MOONEY
M20R
AFM SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
ISSUED 11 - 2004
27 of 33
REVISION A 06 -- 2005
FAA APPROVEDREVISION B 03 -- 2006
SECURING AIRCRAFT
Magneto/Starter Switch Verify Off/Key Removed.................
Master Switch Verify Off.......................................
Electrical Switches Verify Off..................................
Interior Light Switches Verify Off...............................
Emergency Bus Switch Verify Off...............................
Parking Brake Release – Install Wheel Chocks...................
Extended Parking Control Wheel Secured.......................
Cabin Windows and Doors Closed and Locked..................
SECTION V -- PERFORMANCE
No change.
SECTION VI -- WEIGHT AND BALANCE
See current weight and balance data.
SECTION VII -- SYSTEM DESCRIPTIONS
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 Com-
puter (ADC), and the sensors and computers to process flight and en-
gine information for display to the pilot. The system contains dual GPS
receivers, dual VOR/ILS receivers, dual VHF communications trans-
ceivers, a transponder, and an integrated annunciation system to alert
the pilot of certain abnormal conditions.
The Primary Flight Display (PFD) typically displays airspeed, attitude,
altitude, and heading information in a traditional format. Slip informa-
tion 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):
S Communications frequency volume and squelch knob
S Communications frequency set knobs
S Communications frequency transfer button
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