Change 23 3-2.1/(3-2.2 blank)
TM 55-2840-241-23
c. Inspect oil falter for damage.
d. Inspect fuel control assembly for cracked
flanger.
e. Inspect engine mounting pads for cracks.
If cracked engine mounting pads are suspected,
refer to TM 1-1520-254-23, Technical Manual
Aviation Unit Maintenance (AVUM) and
Aviation Intermediate Maintenance (AVIM)
Manual Nondestructive Inspection Procedure
for OH-58 Helicopter Series.
g. Check all accessories for loose bolts,
nuts, and connections
f. Check air, oil, and fuel hose connections
for security.