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AGUSTA A109E - Page 158

AGUSTA A109E
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FTR pushbutton (cyclic) : Trim as desired for attitude ref-
erence changes during hover
and climb out.
RPM switch : Set 100%.
NOTE
RPM shall be set to 102% during take-off and landing in the airspeed
range from 0 knot to 60 knots and in hovering conditions.
NR/N2 speed : 100% stabilized, check.
ROLLING TAKE-OFF
Collective and cyclic : Apply collective and forward
cyclic as necessary to obtain
forward speed on the ground.
Apply collective as necessary
to become airborne. Accelerate
to 60 Knots and to desired
climb.
Tail rotor pitch : Apply as necessary to maintain
direction.
Flight instruments : Check.
Engine instruments : Within limits.
Main hydraulic system instruments : Within limits.
Utility hydraulic system instruments : Within limits.
Landing gear : UP (by 200 ft AGL).
Check light sequence:
- Green light off
- Red light on (retraction)
- Red light off (retracted and
locked)
RFM A109E
2-38 R.A.I. Approved
Rev. 2
UNMAINTAINED COPY