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system exam 767 > exam 767 > Flashcards

exam 767 Flashcards

1
Q

Where are the red anti-collision lights located?

A

On the top and the bottom of the fuselage

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2
Q

Which statement is true regarding the Engine Anti-ice System?

A

The system uses engine bleed air to provide engine cowl inlet ice protection

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3
Q

Why is the right engine bleed air switch turned off as a Non-Normal Checklist procedure after
landing when the right wing anti-ice failed in the open position?

A

To prevent structural damage to the right wing due to overheat

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4
Q

What does the illumination of the Captain Pitot (CAPT PITOT) light on the overhead panel
indicate?

A

A captains pitot probe heat is inoperative

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5
Q

What does the illumination of the VALVE light mean on the Anti-Ice panel

A

The VALVE position disagrees with the switch position

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6
Q

Which of the flight deck windows are electrically heated?

A

All windows as soon as electric power is established

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7
Q

Which statement is true regarding the Wing Anti-Ice system?

A

Bleed air is provided in flight to the three outboard leading edge slats on each wing

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8
Q

What is the flight mode annunciation (FMA) for the roll axis in the Go-Around mode?

A

GA

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9
Q

What indicates that the selected autopilot is engaged?

A

CMD is displayed as the AFDS status Flight Mode Annunciation (FMA)

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10
Q

What does the THR HOLD mode accomplish?

A

Thrust levers remain in existing position or where manually placed

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11
Q

What pitch and roll modes will the flight director (F/D) use if the left autopilot is in command in
flight and both FD switches are OFF and the F/D switches both are positioned to ON?

A

The first F/D switch positioned to ON activates the flight director in the selected autopilot
modes

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12
Q

What happens when you squeeze and pull the Oxygen Mask Release Levers?

A

“Unlocks the oxygen panel doors, releases the mask, and oxygen turns on when the
oxygen panel doors open”

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13
Q

What pitch mode will engage when the first autopilot is placed in the Command with both flight
directors OFF?

A

V/S

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14
Q

What roll mode will engage when the first autopilot is placed in Command with both flight
directors off and wings level?

A

HDG HOLD

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15
Q

Which of the following modes is used to acquire and hold heading shown in heading window
and on a map display heading markers?

A

HDG SEL

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16
Q

What is the function of the Service Interphone (SERV INTPH) Switch?

A

Allows you to add external (unpressurized area) headphone jacks to the cabin
interphone system

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17
Q

What causes the GND CALL light on the Pilot Call Panel to illuminate?

A

A call from ground personnel

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18
Q

What are the controls for the Cockpit Voice Recorder located?

A

On the overhead panel

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19
Q

What is required before the crew can communicate after donning their oxygen masks?

A

Ensure that the oxygen mask microphones are enabled with the BOOM/OXY switch on
the Audio Control Panel (ACP)

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20
Q

What precautions should be taken if a fire extinguisher is to be discharged in the flight deck
area?

A

All flight crew members must wear oxygen masks and use 100% oxygen with emergency selected

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21
Q

What limits are set by the cabin altitude AUTO RATE Control?

A

Cabin Altitude rate of climb and descent limits during auto control

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22
Q

The airplane is climbing through 20,000 ft, airspeed is 290 kts and pressurization is being automatically controlled. What is the cabin altitude rate of change based on?

A

Cabin altitude increases on a schedule related to the takeoff field elevation, airplane altitude, and the selected auto climb limit

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23
Q

“During cruise flight, how many feet must the airplane climb before the cabin altitude begins to climb?”

A

A significant altitude change

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24
Q

“When the cabin altitude AUTO RATE Control is at the index mark, what rate of climb and descent does it establish?”

A

Approximately 500 fpm climb and 300 fpm descent

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25
Q

“When the air conditioning system is operating with the trim air switch off, what temperature
does the packs try to maintain?”

A

Attempts to maintain all compartments at an average temperature

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26
Q

What is the energy source for the flight crew shoulder heaters?

A

Electric heaters in ducts that supply conditioned air

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27
Q

Where is the Audio Control Panel located?

A

On the left and right sidewalls (on the aft aisle stand)

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28
Q

What is accomplished by pushing the AC bus tie switches to AUTO?

A

It arms the automatic AC and DC bus tie circuits and the flight instruments transfer bus Circuits

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29
Q

Each engine has an integrated Drive Generator (IDG). How can the IDG be electrically disconnected from the busses?

A

Pushing the GEN CONT switch to OFF

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30
Q

“On the ground, advancing the thrust levers to the takeoff range with the engines shut down may cause inadvertent load shedding of the utility busses to occur. How do you reset the utility busses?”

A

“Return the thrust levers to IDLE, push the UTILITY BUS switches to OFF, then ON”

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31
Q

What is the electrical configuration during autoland?

A

The busses isolate to allow three independent sources to power the three autopilots

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32
Q

“If both main AC buses are unpowered, the transfer busses are powered by the:

A

Hydraulic Driven Generator (HDG)

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33
Q

“Prior to establishing electrical power, when the battery switch is ON and the standby power selector is in AUTO, what powers the ““standby DC”” bus?”

A

The Main Battery

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34
Q

Which statement is true regarding the Ground Service Bus?

A

Prior to engine start, the ground service bus can be powered only from the APU generator or external source”

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35
Q

The APU starter engages when

A

The APU inlet door is open

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36
Q

What is the maximum altitude for operating the APU?

A

The airplane’s maximum certified altitude

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37
Q

“What is an indication that the Engine Anti-ice is ““on””?

A

TAI ( Thermal Anti-Ice) is displayed in green on EICAS

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38
Q

What thrust reference mode annunciation indicates an assumed temperature takeoff

A

D-TO

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39
Q

APU bleed air is available to an approximate altitude of:

A

17,000 ft

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40
Q

How is the engine oil pressure indication affected when oil pressure reaches the low (minimum) operating limit?

A

Indication changes color to red

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41
Q

When can the reverse thrust levers be raised after touchdown?

A

Only when the forward thrust levers are in the idle (closed) position

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42
Q

What indicates a failure of the engine fire and overheat detection system?

A

The SYS FAIL light illuminates and the EICAS message FIRE / OVHT SYS displays

43
Q

On the FIRE / OVHT test panel, the illumination of the SYS FAIL light indicates a failure in which
of these systems?

A

The APU fire, cargo fire or engine overheat detection system

44
Q

Which system best describes the wheel well fire detection and extinguishing system?

A

There is no fire extinguishing system

45
Q

What is the indication that the APU fire bottle has been discharged or has low pressure?

A

The APU BTL DISCH light illuminates and the EICAS message APU BTL displays

46
Q

What happens when you pull out an engine fire switch?

A

Arms both fire extinguishing bottles

47
Q

The airplane is equipped with a fire extinguishing system for which fires?

A

Engines, APU, and Forward / Aft cargo compartments

48
Q

You have an Engine Fire Warning and pull the respective Engine Fire switch but it won’t come out. What should you do?

A

Push on the respective Engine Override Switch to unlock the Engine Fire Switch

49
Q

What does the rudder trim indicator display?

A

Shows the units of rudder trim commanded

50
Q

Which statements are true regarding the speedbrake lever?

A

On the ground, the speedbrake lever moves to DOWN and all spoiler panels retract if either thrust lever is advanced to the takeoff thrust position

51
Q

What stabilizer trim condition exists when both Stabilizer Trim Cutout Switches are in the CUTOUT position?

A

Hydraulic system power is shut off to both stab trim control modules

52
Q

Roll control is provided by which of the following?

A

Ailerons and spoilers

53
Q

What is the function of rudder ratio changers?

A

Reduce rudder deflection as airspeed increases

54
Q

What does the flap load relief system do if airspeed is excessive?

A

Protects the flaps from excessive air loads

55
Q

What EICAS caution message will display if the flap lever is not in a detent for an extended period of time?

A

TE FLAP DISAGREE

56
Q

When is the EICAS caution message ALT DISAGREE inhibit?

A

At low altitude

57
Q

Which instrument source selector switch controls the source of the Captain’s RDMI heading?

A

The First Officer’s IRS switch

58
Q

What indicates that the Flight Director Pitch and Roll Bars on the ADI are not supplying valid commands?

A

An ‘F/D’ flag in the ADI or disappearance of the respective steering bar/command bars

59
Q

When the Left Instrument Source Selector Panel (lower) AIR DATA Switch is in the ALTN position, it selects the ______ air data computer used.,

A

Right, Captain’s

60
Q

Where is the Decision Height displayed?

A

On the right side of the ADI display

61
Q

During an ILS approach, the crew observes the Radio Altitude display on the ADI change from white to amber. What does this indicate?

A

The airplane is below the selected decision height on a descent

62
Q

What does the FMC alerting message “ENTER IRS POSITION” mean?

A

The IRS is ready to change to navigate mode and has not received a present position entry, or the flight deck crew entered present position did pass one of the IRS
comparison check

63
Q

When LNAV is selected after take off, within which distance from the active leg does LNAV mode engage?

A

2.5 nautical miles

64
Q

A white dashed LNAV route displayed means:

A

The route is activated but not yet executed

65
Q

The FMC alerting message “THRUST REQUIRED” means which of these?

A

VNAV active, autothrottle disconnected and additional thrust required to track VNAV descent path and maintain speed

66
Q

How do you begin the IRS alignment?

A

Rotate the IRS mode selector from OFF to NAV

67
Q

Which statement is true regarding operating in Polar Regions?

A

The FMC switches all flight display inputs to reference true north while in polar regions

68
Q

Regarding operations in Polar Regions, what changes on the HSI if the airplane descends while the heading reference is TRU (true north)?

A

The HSI displays an amber box around the word TRU

69
Q

The EICAS message L FUEL SYS PRESS means:

A

All fuel pumps on the left side have low output pressure and the crossfeed switches are off, or all fuel pumps have low output pressure

70
Q

Where does the fuel quantity data from each tank come from?

A

It is measured by probes in each tank and corrected for density and then displayed on a fuel quantity indicator for each tank

71
Q

When does the DC fuel boost pump in the left main tank operate?

A

When the APU selector is on and AC power is not available

72
Q

After engine start, the FUEL CONFIG EICAS message is displayed. What could be the reason?

A

The center pump switches are off with fuel in the center tank

73
Q

How many AC fuel pumps are in each tank?

A

Two

74
Q

What is the normal sequence for fuel usage?

A

“Center tank fuel first, because two center tank fuel pumps have more output than the main fuel pumps

75
Q

A hydraulic pump ““press”” light illuminates. This means:

A

Pump output pressure is low

76
Q

The Ram Air Turbine powers the flight control portion of which hydraulic system?

A

Center

77
Q

Which of the following indicates a hydraulic pump overheat?

A

An illumination pump overheat (OVHT) light and the associated EICAS message

78
Q

The primary hydraulic system pump on the left and right side is which of these?

A

An engine-driven pump

79
Q

Where is hydraulic fluid quantity displayed?

A

On the Status Display

80
Q

Which statement is true regarding the hydraulic reservoirs?

A

The reservoirs are pressurized by the bleed air system

81
Q

How do you set the parking brake?

A

Depress both pedals fully while simultaneously pulling the parking brake handle up

82
Q

How many degrees can the tiller turn the nose wheel in either direction?

A

65 degrees

83
Q

What is the maximum speed to hydraulically extend the landing gear?

A

270 KTS / .82M

84
Q

With RTO selected prior to takeoff, maximum brake pressure is applied when thrust levers are retarded to the closed or idle position above what airspeed:

A

85 knots

85
Q

How does the landing gear extend into position when using the alternate landing gear extension
system?

A

The landing gear free-fall into position

86
Q

In flight, the landing gear lever lock is automatically released after signals are received from?

A

The air/ground sensing system

87
Q

What is the indication of an EICAS cathode ray tube (CRT) failure?

A

The faulty display is blank

88
Q

What action is required to display the second page of EICAS messages?

A

Push the CANCEL switch

89
Q

What warnings are inhibited during takeoff from rotation to 400’ RA or 20 seconds elapsed time?

A

Both the master WARNING lights and the fire bell

90
Q

How may EICAS events may be recorded with the EICAS event record switch?

A

Only the last EICAS event is recorded

91
Q

When does the Status Cue message appear on the lower EICAS screen?

A

It appears when a new STATUS message exists

92
Q

What is the maximum allowable headwind when landing weather minima are predicated on autoland operations?

A

25 knots

93
Q

When may reverse thrust be used?

A

Reverse thrust is for ground use only

94
Q

Do not engage the autopilot after takeoff below:

A

200 feet AGL

95
Q

Your first action with an engine fire should be:

A

AUTOTHROTTLE ARM Switch - OFF

96
Q

“After attempting to extinguish and engine fire, the engine fire warning light remains illuminated.
What should be your next action:

A

Wait 30 seconds and if engine fire warning light remains illuminated then rotate the engine fire switch in the opposite direction and hold for 1 second

97
Q

“With AUTO selected on the RTS / FSB selector, what condition would cause the fasten seatbelt sign to illuminate?”

A

When the flap handle is moved out of the up position and/or the gear is extended

98
Q

Where can flight crew oxygen pressure be checked from the flight deck?

A

On the lower EICAS status page

99
Q

How can a check of the oxygen pressure located within the secondary oxygen cylinder be accomplished?

A

By pushing the PAX OXY switch on the overhead panel and reading pressure on the EICAS status display

100
Q

When does the Cockpit Voice Recorder system automatically operate?

A

Operates continuously anytime AC power is applied to the airplane

101
Q

With AUTO selected, what condition causes the FASTEN SEAT BELT sign to illuminate?

A

Cabin altitude above 10,000 feet

102
Q

The passenger oxygen system is supplied by which of the following sources?

A

Individual chemical oxygen generators

103
Q

Where is the passenger oxygen switch located?

A

On the overhead panel

104
Q

Where are the controls for the Cockpit Voice Recorder located?

A

On the overhead panel

system exam 767 (1 decks)

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