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