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Module 8 Set-7 | DGCA MODULE

Module 8 Set-7

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#1. LANDING SPEED IS ____________ WHEN FLAP & SLAT IS OPEN

#2. WHEN BANKING ON A TURN STALLING SPEED IS ________________ THEN WHEN LANDING.

#3. THE INCREASE IN LIFT TENDS TO ______________ THE GLIDE ANGLE.

#4. THE STEEPER THE ORIGINAL GLIDE THE GREATER THE CHANGE IN FLIGHT PATH INVOLVED AND SO THE MORE SPEED MUST BE THERE IN HAND FOR _____________

#5. AFTER FLATTENING OUT WE MUST LOSE ANY EXCESS SPEED THIS MAY CALLED ___________




#6. THE GLIDING PATH IS FLATTER SO THERE IS ______________ CHANGE OF PATH IN FLATTENING OUT AND SO.

#7. IN STRAIGHT AND LEVEL FLIGHT WHEN CRUISING POWER REQUIRED CURVE AND POWER AVAILABLE CURVE ARE PERPENDICULAR IS ________________

#8. DURING TURN, THE OUTER WING OFFERS MORE __________

#9. WHEN ENGINE FAILURE OCCURS AND LIFT IS FORWARD OF THE WEIGHT THEN _________________

#10. HIGHER WEIGHT IN GLIDING FLIGHT IS NOT AFFECTED BY ___________




#11. DURING FLAT TURN ____________

#12. IN CASE OF A/C NOSE DROP THRUST LINE IS PLACED __________ AND DRAG LINE IS ____________

#13. DURING TURN STALLING ANGLE _________

#14. DURING TAKE OFF BEFORE PULLING OFF __________

#15. SPEED OF SOUND AT MEAN SEA LEVEL _____________




#16. PERFORMANCE CAPABILITY OF JET ENGINE WITH PROPELLER IS DEPENDS ON ______________

#17. PERFORMANCE CAPABILITY OF JET ENGINE IS DEPENDS ON _____________

#18. IF LANDING SPEEDS GO UP WITH ____________ WING LOADING

#19. A SLIGHT INCREASE IN THE ______________ TO USE FOR CLIMBING.

#20. FOR EQUILIBRIUM LEVEL FLIGHT ____________




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