B Remove protection cap and check pitot mounted on left strut is
unobstructed, do not blow inside vents, place protection cap inside aircraft.
C Left side leading edge and wing skin: visual inspection
D Left aileron: visual inspection
E Left flap and hinges: visual inspection
F Left main landing gear; check inflation 14 psi (1.0 bar), tire condition,
alignment, fuselage skin condition.
G Horizontal tail and tab: visual inspection.
H Vertical tail and rudder: visual inspection.
I Right side main landing gear; check inflation 14 psi (1.0 bar), tire
condition, alignment, fuselage skin condition.
L Right flap and hinges: visual inspection.
M Right aileron: visual inspection.
N Right leading edge and wing skin: visual inspection.
O Check freedom of movement of stall detector microswitch on right side
leading edge, activate Master switch and check cabin acoustic warning
signal is operative, deactivate Master switch.
P Right side fuel filler cap: check visually for desired fuel level and secure.
Right side tank vent: check for obstructions.
Q Right side static port: check for obstructions, do not blow inside vents (read
note).
R Nose wheel strut and tire: check inflation 11 psi (0.8 bar), tire condition
and condition of rubber shock absorber discs.
S Propeller and spinner condition: check for nicks and security.
T Open engine cowling and perform the following checklist:
I. Check no foreign objects are present.
II. Check the cooling circuit for losses, check coolant reservoir level,
insure radiator honeycomb is unobstructed.
III. Check lubrication circuit for losses, check oil reservoir level,
insure radiator honeycomb is unobstructed.
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