FIG. 4-1
A
Left hand fuel filler cap: check visually for desired fuel level and secure. Left tank
vent: check for obstructions.
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, align-
ment, 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, align-
ment, 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 micro-switch 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).
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