A330 NEO

What does the red line on the fan cowl show. Hazard are ate performing thrust operation. Hazard ares forward of th line when engine operate. Hazard area aft of the line when engine operates.

What is the purpose of the compressor airflow control system?. To help prevent an engine stall. To keep thrust the same. To keep the engine cool.

What is the arrangement of the turbine section?. 1 HP AND 8 LP STAGES. 2 stage high press turbines, 3 stg interm press turbine and & stg how press. 1 HP, 1IP AND 6 LP STAGES.

Where are engine parameters displayed?. EWD and SD. EWD and ND. EWD and PFD.

What is the main component for engine starting?. Pneumatic starter. Variable Frequency starter generator (VFSG). Electric starter.

How many fire detection loops are on an engine zone?. 1. 2. 4.

How many fuel tanks we have on the A330-800?. 6. 5. 4.

What are the users of the Pneumatic System?. Air conditioning, Wing anti-ice protection and hydraulic reservoirs. Air conditioning, Wing anti-ice protection, water tanks and hyd reservoirs. Wing anti-ice protection, water tanks and hydraulic reservoirs.

Where are the entry corridors when engine in operation. Inlet area. Exhaust area. Between the inlet and exhaust area.

How can the engine be described?. High bypass ratio turbofan fan engine. High bypass ratio geared fan engine. Low bypass ratio turbofan fan engine.

What are the hazards around an operating engine?. Inlet suction, exhaust, heat and noise. Inlet suction, exhaust, heat and lightning. Inlet suction, exhaust, heat, noise and ionizing radiation.

What is the function of the engine fuel and control system?. To control the fuel to the fuel servo in response to commanded power. To control the fuel to the combustion chambers in response to commanded pwr. To the control the air to the combustion chambers in response to commanded pwr.

What is the purpose of the lgnition system?. The ignition system supplies sparks to ignite the fuel/air mixture. The ignition sys supplies sparks to ignite the fuel/air compression chamber. The ignition sys supplies sparks to ignite the fuel/air gass charm.

What is the purpose of the thrust reverse systems?. To let the airplane go backwards/hover. To supplement braking. To make the engine rotate in reverse.

What are the functions of the engine oll system?. To lubricate the shaft(s) bearing, gearbox bearing, gears and drive. To lubricate, cool and clean bearings, gearbox, gears. To eliminate friction of the shaft(s) bearing, gearbox bearing, gears, an.

How many fire detector assemblies are installed on each engine fire detection loop A or B ?. Five detector assemblies. Four detector assemblies. One detector assemblies.

What is the correct fan cowl door latch opening and closing sequence?. Opening sequence L1, L2, L3 and L4; closing latch sequence L2, L3, L4, L1. Opening sequence L4, L2, L1 and L3; closing latch sequence L4, L3, L2, L1. Opening sequence L1, L2, L3 and L4; closing latch sequence L4, L3, L2, L1.

What valve gives primary regulation for the engine anti-ice system?. Both at the same time. PRSOV(pressure regulating and shutoff valve). PRV(pressure regulating valve).

How is the engine Anti-lce System controlled and monitored?. It's controlled by the EEC. It's controlled by BMC. Its's controlled by the EIVMU.

What is the purpose of the engine nacelle. Reduce noise of cold and hot air stream. Aerodynamic structure around the engine. Attaches the engine to the strut.

What changes the TLA to TRA?. The EEC. The EIVMU. The TCU.

How many ignition system are on the engine. One. Two. Three.