STATUS messages are checked during prefight to assess acceptability of the air plane TRUE FALSE.
After the engine start, it is not necessary to check the STATUS page, as any message having an adverse effect on the safe continuation of the flight, requiring crew attention, will appear in the upper EICAS. TRUE FALSE.
When using autothrottles, approach speeds corrections for wind are not required, as sufficient gust protection is available with autothrottle engaged by using Vref + 5 TRUE FALSE.
Main wheel braking is automatically applied when the landing gear lever is placed in the UP position after takeoff. TRUE FALSE.
The B-767-200 has a tailskid TRUE FALSE.
What are the electrical power sources for pressurization control? A. Left AC # 1 automatic. right, AC # 2 automatic and standby DC for manual. B. Left AC # 2 automatic. right, AC # 1 automatic and standby DC for manual. C. Standby DC for manual and standby for both automatics.
The CABIN ALTITUDE light will illuminate when: A. The cabin altitude climbs above 8.500 ft. B. The cabin altitude climbs above 10.000 ft. C. The cabin altitude climbs above 14.000 ft.
What does the AUTO INOP light indicate? A. Both auto pressurization controller have failed B. Manual has been selected C. Either A or B above.
If FWD EQPT COOLING message does not extinguish, how long can you operate avionics and electrical equipment NOT on standby busses? A. 30 minutes B. 60 minutes C. 90 minutes D. They are subject to imminent failure.
What equipment cooling situation causes the ground crew horn to sound? A. Smoke in the exhaust duct B. An inoperative skin heat exchanger C. Equipment cooling overheats and OVRD is selected on the ground.
What is a possible cause for only a PACK OFF EICAS message? A. The pack trip has occurred B. The pack control selector is OFF C. Loss of air to the pack D. All of the above.
In flight how does the STBY position affect the equipment cooling system? A. Changes source of air outside supply B. Use the supply fan instead of the exhaust fan C. Shut off the airplane skin-heat exchanger.
Will the auto land mode activate with only the flight director ON? A. YES B. NO.
What occurs when the autothrottle switch is moved to OFF? A. Power is removed from the autothrottle servo system B. A/T can only be engaged in certain modes C. A/T can be engaged in any mode.
Which mode is affected by the bank limit selector? A. All roll modes B. Only HDG select C. Only LOC and APP modes.
To confirm that particular AFDS mode is armed you would observe one of the following? A. The Sitch flow bar is iluminated B. The mode indicated in the FMA is white C. The mode indicated in the FMA is green .
In order for land 3 to be active, which of the following events must have occurred? A. RA must be 1500' or less B. GS and LOC must be capture C. Both A and B.
What does the THR HOLD mode accomplish? A. Moves the throttles to hold takeoff N1 (or EPR) B. Moves the throttles to hold selected speed C. Removes power from the autothrottle servo system.
When the left autopilot is in command, what mode will the flight directors use? A. Whatever modes are selected for them independently B. The left FD will use the same modes as the A/P. The others will use whatever is selected for them. C. All FD's will use the same modes as the engaged A/P.
When go-around mode is deactivated (for example 400' AGL), which autopilot will remain engaged? A. Left autopilot B. First autopilot placed in CMD C. Last autopilot laced in CMD .
Which controls do the autopilot use to track the localizer in the ROLL-OUT mode? A. Rudder and Nose wheel sterring B. Only Rudder C. Only nose wheel steering.
When the Go-Around mode is engaged, the autothrottle? A. Advances the thrust lever to CLB thrust B. Annunciate SPD in the ADI C. Control thrust to maintain a 2.000 FPM climb rate.
What happens to APU fault light when the APU selector is placed to ON or START? A. Comes on until the fuel valve is open B. Remains out until an APU malfunction C. Comes on until the fuel valve and inlet door are open.
what is the minimum power needed to start and operate the APU? A. APU battery only B. APU and main battery C. APU battery and ground handling busses.
What is cut off first when the APU selector is moved off? A. Fuel B. Bleed Air C. Generator output.
The APU selector is moved from OFF to START and place to ON. When does the starter engage? A. Immediately B. When the fuel valve is opened C. When the inlet door has opened.
What does the APU FUEL VALVE advisory EICAS message mean? A. The fuel valve did not close B. The fuel valve is not in the commanded position C. The fuel valve did not open.
With the APU operating what happens when the FAULT light illuminates? A. A normal shutdown sequence starts B. The shutdown immediately C. The APU FUEL VALVE EICAS message also illuminates.
Which of the following describes the START position of the APU Selector? A. Momentary. Returns to ON when released B. Latched. Remains in START until moved C. Magnetically held until starter cutout.
Where is the switch that returns on to the cockpit GROUND CALL light? A. APU ground control B. FWD Cabin attendant panel C. AFT Cabin attendant panel.
Can communication with a cabin attendant be established using an oxygen mask microphone? A. Yes B. No .
How is operation of the oxygen mask microphone verified during the oxygen mask/regulator and microphone check? A. By the sound of oxygen flowing through the mask heard on the flight interphone system B. By removing the mask and speaking through the microphone over the flight interphone system C. By the sound of a fixed pitch tone heard when the PTT button is pushed.
When is the flight data recorder (FDR) automatically activated? A. After both engines are started or inflight B. After either engine is started or inflight C. After ACARS out tune is recorded.
How is the flight recorder manually activated A. Move flight recorder switch to normal B. Move flight recorder switch to ON C. Push OFF light.
A generator DRIVE light can indicate a high or low drive output RPM A. TRUE B. FALSE.
What normally powers each UTILITY BUS? A. The respective main AC BUS only B. The respective main AC or opposite UTILITY BUS only C. The respective main AC, opposite UTILITY or AC BUS.
The APU can be used to power the L AC BUS while the right engine generator is powering the R AC BUS A. TRUE B. FALSE.
The BUS tie system parallels engine generator but prevents any other source from being paralleled A. TRUE B. FALSE.
The APU can be used to power the L AC BUS while external power is powering the R AC BUS A. TRUE B. FALSE.
Which BUS is powered automatically when external power is plugged in? A. STANDBY AC B. GROUND SERVICE BUS C. GROUND HANDLING BUS .
What has the highest automatic priority on the L AC BUS? A. APU generator B. External Power C. Left engine driven generator.
With the APU supplying electrical power, what happens when the first engine is started? A. The engine powers both AC buses B. The engine powers its respective buses obly C. Nothing happens until the APU is shutdown.
The APU is powering the buses. What would pushing the external power switch accomplish? A. Arm external to power the buses when the APU is shutdown B. Turn off the external AVAIL light to enable unplugging external power C. Trip off the APU and power buses from external power.
What bus powers the fire extinguisher? A. HOT BATTERY BUS B. BATTERY BUS C. STANDBY DC.
To what bus is the utility bus connected when the utility bus switch in ON? A. respective main AC bus B. Opposite utility bus C. External power.
With APU supplying both electrical and pneumatic power, what happens as the first engine is started? A. Both utility buses trip off B. Only the respective UTILITY bus trip off C. No UTILITY buses trip off because external power is available.
When can the GROUND HANDLING BUS be powered? A. Only on ground B. Only when the APU is running C. Either on the ground or in flight.
Three autopilots are armed for a triple channel approach at 1200 feet radio altitude. The left generator fails and as a result the L AC BUS fails A. TRUE B. FALSE.
What is required to allow the captain FLIGHT INSTRUMENT TRANSFER BUS to transfer with the loss of the L AC BUS? A. Only the LEFT BUS TIE switch mus be in AUTO B. Only the RIGHT BUS TIE switch mus be in AUTO C. Both the LEFT and RIGHT BUS TIE switch must be in auto.
Which of the following arms the load shed system to trip off both UTILITY BUSES with the loss of generators? A. Both engine generator breakers close B. Airplane is in flight C. Both engine generators DRIVE lights extinguished.
In-flight the left generator trip off. What electrical buses are lost? A. Only the respective UTILITY BUS B. Only the two UTILITY buses and the gallery buses C. Both UTILITY buses and the R DC BUS .
What is accomplished by pushing the AC BUS TIE switch to AUTO? A. Close the BUS TIE breaker B. Open the BUS TIE breaker C. Arm the automatic operation of the BUS TIE breaker.
What does the external power AVAIL light indicate A. Only the external power is plugged in B. External power quality is acceptable C. External power is in use on the main airplane buses.
When does the UTILITY BUS OFF light illuminates A. Only when the switch is off B. Whenever the bus is unpowered C. Only when the switch is on and the bus is unpowered.
With the BUS TIE switch in AUTO, what causes the BUS TIE ISLN light to illuminate? A. Open BUS TIE breaker B. BUS TIE fault C. Closed BUS TIE breaker.
What does the generator control OFF light indicate? A. Bus tie breaker open B. Generator breaker open C. Respective AC bus not powered.
Pushing the generator control switch to OFF opens the generator breaker A. TRUE B. FALSE.
Pushing the generator control switch to OFF reset the fault trip circuitry A. TRUE B. FALSE.
Pushing the generator control switch to OFF causes the generator control OFF and generator DRIVE light to illuminate A. TREU B. FALSE.
What causes the STANDBY power bus OFF light to illuminate? A. Battery charger failure B. Loss of left system power to STANDBY buses C. Loss of power on either the STANDBY AC or DC BUS.
The OFF position on the STANDBY power selector de-energizes the BATTERY BUS, STANDBY AC BUS, and STANDBY DC bus. A. TRUE B. FALSE.
The normal source of power for the L BUS (AC) is the : A. Left generator B. Left inverter Left bus tie.
The normal source of power for the STBY DC bus is the: A. Hot battery bus B. Left DC bus C. Battery bus.
The DRIVE light on GEN DRIVE DISC indicates A. High oil temperature B. Low pressure C. Either or both of A and/or B.
What is the alternate source of power for STBY AC? A. Right AC bus B. Left AC bus C. Battery bus (through an inverter).
Can a chemical oxygen generator be shut off after it is activated? A. Yes B. No.
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