HP d212 Manual do Utilizador Página 112

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FMS-D212-725-1
Page 4-5
• 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
PSI (95.5%)) is no less than the chart maximum torquemeter pressure (52.0
PSI (93.4%)) the maximum torquemeter pressure available is satisfactory.
The recorded N
1
RPM shall be plus or minus 0.5 percent of the placarded
Maximum Gas Producer Speed for Takeoff Power. (This is N
1
topping.)
If this check is satisfactory, it can be concluded that the installed engine is at
least as good as a minimum specification engine and that full power can be
obtained. If this check is not satisfactory, there is reason to believe that the
engine has deteriorated to the extent that published performance may not be
obtained. If this occurs, the cause of the deterioration should be determined.
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