Light Jets
HAWKER 800XP/850XP
AIRCRAFT DESCRIPTION
The Hawker 800XP is one of the most successful private jets that British Aerospace has ever made. It is a third-generation model of the 800 series, and is similar in part to the ubiquitous Hawker 400XP. It is designed to complete transcontinental and international flights as needed, as well as have good short range capabilities. Since it is the third member of the 800 series, it has undergone many small improvements to the features that made it successful in the private jet market to begin with — its cruise and climb speeds, runway performance, and weight limits.
The cabin of the Hawker 800XP is typically configured with eight seats: a four-person club section, a three-person divan, and one forward-facing seat. The seats are fully adjustable and can swivel 360°. Different soundproofing options are available, but cabin noise levels usually stay in the low 70-decibel range. The cabin itself measures 21.3 feet long, 5.7 feet high and 6 feet wide. There is a baggage compartment accessible in-flight which holds 48 cubic feet of luggage.
One of the Hawker 800XP’s strong points is its ability to take off from runways much shorter than are typically required for private jet international flights. At sea level, 5,032 feet of runway is required; at an elevation of 5,000 feet, the requirement increases to 7,952 feet. The useful load of the Hawker 800XP is slightly higher than the loads of the Hawker 800 and 800A.Modifications were made to the wing as well – the wing used on the Hawker 1000 was chosen over the previous Hawker 800 wings with winglets, resulting in a longer range and higher loading capacity.
When carrying six passengers, crew, and their baggage, the Hawker 800XP’s maximum range is 2,900 miles (2,540 nautical miles). Possible flights would include New York to Los Angeles or Singapore to Beijing.
AIRCRAFT CHARACTERISTICS & SPECIFICATIONS
External Dimensions |
|
Length |
51 ft. 2 in. (15.60 m) |
Height |
18 ft. 1 in. (5.51 m) |
Span |
51 ft. 4 in. (15.66 m) |
Cabin Dimensions |
||
Length |
21 ft. 4 in. |
(6.49 m) |
Height |
5 ft. 9 in. |
(1.75 m) |
Span |
6 ft. 0 in. |
(1.83 m) |
Pressurization |
|
Differential |
8.6 PSI |
Sea Level Cabin To (ft.) |
22,200 ft. |
Airport Performance |
|
Takeoff Field Length |
|
Max. TO Wt., SL, ISA |
5,030 ft. (1,533 m) |
26,964 lb. TOW, 5,000 ft. elev, 25°C/77°F |
7,965 ft. (2,428 m) |
Landing Distance |
|
Max Landing Wt., SL, ISA |
2,650 ft. (808 m) |
Climb Performance (Max Takeoff Weight) |
|
Time to Climb / Altitude |
2,650 ft. (808 m) |
| FAR 25 Engine-out Rate |
470 fpm (143 m/min) |
FAR 25 Engine-out Gradient |
201 ft/nm (33 m/km) |
Ceilings |
|
Certified |
41,000 ft. (12,497 m) |
All Engine Service |
39,000 ft. (11,887 m) |
Engine-out Service |
18,800 ft. (5,730 m) |
Cruise Performance |
|
High Speed Cruise |
|
Speed |
447 kt/514 mph (828 km/hr) |
Fuel Flow |
1,824 lb./hr. (827 kg./hr) |
Altitude |
FL 370 |
Intermediate Cruise Speed |
|
Speed |
428 kt/493 mph (793 km/hr) |
Fuel Flow |
1,528 lb./hr. (693 kg./hr) |
Altitude |
FL 410 |
Long Range Cruise |
|
Speed |
402 kt/463 mph (745 km/hr) |
Fuel Flow |
1,209 lb./hr. (548 kg./hr) |
Altitude |
FL 390 |
Maximum Range Performance (NBAA IFR reserves)
Maximum Payload with Available Fuel
|
|
Range |
2,285 nm 4,232 km |
Average Speed |
393 kt. 728 km/hr |
Trip Fuel |
7,921 lb. 3,593 kg |
Maximum Fuel with Available Payload
|
|
Range |
2,407 nm 4,458 km |
Average Speed |
392 kt. 726 km/hr |
Trip Fuel |
8,308 lb. 3,768 kg |
4 passengers (800 lb. payload) |
|
Range |
2,540 nm 4,704 km |
Average Speed |
394 kt. 730 km/hr |
Trip Fuel |
8,366 lb. 3,795 kg. |
Ferry (Zero payload) |
|
Range |
2,621 nm 4,854 km |
Average Speed |
394 kt. 730 km/hr |
Trip Fuel |
8,409 lb. 3,814 kg |
Mission Performance (4 passengers) |
|
300 nm mission |
|
Flight Time |
0 hr. 50 min |
Trip Fuel |
1,330 lb. 603 kg |
Flight Level |
FL 370 |
600 nm mission |
|
Flight Time |
1 hr. 33 min |
Trip Fuel |
2,253 lb. 1,022 kg |
Flight Level |
FL 390 |
1,000 nm mission |
|
Flight Time |
2 hr. 29 min |
Trip Fuel |
3,554 lb. 1,612 kg |
Flight Level |
FL 390 |
Characteristics |
||
Seating (Crew + Pax) |
2 + 8 / 15 |
|
Engines |
|
Manufacturer |
Honeywell |
Model |
TFE731-5BR |
Output |
4,660/ISA+10°C |
Inspection Interval |
4,200 hrs. |
Weights |
|
Max Takeoff |
28,000 lb. (12,700 kg.) |
Max Landing |
23,350 lb. (10,591 kg.) |
Capacity |
|
Max Payload |
2,205 lb. (1,000 kg.) |
Max Fuel Capacity (1 U.S. gal = 6.7 lb./U.S. gal.) |
1,492 US gal |
Payload w/max fuel |
1,875 lb. (850 kg.) |
Fuel w/max payload |
9,670 lb. (4,386 kg.) |