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The lift detector vane, the mounting plate and the complete housing are heated to prevent icing. Heating is engaged together with the Pitot heating.
Page 7 - 64 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
7.13 GARMIN G1000 INTEGRATED AVIONICS SYSTEM
7.13.1 GENERAL
The Gamin G1000 is a fully integrated flight, engine, communication, navigation and surveillance instrumentation system. This Integrated Avionics System consists of a Primary Flight Display (PFD), a Multifunction Display (MFD), an Audio Panel, an 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, and an integrated annunciation system to alert the pilot of certain abnormal conditions.
A remote avionic box is located behind the aft baggage compartment frame. A push-to-talk (PTT) button for the COM portion of the G1000 is mounted on the end of each control stick. There are connection facilities for up to 4 headsets between the front seats.
Refer to the Garmin G1000 Cockpit Reference Guide, Garmin P/N 190-00406-00, dated September, 2004, and Pilot*s Guide, P/N K00-00138-00, dated September, 2004, for complete descriptions of the G1000 system and operating procedures.
NOTE
Near the DME ground station, it can happen under certain adverse conditions that the Bendix/King KN 63 DME loses the direct signal from the ground station and locks onto an "echo". This will result in an inaccurate indication of the distance.
' NOTE ' During retraction and extension of the landing gear the ' ADF-indication may be inaccurate.
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 7 - 65
7.13.2 PRIMARY FLIGHT DISPLAY (PFD)
The Primary Flight Display (PFD; see figure below) 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
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Communications frequency set knobs
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Communications frequency transfer button
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Altimeter setting knob (baro set)
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Course knob
*
Map range knob and cursor control
*
FMS control buttons and knob
*
PFD softkey buttons, including master warning/caution acknowledgment
*
Altitude reference set knob
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Heading bug control
*
Navigation frequency transfer button
*
Navigation frequency set knobs
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