EXAMEN ATA 26 FIRE PROTECTION

The Engine Fire protection system has. 1 FDU for both engines. 2 FDU for both engines, 1 FDU for Lh Engine and 1 FDU for the Rh Engine. 2 FDU for each engine.

The engines are provided by: Fire detection only. Fire detection and fire extinguishing. Smoke detection and extinguishing.

In reference of the Engine fire extinguishing bottles: There are 4 bottles for each engine. There are 2 bottles for each engine. there is 1 bottle for each engine.

The avionics smoke detector is located: In the E/E Compartment access 810/811. In the extraction duct downstream of the avionics equipment. In the Inlet Air duct Upstream of the of the avionics equipment.

Which is the computer that monitors the Avionics compartment (In reference with Fire system)?. FDU of Avionics compartment. AEVC 1 for 810/811 & 812 and AEVC 2 for 822 & 824. AEVC.

In reference with Fire system the Avionics compartments have?. Fire detection only. Smoke detection. Fire detection and extinguishing.

The APU Fire protection system has: 1 FDU of APU. 2 FDU of APU.

In reference of the APU fire extinguishing bottles: There are 2 bottle for the APU. There is 1 bottle located fwd of the APU compartment. There is 1 bottle in the Pylon for the APU.

In reference with Fire system, the Cargo compartments have?. Fire detection system only. Extinguishing system only. Fire detection and extinguishing.

The cargo compartment smoke detectors are monitored in Enhanced configuration by: AEVC. CIDS-SDF. FDU of cargo compartment.

In reference of Cargo compartment fire extinguishing bottles: (Standard System). There are 1 bottle for the fwd and aft compartment. There are 2 bottle for the fwd and aft compartment. There are 2 bottles: 1 for the fwd and the other for the aft compartment.

Which extinguishing system has this Aircraft? (implied from context). Standard System. Enhanced System. Both systems available.

The engines and APU fire protection is provided by: Fire detection only. Fire detection and extinguishing. Smoke detection and extinguishing.

The engines have the detector elements mounted in: Fan case, core and pylon areas. Fan case and core areas. Core, exhaust and fan case areas.

To obtain an engine fire warning in the cockpit, the loops A and B must: Fire on loop A and loop B. Fire on loop A and fault on loop B. Both of above. Only a is true.

The cargo compartments are protected against fire with: Smoke detection. Fire detection and extinguishing. Smoke detection and extinguishing.

The extinguishing bottle located in the lavatories is activated: Automatically. Manually from the cockpit. Manually from the FAP.

To accomplish the auto-extinguishing test of the APU: The APU must be running. The APU must be shutdown. The APU must be shutdown and Master SW selected ON.

The cargo compartment smoke detectors are monitored by: AEVC. CIDS-SDF. SDCU.

In reference with the ENGINE FIRE P/B interfaces: FADEC system will be de-energized is Fire P/B is released out. FADEC system will still energized regardless of Fire P/B position. Fire P/B doesn't affect the electrical supply to the FADEC system.

The system has: 1 FDU for both engines and 1 FDU for the APU. 1 FDU for both engines, 1 FDU for APU and 1 STDBY FDU. 1 FDU for each engine and 1 FDU for APU.

The engines and APU fire protection is provided by: Fire detection only. Fire detection and extinguishing. Smoke detection and extinguishing.

In reference of the fire extinguishing bottles: There are 4 bottles for each engine and 1 for APU. There are 2 bottles for each engine and 1 for APU. There are 2 bottles for each engine and 2 for APU.

To obtain an engine fire warning in the cockpit, the loops A and B must: Fire on loop A and loop B. Fire on loop A and fault on loop B. Both of above. Only a is true.

The Lavatories are protected against fire with a smoke detector and extinguishing. The statement above is TRUE. The statement above is FALSE.

The avionics smoke detector is located: Down stream of avionics equipments. Up stream of avionics equipments. Down stream of the extract fan.

The extinguishing bottle located in the lavatories is activated: Automatically. Manually from the cockpit. Manually from the FAP.

what is a cartrige. a detector devices. an explosive device. a sensing device.