AFMS
N"
D07
FOR
GARMIN
GFC700
AUTOPILOT
AND
VARIABLE
PITCH
PROPELLER
EQUIPPED
AEROPLANES
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Page
APVJ-19
7.
I
NFLIGHT
ENGINE
REST
AR
T
7.1.PROPELLER
WIN
DMILLING
I
•
In
case
of
engme shutdown, propeller will keep windm1llmg
and
will not stop, preventing the use
of
ignlllon key. Engine
mj11ght
restart must be performed without usmg ignition key with propel-
ler wmdmtllmg m order to avo
id
possible engme damages.
Typical mdicatwn
of
a potential engine shutdown, with wmdmi/1-
mg
pr
opeller, will be
RPM
running sub-idle below 600-500 RPM.
to be confirmed by other engine mstrumenJ
(Oil
Pressure, CHT.
EGT
running down abnormally).
lnj11ght
engine restart may be
perf
o
rmed
during
lg
j11ght anywhere
w1thm the normal operatmg envelope
of
the airplane.
I. Master switch ....
.....................
.. .
Check
ON
ON
CHECK
2. Fuel pump
..
.. ..
........
.
.....
......
... .
3. Fuel quantity indicator
.................
.
4. Fuel Selector ...
..
.......
.........
......
.
SW/T
C H TANK
(if
empty required)
Minimum fem. above IDLE
5.
6.
7.
8.
Throttle Lever
.........
.
.......
...
.......
.
Propeller Lever
....
................
, .
...
. Full
fomard
Mixture
..................................
.
FULL rich
Throttle lever
.......
.
..
......
.......
, .. .
SET
as
required
Ip
case
of
ynsurcessful
epgjnc
restart;
);.
Land
as
soon
as
possible applying Forced landi
ng
procedure.
(See Para
//)
Ip
case
of
successful engjne restart;
);.
La
nd as so
on
as
possible
After engine restart,
if
pract1ca/, moderate propeller rpm to al-
low the temperatures/or
stab1f1=mg
m the green arcs.
Section
3 -
Emergency
procedures
POWERPLANT
EMERGENCIES
Ed.
2.
Rev . ./
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