Systems Boeing 737 CL/NG/Max

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Created on By Dan Alexandru Pod

Systems Boeing 737 CL/NG/Max

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1. Which is the minimum altitude at which the autopilot can be engaged after T/O?

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2. Which is the maximum T/O and landing altitude?

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3. Depending on the actual temperature and pressure.
(Classic) Which is the maximum operating altitude?

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4. (NG) Which is the maximum operating altitude?

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5. Which is the maximum tank fuel temperature?

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6. Which is the maximum fuel imbalance for all the phases of flight?

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7. During engine start when is MaxMotoring reached?

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8. If the Left DUCT OVERHEAT light illuminates on the B737-300/500 aircraft:

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9. The Re-circulating Fan operates with the switch in the AUTO position except:

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10. The cabin Altitude Warning horn will:

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11. The AUTO FAIL light will illuminate when there is:

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12. NG the maximum differential pressure is:

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13. The OFF SCHED DESCENT light illuminates if:

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14. Which A/T modes permit manual thrust changes without A/T interference?

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15. Which flight modes will be annunciated when the autopilot is initially engaged in the CMD mode and both F/D’s are OFF?

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16. Which of the following occurs during a single Autopilot ILS approach and the TO/GA switch is pressed for a missed approach at minimums?

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17. Which is the minimum altitude (AGL) to engage the second A/P to execute a dual channel A/P approach?

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18. What is indicated by a blank IAS/MACH window on the MCP while in flight?

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19. The cockpit voice recorder uses a:

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20. The GRD CALL switch on the Fwd. Overhead panel when pressed?

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21. The MASK-BOOM switch allows selection of the oxygen mask microphone or the boom microphone. The MASK-BOOM switch does not affect the operation of the hand microphone?

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22. The AC STANDBY BUS power can be supplied from:

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23. The STANDBY PWR OFF light (amber) illuminated. What happened?

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24. In flight, both engine generators fail, the APU generator should be connected to?

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25. The blue GRD POWER AVAILABLE light when illuminated indicates:

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26. NG ELEC light means:

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27. NG the STANDBY POWER OFF light illuminates if there is no power to either:

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28. The passenger oxygen system is activated when the cabin reaches an altitude of:

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29. The cockpit door blow-out panels:

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30. The NO SMOKING signs when selected to AUTO:

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31. With the oxygen NORMAL/100% selector in the N (normal) position:

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32. The crew oxygen Flow Indicator will:

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33. The lavatory fire extinguisher system will automatically discharge when heat levels exceed?

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34. With the OVHT DET switch in the B position:

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35. Holding the TEST switch to the FAULT/ INOP position?

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36. Pulling the engine fire switch up will closes the hydraulic fluid shutoff valve.

The engine driven hydraulic pump LOW PRESSURE light will be deactivated.

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37. During an OVHT/FIRE test the No 1. Fire Handle light and associated overheat light do not illuminate indicating:

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38. The power source for the Engine Fire Extinguishing system is the (NG):

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39. The APU horn in the main wheel well can be silenced by:

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40. Positioning the Yaw Damper switch to ON?

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41. Loss of hydraulic system B pressure:

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42. The LE FLAPS TRANSIT amber light on the center instrument panel:

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43. Auto Slat operation can be monitored:

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44. The Ground Spoilers are powered by:

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45. The auto slat system is armed:

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46. An alternate source of power for Auto slat operation is:

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47. In the event of a runaway stabilizer, first:

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48. The elevator Feel Differential Pressure light illuminated indicates that there is:

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49. The LE FLAPS TRANSIT light will illuminate when:

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50. In the event of total hydraulic power failure, rotation of the pilots' control wheels mechanically positions the:

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51. In the event of jammed aileron system, rotation of the co-pilot's control wheel operates the:

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52. Fuel Quantity indicators will display:

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53. When the APU is inoperative and no external power is available, refueling can be accomplished as follows:

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54. To defuel No. 1 tank:

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55. The Fuel Temperature Indicator reads the temperature of the fuel in:

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56. The Centre Tank Fueling Valve Position light on the External Fueling Panel is:

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57. The External Fueling Panel is located:

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58. Each fuel tank contains:

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59. A digital fuel quantity indicator has an accuracy of

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60. The fuel quantity indicators require:

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61. If the center tank is scheduled to contain more than 453 Kgs then:

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62. For the center tank Scavenge Jet Pump to operate:

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63. With the Fuel LOW Alert displayed (amber) what is the fuel quantity?

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64. The Fueling Valve Position Lights from the External Fueling Panel when illuminated blue:

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65. A leak in the hydraulic system B engine driven pump or its associated lines would be indicated by:

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66. If a total failure of both pumps supplying system B pressure occurs, which of the primary flight controls will be totally inoperative?

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67. The A and B hydraulic reservoirs are pressurized by:

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68. The standby hydraulic pump only supplies pressure to the following:

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69. Hydraulic system A power sources are:

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70. Pulling NO.1 Engine Fire switch will:

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71. Minimum fuel for ground operation of electric motor-driven pumps is:

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72. When does the RF symbol next to the quantity indicator appear?

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73. Can you perform an Autoland approach in case of Loss of System A and B?

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74. For pressurization and servicing, the stby System Reservoir:

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75. How can you recognize foaming?

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76. What is the normal precharge of Hydraulic brake pressure indicator?

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77. What is the purpose of the Landing Gear transfer unit?

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78. If a No.1 window outer pane cracks:

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79. Thermal air for wing anti-icing is obtained from:

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80. The right No.2 window heat is supplied from which circuit?

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81. The COWL ANTI-ICE light when illuminated indicates:

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82. The Flight Director Comparator monitors:

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83. The underspeed symbol in the MCP Speed window is a:

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84. What is the minimum Mach number that can be selected in the IAS/MACH display of the MCP panel?

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85. When using manual extension to extend the landing gear, what should you do?

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86. How should you be doing the Pushback if the nose gear lockout pin is not installed?

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87. Rudder pedal steering is:

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88. The autobrake system is armed:

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89. Selecting the Nose Wheel Steering switch on the Captain's Instrument panel to ALT provides the:

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90. After manual extension of the landing gear, the indication on the flight deck that the correct procedure has been carried out is:

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91. Placing the Lights Est Switch to the TEST position inhibits what?

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92. If you have a failure of one main A.C. bus, this causes:

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93. When ARMED, the emergency exit lights will automatically be active:

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94. The emergency exit lights and signs are powered from:

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95. A flashing IRS ALIGN light indicates:

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96. Selecting an IRS mode selector from OFF to ALIGN will initiate:

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97. While in flight the right IRS DC FAIL amber light (only) illuminates indicating that:

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98. The REF NAV DATA pages allow the crew to inhibit:

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99. The Message UNABLE NEXT ALTITUDE means:

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100. The Message TAI ON ABOVE 10° means:

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101. The left IRS is normally powered by:

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102. The right IRS in normally powered by:

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103. When the IRS mode selector is turned OFF, how many minutes does the IRS remain powered?

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104. Normal pressure of the flight crew oxygen system is:

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105. The passenger oxygen mask stowage units are activated:

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106. In each lavatory there is:

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107. The engine bleed valves are:

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108. The amount of fan air that is ducted through the pre-cooler is controlled by the:

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109. Where is the water tank indicator located?

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110. The water system is pressurized by:

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111. The maximum aircraft altitude for APU electrical load is:

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112. When does the APU fuel solenoid valve open?

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113. The APU Electrical Generator and APU Oil Cooler are cooled by:

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114. How long is the maximum APU start cycle?

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115. The Proximity Switch Electronic Unit (PSEU) light illuminates:

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116. EGPWS terrain display changes from dotted to solid yellow:

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117. The weather radar automatically begins scanning for windshear when:

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118. The PSEU light is inhibited:

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119. If the E&E compartment external access door is left open, will the pilot have any indication in the cockpit?

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120. The FMC Climb Phase begins at thrust reduction altitude and is terminated at which point?

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121. Actual navigation performance represents the estimated maximum position error with percentage probability of:

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122. If a return to land is necessary after take off, the following FMC requirement is necessary:

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123. If the ANP exceeds the RNP value, the following message will appear on the CDU scratch pad:

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124. The transition Altitude of the PERF INT PAGE:

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125. What does MOD on the RTE legs page indicate?

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126. The purpose of the Fix INFO page is to:

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127. The FMC gets position information from:

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128. The FMC Advisory Message Buffet ALERT indicates:

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129. What information is available with the IRS mode selector in ATT?

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130. LNAV automatically disconnects when:

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131. What is the aircraft's source of attitude and heading information?

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132. During a DUAL Channel ILS approach, at which RADIO ALTITUDE should the FLARE mode engage?

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133. What pitch mode is annunciated after take off when the auto-pilot is first engaged in CMD?

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134. When are the GPWS windshear warnings available?

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135. On takeoff the configuration warning sounds. What can be the cause?

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136. Which following systems are not monitored by the PSEU?

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137. How can you silence the Mach/Airspeed warning inflight?

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138. Which of the following will illuminate a landing gear configuration warning?

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139. When GPWS provides the aural alert BANK ANGLE, BANK ANGLE the alert is silent for that bank angle until the system is reset by decreasing the bank angle to ...... degrees or less?

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140. Which of the following is NOT a GPWS mode?

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141. The Predictive Windshear alerts are issued:

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142. Engine warm up recommendations for B 737 Max?

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143. After take off how do you position the Landing Gear Lever?

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144. What is the exhaust velocity for B Max 8/-9?

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145. How is working the Emergency Descent Speedbrakes (EDS) new function included for MAX?

How do the Emergency Descent Speedbrakes (EDS) work? (new function included for MAX)

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146. When the MAX REVERSE warning is enforced:

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147. What is the Tail Radius for Boeing 737 MAX-8?

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148. Where is Bleed Air obtained from in the Boeing 737 MAX?

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149. (B 737 MAX) Eng-ANTI ICE light illuminates:

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150. Starter Cutout N2 % is ...... and Normal Starter Duty Cycle is ...... for the B 737 MAX.

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