
FMS-D212-725-1
Page 3-4
• 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
consideration is to ensure the survival of the occupants. Landing in water,
trees or other unsafe area should be considered only as a last resort.
Following terms are used to describe operating condition of a system,
subsystem, assembly, or component:
AFFECTED – Fails to operate in intended or usual manner.
NORMAL – Operates in the intended or usual manner.
3.3 Engine
3.3.1 Engine Failure
3.3.1.1 Engine Failure – Hovering
Indications:
1. Left Yaw
2. ENGINE RPM warning lights illuminated (N
2
below 89 ± 1%)
3. ROTOR RPM caution lights illuminated (N
R
below 97%)
4. Rotor RPM audio tone
5. ENG OIL PRESS and DC GENERATOR caution lights may be
illuminated
Procedure:
1. Maintain heading and attitude control.
2. Collective – Adjust to control N
R
and rate of descent.
Increase prior to ground contact to cushion landing.
Note
The magnitude and rate of collective movement is a
function of height above ground. Any forward airspeed
will aid in ability to cushion landing.
3. Land.
4. Complete shut down.
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