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Beechcraft Hawker 1000

hawker-1000-exterior.jpg

Jet Description

The Hawker 1000 was the largest member of the DH/HS/BAE-125/Hawker 800 series of corporate jets.

The BAE-125-1000 became the Hawker 1000 in mid-1993, when Raytheon purchased BAE's Corporate Jets division. The first BAE-125-1000 development aircraft flew on June 16, 1990.

​

​The Hawker 1000 is based on the smaller Hawker 800 but has a cabin 3 feet longer and is powered by Pratt & Whitney Canada PW-305 turbofans, instead of the Honeywell TFE-731 on the Hawker 800. These engines give the Hawker 1000 an extra 565 pounds of thrust on each engine.

Beechcraft Hawker 1000

RANGE

2,970 nm

SPEED

470 kts

PASSENGERS

8 people

Interior

PASSENGERS

8 people

CREW

2 people

​TYPICAL VOLUME PER PASSENGER

-

CABIN VOLUME BREAKDOWN

-

TOTAL CABIN VOLUME

-

​PASSENGER AREA

-

MISC SPACE (GALLEY, LAV, ETC.)

-

CABIN WIDTH

6 ft

CABIN LENGTH

24.4 ft

CABIN HEIGHT

5.75 ft

TOTAL BAGGAGE VOLUME

72 cu ft

INTERNAL

50 cu ft

DOOR

16.47 sq ft

WIDTH (DOOR)

2.25 ft

LENGTH (DOOR)

4.25 ft

Costs

ACQUISITION COST

$1,269,394

ANNUAL COST

-

VARIABLE COST

-

FIXED COST

-

Exterior

WINGSPAN

51.4 ft

FUSELAGE

53.9 ft

POWERPLANT

Pratt & Whitney Canada PW305B 2

Long-Range Cruise

RANGE

-

AVERAGE SPEED

400 kts

ENDURANCE

-

PASSENGERS

4 people

Maximum Cruise

RANGE

-

AVERAGE SPEED

440 kts

ENDURANCE

-

PASSENGERS

4 people

Performance

NORMAL CRUISE

440 kts

LONG-RANGE CRUISE

400 kts

MAXIMUM CRUISE

470 kts

MAX CERT. ALTITUDE:

43,000 ft

RATE OF CLIMB:

3,577 ft/min

ENGINE OUT RATE OF CLIMB

797 ft/min

ENGINE OUT RATE OF CLIMB

-

ENGINE OUT CEILING

21,000 ft

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