----AEROPLANE POSITIONED CLEAR BEHIND----
1. Brakes ………………………………………………………………………………… HOLD
2. Throttle …………………………………………………………………….… 1700 RPM
CONFIRM AEROPLANE NOT MOVING
3. Engine Instruments ………………………………………………………… CHECKED
4. Vacuum Pressure Indicator ………………………………… CHECK IN GREEN
5. Magnetos …………………………………… CHECK LEFT/BOTH/RIGHT/BOTH
(MAX DROP 150RPM & MAX DIFF 50RPM)
6. Carburettor Heat ..………………………… CHECK (MAX DROP OF 75RPM)
7. Propeller ………………….…………….……… EXERCISE HIGH TO LOW RPM
Return to HIGH RPM (FULL FORWARD)
8. Ammeter ………………….…………………………………..………………….. CHECK
9. Air Conditioner (if Installed) …………………………………………… CHECKED
10. Carbon Monoxide Indicator …………………..…… NO COLOUR CHANGE
11. Throttle ………………………………….…………………………CHECK SLOW IDLE
12. Throttle …………………………………………………………………. SET 1000 RPM
NOTE: During Night & IFR flights proper verification of the alternator and
Alternator control unit operation is essential. This can be verified by loading
the electrical system momentarily (3-5 Secs) with the landing light during
engine runup (at 1700RPM). The ammeter will remain within one needle width
of its original position with the Alternator and Alternator control unit operating
properly
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