A330 NEO MAR26
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Título del Test:
![]() A330 NEO MAR26 Descripción: test de A330 NEO |



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1. According to the "AIRCRAFT DIMENSIONS" (Page 10), the total wingspan for the A330-900 (NEO) is: A) 60.30 m. B) 62.83 m. C) 64.00 m. (p. 10). is the required position of the aircraft relative to the wind in open-air conditions?. A) Pointing downwind. B) Parallel to the wind direction. C) Pointing upwind. 3. Referring to "ENGINES DANGEROUS AREAS" (Page 31), the intake suction danger area for a Trent 7000 at "Minimum Idle" is: A) 1 meter. (p. 31). B) 2.4 meters. C) 3 meters. 4. In the access panel code "196BB" (Page 24), the fifth character represents the: . . A) Sequence of the panel. B) Major sub-zone. C) Location of the panel (e.g., Bottom). Per the "MAXIMUM TAKEOFF WEIGHT" table (Page 37), the MTOW range for an A330-800 (NEO) is: A) 192,000 to 233,000 KGS. B) 184,000 to 233,000 KGS. C) 230,000 to 242,000 KGS. 6. When the alphabet for the first letter identifier is exhausted (Page 25), which letter is used as a locator for "Ceiling Panels"?. A) C. B) Z. C) Y. According to "SECTION AND STATION NUMBERS" (Page 14), the "Nose Forward Fuselage" is located between: A) The Radome and STA 1764. (p. 14) B) STA 1764 and STA 2294. C) STA 2294 and STA 5410. A) The Radome and STA 1764. B) STA 1764 and STA 2294. C) STA 2294 and STA 5410. Which slats are specifically protected by the Wing Ice Protection system?. A) Slats 1 to 7. B) Slats 3, 4, 5 and 6. C) Slats 4, 5, 6 and 7. What is the source of air for the Engine Air Intake ice protection?. A) HP 6th stage bleed air. B) HP 3rd stage bleed air. C) IP 8th stage bleed air. In the Wing Anti-Ice (WAI) system, which component sends a failure signal to the CMC?. A) The SDAC. B) The FWC. C) The Zone Controller (ZC). . When are the Pitot Probes heated?. A) Only in flight. B) Only on ground with engines running. C) Low level on ground and normal level in flight. Which probes are heated ONLY in flight?. A) Pitot probes. B) Angle of Attack (AOA) sensors. C) Total Air Temperature (TAT) probes. Regarding the Windshield heating, how many heating levels are available?. A) One single level for both ground and flight. B) Two levels: low on ground and normal in flight. C) Three levels based on TAT. What units control and monitor the Potable and Waste water ice protection?. A) Two Window Heat Computers (WHCs). B) Two Ice Protection Control Units (IPCUs). C) one Ice Protection Control Units (OPCUs). Which computer manages the Engine Nacelle Anti-Ice (NAI) valves and solenoids. A) The PHC. B) The WHC. C) The Engine Electronic Control (EEC). (p. 35). When the NAI Push Button is set to OFF, which solenoid is energized by the EEC?. A) Solenoid S1 only. B) Solenoids S1 and S2. C) Solenoid S3 (which closes the PRSOV). What is the main difference between the A330-800 and A330-900 fuel systems?. A) The A330-900 has additional outer tanks. B) The A330-900 does not have a Center Tank facility. C) The A330-800 uses different fuel pumps. Which computer is responsible for the control function of the fuel system in normal conditions?. A) FCMC 2. B) FCMC 1. C) The Zone Controller. What is the maximum refuel pressure allowed at the refuel hoses?. A) 11 psi. B) 35 psi. C) 50 psi. What is the purpose of the Heat Shield panels over the air conditioning packs?. A) To keep the packs warm during flight. B) To prevent contact between leaked fuel and hot areas of the packs. C) To provide structural support to the Center Tank. During a refuel on batteries, what information is NOT received by the FCMCs?. A) Fuel temperature. B) High-level sensor status. C) Aircraft attitude information from ADIRS. To start an automatic refuel, the PRESELECTED quantity must be at least how much greater than the ACTUAL indication?. A) 100 kg. B) 200 kg. C) 500 kg. Which valve releases remaining pressure in the refuel gallery into the right inner tank after refuelling?. A) Surge-Pressure Relief Valve. B) Refuel Isolation Valve. C) Depressurising Valve. What happens if an overflow sensor in a surge tank becomes "wet" during refuelling?. A) The FCMC opens the Jettison valves. B) The FCMC closes the refuel/defuel isolation valves and stops the operation. C) A warning is displayed, but refuelling continues. What is the primary source of bleed air to minimize fuel penalty during normal high engine speed?. A) High Pressure (HP) 6th stage. B) Intermediate Pressure (IP) 8th stage. C) Fan Air discharge. 2. When is air automatically bled from the High Pressure (HP) compressor stage 6?. A) During high altitude cruise only. B) When IP stage pressure is insufficient (e.g., engines at idle). C) Whenever Wing Anti-Ice is selected ON. Which valve prevents reverse flow into the IP stage when air is bled from the HP stage?. A) Pressure Regulating Valve (PRV). B) Overpressure Valve (OPV). C) IP Check Valve. What is the target regulated pressure of the High Pressure Valve (HPV)?. A) 12 psi. B) 40 psi. C) 50 psi. The Pressure Regulating Valve (PRV) is pneumatically operated and electrically controlled by which component?. A) The Bleed Monitoring Computer (BMC) directly. B) The Thermostat control Solenoid (ThS). C) The Electronic Engine Controller (EEC). At what upstream pressure does the Overpressure Valve (OPV) start to close automatically?. A) Above 50 psi. B) Above 60 psi. C) Above 75 psi. What are the two temperature settings provided by the temperature regulation system?. A) 100°C and 200°C. B) 150°C and 200°C. C) 150°C and 235°C. Which condition will cause the BMC to automatically isolate the engine bleed air supply?. A) Low engine oil pressure. B) High fuel flow. C) Pylon or wing leak detection. Up to what altitude can the APU supply bleed air during climb?. A) 15,000 feet. B) 20,000 feet. C) 23,000 feet. In "AUTO" mode, when does the crossbleed valve automatically open?. A) Whenever Engine 1 is started. B) When the APU bleed valve is NOT Fully Closed (FC) and no leak is detected. C) Only when a ground cart is connected. What is the function of the Fan Air Valve (FAV)?. A) To regulate the bleed air pressure to 50 psi. B) To modulate fan airflow through the precooler heat exchanger. C) To provide backup overpressure protection. What precaution must be taken before the crossbleed manifold is pressurized by a ground cart?. A) All engine throttles must be at idle. B) The APU must be running at 95% speed. C) All A/C bleed systems must be switched OFF. |




