Module 14 Set-1

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#1. How is fuel flow varied in a variable displacement pressure type pump?

#2. The majority of power in a free turbine engine is used to

#3. Supervisory EEC sends its output to the

#4. A modular constructed gas turbine engine means that

#5. The EEC is powered and able to operate via




#6. E.G.T. thermocouples are usually made of

#7. Propeller speed is measured from

#8. The bleed valve on a engine at start up is

#9. . Modern oil pressure servo transmitters sense

#10. In a FADEC engine with a hydro mechanical fuel system, how is fuel flow controlled?




#11. How does a boost gauge compensate for altitude changes?

#12. Where is EGT measured?

#13. The basic gas turbine engine cycle is

#14. An increase in fuel flow through the impeller type fuel flow transmitter is measured by

#15. The total power in a turboprop engine is the




#16. Manifold pressure is measured

#17. To measure oil temperature, which of the following would most likely be used?

#18. Ratiometer pointer movement is achieved by

#19. On a twin spool engine, the HP compressor is driven by

#20. . The principle of operation of a DC ratio meter is




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