Domande esame ATPL per Aircraft General Knowledge -

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Test 10 domande Aircraft General Knowledge - Airframe, Systems, Powerplant, tempo libero

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1 - The principle of the SAFE LIFE design of an aircraft is based on the: Replacement of parts after a given number of cycles or hours of use. Monitoring of critical parameters and the replacement of parts if a limit value is exceeded. Capability to withstand a certain amount of weakening of the structure without catastrophic failure. Redundancy Of The Structure Equipment.

2 - The function of the selector valve is to: Select The System To Which The Hydraulic Pump Should Supply Pressure. Communicate system pressure to either side of an actuator. Discharge some hydraulic fluid if the system pressure is too high. Automatically Activate The Hydraulic System.

3 - Regarding a jet engine: 1) The maximum thrust remains constant as the pressure altitude decreases. 2) The specific fuel consumption remains constant as the pressure altitude decreases at constant TAS. 1) Is Correct, 2) Is Correct. 1) is incorrect, 2) is correct. 1) is correct, 2) is incorrect. 1) is incorrect, 2) is incorrect.

4 - Which is the correct statement regarding a large aircraft fitted with both inboard and outboard ailerons? The Outboard Ailerons Are Typically Used Only When The Flaps Are Retracted. The Outboard Ailerons Are Typically Used Only When The Landing Gear Is Selected Down. The Inboard Ailerons Are Typically Only Used When The Flaps Are Extended. The outboard ailerons are typically used only when the flaps are extended.

5 - A CSD of an AC generator may be disconnected in flight. The primary reason(s) for disconnection are: Low oil pressure and/or high oil temperature of the generator drive. Slight variation about the normal operating frequency. Illumination of the CSD disconnect warning light. Excessive Variation Of Voltage And Kvar.

6 - The mixture control for a carburettor achieves its control by: Moving The Butterfly Valve Through A Separate Linkage To The Main Throttle Control. Varying the fuel supply to the main discharge tube. Varying the air supply to the main discharge tube. Altering The Depression On The Main Discharge Tube.

7 - When powering up a hydraulic system, the level in the reservoir will: Increase As Ambient Temperature Decreases. Always remain the same. Decrease slightly. Initially Increase With System Pressurisation.

8 - The wing ice protection system currently used for most large turboprop transport aeroplanes is a(n): Electrical De-icing System. Hot air system. Pneumatic system with inflatable boots. Liquid De-icing System.

9 - The capacity of a battery is the: Intensity Withstood By The Battery During Charging. Amount of ampere-hours that a fully charged battery can supply. No-load voltage of the battery multiplied by its rated output current. Number Of Cycles (charging And Discharging) That A Battery Can Withstand Without Deterioration Of Its Cells.

10 - The wing ice protection system currently used for most large jet transport aeroplanes is a(n): Pneumatic System With Inflatable Boots. Hot air system. Electrical de-icing system. Liquid De-icing System.

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