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3. Pilot’s pedal area — Check.
4. Right AFCS yaw ports — Check.
5. Pitot tubes — Check.
6. Antennas — Check.
7. Searchlights — Check.
8. Windshield and wipers — Check.
9. Left AFCS yaw ports — Check.
10. Copilot’s pedal area — Check.
11. Copilot’s jettisonable door — Check.
8-2-14. Left Cabin.
1. Fuselage — Check as other items are
checked.
2. Left electrical compartment — Check.
3. Forward landing gear area — Check condition
and security of all components as follows:
a. Tire.
b. Shock strut for extension.
c. Brakes.
d. Fluid lines.
e. ERFS II refuel valve.
4. Forward and aft cargo hooks — Check hooks
clear and load beam closed. Electrical harTM
1-1520-240-10
8-2-5
ness and release cable connected and dust
caps stowed. If hook not installed, check for
dust caps on the electrical and release cable
receptacles.
5. Lower anti-collision light — Check condition.
6. Static port — Check unobstructed.
* 7. Fuel system — Check as required, caps secure.
O 8. ERFS II Installed. Aircraft Overboard Drain
Outlets — Check. Check for any fuel seepage.
O 9. ERFS II Installed. Aircraft Overboard Vent
Outlets — Check. Check for signs of excessive
fuel venting.
10. NO. 1 Engine.
a. Inlet for foreign objects. Check condition
and security of FOD screens.
O b. EAPS — Check general condition,
check vortex tubes for erosion and damage.
Check seals for condition and
damage. Check rail and slide mechanisms.
Inspect blower fan blades damage
and erosion.
c. Check fuel, oil, hydraulic, electrical, (O)
wash kit, and drain lines connections
and leaks.
d. Cowling for security.
11. Left aft landing gear area — Check condition
and security of all components as follows:
a. Gear support structure.
b. Tire.
c. Shock strut extension and static lock
stowed.
d. Static ground wire contacting the ground.
e. Fluid lines.
f. Electrical wiring.
g. Ground proximity switch and linkage.
h. Brakes.
i. Swivel lock.
12. Vent and fluid drain lines — Check unobstructed.
O 13. M-130 Safety Pin — Installed with streamer.
8-2-15. Top of Fuselage.
* 1. No. 2 engine — Check as follows:
a. Inlet for foreign objects. Check condition
and security of FOD screens.
b. EAPS — Check for foreign objects,
condition and security. Seals around
driveshaft fairing and engine inlet for
damage. Rails and slide mechanisms
for damage.
c. Oil level and cap secure.
d. Cowling for security.
e. Tailpipe condition and security, presence
of fuel, oil, and foreign objects.
2. Anticollision light and formation lights —
Check condition.
* 3. Aft rotor (right side) — Check blades for condition
and reservoir levels.
O 4. Droop stop shrouds — Check condition and
security. Check inspection cover closed.
5. Upper boost actuator — Check for extended
jam indicators and exposed piston rods for
cleanliness.
6. Hydraulic compartment — Check as follows:
a. Condition and security of lines and
coolers.
b. No. 2 flight control system accumulator
for proper indication (see figure 2-15-3).
c. Utility reservoir pressurization accumulator
for 2500 to 3500 psi charge.
* 7. Combining transmission area — Check for
obstructions. Check filter buttons for engines
and combining transmission.
* 8. Aft rotor (left side) — Check blades for condition
and reservoir oil levels.
O 9. Droop stop shrouds — Check condition and
security.
10. Upper boost actuator — Check for extended
jam indicators and exposed piston rods for
cleanliness.
* 11. No. 1 engine — Check, same as NO. 2..
12. Drive shaft area — Check condition and security
as follows:
a. Drive shaft, couplings, and mounts.
b. Fluid lines.
c. Control linkage.
d. Foreign objects.
e. Drive shaft fairing.
* 13. Forward rotor (right side) — Check same as
aft rotor.
14. Forward transmission oil cooler inlet — Check
for obstructions.
TM 1-1520-240-10
8-2-6
15. Upper boost actuator — Check for extended
jam indicators and exposed piston rods for
cleanliness.
16. Forward transmission — Check for foreign objects,
cooler condition, and fluid level..
17. Hydraulic compartment — Check as follows:
a. Condition and security of lines and
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