6.2.1.2 External Inspection
It is best to follow to follow the external inspection in the station order outlined in fig. 6-1 so nothing is missed.
Visual inspection is defined as follows: check for defects, cracks, detachments, excessive play, and unsafe or improper
installation as well as for general condition. For control surfaces, visual inspection also involves additional checks for
freedom of movement and security.
FIG. 6-1
A. Left fuel filler cap: CHECK visually for desired fuel level and secure
B. Pitot tube: Remove pitot tube cover and check that the pitot tube mounted on the left wing is unobstructed. Do not
blow inside pitot tube.
C. Left side leading edge and wing skin: CHECK for damage
D. Left aileron: CHECK for damage, freedom of movement: Left tank vent: CHECK for obstructions
E. Left flap and hinges: CHECK security
F. Left main landing gear: CHECK inflation 40 PSI (2.7 bar), tire condition, alignment, fuselage skin condition
G. Horizontal tail and tab: CHECK for damage, freedom of movement
H. Vertical tail and rudder: CHECK for damage, freedom of movement (NOTE: do not move rudder unless
nosewheel is lifted off the ground)
I. Right side main landing gear: CHECK inflation 40 PSI (2.7 bar), tire condition, alignment, fuselage skin condition
J. Right flap and hinges: CHECK security
K. Right aileron: CHECK for damage, freedom of movement; Right side tank vent: check for obstructions
L. Right leading edge and wing skin: CHECK for damage
M. Stall indicator micro switch : Check freedom of movement, turn on Master switch and check cabin acoustic
warning signal is operative, turn off Master switch
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