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Mooney Executive 21 1968 - Page 66

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FAAIDOA APPROVED MOONEY
M20F
The lateral stability augmentation system cutoff
valve, located in the left hand grip of the
pilot's
control wheel, cuts off the system when depressed.
The roll- trim knob on the turn coordinator provides
a
command trim function. Rotation in
a
clockwise
direction trims right; counterclockwise rotation
trims left.
To preclude fuel starvation, avoid extreme sus-
tained side slips toward the tank in use when that
tank contains
less than
48
pounds of
fuel.
EMERGENCY
Emergency procedures are contained in the Emer-
gency Procedures section of the Owners Manual.
PERFORMANCE INFORMATION
Up
to
220
FT altitude loss
may
occur during
stalls
at maximum weight.
LOADING INFORMATION
Loading information
is
contained in the aircraft
Weight
&
Balance Record.
Load in accordance with loading schedule.
Maximum weight in baggage compartment
120pounds.
Maximum weight in hatrack 10 pounds.

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