TM 1-1510-224-10
(b)
Warmup Allow two minutes.
(c)
Mode I and mode 3/A codes Set.
(d)
Lamp indicators Press to test.
(e)
Antenna switch Select TOP.
(f)
Mode selector NORM.
(g)
Modes 1, 2, 3/A, and C Hold to
TEST and observe GO light.
(h)
Antenna switch Select BOT and
repeat step (g).
(i)
Antenna switch Select DIV and
repeat step (g).
(j)
Mode 4 Hold to TEST
and
observe GO light (if code has
been set in external computer).
27.
BATTERY switch As required.
28.
Toilet Check condition.
29.
Emergency equipment Check that all required
emergency equipment is available and that fire
extinguishers and first-aid kits have current
inspection date.
O 30.
Parachutes Check.
8-10. FUEL SAMPLE AND OIL CHECK.
NOTE
Fuel and oil quantity check may be
performed prior to exterior check.
During warm weather, open fuel cap
slowly to prevent being sprayed by
fuel under thermal pressure.
*1.
Fuel sample Check collective fuel sample from all
drains for possible contamination. Thru-flight
check is required only if aircraft has been
refueled.
8-11. EXTERIOR CHECK.
a.
Left Wing Area. Check as follows (fig. 8-1):
1.
Left wing Check.
*a.
General condition Check.
b.
Flaps
Check
for
full
retraction
(approximately 0.25 inch play) and
skin damage, such as buckles, splits,
dents, or distortion.
c.
Fuel sump drains Check for leaks.
d.
Aileron and movable trim tab Check
security and trim tab rig.
e.
Outboard wing fuel vent (in aileron
cove) Check free of obstruction.
f.
Static wicks (4) Check security and
condition.
g.
Wing pod, navigation lights, and
deice boots Check condition and pod
tip latches closed.
h.
Recognition light Check condition.
i.
Outboard antennas Check condition.
*j.
Main tank fuel and cap Check fuel
level visually, condition of seal, and
tap tight and properly installed.
k.
Outboard
deice
boot
Check
for
secure
bonding,
cracks,
loose
patches, stall strip, and condition.
i.
Stall warning vane Check freedom of
movement.
*m.
Tiedown Released.
n.
Inboard dipole antenna sets Check
for security and cracks at mounting
points.
Check bonding secure, boots free of
cuts and cracks.
o.
Wing ice light Check condition.
p.
AC GPU access door Secured.
q.
Recessed and heated fuel vents
Check free of obstructions.
r.
Inverter inlet and exhaust louvers
Check free of obstructions.
2.
Left main landing gear Check.
*a.
Tires Check condition.
b.
Brake assembly Check.
c.
Brake deice assembly and bleed air
hose
Check
for
condition
and
security.
*d.
Shock
strut
Check
for
signs-of
leakage, minimum strut extension
(5.5 inches), and that left and right
strut
extension
is
approximately
equal.
e.
Torque links Check condition.
f.
Safety switch Check condition, wire,
and security.
g.
Wheel,
well,
doors,
and
linkage
Check
8-9