TM 1-1520-240-MTF
2-43
STARTING ENGINES (CONT.)
B* 32. FUEL QUANTITY Indicator — Check as follows.
a. Check individual tank indications coincide
with known contents.
b. Note digital readout remains constant
during individual tank readings.
c. Select TOTAL. Check pointer rotates
behind mask. Check total fuel indicated is
within 420 pounds of known fuel on board.
B* 33. CYCLIC TRIM Indicators — Check both in GND
position.
34. CYCLIC TRIM switch — MANUAL.
a. Check for proper operation and indicator
movement by first retracting the FWD then
AFT actuator into the RET position.
b. Check actuators by fully extending the FWD
and AFT actuator into the EXT range on the
indicator. (Full RET to full EXT not to exceed
25 seconds).
c. CYCLIC TRIM switch — AUTO. Observe
both indicators move from the full EXT
position to the GND position.
BF* 35. Rotor Blades — Check position.
CAUTION
Prior to performing the static flight control
check, be sure that an aft rotor blade is not
within 30_ of the centerline of the fuselage,
since blade-fuselage interference may occur.
In addition, the rotor blades may rotate due to
wind or APU operation.
B* 36. AFCS Check. (Refer to Section IV). Not required
if mechanical rig check is to be performed.
