OBJECTIVE CESSNA 172

 

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#1. Ignition operation is controlled by rotary switch which is controlled by

render function for question type not found

#3. Oil pressure gauge markings

#4. Examination of fuel in the system for contamination

#5. Weak intermittent firing with puffs of black smoke is caused by

#6. There was an obvious power loss when the ignition switch was momentarily turned from “Both” to “Left.” The cause is

#7. To apply parking brake

#8. The VSI depicts

#9. The engine-driven vacuum system provides

#10. The center area of the instrument panel contains

#11. The center area of the instrument panel contains

#12. In a long flight, the maximum deviation in the compass due to precession error is

#13. For maximum cabin heat

#14. Stall warning is activated

#15. ELT annunciator does not activate on

#16. Oil pressure should register in cold weather within

#17. In the event of the alternate static door opening

#18. Propeller ground clearance

#19. Minimum turning radius of A/C

#20. Abrupt use of controls is prohibited beyond

#21. Yellow arc of ASI

#22. Minimum oil pressure of A/C

#23. The alternator should be switched off in the event of an ammeter reading

#24. Compass error of up to 25° may occur in the event of the alternator

#25. D.G.I (or compass) has to be aligned regularly on a long flight for

#26. Maximum window open speed

#27. Maximum oil pressure

#28. Unusable fuel quantity in each tank

#29. Maximum ramp weight is

#30. Maximum slip duration with one tank dry

#31. Color of 100LL (Low Lead) fuel

#32. Minimum oil quantity for extended flights is

#33. Concentration in fuel of DiEGME (Diethylene Glycol Monomethyl Ether)

#34. Concentration in fuel of isopropyl alcohol

#35. Which oil is to be used after 50 hours of engine running or when the oil consumption has stabilized

#36. Maximum deflection of the nose wheel by use of the rudder pedal on the ground is

#37. Mechanical stops on flaps are

#38. Best rate of climb speed at sea level is

#39. Shock absorption on the nose wheel

#40. Shock absorption on the main wheel

#41. If the engine floods

#42. Standard temperature lapse rate

#43. Starter cycle for engine is

#44. Enroute climb speed is 5 to 10 knots above best rate of climb speed for

#45. Until 50 hours have been accumulated, the engine should be run at

#46. An open alternate door will result in

#47. Carburetor icing is indicated by

#48. Nose gear shock strut pressure

#49. Outside air temperature (OAT) / voltmeter gauge select switch may be used by putting the select button down for

#50. If the PTT button of the microphone is kept pressed for more than 33 seconds continuously, the transmission is

#51. In Voltmeter/OAT/CLOCK, pushing the upper control button will change the display on the window to

#52. Maximum fuel capacity of each tank

#53. Spark plug fault causes

#54. Magneto malfunction causes

#55. Brake of the A/C

#56. Tyre pressure of nose wheel tyre

#57. Propeller diameter

#58. Engine model number

#59. Tyre pressure of main wheel tyre

#60. Nosewheel strut length

#61. Standard empty weight of A/C

#62. Baggage compartment contains

#63. Max useful load of A/C

#64. Wing loading of A/C

#65. Power loading of A/C

#66. Wing area of A/C

#67. Elevator span of an A/C

#68. Wheelbase length of A/C

#69. Horsepower rating & engine power

#70. Propeller model no. of A/C

#71. Airspeed when fails after takeoff

#72. Landing with a flat main tire, flaps will be

#73. Landing with a flat nose tire, flaps will be

#74. Engine failure during takeoff roll, the first action will be

#75. If fire occurs during start on ground, the throttle & mixture will be

#76. Descending through clouds to go around against spiral dive and to minimize compass card swings due to changing bank angle

#77. The magneto check should be made

#78. The A/C is equipped with

#79. The electrical system of A/C is powered by

#80. The desired vacuum range of an A/C is

#81. The communication receiver transmitter receives & transmits signals

#82. The navigation receiver receives VOR & Localizer signals

#83. A/C has clock model

#84. The clock of an A/C combines the feature of

#85. Takeoff speed for normal climb

#86. Enroute climb at sea level airspeed is

#87. Engine manufacturer of an A/C

#88. Engine type of A/C

#89. MIL-L-6082 or SAE J1966 Aviation Grade Straight Mineral Oil is used

#90. At sea level, best rate of climb speed is

#91. At 10,000 ft, best angle of climb speed is

#92. Landing approach speed

#93. Max oil temp

#94. Max flap extended speed of A/C

#95. Vne of A/C

#96. Max structural cruising speed of A/C

#97. Which of the following statement is incorrect

#98. While ditching

#99. The set of radius contains

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