MOONEY
M20R
SECURING AIRCRAFT
Magneto/Starter Switch
Master Switch
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Electrical Switches
Interior Light Switches
Emergency Bus Switch
Parking Brake
. . . . . . . . . . . . . . . . . . .
Extended Parking
Cabin Windows and Doors
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):
Communications frequency volume and squelch knob
S
Communications frequency set knobs
S
Communications frequency transfer button
S
ISSUED 11 - 2004
REVISION A 06--2005
REVISION B 03--2006
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
. . . . . . . . . . . . . . . . .
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. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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SECTION V - - PERFORMANCE
AFM SUPPLEMENT
Verify Off/Key Removed
Release – Install Wheel Chocks
Control Wheel Secured
Closed and Locked
Verify Off
Verify Off
Verify Off
Verify Off
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FAA APPROVED