FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-11 Rev 8 Diamond DA 40 / DA 40F
7-1
SECTION 7
SYSTEM DESCRIPTIONS
G1000 SYSTEM
The Garmin G1000 Integrated Avionics System consists of a Primary Flight
Display (PFD), a Multi-Function Display (MFD), an Audio Panel, and Attitude
and Heading Reference System (AHRS), an Air Data Computer (ADC), and the
sensors and computers to process flight and engine information for display to
the pilot. The system contains dual GPS receivers, dual VOR/ILS receivers,
dual VHF communications transceivers, a transponder, an Automatic Direction
Finder (ADF) receiver, Distance Measuring Equipment (DME), and an
integrated annunciation system to alert the pilot of certain abnormal conditions.
The GPS receivers will either be non–WAAS capable (if GIA 63 units are
installed) or WAAS capable (if GIA 63W units are installed).
The Primary Flight Display (PFD) typically displays airspeed, attitude, altitude,
and heading information in a traditional format. Slip information is shown as a
trapezoid under the bank pointer. One width of the trapezoid is equal to a one
ball width slip. Rate of turn information is shown on the scale above the
compass rose; full scale deflection is equal to a standard rate turn. The
following controls are available on the PFD (clockwise from top right):
• Communications frequency volume and squelch knob
• Communications frequency set knobs
• Communications frequency transfer button
• Altimeter setting knob (baro set)
• Course knob
• Map range knob and cursor control
• FMS control buttons and knob
• PFD softkey buttons, including master warning/caution acknowledgement
• Altitude reference set knob
• Heading bug control
• Navigation frequency transfer button
• Navigation frequency set knobs
• Navigation frequency volume and Identifier knob
The PFD displays the crew alerting (annunciator) system. When a warning or
caution message is received, a warning or caution annunciator will flash on the
PFD, accompanied by an aural tone. A warning is accompanied by a repeating
tone, and a caution is accompanied by a single tone. Acknowledging the alert
will cancel the flashing and provide a text description of the message. Refer to
the Emergency or Abnormal Procedures Sections of the AFM or this
Supplement for the appropriate procedure to follow for each message.
Advisory messages related to G1000 system status are shown in white and are
accompanied by a white flashing ADVISORY alert. Refer to the G1000 Pilot’s
(4 Seiten)
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