767.200.300

How can the yaw movement be manually controlled?. A. By the control wheels. B. By the rudder pedals. C. By the control columns.

Which of the following are the primary flight controls: A. Speedbrakes, flaps and the yaw damper. B. Aileron, rudder, elevator and spoiler systems. C. Flaps, slats and the horizontal stabilize.

How are the overwing escape slide auto arm/fire switches actuated during door opening?. A. By a proximity sensor when the door handle is rotated. B. By the actuation link when the door moves inward about 1.25 inches. C. By slide pressure when the inflation cylinder activates.

What occurs when both deadbolt handles on the flight compartment door are in the horizontal position?. A. The deadbolt is extended and the door is locked, the key can still unlock the door. B. The deadbolt is retracted and the door is unlocked, the key can lock the door. C. The deadbolt is extended and the door is locked, the key cannot operate the lock.

f both FWD access door and E/E access door are open what is the indication shown on EICAS?. A. "FWD ACCESS DOOR" and "E/E ACCESS DOOR" advisory messages. B. "FWD ACCESS DOOR" and "E/E ACCESS DOOR" caution messages. C. Only one "ACCESS DOORS" advisory message.

Which flight compartment windows contain two temperature sensors?. A. All of them. B. Only windows #1 and #2. C. Only windows #1 and #3.

What care should be taken when the vertical fin internal access door has been removed?. A. Door gasket must be replaced and tested. B. Cabin pressurization test must be carried out. C. Access door must be replaced.

Which material consists of the vertical fin removable leading edge?. A. Aluminium. B. Carbon fiber. C. Fiberglass.

Using the keypad of the flight compartment door, how can a person activate the doorbell function?. A. By pressing the access code followed by "ENT" key twice. B. By pressing and holding the "ENT" key for 3 seconds. C. By pressing key "1" followed by the "ENT" key.

Which unit prevents parallel operation of the two sources on the main buses?. A. Bus tie breaker (BTB). B. Auxiliary power breaker (APB). C. External power contactor (EPC).

What condition will trip GCB (GCR stays closed)?. A. Over voltage. B. EPC request. C. Open phase.

What action is necessary to reset APU's generator GCR trip?. A. Perform APU restart. B. Recycle GEN FIELD pushbutton. C. Recycle GEN CONT pushbutton.

When does the ground handling bus have power?. A. In flight, if main buses do not have power. B. In flight, if APU power is available. C. On the ground, if external power is available.

Which electrical bus provides the power for the main battery charger?. A. Ground service bus when powered. B. Left AC bus when powered. C. Ground handling bus when available.

What does the battery switch connect?. A. Battery to the hot battery bus. B. Hot battery bus to the battery bus. C. DC buses to the battery bus.

What is the time limit for hydraulic motor generator (HMG) operation?. A. 60 min. B. 180 min. C. Unlimited.

During engine start using APU as bleed source how is the load shed of non essential loads control achieved?. A. Load shedding is controlled by BPCU. B. There is no load shedding on engine start with APU. C. Load shedding is controlled by relays.

What unit does turn on the AC CONNECTED light in the external power panel (P30)?. A. Bus power control unit (BPCU). B. Generator Control Unit (GCU). C. External power contactor (EPC).

Which are the hydraulic systems on the B767: A. Left,Center and Right. B. Green, Yellow and Blue. C. System A and System B.

Which system recordss flight parameters on magnetic tape for the purpose of providing information on flight conditions and airplane systems operation for analysis in the event of a crash or accident?. A. The Aircraft Condition Monitoring system. B. The Flight Data Recorder system. C. The Cockpit Voice Recorder system.

How is the landing gear actuation normally powered: A. Electrically, by retraction motors. B. Mechanically, by springs. C. By the hydraulic system.

Where is most of the electronic equipment located?. A. In the ceiling of the aft galley. B. In the main forward cargo compartment. C. In the Main Equipment Center.