CBT 2

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1. When does the amber dual bleed light illuminate?
- a. When the APU Bleed Valve is open and the No.1 Engine bleed valve is closed.
- b. When the APU Bleed Valve is open and the No.1 Engine bleed valve is on.
- c. When the APU Bleed Valve is open and the No.2 Engine bleed valve is on and the isolation valve is open.
- d. Both B and C are correct.
- d. Both B and C are correct.
2. During flight Auto-Fail light illuminate on pressurization panel. Which statement is correct?
- a. Both pressure controllers have failed. You must manually control the pressurization system.
- b. The primary controller has failed. You must select alternate mode to extinguish the auto-fail light.
- c. The alternate pressure controller has failed. Action is not necessary.
- d. None of above.
- a. Both pressure controllers have failed. You must manually control the pressurization system.
3. During cruise, it becomes necessary to divert to an alternate airport. What must be done to the pressurization system?
- a. Adjust the flight altitude.
- b. Adjust the landing altitude.
- c. Change to alternate mode.
- d. Change to manual mode.
- b. Adjust the landing altitude.
4. Illumination of an Amber Cowl Anti Ice light indicates;
- a. An over pressure condition.
- b. An over temperature or over pressure condition.
- c. The respective Cowl Anti Ice valve is open.
- d. The respective Cowl Anti Ice valve is in transit, the cowl anti ice valve position disagrees with respective engine anti ice switch position.
- a. An over pressure condition.
5. The R Elev Pitot light is illuminated. What does this indicate?
- a. The right elevator pitot is blocked.
- b. System B Hydrolic pressure is low.
- c. The right elevator pitot is not heated.
- d. None of the above.
- c. The right elevator pitot is not heated.
6. The engine anti ice should be turned on ..
- a. Anytime if there is visible moisture.
- b. If the temperature is 10C or less and there is visible moisture.
- c. If the temperature is 10C or more and there is visible moisture.
- d. All above correct.
- b. If the temperature is 10C or less and there is visible moisture.
7. Radio altitude is displayed:
- a. On the PFD when below 1500 feet AGL.
- b. On the PFD between DA/(DH) and 2500 feet AGL.
- c. On the PFD when below 2500 feet AGL.
- d. On the ND when below 2500 feet AGL.
- c. On the PFD when below 2500 feet AGL.
8. The landing gear is normally extended and retracted by which hydrolic system?
- a. A Hyd. Syst.
- b. B Hyd. Syst.
- c. STBY Hyd. Syst.
- d. A and STBY Hyd. Syst.
- a. A Hyd. Syst.
9. What is the maximum airspeed for retracting landing gear?
- a. 235 KIAS
- b. 270 KIAS
- c. 320 KIAS
- d. 250 KIAS
- a. 235 KIAS
10. The Cockpit voice recorder (CVR) switch_________.
- a. When the switch in "Auto" position, powers the cockpit voice recorder from first engine start until 5 minutes after last engine shut down.
- b. When the switch in "ON" position, trips the switch to the "Auto" position after the first engine start.
- c. Position of the switch is in the center instrument paneld. Both A and B are correct.
- d. Both A and B are correct.
- d. Both A and B are correct.

Author

seafire

327492

Card Set

CBT 2

Description

Boeing

Updated

2017-01-18T11:09:15Z

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