Hawker 800 XP, Руководство по подготовке пилотов

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LANDING GEAR AND BRAKES
T h e H aw ke r 8 0 0 X P l a n d i n g g e a r i s h y -
draulically actuated and fully enclosed by hy-
draulically and mechanically actuated doors.
Gear position and warning are provided by
indicator lights and a warning horn. Nosewheel
steering is also hydraulically powered. The
brake system is controlled by master cylinder
pressure and provides for normal and emer-
gency braking. Antiskid braking is available
during normal braking. Parking brakes are ap-
plied with a lever in the cockpit.
FLIGHT CONTROLS
Primary flight controls include ailerons, rud-
der, and elevators. All are mechanically ac-
tuated. Secondary flight controls include flaps
and airbrakes which are powered by the main
hydraulic system. The flaps also can be pow-
e r e d b y t h e a u x i l i a r y h y d r a u l i c s y s t e m .
Trimming of the primary flight controls is
mechanical in all three axes, with electric el-
evator trim available. A spring-loaded strut,
compressed during rudder deflection, assists
in return of the rudder to neutral. The rudder
also incorporates a pneumatically actuated
bias system to counter asymmetric thrust dur-
ing single-engine operation.
PITOT-STATIC SYSTEM
The pitot-static system serves the computers
of air data systems, a standby altimeter, a
standby airspeed indicator, the cabin differ-
ential pressure gage, and stall warning and
identification system. Provision is made for ad-
dition of optional equipment. Pitot pressure
supplied to the stall detectors and additional
equipment can be isolated by manual selection.
Two pitot heads provide impact pressure, four
static vent plates provide static pressure, and
two wing vents provide stall vent pressure.
Water traps and drains are provided in the
pipelines. The pitot heads and forward static
vent plates are heated to prevent icing.
AVIONICS
Standard avionics includes the EFIS 86 E or SPZ
8000 Electronic Flight Instrument Systems.
The system consists of four identical electronic
flight display units and one multifunction dis-
play unit together with the necessary processor
units and control panels. Two of the four dis-
play units are installed one above the other on
each main instrument panel. They replace the
conventional electromechanical ADI and HSI
on each side. The multifunction display unit
occupies the weather radar position with a
weather radar control panel mounted directly
below the unit. In addition to information pre-
viously displayed on a conventional ADI and
HSI, items such as air data, annunciation of
flight director modes, waypoint and VOR/LOC
locations, weather patterns, together with check-
lists and diagnostic messages, are also available.
The flight director function can be used inde-
pendently of the autopilot system with the pilot
steering the airplane to satisfy the flight direc-
tor commands as programmed, or the autopilot
may be coupled to automatically steer the air-
plane to satisfy flight director commands as
programmed. The yaw damper system operates
independently of the autopilot and may be en-
gaged with or without the autopilot engaged.
OXYGEN SYSTEM
The Hawker 800 XP oxygen system provides
oxygen for crew and passenger use from two
high-pressure steel cylinders. In flight, oxy-
gen is available to the crew at all times. The
passenger’s oxygen is available automatically
at high cabin altitudes or manually anytime at
the pilot’s discretion. Oxygen for therapeutic
purposes is available at all times at selected
cabin outlets. A portable oxygen system
(smoke set) is stowed in the cockpit.
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FOR TRAINING PURPOSES ONLY
HAWKER 800 XP PILOT TRAINING MANUAL
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