HP d212 Manual do Utilizador descarregar pdf (Página 82)

FMS-D212-725-1

Page 3-6

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:

TC Approved Date: 07.06.01

CAUTION

IF CAUSE OF FAILURE IS OBVIOUSLY MECHANICAL, AS

EVIDENCED BY ABNORMAL METALLIC OR GRINDING

SOUNDS, DO NOT ATTEMPT A RESTART.

Procedure:

Note

Minimum rate of descent airspeed of 65 KIAS and will

allow the pilot more time for air start.

1. Collective – Establish autorotative descent

Adjust to maintain N

2. AIRSPEED – Establish 65 KIAS

3. Throttle – Decrease to top of idle stop

4. Fuel – ON

5. START FUEL switch – ON

6. Battery – Verify ON

7. N

– Verify 25% or less

8. Starter switch – Switch to START position.

9. N

and EGT/MGT – Observe for engine start indication.

10. START FUEL switch – OFF at 400°C (MGT or EGT).

11. Starter – OFF at 45% N

12. Throttle – Open slowly to normal operational RPM

13. Engine oil pressure and temperature – Within limits.

14. Generator – RESET, then ON

15. START FUEL switch – ON

16. Land as soon as possible

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HP d212 Manual do Utilizador Página 82