range, and a redesigned fuel system; however, it retained the same Pratt & Whitney Canada JT15-D engines. When production ended in 2010, it became the last small-cabin business jet to be powered by this engine. A total of 225 Hawker 400XP aircraft were manufactured with 223 in operation worldwide.

Worldwide Appeal

There are 223 Hawker 400XP aircraft in operation today. Most of these are wholly owned (210) with 9 in shared and 4 in fractional ownership. 22.4% are currently leased. North America has the largest percentage of wholly owned Hawker 400XP aircraft (70%), followed by Asia (11%) and South America (11%).


Highlights

Performance

Two Pratt and Whitney Canada JT15D-5 engines power the Hawker 400XP each offering 2,965 pounds of thrust and using 214 gallons per hour (GPH). The range of the Hawker 400XP is 1,333 nm operating under NBAA IFR 4 passengers with available fuel.

Interior

The cabin volume for the Hawker 400XP is 305 cubic feet. Typical configuration features 9 passenger and 2 crew seats.

Speed

Maximum Cruise Speed: 450 kts 833 km/h
Long-range Speed: 414 kts 767 km/h

Airfield Performance

Takeoff distance: 3,906 ft (1,191 m) (SL, ISA, MTOW)
Landing distance: 2,960 ft (902 m) (SL, ISA, MLW)

Operating Altitude

Maximum operating altitude: 45,000 ft (13,716 m)

Noise Level (EPNdB)

Takeoff: 89
Flyover: 93.7
Approach: 91.7

Weights

A. Maximum ramp weight: 16,500 lb (7,484 kg)
B. Maximum takeoff weight: 16,300 lb (7,394 kg)
C. Maximum landing weight: 15,700 lb (7,122 kg)
D. Maximum zero fuel weight: 13,000 lb (5,897 kg)
E. Standard basic operating weight: 10,985 lb (4,983 kg)

Avionics

Collins Pro Line 4 avionics

Resources

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