AFMS
N•D07
FOR
GARMIN
GFC700
AUTOPILOT
AND
VARIABLE
PITCH
PROPELLER
EQUIPPED
6.10.
AEROPLANES
1?~®1l
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a Page APV3-l 8
DEFECTIVE
ENGINE
CONTROLS
Defectjye Mjxturc Control
Cable
I. Maintain altitude to the nearest arfield
2.
During descent, check engine behaviour to a higher power setting.
A lean mixture can lead to engine roughness and loss
of
power.
Landing approach must be planned accordingly.
Go-around may then be impossible.
Defectjvc
Throttle
Control
Cable
If
power
is
sufficient to continue flight:
I. Approach nearest airfield, control engine power with Propeller
le
ver
2.
Perform landing with shut-down engine applying
Forced landing procedure. (See Para I
1)
If
power
is
not sufficient
to
continue flight:
I. Carry out Forced landing procedure. (See Para
11)
pefcctjyc
Proneller
I.eyer
Coptrol
Cable
If
power
is
sufficient
to
continue
fli
g
ht:
I. Approach nearest airfield, control engine power with throttle
2.
Perform normal landing.
Go-around may then be impossible.
If
power
is
not sufficient
to
continue flight:
I.
Carry out Forced landing procedure. (See Para
11
)
Section
3 -
Emergency
procedures
POWERPLANT
EMERGENCIES
Ed.
2.
Rev.O
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