HP d212 Uživatelský manuál stáhnout pdf (Strana 48)

FMS-D212-725-1

Page 2-4

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: 13.08.09

2.2.1 Takeoff and Landing

Refer to Section 1 for takeoff and landing weight limits and to Section 4 for

takeoff and landing data.

2.2.2 Weight and Balance

Determine proper weight and balance of helicopter as follows:

 Consult applicable weight and balance instructions provided in

Section 5.

 Determine weight of fuel, oil, load etc., compute takeoff and

anticipated landing GW, and check helicopter CG locations.

 Ensure weight and balance limitations in Section 1 are not exceeded.

2.3 Preflight Check

Pilot is responsible for determining whether helicopter is in condition for safe

flight. Refer to Figure 2-1 for preflight check sequence.

Note

Preflight check is not intended to be a detailed

mechanical inspection but a guide to check condition of

helicopter. This check may be made as comprehensive

as conditions warrant.

All areas checked shall include a visual check for

evidence of corrosion, particularly when helicopter is

flown near or over salt water or in areas of high industrial

emissions.

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HP d212 Uživatelský manuál Strana 48