Airbus A330 – Fire Protection - SmartCockpit - Airline training guides, Aviation, Operations, Safety

Cargo fire protection is provided by:

Automatic smoke detection, automatic fire extinguishing.

Automatic fire detection, automatic fire extinguishing.

Automatic smoke detection, manual fire extinguishing.

Correct! Wrong!

There is an automatic and manual fire extinguishing system in the wastebin of each lavatory.

False.

True.

Correct! Wrong!

There is only an automatic fire extinguishing system in the wastebin of each lavatory.

Each lavatory is equipped with:

One smoke detector.

One heat sensor.

Two smoke detectors.

Correct! Wrong!

Smoke has been detected in the AFT cargo compartment. The pilot has pushed the AFT AGENT pb and bottle 1 has discharged. The bottle 2:

Will automatically discharge its contents over a period of 260 minutes.

Will discharge all its contents immediatly after bottle 1.

Is now held in reserve to fight a fire in the FWD compartment.

Correct! Wrong!

If smoke has been detected in one of the lavatories:

Waste fire extinguisher is automatically triggered.

Lavatory ventilation is automatically cut off.

ECAM message SMOKE LAVATORY SMOKE appears in the cockpit and cabin crew is automatically alerted.

Correct! Wrong!

Engine fire protection is provided by 2 detection loops which provide information to a computer (Fire Detection Unit).

If both loops break and breaks occur more than 5 seconds apart, a fire indication is generated.

If both loops are working and one loop senses a certain temperature, a fire indication is generated.

If both loops are working, both loops must sense a certain temperature to generate a fire indication.

Correct! Wrong!

The avionics smoke warning triggers, if both smoke detectors detect smoke for:

More than 5 seconds, or one smoke detector detects smoke for more than 5 seconds, and the other smoke detector is inoperative.

More than 10 seconds, or one smoke detector detects smoke for more than 15 seconds, and the other smoke detector is inoperative.

More than 5 seconds, or one smoke detector detects smoke for more than 10 seconds, and the other smoke detector is inoperative.

Correct! Wrong!

Each engine has two extinguisher bottles equipped with electrically-operated squibs to discharge their agents. Each squib has a single electric supply.

True.

False.

Correct! Wrong!

When a red ECAM message SMOKE LAVATORY SMOKE is displayed:

No indication is available in cabin.

The cabin crew is alerted by the pilot using the cabin call button.

Cabin warnings are also generated for the Cabin Crew.

Correct! Wrong!

When the cargo smoke warning triggers, each isolation valve of the cargo ventilation system of all compartments close automatically, and the extraction fan stops.

False.

True.

Correct! Wrong!

When the cargo smoke warning triggers, the isolation valves of the cargo ventilation system of the affected compartment close automatically, and the extraction fan stops.

What does an amber ECAM warning ENG 1 FIRE DET FAULT mean?

It is not possible to fight a fire in engine 1.

Both loops in the engine fire detection system have failed.

One loop in the engine fire detection system has failed.

Correct! Wrong!

If the APU fire system detects a fire in flight will the extinguisher discharge automatically?

Yes.

No.

Correct! Wrong!

The gas detection loops consist of three sensing elements for each engine, located in the pylon nacelle, in the engine core sections and:

One sensing element in the APU compartment.

Three sensing elements in the APU compartment.

Two sensing elements in the APU compartment.

Correct! Wrong!

When a sensing element is subjected to heat, it sends a signal to the fire detection unit. As soon as loops A and B detect temperature at a preset level, it triggers the fire warning system.

Which of the following statements is true?

Two Smoke Detection Control Units (SDCU) are installed for the cargo compartments.

Only fire detection is provided for each engine and the APU.

Each engine and the APU are equipped with a fire and overheat detection, and extinguishing system.

Correct! Wrong!

When an APU fire is detected on ground, the APU fire light on the External Power Control panel comes on. In addition:

A horn sounds, APU Auto shut down occurs, and the APU fire extinguisher bottle is automatically discharged.

A horn sounds, APU auto shut down occurs, pilot must discharge fire bottle.

A horn sounds, APU must be shut down using APU shut off switch on External Power Control panel.

Correct! Wrong!

If the system detects an APU fire while the aircraft is on the ground, it shuts down the APU automatically and discharges extinguishing agent.

False.

True.

Correct! Wrong!

On CARGO SMOKE overhead panel, SQUIB illuminates white:

When both bottles are empty.

Only during cargo smoke test.

When both FWD AGENT and AFT AGENT pb are pushed.

Correct! Wrong!

AGENT pb on FIRE overhead panel can be operated when:

ENG FIRE pb illuminates red.

ENG FIRE pb is pushed and released.

DISCH light illuminates.

Correct! Wrong!

A red disk, which is outside at the rear of the fuselage, signals that:

The APU agent is not discharged overboard due to bottle overpressure.

The pilot must check the indicator for the second APU bottle on right side of the aircraft.

The APU extinguishing bottle has experienced technical fault but it is still available.

Correct! Wrong!

What is the true statement about the fire extinguishing system?

There are two bottles per engine.

There is one bottle per cargo compartment.

There is one bottle for each engine.

Correct! Wrong!

Smoke has been detected in the FWD cargo compartment and the pilot has pushed FWD AGENT pb. Bottles 1 and 2 have discharged.

All statements are correct.

SMOKE red light on CARGO SMOKE overhead panel turns off when there is no more smoke.

SMOKE red light on CARGO SMOKE overhead panel stays on because smoke is held in cargo compartment.

Correct! Wrong!

What does an amber ECAM warning SMOKE DET FAULT mean?

Avionics smoke detection is lost.

Engines smoke detection is not available.

Both SDCU (Smoke Detection Control Units) channels fault or loss of all smoke detections.

Correct! Wrong!

A fire has been detected on engine 1. ENG 1 FIRE pb and FIRE light on ENG 1 MASTER will extinguish:

When the fire on engine 1 no longer exists.

When the ENG 1 MASTER is selected to OFF.

When the ENG 1 FIRE pb is pressed and released.

Correct! Wrong!

The APU fire extinguishing system includes:

One fire extinguishing bottle.

Two fire extinguishing bottles.

No fire extinguishing bottle.

Correct! Wrong!

The smoke detection system of the cargo compartments consists of smoke detectors, that are housed in:

Pairs in cavities within the cargo compartment ceiling panels.

Cavities within the cargo compartment floors.

Cavities within the cargo compartment walls.

Correct! Wrong!

There are 2 cavities in the forward cargo compartment, 2 cavities in the aft cargo compartment and 1 cavity in the bulk cargo compartment.

The engines and the APU each have a fire and overheat detection system consisting of two identical gas detection loops (A and B) mounted in parallel and a Fire Detection Unit (FDU).

True.

False.

Correct! Wrong!

If the ENG FIRE pb is depressed:

Both Fuel HP and LP Valves are closed.

Fuel LP Valve is closed.

Fuel HP Valve is closed.

Correct! Wrong!

What does this SMOKE light indicate?

Smoke is detected in the avionics ventilation duct.

Smoke or fire is detected underneath the cockpit in the electronics and avionics bay.

Smoke is detected underneath the cockpit in the electronics and avionics bay.

Correct! Wrong!

When smoke is detected in the avionics compartment:

Cabin fans are automatically stopped.

FWD AGENT SMOKE pb on the CARGO SMOKE panel illuminates red.

AVNCS SMOKE on VENTILATION panel illuminates red.

Correct! Wrong!

Airbus A330 – Fire Protection