AFMS
N•
D07
FOR
GARMIN
GFC700
AUTOPILOT
AND
VARIABLE
PITCH
PROPELLER
EQUIPPED
AEROPLANES
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Page APV3-14
6.3
PROPELLER
OVERSPEED
I
•
In
case ofpropelleroverspeed
in
flight, apply following procedure:
I. Throttle Lever ... .. .
......
. . .
2. Propeller Lever
...............
.
3. Mixture Lever ...
......
..
..
.. .
4. RPM indicator
............
...
.
REDUCE power
Decrease RPM
As required
CHECK
If
it
is
not possible to decrease propeller rpm.
land
as
soon
as
possible ap-
plying
Forced landing procedure.
(See
Para
11)
Maximum propeller
rpm
exceedance may cause engine com-
ponents damage .
~
Monitor engme
RPM;
overspeed shall
be
prevented by retarding propeller lever.
6.4
I
RREGULAR
RPM
I.
Fuel pump:
...........
..
.
..
...
..
...
....
............
ON
2. Fuel quantity and pressure indicators:
.........
CHECK
3.
If
necessary: ..
...........
.
......
...
....
..
.........
SWITCH TANK
If
engine continues to
run
irregularly
,.
Land
as
soon as possible.
Section
3 -
Emergency
procedures
AVIONIC
SUITE
FAILURES
Ed.
2. Rev.0
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