Fire Protection Flashcards

1
Q

Three conditions that would trigger an engine FIRE warning

A

1) Both loops detect a fire
2) One loop inop and remaining loop detects fire
3) Break occurs in both loops w/in 5 sec of each other

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2
Q

Will the APU auto-shutdown in flight with APU FIRE detected?

A

No

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3
Q

With an APU FIRE indication on the ground, what two things occur?

A

Emergency shutdown begins

Fire extinguishing bottle discharges

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4
Q

ENG FIRE pushbutton pushed and released, what occurs? (2-1-2-1-2)

A
Hydraulic shutoff valve closes
Low pressure fuel valve closes
Engine bleed closes
Pack FCV closes
2 squibs armed
IDG deactivated
Alarm silenced
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5
Q

What should we see when we do an ENG FIRE TEST?

A
FIRE light
SQUIB lights
DISCH light
Master Warning
ECAM
Pedestal FIRE p/b
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6
Q

What occurs when we push/release APU FIRE pushbutton?

A
APU shutdown
Arms squib
Closes low press fuel valve
Shuts off APU fuel pump
Closes APU bleed valve
Closes Crossbleed valve
Deactivates generator
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7
Q

Cargo extinguishing agents have ____ nozzles in fwd compartment and ____ nozzles in aft compartment.

A

2, 4

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8
Q

Cargo smoke indication causes what two actions to occur?

A

Aft isolation valve closes

Extract fan stops

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9
Q

What’s the sequence of events with FWD/AFT SMOKE?

A
Agent 1 toggle
~60 minutes later DISCH 1 appears
DISCH AGENT 2 appears
Agent 2 toggle
DISCH 2 appears
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10
Q

What does SMOKE indication in GEN 1 LINE indicate?

A

Smoke in the avionics duct

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11
Q

What occurs when GEN 1 LINE pushbutton is pushed?

A

GEN 1 Line contactor opens
AC Bus 1 powered by GEN 2 via bus tie
Separate circuit from GEN 1 to one fuel pump in each tank

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12
Q

What does FAULT indicate in RAT & EMER GEN pushbutton?

A

AC 1&2 not powered and Emer Gen not providing power

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13
Q

What will cause RAT to auto-deploy? (2)

A

Airspeed > 100 kts

AC 1&2 not powered

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