
FMS-D212-725-1
Page 2-28
• COPYRIGHT © 2007 BY DART AEROSPACE LTD •
This document is private and confidential and is supplied on the express condition that it is not to be used for any
purpose or copied or communicated to any other person without written permission from Dart Aerospace Ltd.
Revision:
G
TC Approved Date: 13.08.09
Passenger seat belts – Fastened.
All doors – Secured.
Throttle friction – Apply
Cyclic and collective control – Friction as desired
2.8 Takeoff
Cyclic control – Neutral or slightly into the wind.
Collective – Increase to attain a hover altitude of four feet.
Note
The bleed air heater valve will automatically shut off at high collective. The
heater OFF light will illuminate momentarily as the bleed air valve closes. If
the bleed air valve malfunctions the heater OFF light will remain illuminated.
Pedals – apply pressure to maintain heading.
Cyclic control – Apply forward cyclic to accelerate smoothly while increasing
torque.
For proper maximum torque refer to Power Limits for Takeoff,
Section 1.
Maintain an altitude of 7 ft until 30 kias.
At 40 KIAS, adjust the pitch attitude to attain 65 KIAS and 30
feet AGL.
Adjust power as required up to takeoff power to obtain
necessary rate of climb after obtaining 65 KIAS.
Comentários a estes Manuais