Page 7
Pilot’s Operating Manual
Revision A1: Nov, 2002
Hawker 800XP Pro Line 21
Section I - GENERAL
DIMENSIONAL DATA
Wing
Span .................................................. 51 ft 4 1/2 in ..........................15.66 m
Aspect Ratio ...................................... 7.06
Gross wing area ............................... 374 sq ft ................................34.75 sq m
Fuselage
Overall length (including tail) ............. 51 ft 1.64 in ...........................15.59 m
Cabin
Length (including vestibule) ............... 21 ft 8 in ................................6.6 m
Head room......................................... 5 ft 9 in ..................................1.75 m
Width ................................................. 6 ft 0 in ..................................1.83 m
Aisle width ......................................... 1 ft 6 in ..................................0.41 m
Passenger Entry Door
Height ................................................ 4 ft 3 in ..................................1.30 m
Width ................................................. 2 ft 3 in ..................................0.68 m
Average height of
door sill above ground ....................... 3 ft 6 in ..................................1.07 m
Windows
Height ................................................ 1 ft 2 1/2 in ............................0.36 m
Width ................................................. 10 in ......................................0.25 m
Emergency Exit
Height ................................................ 3 ft 0 in ..................................0.91 m
Width ................................................. 1 ft 8 in ..................................0.51 m
Forward Luggage Bay Capacity
Traditional .......................................... 21.0 cu ft ...............................0.593 cu m
Open Plan.......................................... 13.9 cu ft ...............................0.394 cu m
Aft Luggage Bay Capacity
Capacity............................................. 38.0 cu ft ...............................1.076 cu m
Landing Gear
Track (Main gear)............................... 9 ft 2 in ..................................2.79 m
Wheel base........................................ 21 ft 1/2 in .............................6.41 m
Maximum nose wheel angle
(using cockpit control)........................ 45
°
each side
NOTE: With nose wheel steering disconnected the nose wheel is free to castor through 360
.