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#1. TYPE OF INLET DUCT USE IN GAS TURBINE ENGINE _______________
#2. CORROSIVE TYPE OF COMPOUND ARE WHICH TYPE OF PRODUCT ?
#3. PRESSURE RELIEF VALVE SYSTEMS
#4. THE BASIC PARAMETER FOR DESCRIBING THE FUEL ECONOMY OF THE AIRCRAFT ENGINE _____________
#5. PURPOSE OF EEC
#6. TURBOSHAFT PREFERRED WHERE REQUIRED IS OF _______________
#7. TURBOJET ENGINE PRODUCE BY ______________
#8. WHICH TYPE DUCT HAVE A BELL SHAPE FUNNEL HAVING CAREFULLY ROUNDED SHOULDER WHICH OFFER PRACTICALLY NO AIR RESISTANCE ?
#9. IN CAN TYPE COMBUSTION CHAMBER THE AIR ENTER THROUGH THE ____________
#10. WHICH TYPE FILTER USE JUST BEFORE OIL PASS FROM THE SPRAY NOZZLE ON TO THE BEARING SURFACE __________
#11. THERMAL EFFICIENCY IS DEPENDS ON ________________________
#12. VAPOUR LOCK IS DUE TO _____________
#13. VAPOUR LOCK ?
#14. THE THRUST OF GAS TUBINE ENGINE ________________
#15. WHICH TYPE OF ENERGY EXTRACT BY TURBINE ?
#16. THE ABILITY OF AN ENGINE TO RUN SMOOTHLY AND GIVE DESIRED PERFORMANCE AT ALL SPEED FROM IDLING TO FULL POWER OUTPUT ?
#17. IN TURBOPROP ENGINE CONSTANT RPM IS FUNCTION OF ____________
#18. THE THRUST OF ENGINE CALCULATED BY ____________
#19. THE POWER PRODUCED BY A TURBINE ENGINE DEPENDS ON __________
#20. TO PREVENT SEIZURE OF CASE AND TURBINE
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