General Technical Knowledge

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Quizzes Created: 2 | Total Attempts: 206
| Attempts: 80 | Questions: 200
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1. 47572
What is the purpose of fitting the engines to an aircraft using wing mounted pylons?
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General Technical Knowledge - Quiz

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2. 52748 In an aircraft having a battery of 24 volts nominal and fully charged the voltmeter would read:
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3. 52877 The purpose of an inverter is:
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4. 53262  In a turbo charger; which item controls the MAP?
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5. 53094  The electromagnetic brake on an actuator is only energized:
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6. 47716 The purpose of a reservoir is:
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7. 52745 A battery is checked for serviceability by:
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8. 52876 Where the aircraft's main electrical supply is A.C; DC requirements are met by:
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9. 45940  Shock-induced seperation of airflow occuring symmentrically near the wing-root of a swept-back wing; may result in:
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10. 52756 When the battery master switch is switched off in flight:
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11. 45922 Vle is defined as:
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12. 47062  What is the free stream MACH number which produces first evidence of local sonic flow?
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13. 47063  What is the movement of the center of pressure when the wingtips of a swept wing airplane are shock-stalled first?
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14. 52753 The electrolyte used in an alkaline battery is a diluted:
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15. 52882 The basic principle of operation of a 3 phase induction motor is:
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16. 47549 For a multi-engine aircraft; V MCG is defined as the minimum control speed on the ground with one engine inoperative. The aircraft must be able to:
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17. 47708 The purpose of an accumulator is to:
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18. 48404 Fuel tank booster pumps are:
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19. 52746 The specific gravity of a fully charged lead acid cell is:
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20. 47541 Skidding outward in a turn is caused by
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21. 52752 The electrolyte used in the lead acid cell is diluted:
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22. 52884 In a synchronous motor; the rotor is:
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23. 47044  Which factor has the effect of increasing V1 speed?
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24. 47101  A cargo aircraft loaded to maximum takeoff gross weight of 75;000 kgs is out of the aft CG limit. How many 24 kgs boxes must be moved from the 1;200' station to the 710' station to move the CG forward 3.1 inches?
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25. 53283 The optimum angle of attack for a propeller-blade is:
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26. 47395 [Refer to the attached figure] Which aircraft has the highest aspect ratio?
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27. 47537 During a turn the lift force may be resolved into two forces; these are
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28. 48398 The aircraft cannot be refuelled while:
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29. 52750 The nominal voltage of an alkaline cell is:
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30. 45950  In a turbojet engine the turbine's purpose is to:
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31. 47603  Thrust is being managed to maintain desired indicated airspeed and the glide slope is being flown. Which of the following is the recommended procedure when you observe a 30 kt loss of airspeed and the descent rate increases from 750 ft/min to 2;000ft/min?
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32. 47431 Formation of ice on the wing leading edge will:
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33. 52853 An aircrafts constant frequency supply is maintained at:
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34. 52886 A squirrel cage rotor:
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35. 53223 When the mixture lever is at the idle cut-off position:
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36. 52743 Battery capacity percentage efficiency must always be:
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37. 52887 A starting circuit for a powerful single phase induction motor might be:
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38. 45908 The trimming devices on a particular airplane include trailing edge tabs on the rudder and on the right aileron, operated by the pilot. If the airplane is trimmed to a more nose-right and right-wing up position:
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39. 48397 During fuel jettison; the aircraft is protected against running out of fuel by:
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40. 45956 What is the difference between turbine fuel jet A and A1?
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41. 46558 If during a descent the static line becomes blocked; the ASI will:
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42. 47437 Sweepback on a wing will
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43. 47446 In a 30 Degrees bank level turn; the stall speed will be increased by:
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44. 47544 An increase in airspeed while maintaining a constant load factor during a level; coordinated turn would result in
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45. 45924  The cabin pressure control setting had a direct effect upon the:
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46. 48396 Baffles are fitted in aircraft fuel tanks:
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47. 50281 During the starting; the engine should be stopped if:
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48. 45946  The purpose of flight spoilers is to...
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49. 47443 The input data to a stall warning device [e.g. stick shaker] system is
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50. 48045 Mach number is:
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51. 47037 An airplane loaded at its aft CG limit; [in comparison to the same airplane if loaded at its fwd CG limit]; will have which effects on the longitudinal static stability and longitudinal controllability?
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52. 47052  Why must angle of attack be increased during a turn to maintain altitude?
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53. 47429 For an aircraft with a 1g stalling speed of 60 kt IAS; the stalling speed in a steady 60 Degrees turn would be:
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54. 48435 מהן פעולותיך במקרה של אובדן מנוע חלקי אשר ההמראה מבוצעת ממסלול קצר
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55. 47036  How does heavy rain affect airplane performance in flight?
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56. 47433 The stalling speed of an aeroplane is most affected by:
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57. 48426 Failure of an aircraft generator is indicated by:
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58. 47436 On a highly tapered wing without wing twist the stall will commence:
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59. 53088  Capacitive reactance is the:
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60. 48401A 'wide cut' fuel is:
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61. 52851 Warnings of C.S.D.U. oil overheat are given in the cockpit by:
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62. 52880 A synchronous motor runs at a speed that depends upon the supply:
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63. 52879 Reversing two phases to a three phase motor will:
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64. 47600  Which of the following would be acceptable techniques to minimise the effects of a windshear encounter?
  1. 1. To prevent damage to the engines; avoid the use of maximum available thrust.
  2. 2. Increase the pitch angle until the stick shaker activates; then decrease back pressure to maintain that angle of pitch.
  3. 3. Maintain a constant airspeed.
  4. 4. Use maximum power available as soon as possible.
  5. 5. Keep to noise abatement procedures.
  6. 6. Wait until the situation resolves itself before taking any action.
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65. 47026 When considering air density:
  1. 1 -Density is measured in millibars
  2. 2 -Density increases with increasing altitude
  3. 3 -If temperature increases the density will increase
  4. 4 -As altitude increases; density will decrease
  5. 5 -Temperature decreases with increasing altitude; this will cause air density to increase
  6. The combination of correct statements is:
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66. 47434 Stalling may be delayed to a higher angle of attack by:
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67. 48436 מהן פעולותיך במצב של אובדן מנוע חלקי כאשר יש לפניך מסלול ארוך
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68. 52881 If one phase of the supply to a three phase motor fails; then:
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69. 47426 If the aircraft weight is increased without change of CG position; the stalling angle of attack will:
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70. 47074  What is the purpose of a servo tab?
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71. 50293  The micro-switch incorporated in the throttle quadrant activates a warning horn in flight under the following conditions:
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72. 47439 A rectangular wing; when compared to other wing planforms; has a tendency to stall first at the
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73. 47123  When considering the effect of changing angle of attack on the pitching moment of an aerofoil; which of the following statements is correct:
  1. 1 -At 'normal' angles of attack the pitching moment is nose up.
  2. 2- The pitching moment about the aerodynamic centre [AC] is constant at 'normal' angles of attack.
  3. 3 -The aerodynamic centre [AC] is located approximately at the 25% chord point.
  4. 4 -The moment about the aerodynamic centre [AC] is a product of the distance between the aerodynamic centre [AC] and the centre of pressure [CP] and the magnitude of the lift force.
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74. 47575 If flutter is experienced during flight; the preferable action would be
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75. 47714 Fluid level in a reservoir will; when pressurised:
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76. 47046  What true airspeed and angle of attack should be used to generate the same amount of lift as altitude is increased?
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77. 53271  A ground boosted turbocharger is designed to:
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78. 47424 An aeroplane will stall at the same:
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79. 46639  If the sub-scale of an altimeter which reads 1;500 FT is changed from 1;006 MB to 998 MB. What will be the new reading if 1MB=27FT?
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80. 47447 Heavy rain can increase the stall speed of an aircraft for which of the following reasons?
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81. 47035  Which is an effect of ice; snow or frost formation on an airplane?
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82. 47445 High speed buffet [shock stall] is caused by:
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83. 45954  How does compressor RPM affect the output of a turbofan engine?
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84. 47440 Vortex generators are used
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85. 45920 What effect; if any; does CG location have on Vmc?
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86. 47090  Refer to figures 76; 79 and 80]. What is the CG in inches AFT of datum for a loading conditions WT-4?
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87. 53307  What visual indication is given to show that the thrust reverses are correctly stowed?
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88. 53235 To prevent a loss of power when the throttle is opened rapidly; the carburtor may include:
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89. 45918  Vmc for a propeller driven airplane; is defined as:
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90. 47081  What is the primary function of the leading edge flaps in landing configuration during flare before touchdown?
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91. 50314  During single engine operation; when using fuel from tank on the side opposite the operating engine; fuel system management should be as follows:
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92. 45925  If cabin ROC is too great; how should the pressurization control be adjusted?
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93. 48402Fuel is heated:
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94. 52878 Synchronous motors are usually supplied by:
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95. 47432 Dividing lift by weight gives:
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96. 47720 A hand pump is usually fitted :
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97. 52716 Electro-motive force is measured in:
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98. 47041 What effect would a change in ambient temperature or air density have on gas turbine engine performance?
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99. 47042  A turbofan engine with a high bypass ratio; means:
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100. 47428 The angle of attack at which an aeroplane stalls:
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101. 52751 The specific gravity of a fully charged alkaline cell is:
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102. 52885 An induction motor has:
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103. 47039  Vr may not be less than:
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104. 47448 If the tailplane is supplying a download and stalls due to contamination by ice:
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105. 48400 The fuel cross feed valves are fitted in order to facilitate:
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106. 48419 When a generator is on line and its associated ammeter reads 10 amps; this is an indication of:
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107. 46651  The radio altimeter in an aircraft indicates:
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108. 47701 The pressure gauge of an hydraulic system provides information regarding the pressure of:
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109. 52672 A Reverse Thrust Warning Light illuminates:
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110. 52704 The unit measurement of electrical resistance is:
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111. 52737 Battery voltage is tested with:
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112. 52883 In an induction motor:
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113. 47438 Slots increase the stalling angle of attack by:
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114. 45955  What is meant by ESHP in turboprop engine?
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115. 47430 For an aircraft in a steady turn the stalling speed would be:
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116. 47707 A high pressure hydraulic pump
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117. 45975 An aircraft has the following weight data:
  • Basic operating weight: 68200 kgs
  • MZFW: 106600 kgs
  • MLDWT: 120400 kgs
  • MTOWT: 154500 kgs
  • Fuel tank load: 46400 kgs
  • Estimated fuel burn en-route:35300 kgs
  • Fuel burn in start + taxi: 500 kgs
  • What is the maximum payload under these conditions?
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118. 47069  Why do some airplanes equipped with outboard/inboard ailerons use the outboards for slow flight only?
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119. 47507 The purpose of a trim tab is:
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120. 48383 A pressurisation system works by:
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121. 47055  What is the relationship of the rate of turn with the radius of turn with a constant angle of bank but increasing airspeed?
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122. 52781 A free power turbine:
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123. 52860 In a Star wound three phase system:
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124. 53310  The propulsive thrust of a gas turbine is produced by:
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125. 47573 Controls are mass balanced in order to:
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126. 52668 Use of reverse thrust below the recommended speed may cause:
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127. 52842 An AC generator's I.D.U. oil system:
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128. 47061  What is the highest speed possible without supersonic flow over the wing?
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129. 48326 If flaps are lowered during the take-off run:
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130. 48361An elevon is:
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131. 47343 What true airspeed and angle of attack should be used to generate the same amount of lift as altitude is increased:
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132. 47450 When flaps are lowered the stalling angle of attack of the wing:
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133. 52784 EPR is a:
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134. 47349 What effect would a light crosswind have on the wingtip vortices generated by a large aeroplane that has just taken off:
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135. 48359 Aileron reversal would be most likely to occur:
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136. 48378 During a normal pressurised cruise; the discharge valve position is:
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137. 52854 A frequency wild alternator must be:
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138. 49724 Before a cargo change is made; the following information is known about an airplane:Aircraft weight 165;000 lbCG 30.5 percent of MACLength of MAC 860.2 to 1040.9 inIf 5;000 pounds of cargo is added to an average location of station 680.0; what is the new CG relative to MAC
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139. 47499 A horn balance on a control surface is:
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140. 52780 Nozzle guide vanes are fitted before the turbine:
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141. 45931  Why do some airplanes; equipped with inboard and outboard ailerons; use the outboard ailerons for slow flight only?
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142. 47085  What is the maximum allowable payload under the following conditions?
  • Basic operating weight 100;500 kgs
  • MZFW 138;000 kgs
  • MLDWT142;000 kgs
  • MTOWT184;200 kgs
  • Fuel tank load 54;000 kgs
  • EST. fuel Burn EN-ROUTE 40;000 kgs
    • Fuel for start + taxi 500 kgs
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143. 47045  What will be the ratio between airspeed and lift; if the angle of attack and other factors remain constant and airspeed is doubled?
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144. 53226  If carburator heat is selected density will:
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145. 48451 A three phase AC system can be used to supply:
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146. 47059  What characteristic should exist; if an airplane is loaded to the AFT limit of ITS CG range?
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147. 47080  The primary purpose of high-lift devices is to increase the:...
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148. 47120  When the angle of attack of a positively cambered aerofoil is increased; the centre of pressure will:
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149. 52783 The net operating temperature of a gas turbine engine is limited by:
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150. 52681 The power supply for the spark in the combustion chamber is:
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151. 48448 To ensure correct load sharing on paralleled alternator:
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152. 47339 Which of the following statements is correct:
  1. 1.To generate a constant lift force; any adjustment in IAS must be accompanied by a change in angle of attack.
  2. 2. For a constant lift force; each IAS requires a specific angle of attack.
  3. 3. Minimum IAS is determined by CL MAX.
    1. 4. The greater the operating weight; the higher the minimum IAS.
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153. 48376 With the QFE set on the cabin controller; against an altitude of zero
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154. 48399 De-refuelling fuel:
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155. 52785 In a high by pass engine whose fan max rpm is 20000rpm; when turning at 5000rpm will develop approx.
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156. 45926  While cruising at 300 mb and maintaining a 10000 feet cabin altitude; what is the approximate differential pressure? [10000 feet is 693 mb]
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157. 47070  For which purpose may flight spoilers be used?
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158. 47398 [Refer to the attached figure] Consider only aspect ratio [other factors remain constant]. Which aircraft will generate greatest lift?
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159. 47489 The secondary effect of yawing to left is to
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160. 48403 What is the function of a collector tank [feeder box]
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161. 52848 Oil for the operation of a C.S.D.U. is:
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162. 49722 Before a cargo change is made; the following is known about an airplane:Aircraft weight 250;000 lbCG 30.5 percent of MACLength of MAC station 763.0 to 1035.3If 5000 pounds of cargo is removed from an average location of station 1010.0; what is the new CG relative to MAC ?
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163. 47591   Takeoff power is being delivered by all engines and the take-off is proceeding normally; the undercarriage has just retracted. Which initial indications may be observed when a headwind shears to a downdraught?
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164. 47511 On a servo tab operated elevator; if the pilot's control column is pushed forward in flight:
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165. 48372 A/C in level flight; if cabin altitude increases does pressure diff:
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166. 52673 The low energy ignition system would be used:
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167. 47083  Which is a purpose of leading edge slats on high performance wings?
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168. 52649 The By-Pass Ratio of an engine is the ratio of:
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169. 49730 A cargo airplane loaded to a maximum takeoff gross weight of 165;000 pounds is tail heavy. How many 50 pounds boxes must be moved from station 1200.0 to station 710.0 to move the CG forward 3.2 inches?
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170. 50308  If the engine is being feathered; the pilot must be sure:
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171. 47594  What is the expected duration of an individual micro burst?
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172. 48360 The control surface which gives longitudinal control is
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173. 48381 If pressure is manually controlled:
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174. 52845 In the event of a mechanical malfunction of the alternator:
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175. 47401 With reference to the attached figure; the type of flap illustrated is a
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176. 52648 Gas turbine engine efficiency increases with:
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177. 52789 From a standing start with an increase in forward speed jet thrust will:
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178. 52680 The rate of discharge of a High Energy Ignition Unit is:
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179. 47407 Which statement is true relative to changing angle of attack?
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180. 47715 The purpose of a reservoir is to
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181. 48380 When air is pressurised; the % oxygen:
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182. 52677 A high energy ignition system works on the principle of:
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183. 47506 The purpose of a spring tab is:
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184. 47569 The maximum allowable airspeed with flaps extended [VFE ] is
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185. 52839 Paralleled alternators will have:
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186. 52653 In a by-pass engine; the by-pass air:
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187. 48443 The number of separatre stator windings in an AC generator determines:
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188. 47567 The speed VNE is:
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189. 52788 As temperature _____ air density _____ and the mass of air for given enginespeed _____ therefore thrust _____. To maintain the compressor speed however _____ fuel must be added or the compressor will _____.
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190. 52675 Precautionary use of igniters may be necessary during:
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191. 49915  In a cable control system cables are tensioned to:
  1. 1. Remove backlash from the control linkage.
  2. 2. Provide tension on the turnbuckle.
  3. 3. Provide positive action in both directions.
  4. 4. Ensure the full range is achieved.
    1. 5. Compensate for temperature variations.
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192. 47025 With increasing altitude; up to about 40;000 ft; the characteristics of air change:
  1. 1 -Temperature decreases continuously with altitude
  2. 2 -Pressure falls steadily to an altitude of about 36;000 ft; where it then remains constant
  3. 3 -Density decreases steadily with increasing altitude
  4. 4 -Pressure falls steadily with increasing altitude
  5. The combination of true statements is:
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193. 52655 During the Brayton cycle; combustion takes place:
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194. 52747 A lead acid battery voltage should be checked:
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195. 47087  [Refer to figures 76; 79 and 80]. What is the CG in percent of MAC for a loading conditions WT-1?
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196. 50284  When the CO2 emergency gear extension system control is pulled; the landing gear control on the selector valve must be:
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197. 47738 A nose wheel steering control system:
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198. 47088  [Refer to figures 76; 79 and 80]. What is the CG in inches AFT of datum for a loading conditions WT-2?
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199. 53229 Throttle icing is formed when:
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200. 52782 Blade creep is:
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47572...
52748 In an aircraft having a battery of 24 volts nominal and...
52877 The purpose of an inverter is:
53262  In a turbo charger; which item controls the MAP?
53094  ...
47716 The purpose of a reservoir is:
52745 A battery is checked for serviceability by:
52876 Where the aircraft's main electrical supply is A.C; DC...
45940  ...
52756 When the battery master switch is switched off in flight:
45922 Vle is defined as:
47062  ...
47063  ...
52753 ...
52882 The basic principle of operation of a 3 phase induction...
47549 ...
47708 The purpose of an accumulator is to:
48404 Fuel tank booster pumps are:
52746 ...
47541 Skidding outward in a turn is caused by
52752 ...
52884 In a synchronous motor; the rotor is:
47044  Which factor has the effect of increasing V1 speed?
47101  ...
53283 The optimum angle of attack for a propeller-blade is:
47395 ...
47537 ...
48398 The aircraft cannot be refuelled while:
52750 The nominal voltage of an alkaline cell is:
45950  In a turbojet engine the turbine's purpose is to:
47603  ...
47431 Formation of ice on the wing leading edge will:
52853 An aircrafts constant frequency supply is maintained at:
52886 A squirrel cage rotor:
53223 When the mixture lever is at the idle cut-off position:
52743 Battery capacity percentage efficiency must always be:
52887 ...
45908 The trimming devices on a particular airplane include trailing...
48397 ...
45956 What is the difference between turbine fuel jet A and A1?
46558 ...
47437 Sweepback on a wing will
47446 ...
47544 ...
45924  ...
48396 Baffles are fitted in aircraft fuel tanks:
50281 During the starting; the engine should be stopped if:
45946  The purpose of flight spoilers is to...
47443 ...
48045 Mach number is:
47037 An airplane loaded at its aft CG limit; [in comparison to the...
47052  ...
47429 ...
48435 ...
47036  ...
47433 The stalling speed of an aeroplane is most affected by:
48426 Failure of an aircraft generator is indicated by:
47436 ...
53088  Capacitive reactance is the:
48401A 'wide cut' fuel is:
52851 ...
52880 ...
52879 Reversing two phases to a three phase motor will:
47600  ...
47026 ...
47434 Stalling may be delayed to a higher angle of attack by:
48436 ...
52881 ...
47426 ...
47074  What is the purpose of a servo tab?
50293  ...
47439 ...
47123  ...
47575 ...
47714 Fluid level in a reservoir will; when pressurised:
47046  ...
53271  A ground boosted turbocharger is designed to:
47424 An aeroplane will stall at the same:
46639  ...
47447 ...
47035  ...
47445 High speed buffet [shock stall] is caused by:
45954  ...
47440 Vortex generators are used
45920 What effect; if any; does CG location have on Vmc?
47090  ...
53307  ...
53235 ...
45918  Vmc for a propeller driven airplane; is defined as:
47081  ...
50314  ...
45925  ...
48402Fuel is heated:
52878 Synchronous motors are usually supplied by:
47432 Dividing lift by weight gives:
47720 A hand pump is usually fitted :
52716 Electro-motive force is measured in:
47041 What effect would a change in ambient temperature or air density...
47042  A turbofan engine with a high bypass ratio; means:
47428 The angle of attack at which an aeroplane stalls:
52751 ...
52885 An induction motor has:
47039  Vr may not be less than:
47448 If the tailplane is supplying a download and stalls due to...
48400 The fuel cross feed valves are fitted in order to...
48419 ...
46651  The radio altimeter in an aircraft indicates:
47701 ...
52672 A Reverse Thrust Warning Light illuminates:
52704 The unit measurement of electrical resistance is:
52737 Battery voltage is tested with:
52883 In an induction motor:
47438 Slots increase the stalling angle of attack by:
45955  What is meant by ESHP in turboprop engine?
47430 ...
47707 A high pressure hydraulic pump
45975 An aircraft has the following weight data: ...
47069  ...
47507 The purpose of a trim tab is:
48383 A pressurisation system works by:
47055  ...
52781 A free power turbine:
52860 In a Star wound three phase system:
53310  The propulsive thrust of a gas turbine is produced by:
47573 Controls are mass balanced in order to:
52668 Use of reverse thrust below the recommended speed may cause:
52842 An AC generator's I.D.U. oil system:
47061  ...
48326 If flaps are lowered during the take-off run:
48361An elevon is:
47343 ...
47450 ...
52784 EPR is a:
47349 ...
48359 Aileron reversal would be most likely to occur:
48378 ...
52854 A frequency wild alternator must be:
49724 ...
47499 A horn balance on a control surface is:
52780 Nozzle guide vanes are fitted before the turbine:
45931  ...
47085  ...
47045  ...
53226  If carburator heat is selected density will:
48451 A three phase AC system can be used to supply:
47059  ...
47080  ...
47120  ...
52783 ...
52681 The power supply for the spark in the combustion chamber...
48448 To ensure correct load sharing on paralleled alternator:
47339 ...
48376 ...
48399 De-refuelling fuel:
52785 In a high by pass engine whose fan max rpm is 20000rpm;...
45926  ...
47070  For which purpose may flight spoilers be used?
47398 ...
47489 The secondary effect of yawing to left is to
48403 What is the function of a collector tank [feeder box]
52848 Oil for the operation of a C.S.D.U. is:
49722 ...
47591   ...
47511 On a servo tab operated elevator; if the pilot's...
48372 ...
52673 The low energy ignition system would be used:
47083  ...
52649 The By-Pass Ratio of an engine is the ratio of:
49730 ...
50308  ...
47594  ...
48360 The control surface which gives longitudinal control is
48381 If pressure is manually controlled:
52845 In the event of a mechanical malfunction of the...
47401 ...
52648 Gas turbine engine efficiency increases with:
52789 ...
52680 The rate of discharge of a High Energy Ignition Unit is:
47407 Which statement is true relative to changing angle of...
47715 The purpose of a reservoir is to
48380 When air is pressurised; the % oxygen:
52677 A high energy ignition system works on the principle of:
47506 The purpose of a spring tab is:
47569 The maximum allowable airspeed with flaps extended [VFE ] is
52839 Paralleled alternators will have:
52653 In a by-pass engine; the by-pass air:
48443 The number of separatre stator windings in an AC...
47567 The speed VNE is:
52788 ...
52675 Precautionary use of igniters may be necessary during:
49915  ...
47025 With increasing altitude; up to about 40;000 ft; the...
52655 During the Brayton cycle; combustion takes place:
52747 A lead acid battery voltage should be checked:
47087  ...
50284  ...
47738 A nose wheel steering control system:
47088  ...
53229 Throttle icing is formed when:
52782 Blade creep is:
Alert!

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