SKV Flashcards

1
Q

What is the electrical power output of the engine starter/generator?

A

235Vac

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2
Q

What is the minimum pavement width required for a 180 degree turn for 787-8 aircraft?

A

138 feet 4 inches (42.2 meters)

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3
Q

In which lateral mode(s) of the AFDS does the bank limit selector operate?

A

HDG SEL or TRK SEL

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4
Q

When are fuel balance operations inhibited?

A

When a center tank pump is ON

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5
Q

What is displayed by the weather radar within 40 miles?

A

Turbulence

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6
Q

What does the flight director guidance cue of the 787 HUD indicate?

A

Flight director pitch and roll steering commands

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7
Q

What does the left hydraulic system power?

A
  • Flight controls
  • Left engine thrust reverser
  • Right and Left wing spoilers
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8
Q

What information requires re-entry after a complete loss of FMC electrical power?

A

Performance data displayed on the PERF INIT page

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9
Q

When does LNAV activate during a go-around with autopilot engaged?

A

At 200FT radio altitude

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10
Q

What is the primary source of power for the flight control electronics?

A

Three PMGs

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11
Q

Where is the list of aircraft systems affected by load shedding shown?

A

The electrical synoptic

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12
Q

What are the landing altitude selection limits?

A

2000ft below Sea Level to 14000ft above Sea Level

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13
Q

What does the EICAS message RADIO TRANSMIT CA/FO/OBS indicate?

A

A microphone switch is on and has caused a radio to transmit for 30 seconds or more

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14
Q

At what IAS does the auto-throttle annunciation change to HOLD during takeoff?

A

80KT

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15
Q

What indicates that SATCOM control functions are active?

A

Displayed with a caret

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16
Q

What is the function of the aft external power system?

A

To assist the forward system when starting the right engine with external power

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17
Q

What does the VSD display for approaches with a designated glidepath angle?

A

A dashed line that extends 10NM for situational awareness anchored to the missed approach point

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18
Q

When is flap and slat extension inhibited on the 787-9?

A

At greater than 260 KIAS or greater than 20,000 ft

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19
Q

What provides validation that the FMC values are correct regarding the stabilizer takeoff trim green band?

A

Information from the two nose gear pressure transducers

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20
Q

Which statement is correct regarding the audio control panel (ACP)?

A

The MIC/Interphone switch is spring loaded to the center OFF position

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21
Q

What information is displayed on the B787 Auxiliary (AUX) display?

A

The aircraft TAIL and SELCAL numbers on the Flight Data Block

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22
Q

With WX+T selected, turbulence is displayed at _____ NM at all ranges.

A

40 NM

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23
Q

What does the TAMS display indicate on the PFD?

A

Minimum control speed for a large thrust asymmetry

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24
Q

What is the backup power source with loss of electrical power to Captain’s and First Officer’s flight instruments?

A

Ram Air Turbine (RAT)

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25
Q

What information is displayed when the status (STAT) Display Key is pushed?

A

Hydraulic, APU, Oxygen System and liquid cooling fluid indications and status messages

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26
Q

Which flight control surfaces provide roll control in the B787?

A
  • Ailerons
  • Flaperons
  • Spoilers
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27
Q

Which systems have fire detection and fire extinguishing systems?

A
  • Engines
  • APU
  • Cargo compartments
  • Lavatories
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28
Q

What does the NORMAL MODE ROLL CONTROL do?

A

Automatically positions the ailerons, flaperons, and spoilers for commanded roll maneuver

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29
Q

What occurs when the Alternate Gear switch is selected DOWN?

A

Releases all door and gear uplocks

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30
Q

What is the symbol for the BARO Minimums Pointer on the HUD?

A

A green triangular bug and line on the altitude scale

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31
Q

Which statement about HUD takeoff is correct?

A

Selecting HUD takeoff departure in the FMC enables guidance and sets HUD TO/GA as the active FMA roll mode

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32
Q

How many hydraulic systems does the B787 have?

A

Three independent 5000 psi hydraulic systems

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33
Q

What does the upper line and lower line of the altitude window in the mode control panel display?

A
  • Upper line: Selected altitude
  • Lower line: Uplinked ATC altitude target
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34
Q

What provides power to the 28 Vdc system?

A

The 235Vdc system through power conversion devices

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35
Q

What is the function of the Nitrogen Generation System on board?

A

To displace fuel vapors in all fuel tanks

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36
Q

What does the EICAS message BRAKES indicate?

A

Two or more brakes have failed and/or a dragging brake has been detected

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37
Q

When does the reference thrust limit change from CRZ to GA during an approach in VNAV?

A

Extending the flaps from up to flaps 1

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38
Q

What action can be taken to check if the left tank forward pump PRESS light is illuminated?

A

Check the Fuel Synoptic for load-shed label

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39
Q

What element is part of the B787 engine fire and overheat detection system?

A

Multiple dual-channel detector assemblies in each engine nacelle

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40
Q

What happens on the ground with an APU fire signal?

A

Causes APU shutdown and extinguisher bottle discharge

41
Q

What occurs when the Approach (APP) switch is pushed?

A

Arms or captures roll mode and pitch mode for the selected approach

42
Q

During warm weather, how many cabin air compressors will be working with the APU providing electrical power?

43
Q

What rate of descent does the autothrottle set during a cruise descent?

A

1250 feet per minute

44
Q

Why does the EEC select approach idle when flaps are commanded to 25 or greater?

A

To decrease acceleration time for go-around

45
Q

What provides standby power after loss of all electrical power to captain’s and first officer’s flight instruments?

A

The main battery

46
Q

Which systems does the B787 electrical system power in addition to traditionally electrically powered systems?

A
  • Wing ice protection system
  • Press system
  • Wheel brake system
47
Q

When is the magenta X-START displayed on the EICAS?

A

When current altitude and/or airspeed are outside of the windmilling envelope

48
Q

What determines the packs outlet temperature?

A

The temperature zone requiring the coolest temperature

49
Q

What does the purpose of the navigation source annunciation on the PFD?

A

Displays the source of navigation performance for the navigation scales

50
Q

What could the EICAS message LOAD RELIEF signify?

A

Flaps speed exceeded with flaps 15 or greater

51
Q

What does a priority call from the cabin display on the EICAS?

A

CABIN ALERT

52
Q

When does the autopilot add rudder commands during flight?

A

Only during an autopilot approach and landing

53
Q

What occurs when an engaged autopilot mode degrades?

A

Condition is annunciated with a line through the affected flight mode on PFD

54
Q

What does the EICAS indication EAI above N1 mean?

A

An engine anti-ice valve is open

55
Q

What causes the speed brake lever to be driven aft from the ARMED position on landing?

A

When the gear main trucks untilt and both thrust levers are not in the takeoff range

56
Q

What does the BPCU provide in terms of electrical load management?

A

Flight deck control/indication, power transfer functions and overall load management

57
Q

What does the EICAS message FLIGHT CONTROL MODE indicate?

A

The flight control system is in the secondary mode

58
Q

Which control surfaces are locked out during high-speed flight in normal mode?

59
Q

What displays current IRS heading, track and other heading information?

A

The mini-map

60
Q

What does selecting SYS POWER on the TCP allow the crew to do?

A

Remove power from L, R WXR and L, R XPDR

61
Q

What is correct about the wing ANTI-ICE Selector in AUTO?

A

Powered on and off automatically by the ice protection system

62
Q

Which parameters cannot be preselected prior to autopilot activation?

A
  • Vertical speed
  • Flight path angle
63
Q

When can the recirculation fan be selected off during HOT WX operations?

A

Must remain ON unless non-normal checklist directs to select them off

64
Q

What do the tiller position indicator marks indicate?

A

Center mark identifies neutral position; other two identify maximum left and right displacement

65
Q

What is correct about the TCP VHF page display function?

A

New frequencies are entered in the scratchpad; entering decimal/zeros is optional

66
Q

Where are the outflow valves positioned during a non-normal procedure with cargo fire ARM switch selected?

A

Outflow valves move to 50/50 flow split

67
Q

What happens when the APU is started while the airplane is on the ground with only forward external power ON?

A

APU generators energize the four main 235 Vac buses, external power transitions from ON to AVAIL

68
Q

How is low engine oil quantity displayed on the secondary engine display?

A

Quantity displayed in black on white background; LO beside quantity

69
Q

What is correct about the brake system on the B787?

A

There are four EBACs that control all eight main wheel brakes

70
Q

What does the VSD present?

A

A profile view of the airplane and its environment

71
Q

What is the position of the crossfeed valve during normal operations?

72
Q

What happens when the heading reference switch is in NORM and the aircraft enters polar regions?

A

True North is automatically referenced for all AFDS cruise modes

73
Q

What is correct regarding the EEC Alternate Mode?

A

Thrust protection is not provided and maximum rated thrust is reached with thrust lever less than full forward

74
Q

When will the center hydraulic demand pump operate?

A

When flaps or slats are in motion

75
Q

What indicates that the engine anti-ice system is powered (ON)?

A

EAI displayed in green

76
Q

What provides hydraulic power source for the center hydraulic system?

A

Two electric motor-driven pumps (EMPs)

77
Q

When does the Pick Waypoint (PICK WPT) Key appear on the ND?

A

When the cursor is in the ND map area and enabled when the scratchpad is blank

78
Q

What does the automatic ice detection system provide signals to?

A
  • Engine anti-ice
  • Wing anti-ice
  • Pack inlet anti-ice
79
Q

What is correct about the Display Select Panel (DSP)?

A

Provides control of the MFDs for the on-side inboard DU

80
Q

When does the IAS/MACH window automatically change from IAS to Mach?

81
Q

What is the primary and backup source for the brakes?

A
  • Primary: 28V DC bus system
  • Backup: Main battery
82
Q

What is displayed if the DEP/ARR key is pressed at less than 400 NM from the departure airfield?

A

Arrivals for the departure airport

83
Q

What do the control wheel pitch trim switches do in normal mode when airborne?

A

Change the trim reference airspeed

84
Q

What must be selected on the CDU for the take-off reference speeds displayed on the PFD?

A

Must be selected

85
Q

How are the cabin air compressors regulated after normal engine start?

A

Packs restart immediately after the second engine is running

86
Q

How does the exit hold direct the aircraft to leave the hold?

A

Arms a holding pattern exit, returns to holding fix via inbound course

87
Q

Is the statement true or false? The EICAS message FLIGHT CONTROL MODE signifies that the secondary flight control mode has been manually selected.

88
Q

How may manual fuel crossfeed be initiated in case of a fuel imbalance?

A

Open the crossfeed valve and turn OFF the fuel pump switches for the lower quantity tank

89
Q

Under what conditions does the fuel imbalance pointer flash?

A

If fuel or crossfeed is going in the wrong direction

90
Q

How often does load shed occur during the engine start?

91
Q

What describes the navigation performance scales and pointers on the PFD?

A

Indicates the navigation path relative to the airplane position

92
Q

What happens if the rudder signal for the rudder trim indicator is not present?

A

The digital readout, left/right indication and pointer are not displayed

93
Q

When will LNAV activate with armed during takeoff?

A

Above 50 ft radio altitude and in position to turn onto the active route leg

94
Q

What happens when one pack is operating in standby cooling mode?

A

Cooling capacity may be less, resulting in warm flight deck or cabin temperatures

95
Q

What does the EICAS advisory message, PACK MODE (L, R) indicate?

A

STBY COOLING displayed in amber

96
Q

What is the mode of power when the first external power receptacle is connected?

A

Ground Handling mode

97
Q

Below what airspeed is wing anti-ice inhibited on the ground?

98
Q

What does the flight director guidance cue represent?

A

Flight director guidance displayed when flight directors are turned ON