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777 > Test Questions > Flashcards

Test Questions Flashcards

0
Q

Minimum O2 Pressure

A

1250

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1
Q

The standby A/S and Altimeter are powered ONLT by which Pitot Static System

A

Center

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2
Q

Tire pressure

A

190 nose ; 200 mains

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3
Q

Do you have over boost protection in eng alternate mode

A

No

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4
Q

Do you have overspeed protection in eng alternate mode

A

Yes

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5
Q

When is app idle commanded ?

A
  • engine anti–ice is operating
    • the flaps are commanded to 25 or greater
    • one hydraulic system air–driven demand pump is inoperative, and the flaps are out of the UP position
    • the opposite engine bleed air valve is closed
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6
Q

When is auto light active

A

The auto–relight function is activated whenever an engine is at or below idle with the FUEL CONTROL switch in RUN.

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7
Q

When does auto relight stop trying

A

35% N3

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8
Q

Besides dropping below idle RPM when will the EEC activate the igniters and how many

A

The EEC also provides protection against flameout during periods of excessive rain/hail ingestion. When a flameout is detected, the EEC energizes both ignitors.

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9
Q

ENG FAIL message will appear on PFD during what speeds

A

65 knots to 6 knots below V1

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10
Q

When is the ECAS message ENG FAIL displayed ? When does it go out?

A

When an engine unexpectedly decelerates to less than idle speed. The message remains displayed until the engine recovers or the fuel control switch is moved to CUTOFF.

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11
Q

When is the EICAS message ENG THRUST displayed?

A

The EICAS caution message ENG THRUST (L or R) is displayed if:
• actual thrust is significantly less than commanded thrust
• actual thrust is not increasing to commanded thrust, and
• airspeed is V1 - 6 knots or greater.

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12
Q

Loss of what busses will result in APU auto start inflight

A

Both transfer busses

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13
Q

For the following faults, the APU continues to operate and the EICAS message APU LIMIT displays with an engine running:

A
  • high EGT
  • high oil temperature
  • low oil pressure.
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14
Q

To reduce bleed air demand NGS is shut down for

A

engine out operation. NGS is also shut down when the Equipment Cooling switch is off or a Cargo Fire Arm switch is ARMED.

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15
Q

Main tank fuel capacity 200/300

A

64, 000 200

69, 000 300

16
Q

Max fuel quantity 200/300

A

303,100. 200

320, 800. 300

17
Q

Scavage systems starts to scavage center tank when a wing drops below _________ 200/300. Center tank must be below ________

A

29,000 - 200
52,600. -300

35,000

18
Q

When center tank is less than ________ don’t turn center tank pumps on until inflight (message reminds you)

A

10,500

19
Q

Tire pressure preflight nose; main

A

190 Nose

200 Mains

20
Q

Standby A/S and Altimeter on on what pitot Static system

A

Center ONLY!

21
Q

During Eng Start what indicates the start is complete

A

When red start EGT limit goes away

22
Q

What does amber and white doors on door synoptic indicate?

A

Amber = door open

White = door position unknown

23
Q

What thrust is available with EECs in alternate mode?

A

Maximum rated thrust is available in any phase of flight by moving the thrust levers to the full forward positions.

24
Q

If the EEC switches to alternate mode, what do the auto throttles do?

A

The autothrottles remain engaged whenever the EEC automatically switches to the alternate mode.

25
Q

What engine protection is lost with EECs in alternate mode

A

Over boost , over speed works

26
Q

What does the auto start system not monitor

A

oil pressure and temperature.

27
Q

What will cause the APU to start inflight?

A

In flight, if both AC transfer busses lose power, the APU automatically starts,

28
Q

With one or more engines running or in start what will cause the APU to shutdown?

A

In the attended mode, any of the following faults cause the APU to shut down immediately:

  • APU fire/inlet over temperature
  • overspeed/loss of overspeed protection
  • APU controller failure
  • speed droop
29
Q

More than ______ fuel in center tank on start center fuel pumps are _______. Less they are _________.

A

10,500
ON
OFF

30
Q

Main Tank Capacity. 300 / 200

A

64.100#; 69,000#

31
Q

How can FA power Ground Service Bus

A

Switch at 1L with Primary Power

32
Q

What does Service Bus Power that’s important

A

Battery Chargers

33
Q

What does a drive light in CSD indicate

A

Low oil pressure

34
Q

What does drive light and gen off MSG mean

A

High oil temp and shut down

35
Q

When only battery is powering airplane what inst

A

PFD, ND, STANDBY INST, EICAS, L CDU, L VOR, L COM AND C ILS and L FMC

36
Q

With duel FMC failure what buttons work on CDU

A

Legs, progress, NAV radios

777 (2 decks)

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