MQONEY
MODEL
M20J
SECTION IV
NORMAL
PROCEDURES
9.
Propeller
-
.........
Blades
CHECK for nicks, cracks, oil
...
leaks, rotationalmovement.
.......
CHECK de-ice boots(if installed).
Spinner
......
CHECK
for
security, cracks
.......
Cooling Air and Induction Intake
UNOBSTRUCTED
...........
Landing Light
CHECK Lens
&
Bulb
..........
Nose Gear, shock discs and tire
CHECK
........
Nose Gear Door
CHECK for Loose Linkage
Wheel Chock
.............
REMOVE
8.
flight Cowl Area
-
Wight Side Engine Cowl Fasteners
Engine Oil bevel
.....
.....
.....
Exhaust Pipe
.....
Cowl Flap
.....
Windshield
.....
....
Cabin Cooling Vent
..
SECURED
..........
CHECK
.
(full
for
extended flight.(Max.
8
qts.)
.
(Minimum qty.
6
qts.)
.........
SECURED
.........
CHECK
.........
CLEAN
...
UNOBSTRUCTED
9.
Right Wing
-
Fuel Tank Sump Grain
..........
DRAIN until clear
Right Main
Gear,
shock discs and tire
.....
CHECK
Right Main Gear Doors
............
CHECK
Wheel Chock
.............
REMOVE
............
Tank Vent IJNOBSTRUCTED
..............
Tiedown
REMOVE
Right Wing beading Edge
.....
CHECK
Fuel Tank
...
CHECK QUANTITY. SECURE CAP
--"-------
(
NOTE
I
--"-------
The reduced
fuel
indlcatar is located
In
the
Biller
neck. This
indicator
is
used
to
indicate
kaaable
fuel
capacity
of
25
U.S.
gallons
(94.7
liters)
(20.8
IMP.
gal.)
1
NOTE
/
"."-=.------
The
optisrsal
visual fuel quantity gauge is
to
be
used
for
paP%iai
refueiing purposes only;
DO
NOT
use Isr preflight
check.
REV.
B
6-12-87
ISSUED
6-2-86
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