Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 9
Pilot’s Operating Manual
Revision A2: Nov, 2004
Hawker 800XP Pro Line 21
Section I - GENERAL
TERMS and DEFINITIONS
The following terms and definitions are used in this POM when describing locations or functions of
equipment or systems (see Figure 2).
Terms Definitions
Pilot
(No. 1) Side The left side of the airplane looking towards the nose.
Copilot
(No. 2) Side The right side of the airplane looking towards the nose.
Flight Compartment The accommodation for the flight crew, contained within the pressurized
area from forward of the vestibule to the front pressure bulkhead.
Vestibule The space leading from the main entry door, contained within the
pressurized area, bounded by the rear bulkhead of the flight compartment
and the forward bulkhead of the passenger cabin. Usually contains furnish-
ings such as galleys, wardrobes, luggage and other stowages.
Passenger Cabin The accommodation for passengers within the pressurized area from the
front cabin bulkhead to the rear cabin bulkhead.
Toilet Compartment The area between the rear bulkhead of the passenger cabin and the rear
pressure bulkhead. The area contains toilet and washbasin facilities on the
rear pressure bulkhead, and an avionics rack and rear baggage
compartment which is enclosed in a cabinet on the right wall of the
compartment.
Rear Baggage
Compartment
The area above the aft avionics rack in the toilet compartment.
On-Side Term to describe those controls, display devices and equipment of dual
provisioned systems, which are located in the flight compartment on the
same side as the pilot using them:
i.e. On-side to the Pilot are the No. 1 systems.
Cross-Side Term to describe those systems being used by a pilot, but which have con-
trols, display devices and equipment, which are located on the opposite
side of the flight compartment:
i.e. Cross-side to the Pilot are the No. 2 systems.
Reversionary Term used to describe the transfer from a cross-side system to the pilot's
on-side system. The transfer may be made by a pilot's selection, or
automatically within the equipment:
i.e. if a No.1 system fails, the Pilot can make a reversionary selection to
obtain the required data or power supply from the equivalent No. 2 system
for presentation on his on-side display device.