737 Theory

With A/T engaged, what condition could cause the throttles to be separated (not aligned)?

One EEC in ON, one EEC in ALTN. One engine A/T suffering a system fault. Both EECs in ALTN. Throttle stagger cannot occur with A/T engaged as both throttle servo motors work identically to position the throttles symmetrically. 3 / 15

How can the Emergency Exit Lights be illuminated?

By lifting the guard and pushing the ON switch located on the AFT attendant panel. If the three position switch located on the FWD overhead panel is selected to ON. Automatically if the three position switch located on the FWD overhead panel switch is in the ARMED position and electrical power to DC Bus 1 fails or if AC power turned off. All of these answers are correct. 4 / 15

How are the Engine Bleed Air valves powered?

They are pneumatically activated and AC operated. They are DC activated and pneumatically operated. They are pneumatically activated and DC operated. They are AC activated and pneumatically operated. 6 / 15

Following an unpressurised takeoff, when is the first engine bleed switch positioned to ON?

Prior to 400 ft above the ground. At not less than 400 ft, and prior to 2000 ft above field elevation. After the gear is up and obstacle clearance has been achieved. After passing through 2000 ft above the ground. 8 / 15

What are the 737-800s maximum latitude certifications?

All of these answers are correct. Above 82N or below 82S Above 72N or below 50S. All latitudes 9 / 15