HP d212 Manual do Utilizador Página 52

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FMS-D212-725-1
Page 2-8
• 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
Searchlight and landing light – Stowed
Antennas – Condition and security.
Cargo mirror (if installed) – Secure and clean.
Copilot chin window – Check for FOD and clean.
Left static port – Unobstructed.
3. AREA 3 – FUSELAGE LEFT SIDE
Copilot door – Condition and operation; windows clean. Check security of
emergency release handles.
Fuselage – Check condition of skin.
Position lights – Security and condition.
Passenger door – Check condition and operation; glass clean. Condition of
pop-out windows.
Left hydraulic reservoir – Visually check fluid level
Engine compartment – Check fuel and oil lines and connections for condition,
security and leaks.
Engine components – General condition.
Access doors and engine cowling – Secured.
4. AREA 4 – FUSELAGE – AFT LEFT SIDE
Avionics compartment – Security of components.
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