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Old 10th Jul 2011, 13:58
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truefaith
 
Join Date: Feb 2011
Location: Macau - Hong Kong SAR
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Question
Can somebody enlight me? Is it correct?

Q1. The reason for the reduction in thrust setting with increase in altitude is:
(a) increase in TAS for samw as IAS

Q2. For a given engine RPM and gas temperature at sea level and ISA conditions:
(c) fuel delivery from the burners is greatest

Q3. Taking air from compressor for pressurisation and engine deicing will result in:
(a) high EGT and high specific fuel consumption

Q4. Engine running at constant RPM for a free turbine engine the RPM:
(a) cannot be increased
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