HP d212 Manual do Utilizador descarregar pdf (Página 56)

FMS-D212-725-1

Page 2-12

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

Anti-collision light – Condition and security.

Engine air intake – Cover removed. No damage or obstruction.

Main driveshaft and flexture – Condition, security.

Hydraulic reservoirs – Caps secured.

Transmission oil filler cap – Secured.

Hub and sleeve assembly – Check condition.

Main rotor and controls – Condition and fluid levels in dampers (2)

Main rotor pitch links – Security and condition.

Rotor blades – Visually check condition and cleanliness.

Engine and transmission cowling – Secured.

Antenna(s) – Condition and security.

2.4 Interior and Pre-start Check

Main rotor and tail rotor tie-down – Stowed properly.

Pitot tube cover – Stowed properly.

Engine inlet and exhaust covers – Stowed properly.

Cabin interior – Cleanliness and security of equipment.

Cargo and baggage (if applicable) – Check security

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HP d212 Manual do Utilizador Página 56