Refined oral Flashcards

1
Q

Will the IDG DISC work when the engine is off?

A

No, the engine must be running for the worm screw to disc IDG

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2
Q

What does the RAT power?

A

AC ESS and AC stby

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3
Q

What keeps the rat from being messed up by hydraulic over load?

A

Unloader valve when it first pops out, and then the flow limiter.

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4
Q

Why do we get flaps half speed when the rat is powering slats flaps.

A

There are two motors to run the slats flaps, only one works with the rat

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5
Q

What’s the electric priority

A

Onside inside outside cross side

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6
Q

How many amps for the TRU

A

300

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7
Q

What does the Batt 2 do in auto mode?

A

Either powers the DC ESS 2 or powers the APU Start bus depending on what you want?

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8
Q

When will the electronic PBIT start?

A

When System gets AC power

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9
Q

What should EICAS say when power is first turned on?

A

NO EICAS messages at all for the first 5 seconds

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10
Q

Stall protection ?

A

Limits the aircraft angle of attack so it won’t stall

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11
Q

Only _______ can charge the batteries

A

AC Power

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12
Q

What must the thrust lever position be to shut it off? Ground and flight?

A

It’s gotta be in idle. Both ground and flight

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13
Q

Speed brakes are?

A

Outboard three multi function spoilers

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14
Q

When will the emergency lights turn on when armed?

A

DC Bus 1 electrical power loss

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15
Q

You get cargo smoke in flight. You blow the high rate bottle, but forget to blow the low rate bottle. What happens?

A

The low rate bottle will deploy 60 seconds after high rate is deployed automatically

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16
Q

After starting the APU, when will you get pneumatics and electrics?

A

Electrics and pneumatics = 95% and 3 seconds

17
Q

When do hydraulic AC pumps turn on?

A

Flight = flaps greater than 0

Ground = flaps greater than 0 and TLA TO or greater than 50 kts.

18
Q

Hydraulic AC pump will stay on after landing how long?

A

60 seconds after touch down

19
Q

Pitch trim switch on yoke can be held down for how many seconds? What if only one is held down?

A

The pitch trim can only be manually activated for three seconds. After that it is disconnected.

If only half of the switch is actuated for more than 7 s, the switch will be automatically deactivated

20
Q

What items will cause a no takeoff configuration warning? (5)

A
Pitch trim
Spoiler panel deployed
Flaps not at takeoff (1,2,4)
Flaps different from MCDU
Parking brake
21
Q

How do you test the Passenger Emergency lights on the power up flow?

A

Turn them from off to ON: EICAS says “emergency lights on” AND “Emergency Lights not Armed”

Turn them to ARM: all EICAS indications turn off.

22
Q

If smoke is detected in the Recirculation bay, what happens?

A

Recirculation Fans turn off. They move air from cabin/cockpit to mixing manifold, then the recirculation bay, then back into the cabin/cockpit… Bad smoke

23
Q

What important items are on the Hot Battery Busses 1 and 2?

A

Respective side:
Engine extinguishers
HYDRAULIC and FUEL SOVs

Service lights
Refuel panel

24
Q

DVDR test? How many DVDRS?

A

Two.
To test:
Push the button, verify NO EICAS messages. Test Light on dvdr panel flashes for ten seconds, then steady green. NO Amber light

25
Q

Emergency lights come on when and are good for how long?

A

Loss of power to DC busses , 12 minutes

26
Q

How long do Passenger chemical oxygen generators provide O2?

A

12 minutes

27
Q

On take off, When does roll change to track?

A

100 KIAS

28
Q

When is windshear system active?

A

Below 1500’ AGL

29
Q

When will the preview function on the guidance panel be available?

A

Within 30 nm, auto tune, and doing an ILS

30
Q

Cabin pressure controller has

A

Two channels, one active one standby