Various L&S Guide Q's Flashcards

1
Q

What happens when the OVHD PNL knob is turned to off position

A

All annunciation lights will be full bright when illuminated

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2
Q

What lights are not tested with the ANNUNCIATORS TEST button

A

EMER/PRKG BRAKE light, master warning, master caution, GPU push button light, and fire test lights are not illuminated.

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3
Q

CVR ERASE button works when?

A

On the ground with the parking brake set.

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4
Q

what will you see if DVDR test works/fails?

A

After 3 sec, CVR AFT(FWD) fail advisory message on EICAS

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5
Q

When do EMER LT’s come on when ARMED?

A

automatically if DC BUS 1 loses power or if the airplane electrical power is turned off (total loss of power)

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6
Q

When do the Passenger signs (smoking and seatbelt) automatically illuminate?

A

when masks are commanded to deploy

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7
Q

How is emergency access to flight deck prevented

A

Press INHIB push button within 30 seconds of request or door will unlock

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8
Q

What happens when you press the door INHIB button

A

Emergency access is prevented for 500 seconds, when the timer concludes the door remains locked

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9
Q

What does pressing the DUMP button on the pressurization panel do

A

Climbs the cabin to match outside or 12.4k’ at 2000fpm, which ever is higher. Then cabin will climb via natural leak to outside altitude. Packs and recirc fans shutdown

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10
Q

On the ground, what is the AMS bleed priority

A

AMS priorities the APU on the ground for single engine taxi, engine start, and REF ECS OFF t/o’s

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11
Q

In flight what is the AMS bleed priority for packs

A

Packs respective side, opposite side, and then APU

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12
Q

In flight you press Bleed 1 push light. What happens? Do you loose Pack 1?

A

Isolates bleed from engine one.

No, pack 1 supplied via bleed 2 via XBLEED

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13
Q

Smoke in recirc bay. What happens?

A

Recirc fans commanded off.

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14
Q

When are recirc vans commanded off?

A

Both packs are commanded off
Dump button pressed
Smoke detected in recirc bay

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15
Q

When will packs be commanded off?

A

DUMP button pressed
Thrust levers set to MAX
T/O REF ECS OFF and APU BLEED unavailable

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16
Q

What happens (all conditions) when you turn APU switch to off?

What happens if turned back to on?

A

APU enters 1 min cool down. Bleeds removed immediately, AC power available during cool down if only source of AC power.

If turned to on during the 1 min, APU will continue running.

17
Q

What does the APU EMER STOP button do?

A

LIGHTS UP! (White stripe lower half) When pressed
Also closes APU fuel shutoff valve, shutting down APU w/o 1 min cool down.

Red stripe on top half for fire condition

18
Q

What is the AC BUS TIE priority?

A

APU, GPU, then IDG

19
Q

What does the APU GEN button do when pressed??

A

Lights UP! (White stripe)
Also opens APU generator contact or and isolates the APU gen from the AC BUS TIE, the APU generator is tripped off line and de-excited

20
Q

What does AC BUS TIES knob do?

A

Opens bus tie contactor BTC (#) segregating AC BUS (#) from the AC BUS TIE

21
Q

BATT 1 and 2 are “off”. Are all busses depowered?

A

No, hot batt bus 1 and 2 powered

22
Q

What happens when you pull a fire handle?

A

Associated bleed, fuel, and hydraulic valves close. Under speed logic opens generator line contactor

23
Q

During fire test what happens?

A

Aural – Firebell, triple chime
Overhead panel – (6)engine 1&2 fire handles, FWD and AFT cargo smoke, APU fire ext., APU EMER stop all illuminate
EICAS msgs– (5)Eng 1(2) FIRE, APU FIRE, Cargo FWD(AFT) SMOKE
Glareshield EICAS – (4) Master warning(2x) FIRE icon on ITT 1(2)

24
Q

What do we look for before fire det. Test?

A
don't see on EICAS:
FIRE DET FAIL
FIREX FAIL
FIREX ARM
BTL DISCH
25
Q

When do speed brakes automatically retract?

A

“Thrust levers advanced, great or than FLAP 1, or speed drops below 180KIAS”

TLA >60º but not in LSG

26
Q

What happens when you pull the aileron disc handle

A

Disconnects system.
Each pilot gets on side aileron, and a set of MFS, ROLL disconnect MSG on EICAS
Capt keeps artificial feel, FO looses it.(the feel that is)

27
Q

When do the AC fuel pumps turn on automatically?

A

Ejector output insufficient (engine start or failure), XFEED operations, pump 2 for APU start while on AC power

28
Q

When do HYD SYS 1(2) pumps run automatically on ground (switch in AUTO)

A

For takeoff (flaps not 0, thrust levers advanced for t/o, ground speed >50kts)

Pump 2 for single engine taxi (OET) when ENG 1 started and E/P brake released

29
Q

When do HYD SYS 1(2) pumps run automatically in flight (switch in AUTO)

A
Low pressure detected,
For landing (flaps not 0)
30
Q

What does HYD 3B in AUTO allow

A

In flight, on with low pressure.

31
Q

When does A/I turn on if A/I REF OFF?

A

Above 1700’agl or 2 minutes of flight

32
Q

How does the GRND prox G/S INHIB system reset after you push the button?

A

By climbing above 2000’RA or descending below 30’RA

33
Q

T/O config button checks what?

A

(5)E/P brake off, takeoff flaps set, EICAS flap position matches MCDU Takeoff page 2/3 flap setting, “sploilers” retracted and pitch trim in the green band