When a red ECAM message SMOKE LAVATORY SMOKE is displayed:
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Wrong!
What does an amber ECAM warning ENG 1 FIRE DET FAULT mean?
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Each engine has two extinguisher bottles equipped with electrically-operated squibs to discharge their agents. Each squib has a single electric supply.
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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.
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Wrong!
On CARGO SMOKE overhead panel, SQUIB illuminates white:
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When an APU fire is detected on ground, the APU fire light on the External Power Control panel comes on. In addition:
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Each lavatory is equipped with:
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If the ENG FIRE pb is depressed:
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AGENT pb on FIRE overhead panel can be operated when:
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There is an automatic and manual fire extinguishing system in the wastebin of each lavatory.
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There is only an automatic fire extinguishing system in the wastebin of each lavatory.
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If the APU fire system detects a fire in flight will the extinguisher discharge automatically?
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A red disk, which is outside at the rear of the fuselage, signals that:
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What does an amber ECAM warning SMOKE DET FAULT mean?
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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:
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What is the true statement about the fire extinguishing system?
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What does this SMOKE light indicate?
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Which of the following statements is true?
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Cargo fire protection is provided by:
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If smoke has been detected in one of the lavatories:
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When the cargo smoke warning triggers, each isolation valve of the cargo ventilation system of all compartments close automatically, and the extraction fan stops.
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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.
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The smoke detection system of the cargo compartments consists of smoke detectors, that are housed in:
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There are 2 cavities in the forward cargo compartment, 2 cavities in the aft cargo compartment and 1 cavity in the bulk cargo compartment.
Engine fire protection is provided by 2 detection loops which provide information to a computer (Fire Detection Unit).
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The avionics smoke warning triggers, if both smoke detectors detect smoke for:
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The APU fire extinguishing system includes:
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The gas detection loops consist of three sensing elements for each engine, located in the pylon nacelle, in the engine core sections and:
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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.
When smoke is detected in the avionics compartment:
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A fire has been detected on engine 1. ENG 1 FIRE pb and FIRE light on ENG 1 MASTER will extinguish:
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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).
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Smoke has been detected in the FWD cargo compartment and the pilot has pushed FWD AGENT pb. Bottles 1 and 2 have discharged.
Correct!
Wrong!
Airbus A330 – Fire Protection