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Module 14 Set-1 | DGCA MODULE

Module 14 Set-1

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#1. Propeller speed is measured from

#2. Where is EGT measured?

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

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

#5. The basic gas turbine engine cycle is




#6. . Modern oil pressure servo transmitters sense

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

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

#9. A modular constructed gas turbine engine means that

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




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

#12. Manifold pressure is measured

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

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

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




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

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

#18. Ratiometer pointer movement is achieved by

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

#20. Supervisory EEC sends its output to the




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