IF FUEL VENTS OVERBOARD FROM A MAIN FUEL TANK DURING NORMAL FLIGHT OPERATIONS:
a. Perform pressure refueling precheck.
b. Perform pressure check of 2 inch pressure refueling/auxiliary fuel transfer
c. Perform pressure check of vent system for affected tank.
WHEN AN AIRCRAFT HAS BEEN SUBJECTED TO A HARD LANDING OR WHEN EMERGENCY EXIT
LIGHTS (IF INSTALLED) ARE ACTUATED DURING LANDING:
a. Landing gear attachment fittings for misalignment and cracks. Fluorescent
inspect in accordance with TM 1-1500-335-23.
b. Support frames and skin (internal and external) for distortion.
c. Fuselage and transmission support numbers for cracks and distortion.
4, 5, 8
d. No. 1 and No. 2 engine support structure for cracks, distortion, and loose
e. Perform excessive G-Load inspection on engines. Refer to TM
f. Engine mounting pads for cracks and loose bolts.
g. APU support structure for cracks, distortion, and loose rivets.
h. Wheels for cracks and distortion. Fluorescent inspect in accordance with
i. Shock struts for leakage and distortion.
j. Fluorescent inspect shock strut mount fittings for cracks. Refer to TM
k. Tires for damage.
l. Droop stops and hub for distortion.
m. Dynamic absorbers support structure for cracks, distortion, and loose rivets.
n. Fuel pod support structure for cracks and distortion.
o. Perform inspection on crash resistant fuel system (Task 10-4).
WHEN HARD LANDING INSPECTION SHOWS MISALIGNMENT OR CRACKS IN LANDING GEAR, OR
DISTORTION AND/OR LOOSE OR MISSING RIVETS IN SUPPORTING FRAMES OR SKIN:
a. Wheels (disassembled) for cracks. Fluorescent inspect wheel forgings,
welded areas, axles, and attaching bolts in accordance with TM 1-1500-335-23.
Wheel bearings for condition.
b. No. 1 and No. 2 engine supports for cracks. Fluorescent inspect in
accordance with TM 1-1500-335-23.
c. Ramp for proper operation and alignment of pins in sockets.
d. Fuel cells and components for damage and loose attachment fittings (pod