G
H
L
M
N
0
p
Q
R
Left main landing gear
Stabilator, tab and rear light
Vertical tail and rudder
Right main landing gear
Right flap and hinges
Right aileron, hinges and RH tank
vent line
Right strobe light, leading edge
and wing skin
Stall indicator switch
Right fuel filler cap
Nose wheel strut and tire/
RH
static port
Page 4 -
12
CHECK inflation, tire condition, alignment,
fuselage skin condition. Checkfaselage skin
status, tire status
(cuts,
bruises, cracks and
excessive wear), slippage markers integrity,
gear structure and brakes hoses: there
should
be
no sign
of
hydraulic fluid leakage.
CHECK stabilator leading edge. Check the
actuating mechanism
of
stabilator and the
connection with related tab: CHECK free
of
play, friction. CHECK fuselage bollom and
top skin. CHECK antennas for integrity.
Check light/or integrity.
Visual inspection, check free
of
play.friction.
CHECK inflation, tire condition, alignment,
fuselage skin condition. Check fuselage skin
status, lire status
(cuts,
bruises, cracks and
excessive wear), slippage markers integrity,
gear structure and brakes hoses: there should
be
no sign
of
hydraulic fluid leakage.
Visual inspection; Copper bonding strips:
CHECK/or proper connection;
Visual inspection, check free
of
play.friction;
Copper bonding strips: CHECK
for
proper
connection; Right side tank vent: check
for
obstructions.
Visual inspection, CHECK stall strips
(if
pre-
sent), CHECK strobe light/or integrity and
fixing
CHECK/or integrity andfree
of
play,
CHECK desired fuel level
(use
graduated
dipstick). Drain the right Juel tank sump by
quick drain valve using a cup
to
collect fael
(drainage operation must
be
carried with
the
aircraft parked on a level surface). Check/or
water or other contaminants.
Make
sure filler
cap
is
closed
CHECK inflation, lire condition and condi-
tion
of
shock absorber: there should
be
no
sign
of
hydraulic fluid leakage. Check the
right static port
for
obstructions.
2"d
Edition,
Rev.
0
Section
4 -
Normal
procedures
Pre-flight
Inspection
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