ППП конструкции ВС Автор записи Автор: pavel.minyaylov Дата записи 10 сентября, 2023 Фамилия и имя на латинице Место работы, должность 1. A cantilever wing: is externally braced with either struts and/or bracing wires is supported at one end only with no external bracing has both an upper an lower aerofoil section folds at the root section to ease storage in confined spaces Отсутствует 2. Control surface flutter is minimized by: reducing the moment of the critical engine aerodynamic balance of the control cables changing the wings before they reach their critical life mass balance of the control surface Отсутствует 3. What is the purpose of the wing main spar? To withstand bending and torsional loads To withstand compressive and torsional loads To withstand compressive and shear loa To withstand bending and shear loads Отсутствует 4. In the construction of airframes the primary purpose of frames or formers is to: provide a means of attaching the stringers and skin panels oppose hoop stresses and provide shape and form to the fuselage form the entrance door posts support the wings Отсутствует 5. The skin of a modern pressurized aircraft: is made up of light alloy steel sheets built on the monocoque principle houses the crew and the payload provides aerodynamic lift and prevents corrosion by keeping out adverse weather is primary load bearing structure carrying much of the structural loads Отсутствует 6. The pressure filter in a hydraulic system: filters the fluid returning to the tank is fitted down stream of the pump can be by passed when maximum flow is required clears the fluid as it leaves the reservoir Отсутствует 7. Case drain filters are: fitted to prevent debris from the reservoir reaching the system designed to allow hydraulic pump lubricating fluid to drain to atmosphere to enable pump lubricating fluid to be used to monitor pump condition fitted in the reservoir outlet Отсутствует 8. In the case of a failure of a cut-out valve: a full flow relief valve is fitted down stream of it a full flow relief valve is fitted upstream of it a full flow relief valve is not required the terminal pressure will be controlled by adjusting the pump rpm Отсутствует 9. A force of 100 N is applied to 2 separate jacks, the area of one is 0.02 m2 and the other is 0.04 m2: the smaller jack will exert a pressure of 2000 Pa and the larger 4000 Pa the smaller jack will exert a pressure of 5000 Pa and the larger 2500 Pa both jacks will move at the same speed both have the same load Отсутствует 10. Def. Stan 91/48 is ---------- and is ------------- based: red, mineral red, synthetic green, mineral purple, synthetic Отсутствует 11. Accumulator floating piston: pushes the fluid up when being charged pushes the fluid down when being charged provides a seal between the gas and fluid prevents a hydraulic lock Отсутствует 12. The contents of the hydraulic fluid reservoir are checked. They indicate that the reservoir is at the full level. The system is then pressurized. The contents level will: fall below the “full” mark fall to a position marked ‘full accs charged’ remain at the same level rise above the “full” mark Отсутствует 13. A non-return valve: can only be fitted if provided with a by-pass selector closes if inlet pressure exceeds outlet pressure opens if inlet pressure equals outlet pressure. closes if inlet pressure ceases Отсутствует 14. An ACOV will: provide an idling circuit when a selection is made extend the life of the accumulator provide an idling circuit when the accumulator is fully charged ensure the pump is always on load Отсутствует 15. When the hydraulic system pressure is released: reservoir air pressure will increase reservoir fluid contents will rise if reservoir is lower than other components in the system reservoir fluid contents will fall if reservoir is the highest point in the system reservoir contents are dumped overboard Отсутствует 16. A variable displacement pump on system startup will be at: minimum stroke an optimized position depending on fluid viscosity maximum stroke mid stroke Отсутствует 17. Different diameter actuators supplied with the same pressure at same rate: exert the same force will lift equal loads will move at the same speed exert different forces Отсутствует 18. The seal materials used with hydraulic fluids to DEF/STAN 91-48 and SKYDROL 700 specification are respectively: natural rubber and neoprene neoprene and natural rubber butyl and neoprene neoprene and butyl Отсутствует 19. The formula which gives the minimum speed (VP) at which aquaplaning may occur is: VP = 9 × √P where P is kg/cm2 and VP is in knots VP = 9 × √P where P is psi and VP is in mph VP = 9 × √P where P is psi and VP is in knots VP = 34 × √P where P is kg/cm2 and VP is in mph Отсутствует 20. A likely cause of nose wheel shimmy is: aircraft is overweight the tyre pressures are too high the aircraft is incorrectly loaded a torque link is worn or damaged Отсутствует 21. A nose wheel steering control system: prevents the nose wheel from castoring at all times allows the nose wheel to castor within preset limits about the neutral position allows the nose wheel to castor freely at all times prevents the nose gear from lowering if the nose wheels are not centralized Отсутствует 22. Oil is used in an oleo strut to: support the weight of the aircraft limit the speed of compression of the strut lubricate the piston within the cylinder limit the speed of extension and compression of the strut Отсутствует 23. Creep (slippage): is not a problem with tubeless tyres refers to the movement of the aircraft against the brakes alignment can rip out the inflation valve on tubed tyres, and deflate the tyre can be prevented by painting lines on the wheel and tyre Отсутствует 24. When inflating a tyre fitted to an aircraft, the tyre pressure reading on the gauge should be modified by: 10 psi 10% 4 psi 4% Отсутствует 25. The purpose of pulley wheels in cable control systems is: to ensure the cable tensions are equal throughout the system to change the direction of the control cable to ensure smooth operation of the system to prevent the cable from slackening Отсутствует 26. The purpose of the fairleads in a cable control system is to: alter the angle of deflection of the cables to guide the cables on to the pulley wheels to attach the cables to chain drives to keep the cable straight and clear of structure Отсутствует 27. In a manual flying control system the control inputs to the primary control surfaces: 1. are reversible 2. are irreversible 3. are instinctive for the movement required 4. are opposite for the movement required 5. are limited in range by flight deck obstructions 1 and 4 only 2 and 4 only 1 and 3 only 1, 3 and 5 only Отсутствует 28. The advantages of a cable control are: 1. light, very good strength to weight ratio 2. easy to route through the aircraft 3. less prone to impact damage 4. takes up less volume 5. less bolted joints 1, 2 and 4 only 3 and 5 only 1, 2 and 5 only all the above Отсутствует 29. Main and nose wheel bays are: pressurized unpressurized conditioned different, with the mains being unpressurized and the nose pressurized Отсутствует 30. In level pressurized flight what does the outflow valve do? Close Adjust to provide constant flow, and is normally partially open Open to increase air conditioning Adjust to provide maximum flow, and is normally almost closed Отсутствует 31. Fatigue life of the fuselage is based on the: number of pressurization cycles number of explosive decompressions number of landings only number of cycles at maximum differential Отсутствует 32. What is the purpose of the duct relief valve? To protect the undercarriage bay To ensure the compressor pressure is regulated To prevent damage to the ducts To relieve excess pressure to compressor return line Отсутствует 33. What is the purpose of inward relief valves? To prevent negative differential To back up the duct relief valve To allow positive pressure to be bled off in an emergency To back up the outflow valve Отсутствует 34. A humidifier is fitted to: extract the moisture content in the air filter the air increase the moisture content in the air when operating at high altitude to ensure the cabin air is saturated at high altitude Отсутствует 35. Cabin compressors: increase their flow in cruise conditions decrease their flow in cruise conditions increase their flow in proportion to increases of altitude differential pressure and reduction in engine rpm in order to maintain the mass flow deliver minimum air at sea level via the cold air unit Отсутствует 36. The aircraft inhibiting switch connected to the A/C landing gear: allows the aircraft to be pressurized on the ground stops pressurizing on the ground and ensures that there is no significant pressure differential ensures that the discharge valve is closed cancels out the safety valve on the ground Отсутствует 37. Inward Relief Valves operate: in conjunction with the cabin pressure controller when there is a negative diff in conjunction with the cabin altitude selector when there is negative diff when manually selected during the emergency descent procedure automatically when there is a negative diff Отсутствует 38. During a normal pressurized cruise, the discharge valve position is: at a position pre-set before take-off partially open open until selected altitude is reached closed until selected altitude is reached Отсутствует 39. An aircraft is prevented from pressurizing on the ground by: the auto deflating valve on the main oleos inhibiting microswitches on the landing gear inhibiting microswitches on the throttles the pressure control master switch Отсутствует 40. A pressurization system works by: essentially constant input mass flow and variable output essentially constant output mass flow and variable input does not start until an altitude of 8000 ft has been reached supplying hot gases from the engine exhaust unit to the mass flow control system Отсутствует 41. Without added oxygen the time of useful consciousness at 30 000 ft is approximately: twenty seconds eighty seconds one to two minutes six minutes Отсутствует 42. In a continuous flow oxygen system, oxygen is supplied: only when the mask is plugged into the socket connection only on passenger inhalation through the mask only when the cabin altitude is above 18 000 ft only when the supply has been regulated by the pilot Отсутствует 43. Rate of flow of oxygen is given in: litres/minute pounds/minute litres/second kilos/hour Отсутствует 44. Lubrication of an oxygen component thread is by: soap water grease oil graphite Отсутствует 45. In an emergency chemically produced oxygen is supplied for a given period by: sodium chlorate, iron power, an electrical firing system and a filter potassium chlorate, iron powder, an electrical firing system and a filter sodium chlorate, iron powder which is chemically activated by air and then filtered sodium chlorate and an electrical firing system Отсутствует 46. At what altitude will the diluter-demand oxygen regulator provide 100% pure oxygen: 10 000 ft 14 000 ft 24 000 ft 34 000 ft Отсутствует 47. Susceptibility to hypoxia is increased by: heat noise smoking under-breathing Отсутствует 48. Baffles are fitted in aircraft fuel tanks: to assist in correct fuel distribution to prevent fuel surging during aircraft manoeuvres to prevent the static build-up in the tank during refuelling to channel fuel to the vent valve Отсутствует 49. To indicate that a refuelling bowser carries JET A1 aviation kerosene: yellow and black stripes are marked on the refuelling hose JET A1 would be painted in 30 cm high symbols on the side of the container JET A1 is printed in white on a black background label positioned prominently on the vehicle the driver wears a straw yellow water and fuel proof jacket Отсутствует 50. The disadvantage of refuelling the aircraft to “tanks full” the night before a departure in the heat of the day is that: the change in the specific gravity may cause the aircraft to be overweight the change in the volume of the fuel may cause it to spill through the vent system the change in calorific value may reduce engine power to below sufficient the rpm governor will be rendered inoperative Отсутствует 51. If a fuel sample appears cloudy or hazy, the most probable cause is: water contamination anti-microbiological additives mixing different fuel grades oil in the fuel Отсутствует 52. The background colour scheme for fuelling system pipelines carrying the following fuels is: Red Black Black Red Red Yellow Yellow Red Отсутствует 53. Refuelling with passengers on board is not permissible: on a fixed wing aircraft if AVGAS is being used if the aircraft has more than twenty seats and the ratio of cabin attendants to passengers is greater than 1:50 and it is a wide bodied jet in any of the above cases Отсутствует 54. A “wide-cut” fuel is: more flammable than a kerosene type fuel less volatile than a kerosene type fuel coloured red for identification purposes commonly used in civilian transport aircraft Отсутствует 55. Fuel tank booster pumps are: centrifugal, low pressure centrifugal, high pressure gear type, low pressure gear type, high pressure Отсутствует 56. If a fuel tank with a capacitive quantity system was filled with water instead of fuel, the gauge would indicate: full scale low (zero) it would indicate the same as if it were filled with fuel full scale high (max) it would freeze at the last known indication Отсутствует 57. When refuelling an aircraft: the refuelling nozzle must be bonded to the fuel tank the bonding plug must be connected to the earth terminal the continuity between nozzle and hose must be infinity only use plastic nozzles Отсутствует 58. All effects of electricity take place because of the existence of a tiny particle called the: electric proton neutron electron Отсутствует 59. A material with a deficiency of electrons becomes: positively charged negatively charged isolated overheated Отсутствует 60. Chemical action produces electricity in: a light meter a generator a primary cell starter generator Отсутствует 61. The unit measurement of electrical resistance is: the volt the watt the ohm the ampere Отсутствует 62. The unit used for measuring: current - is the volt resistance - is the ohm electric power - is the capacitor EMF - is the amp Отсутствует 63. A device consuming 80 watts at 8 amps would have a voltage supply of: 640 volts 12 volts 10 volts 8 volts Отсутствует 64. If a number of electrical consuming devices were connected in parallel, the reciprocal of the total resistance would be: the sum of the currents the sum of the reciprocals of the individual resistances the sum of their resistances volts divided by the sum of the resistances Отсутствует 65. The current flowing in a circuit is: directly proportional to resistance, indirectly proportional to voltage directly proportional to temperature, inversely proportional to resistance inversely proportional to resistance, directly proportional to voltage inversely proportional to applied voltage, directly proportional to temperature Отсутствует 66. The unit of resistance is the: ampere volt watt ohm Отсутствует 67. 550 k ohms may also be expressed as: 550 000 M ohms 0.55 M ohms 55000 ohms 0.55 ohms Отсутствует 68. In a circuit fitted with a non-trip free circuit breaker if a fault occurs and persists: if the reset button is depressed and held in, the circuit will be made the trip button may be pressed to reset, but not permanently a non-trip free circuit breaker can never be bypassed the reset button may be pressed to make the circuit permanent Отсутствует 69. If the reset button is pressed in the trip free circuit breaker, the contacts with the fault cleared will: be made and kept made only be made if there is a fuse in the circuit reset itself only after a delay of 20 seconds not be made and the reset will remain inoperative Отсутствует 70. A thermal circuit breaker works on the principle of: differential expansion of metals differential thickness of metals differential density of metals differential pressure of metals Отсутствует 71. Overloading an electrical circuit causes the fuse to ‘Blow’. This: increases the weight of the insulation fractures the fuse case disconnects the fuse from its holder melts the fuse wire Отсутствует 72. A fuse in an electrical circuit is ‘blown’ by: cooler air the breaking of the glass tube excess voltage breaking the fuse wire excess current rupturing the fuse wire Отсутствует 73. Battery voltage is tested with: a megometer a voltmeter on rated load an ammeter with a rated voltage a hygrometer Отсутствует 74. An aircraft has three batteries each of 12 volts with 40 Ah capacity connected in series. The resultant unit has: a voltage of 36 and a capacity of 120 Ah a capacity of 120 Ah and a voltage of 12 a capacity of 36 Ah and 120 watts a voltage of 36 and a capacity of 40 Ah Отсутствует 75. A battery is checked for serviceability by: using an ammeter measuring the specific gravity of the electrolyte a boric acid solution using an ohmmeter Отсутствует 76. A lead acid battery voltage should be checked: on open circuit using a trimmer circuit with an ammeter on load Отсутствует 77. The nominal voltage of an alkaline cell is: 2.2 volts 1.8 volts 1.2 volts 0.12 volts Отсутствует 78. The level of the electrolyte must be maintained: just below the top plate above the plates level with the filler cap one inch below the top of the plates just above the top of the plates Отсутствует 79. Acid spillage in an aircraft can be neutralized by using: caustic soda soap and water soda and water bicarbonate of soda and water Отсутствует 80. The area of force around a magnet is termed: conductance stable magnetic resistance magnetic field Отсутствует 81. Which of the two poles has the greatest strength? North seeking pole South seeking pole Both poles have the same strength The saturated pole Отсутствует 82. A soft iron core in an electromagnet: increases flux density decreases flux density reduces arcing increases the lines of strength Отсутствует 83. An EMF is induced in a conductor rotating in a magnetic field by: capacitive reaction the reverse current relay electro transmission electromagnetic induction Отсутствует 84. An internally excited generator is one where: the field is produced within the distribution the field is initiated by a HT and LT coil the field is initiated by the battery the field is initiated within the generator Отсутствует 85. The voltage regulator: senses cut-out pressure and adjusts field current senses generator output pressure and adjusts field current senses generator output current and adjusts the field voltage senses back EMF Отсутствует 86. On aircraft, generator voltage is regulated by: varying the generator field strength increasing and decreasing the load changing the generator speed changing generator load Отсутствует 87. If an aircraft electrical system is quoted as 24 volts DC, the output of the generator is: 12 volts with the generators connected in series 28 volts with the generators connected in parallel 36 volts with the generators connected in series/parallel 42 volts Отсутствует 88. Rotary actuators are used for: undercarriage retraction centre of gravity assessment operation of fuel cocks movement of control surfaces Отсутствует 89. Press-to-test lights are used: to indicate to the pilot that the circuit has power and is complete to control the movement of a rotary actuator to indicate to the pilot that the circuit has operated to indicate to the pilot that the circuit has operated only to indicate to the pilot that the equipment has malfunctioned Отсутствует 90. In an electrical circuit the reverse current cut-out relay will open: when battery voltage exceeds generator voltage when circuit voltage is less than generator voltage when the main output CB is reset when the batteries are flat Отсутствует 91. In the event of the cut-out points sticking in the closed position, the most probable results, when the engine stopped would be: gain of engine power a burnt out generator loss of residual magnetism no apparent reaction Отсутствует 92. A component whose job is similar to a generator cut-out is: a rectifier. a converter an inverter a reverse current relay Отсутствует 93. In an aircraft electrical system which incorporates a voltmeter, the voltmeter indicates: the flow in the electrical system before the battery cut-out contacts close the rate of flow at all times the pressure in the electrical system before and after the cut-out contacts close the flow in the electrical system after the battery cut-out contacts close Отсутствует 94. If a generator fails in flight: the voltmeter will read maximum the ammeter reading will decrease load sharing circuits will operate the watt metre will show an increase Отсутствует 95. Loads on a bus bar are: in series with the generator so that the voltage can be reduced in parallel so the voltage can be varied in parallel so the current can be reduced determined by the cross-sectional area of the lead cable Отсутствует 96. If the ammeter shows ‘no’ charge, yet the battery remains charged, you would look for: loose battery connections a defective voltage regulator a defective CB a defective ammeter Отсутствует 97. In a “2 pole” electrical circuit, a short of the conductors would result in: an item of equipment operating automatically without switches the component not working an increase in voltage an item of equipment burning out because of a large current flow Отсутствует 98. In a double pole circuit: the systems polarity will change the current is supplied by one wire and the current is returned through the aircraft bonding system the current passes out through one wire and is returned through a second wire the current passes out through one wire and is returned via the aircraft’s immune circuit Отсутствует 99. Why are static wick dischargers fitted to aircraft? To smooth the generator output To prevent tyres bursting on landing To minimize radio interference To act as an earth return in a single pole electrical system Отсутствует 100. The electrical components of aircraft systems are screened to: bond the circuit to reduce risk of fire prevent them discharging prevent short circuits in radio equipment prevent them interfering with the function of radio equipment Отсутствует 1 из 100 Ваши ответы приняты. Спасибо большое! 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