AFMS
N"D07
FOR
GARMIN
GFC700
AUTOPILOT
AND
VARIABLE
PITCH
PROPELLER
EQUIPPED
AEROPLANES
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5.
CHECKLISTS
5.1.
BEFORE
STARTING
ENGINE
(AFTER
PREFLIGHT
INSPECTION)
I. Seat position and safety belts: adjuII
2.
Flight controls: operate
full
stroke checking for movement smoothness. free
of
play and fric-
tion.
3.
Parking
brake:
engage
4.
Throttle friction: adjust
5.
Throttle: IDLE
6.
Propeller
Lever:
HIGH
RPM
7.
Mixture control Lever: LEAN
8.
Circuit Breakers: check
all
IN
9.
Master switch:
ON,
wail PFD turn
on,
Check
ALT
OUT
caution
ON,
Check
LOW
FP
and
LOW
OP warning
ON
I
0.
Only before the first flight
of
the day:
Standby Instrument: Check no red crosses displayed.
a.
Press and hold the control knob (approx. 2 sec)
b.
Rotate the knob selecting "INFO>" page then press
it
C.
Select "BA
TIER
Y INFO'" page then press the knob
d. Check "CHARGE
(%)"
to be more than 80%, then exit menu
11.
Avionic Master switch:
ON,
wail MFD turn
on,
check instruments, check Voltage
on Main
and
Essential Buses.
Page
APV4-15
12.
Fuel
quantity: compare the
fuel
quantity indicators information with
fuel
quantity visually
checked into the tanks (see Pre-flight inspection - External inspection), then update the
Garmin
fuel
content in the totali=er accordingly
The
totali=er function available on Garmin Engine page allows input only up to
2301ts (maximum usable fuel). Initial Fuel indication on totali=er must be corrected
manually
(as
it
does not use the aircraft
fuel
quantity indicators
as
input). Once
correctly iniliali=ed,
fuel
consumption on lotali=er is very precise as
ii
take mstan-
laneous
fuel
flow
for
computation
13.
Electric
fuel
pump:
ON
(check/or audible pump noise
and
increase
of
fuel
pressure)
14.
Warning "LOW
FUEL
PRESSURE": extinguished
15.
Electric
fuel
pump: OFF
16.
Flap control: cycle fully extended
and
then set to
TIO
17.
Pitch
Trim:
cycle fully up
and
down, then set to NEUTRAL
18.
Rudder trim: cycle
full
right
and
left, then set to NEUTRAL
•
Pitch trim position other than in neutral position would affect take
off
performance
and
take
off
rotation execution al the correct
VR.
19. Nav & Strobe lights: ON
In
absence
of
RH
seat occupant: fasten seat belts around the seat in order to prevent
any interference with the aeroplane flight control operation
and
with rapid egress
m an emergency
20.
Doors:
Closed
and
locked
Section
4 -
Normal
procedures
CHECKLISTS
Ed.
2,
Rev.O
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