Mooney M20J - Page 64

SECTION IV
NORMAL PROCEDURES
MOONEY
MODEL M20J
4. Left Tail Cone Area -
Fresh Air Vent (on Dorsal Fin)
........... CLEAR
Instrument Static Port
.......... UNOBSTRUCTED
Left Fuselage
..... . .CHECK Skin condition
Tailcone Access Door ............ SECURED
Static System Drain Push Plunger
........... UP
.... (Hold 3-5 Seconds)
5. Left wing -
Skin condition ........ Remove all ice, snow, or frost.
Flap and attach points
............. CHECK
Aileron and attach points
............ CHECK
Control linkages
.......... CHECK
Wing tips and lights
........... CHECK
Left wing leading edge
............. CHECK
Pitot tube ...... UNOBSTRUCTED
(Heat element
............. OPERATIVE)
Stall Switch Vane
..... UNOBSTRUCTED
Fuel Tank
...... CHECK QUANTITY.SECURE CAP
----------
I NOTE I
A reduced fuel indicator is located in the filler neck. This
indicator is used to indicate
useable fuel capacity of 25 U.S.
gallons (94.7 liters) (20.8 IMP. Gal.)
I NOTE I
The optional visual fuel quantity gauge is to be used for
partial refueling purposes
only; DO NOT use for preflight
check.
..............
Tiedown REMOVE
Tank Vent
........... UNOBSTRUCTED
Wheel
chock .............. REMOVE
........
Left main gear, shock discs and tire
CHECK
Left main gear doors
............ CHECK
Fuel
tank sump drain
...... DRAIN Until Clear
Pitot System Drain ........ Push plunger UP
... .(Hold for 3-5 seconds)
Gascolator Drain Valve
.. CLOSED (Check for drips)
G.Left Cowl Area -
...............
Windshield CLEAN
......... Left Side Engine Cowl Fasteners SECURED
REV.
€3 6-12-87
ISSUED 6-2-86