HP d212 Manual do Utilizador Página 63

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FMS-D212-725-1
Page 2-19
• 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
2.5 Engine Start
Note
The T5317A engine utilizes EGT and the T5317B/BCV
engine utilizes MGT. The limitations for EGT and MGT
are significantly different. Therefore, ensure the proper
limitations are utilized during start and flight.
2.5.1 Engine Start – Battery or Ground Power Unit
Rotor Blades – Clear.
LH and RH BOOST PUMP switches – ON. Verify LH FUEL BOOST and RH
FUEL BOOST caution lights – Extinguish
ENGINE FUEL VALVE – ON. Verify FUEL VALVE caution light illuminates
momentarily, then extinguishes. Verify increase of fuel pressure on Fuel
Pressure Indicator.
START FUEL switch – ON.
Throttle – Check travel, cushion and idle stop. Rotate throttle above idle
stop. Press Idle Stop Release button and position throttle slightly below IDLE
detent.
Note
Battery starts can be made when voltage less than 24
volts is indicated, provided voltage is not below 14 volts
when cranking through 10 percent N
1
speed.
START switch – Select switch to START, start timing.
Main rotor – Check main rotor is turning by 15% N
1
. If rotor is not turning,
abort start.
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