Hawker 800 XP, Pilot Training Manual

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INTRODUCTION
The Hawker 800 XP avionics covered in this chapter includes the pitot-static system and
the integrated flight control system. Chapter 16 describes the standard avionics pack-
age available for installation. The user should consult applicable AFM supplements and
vendor manuals for additional information and information on specific systems not in-
cluded in this chapter.
GENERAL
The pitot-static system includes two pitot
heads, four static vent plates, two wing stall
vents, and No. 1 and No. 2 air data computers.
The standard automatic flight control system
includes the air data system, the autopilot and
flight director, the electronic flight instrument
system, the attitude heading reference system,
and the standby instruments. A conventional
flight control system without EFIS is optional
but is not covered in this chapter. With either
system, the flight director function can be used
independently of the autopilot with the pilot
hand-flying the airplane to satisfy the flight
director commands, or the autopilot may be
coupled to automatically steer the airplane to
satisfy the flight director commands. The yaw
damper system operates independently of the
autopilot and may be engaged with or without
the autopilot engaged.
CHAPTER 16
AVIONICS
16-1
FOR TRAINING PURPOSES ONLY
HAWKER 800 XP PILOT TRAINING MANUAL
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