AFMS
N"
D07
FOR
GARMIN
GFC700
AUTOPILOT
AND
VARIABLE
PITCH
PROPELLER
EQUIPPED
AEROPLANES
5.14. E NG
IN
E SH
UT
DO
WN
I. Parking
brake:
set
2.
Keep
engine running
at
1200
RPM
for
about one minute
in
order
to
reduce
latent heat.
3.
4.
5.
6.
7.
8.
9.
10
.
5.15.
I.
2.
3.
4.
5.
Throttle: idle
Ignition
key:
Check
OFF
- BOTH
Mixture: CUT-OFF
Ignition
key:
OFF
, key extracted
Strobe light:
OFF
Avionic Master:
OFF
Master & Generator switches:
OFF
Fuel
selector valve:
OFF
For
safety, verifY propeller
1s
fully stopped before any other act um.
Instruct passengers to
fully
open
RH
doors
and
depart, av01dmg contact
wuh
wheels
and
sharp
wmg
control surfaces
edge<.
POSTFLIGHT
CHECKS
Flight controls: lock by means
of
seat belts
Wheel
chocks and wing mooring lines: Set
Parking brake: Release
Doors: Close
and
lock
Protection plugs: set over pilot tube, stall warning, static ports
Section
4 -
Normal
procedures
CHECK
LISTS
Ed.
2, Rev../
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