Garmin Cessna Caravan G1000, Дополнение к руководству

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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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Guide and Cockpit Reference Guide for descriptions of the messages and
recommended actions (if applicable).
Trend vectors are shown on the airspeed and altimeter displays as a magenta
line predicting 6 seconds at the current rate. The turn rate indicator also
functions as a trend indicator on the compass scale.
The PFD can be displayed in a composite format for emergency use by pressing
the red DISPLAY BACKUP button at the bottom of the audio panel. In the
composite mode, the full crew alerting function remains.
The Multi-Function Display (MFD) typically displays engine data, maps,
terrain, traffic and topography displays, and flight planning and progress
information. The display unit is identical to the PFD and contains the same
controls as previously listed. Additionally, the GFC 700 autopilot mode
controls are located on the MFD. These controls are described later in this
section.
The audio panel contains traditional transmitter and receiver selectors, as well as
an integral intercom and marker beacon system. The marker beacon lights
appear on the PFD. In addition, a clearance recorder records the last 2 ½
minutes of received audio. Lights above the selections indicate what selections
are active. Pressing the red DISPLAY BACKUP button on the audio panel
causes both the PFD and MFD to display a composite mode.
The Attitude and Heading Reference System (AHRS) uses GPS, rate sensors, air
data, and magnetic variation to determine pitch and roll attitude, sideslip and
heading. Operation is possible in a degraded mode if the system loses any of
these inputs. Status messages alert the crew of the loss of any of these inputs.
The AHRS will align while the aircraft is in motion, but will align more quickly
if the wings are kept level during the alignment process.
The Air Data Computer (ADC) provides airspeed, altitude, vertical speed, and
air temperature to the display system. In addition to the primary displays, this
information is used by the FMS and TIS systems.
Engine instruments are displayed on the MFD. Discrete engine sensor
information is processed by the Garmin Engine Airframe (GEA) sub-system.
When an engine sensor indicates a value outside the normal operating range, the
legend will turn yellow for caution range, and turn red and flash for warning
range.