Garmin G1000 Airplane Flight Manual Supplement page 24

AFM SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
Stdby Alt/Emerg Bus switch
Verify Amber Emerg Bus light illuminates
Verify positive charge on battery ammeter
Verify Red ALT VOLTS light extinguishes
Stdby Alt/Emerg Bus switch
Verify Red ALT VOLTS light illuminates
Alt Field Switch
Verify Red ALT VOLTS light extinguishes
Standby Alternator Checks Complete
Ammeter . . . . . . . . . . . . . . . . . . . . .
Main Battery Voltage
Select the other battery using the BAT 1/2 selector
Ammeter . . . . . . . . . . . . . . . . . . . . .
Main Battery Voltage
Select desired Main Battery for use during flight using BAT 1/2
Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Low Fuel Boost
Pump Switch . . . . . . .
Low Fuel Boost Pump Switch
Elevator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Rudder Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
SET AT TAKEOFF POSITION (10 degrees)
Flight Controls
Cabin Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Seats, Seat Belts and Shoulder Harness
Avionics and Autopilot
Annunciator Lights
Internal/External Lights
Strobe Lights/Rotating Beacon
Pilots Window . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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FAA APPROVED
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ON--Verify annunciator light illuminates BLUE
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CHECK Positive Charge Indication
Greater than 26.5VDC
CHECK Positive Charge Indication
Greater than 26.5VDC
selector
RETARD to 1000 RPM
CHECK free and correct movement
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CHECK – (Refer to section IX)
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MOONEY
M20R
TAKEOFF SETTING
TAKEOFF SETTING
CHECK operation
CHECK SECURED
SECURED
CHECK
AS DESIRED
CLOSED
ISSUED 11 - 2004
REVISION A 06--2005
REVISION B 03--2006
ON
OFF
ON
OFF
ON