Hawker 800 XP, Руководство по подготовке пилотов

Страница: 119 / 504

Rear Section
The rear section includes the rear equipment bay,
a tail cone, and attachment points for the verti-
cal stabilizer, ventral fuel tank, and the engine
pylons. A hinged door located in the bottom of
the ventral tank provides access to the unpres-
surized rear equipment bay (Figure 1-16).
WING
The Hawker 800 XP has a swept-back, can-
tilevered, all-metal wing (Figure 1-17). The
center wing section is contoured to fit the fuse-
lage and is attached to the fuselage at four at-
tachment points.
Air flow control devices on each wing consist
of a row of vortex generators, a vortilon and a
stall trigger. The vortex generators are attached
to the upper surface of the wing. The vortilon
is on the bottom surface of the wing leading
edge, inboard of the inner end of the row of vor-
tex generators. The stall trigger is attached to
the anti-icing distributor inboard of the land-
ing lamp.
On the trailing edge a double slotted flap ex-
tends from the wing to the fuselage. An upper
and lower air brake is positioned forward of the
flap; in the closed position the air brakes form
part of the flap shroud.
The major portion of each wing is sealed to
form an integral fuel tank. Top skins are ma-
chined single sheets from root to tip. The bot-
tom skins are machined single sheets from
airplane centerline to tip. The leading edge of
each wing contains the landing and taxi lights
and deicing fluid panels.
Revision 1.02 1-15
FOR TRAINING PURPOSES ONLY
HAWKER 800 XP PILOT TRAINING MANUAL
FlightSafety
international
Figure 1-16. Rear Equipment Bay Hatch
Figure 1-17. Wing