HP d212 Manual do Utilizador Página 53

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FMS-D212-725-1
Page 2-9
• 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
2
nd
tail rotor driveshaft compartment – Check.
Fire extinguisher bottle – Check for proper pressure.
Engine exhaust – Cover removed; unobstructed
All access doors – Secured
Fuselage – Condition.
Drain lines – Clean, unobstructed.
Oil cooler blower exhaust – Unobstructed.
5. AREA 5 – TAILBOOM LEFT SIDE
Tail rotor driveshaft covers – Secured.
Tailboom – Condition
Elevator – Condition and security
CAUTION
DO NOT BEND ELEVATOR TRAILING EDGE TAB.
Main rotor blade – Verify tie down removed.
6. AREA 6 – TAILBOOM AFT
Antennas – Condition and security (if installed)
Tail rotor blades – Visually check condition and cleanliness.
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