Module 14 Set-1

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

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

#3. . Modern oil pressure servo transmitters sense

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

#5. Where is EGT measured?




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

#7. Propeller speed is measured from

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

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

#10. Ratiometer pointer movement is achieved by




#11. A modular constructed gas turbine engine means that

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

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

#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. Supervisory EEC sends its output to the

#17. The basic gas turbine engine cycle is

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

#19. Manifold pressure is measured

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




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