Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 17-4
Section III Sub-section 17
AVIONICS
P/N 140-590032-0007
Revision A4: Sep, 2010
Pilot’s Operating Manual
Each MFD can be used to present a variety of information, including: Present Position Map; TCAS; FMS
based textual data; Navigation Data; Weather Radar and EGPWS. Engine data is typically presented
on the Pilot’s MFD. The Copilot’s MFD can present fuel gauging data, the flap display and the electronic
checklist.
Line select keys are provided on each side of the displays and are used to control the basic display
formats. The bezel mounted line select keys along with the Display Control Panel (DCP) and Flight
Guidance Panel (FGP) provide primary pilot interface to control the PFD and MFD. Control of the radar,
NAV sources and bearing pointers is through the DCP and the PFD line select keys. Control of the
course, preselect heading, altitude and speed references is through the Flight Guidance Panel (FGP).
DISPLAY CONTROL PANELS (DCP) Figure 3
Each PFD/MFD display pair has a dedicated DCP to control the display and menu functions on their
respective PFD/MFDs.
The DCPs are located on the glareshield panels directly above the respective PFD/MFDs they normally
control. The DCP, when combined with the line select keys on the PFD, provides control of the Weather
Radar, NAV source, bearing pointers, V speeds, BARO Minimums (Barometric Altitude-based Minimum
Descent Altitude) and RA Minimums (Radio Altitude-based Decision Height Minimums).
FLIGHT GUIDANCE PANEL (FGP) Figure 3
The FGP is used to control the Flight Guidance System and is located in the center of the glareshield
panel.
Command of the Flight Guidance System is accomplished by using the lateral and vertical mode select
switches, VS/pitch wheel, autopilot switches, FD switches and various control knobs of the FGP along
with the yoke mounted synchronization (SYNC), autopilot disconnect (AP DISC), and go-around (GA)
switches.
Attitude reference, heading reference, airspeed reference, vertical speed reference and VS pitch
reference are also controlled from the FGP.
CONTROL DISPLAY UNITS (CDU) Figure 2
Two CDUs are installed side by side in the lower section of the center instrument panel. Each CDU is
a color LCD-based display unit with an integrated keyboard having 16 keys and a full alphanumeric
keypad. In addition to the integrated keyboard, each CDU has six line select keys located in the bezel
on each side of the color LCD display.
The CDUs are used to control the Radio Sensor System (RSS) and provide integrated control of several
combinations of airplane communications (including a normal means of radio tuning) and navigation
radio subsystems.
The CDUs can also provide the following functions:
• Control display for the Flight Management System (FMS).
• Stand-alone control for radios.
• Back-up display for engine data.
• Back-up display for Global Positioning System (GPS) data.
• MFD menus