TM 1-1510-225-10
8A-8
*
d. Shock strut Check for signs of leakage
and minimum strut extension (5.5 inches
high floatation gear, 4 inches standard
gear), and left and right extension is
approximately equal.
e. Torque knee Check condition.
f. Safety switch Check condition, wire, and
security.
g. Wheel well, doors, and linkage Check for
signs of leakage, broken wires, security,
and general condition.
4. Right wing Check as follows:
a. Recessed and heated fuel vents Check
free of obstructions.
b. GPU access door Secured.
c. Wing ice light Check condition.
d. Outboard deice boot Check for secure
bonding, cracks, loose patches, stall strip,
and general condition.
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e. Tiedown Released.
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f. Main tank fuel and cap Check fuel level,
condition of seal, cap tight and properly
installed. Locking tab aft.
g. Outboard wing fuel vent Check free of
obstruction.
h. Wing tip and position light Check
condition and for cracked lens.
i. Recognition/strobe light Check condition.
j. Static wicks Check security and
condition.
k. Ailerons and trim tab Check security and
condition of ground adjustable tab.
l. Fuel sump drains Check for leaks.
m. Flaps Check for full extension or
retraction (approximately 1/4 inch play) and
skin damage such as buckling, splitting,
distortion, or dents.
*
n. General condition Check for skin damage
such as buckling, splitting, distortion, dents,
or fuel leaks.
8A-17. FUSELAGE RIGHT SIDE, AREA 4.
1. Fuselage right side Check as follows:
*
a. General condition Check for skin damage
such as buckling, splitting, distortion, or
dents.
b. Beacon Check condition.
c. Aft access door Check condition.
d. Cabin air exhaust Clear.
e. Oxygen filler door Check secure.
f. Static ports Check clear of obstructions.
g. Emergency locator transmitter Armed
and antenna check.
8A-18. EMPENNAGE, AREA 5.
1. Empennage Check as follows:
a. Vertical stabilizer, rudder, and trim tab
Check for skin damage such as buckling,
splitting, distortion, or dents, and trim tab
rig.
b. Antennas Check condition.
c. Deice boots Check for secure bonding,
cracks,
loose
patches,
and
general
condition.
If the possibility of ice accumulation on the
horizontal stabilizer or elevator exists, do
not take off.
d. Horizontal stabilizer, elevator, and trim tab
Check for skin damage such as buckling,
splitting, distortion, or dents, and trim tab
rig.
e. Elevator trim tab Verify "0" (neutral)
position. The elevator trim tab "0" (neutral)
position is determined by observing that the
trailing edge of the trim tab aligns with the
trailing edge of the elevator while the
elevator is resting against the downstops.
f. Static wicks Check.
g. Position and beacon lights Check
condition.
8A-19. FUSELAGE LEFT SIDE, AREA 6.
1. Fuselage left side Check as follows:
*
a. General condition Check for skin
damage such as buckling, splitting,
distortion, or dents.
b. Static ports Check clear of obstructions.
c. Cabin door Check seal and general
condition.
WARNING