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Avery Systems Exam V
50問 • 1年前
  • Will Erwin
  • 通報

    問題一覧

  • 1

    What is the primary advantage of AC over DC electrical generation types?

    Saving in space and weight

  • 2

    An aircraft is fitted with NiCad batteries, the crew get a high battery temp warning light. This situation is probably caused by?

    The rate of charging was too high

  • 3

    After a 'wet start' in a turbine engine, what precautions should be taken to prevent a future engine malfunction ?

    Motor over to prevent torching when re starting

  • 4

    With increasing airspeed up to and beyond Mach 1.0, the co-efficient of drag and a constant angle of attack will?

    Initially increase, then decrease

  • 5

    The purpose of a cabin pressure relief valve is to automatically open when ?

    Cabin differential pressure reaches a pre set value

  • 6

    The valve that controls the air pressure in a cabin pressurisation system is known as?

    The outflow valve

  • 7

    Which of the following correctly names the component in a pneumatic system that will automatically shut off the air supply to non-essential services, when system pressure reduces below a certain predetermined value?

    Pressure maintaining valve

  • 8

    In what way is the SG of Avtur effected by changes in ambient temperature ?

    SG decreases with temperature rise

  • 9

    Under which of the following conditions is it necessary to incorporate cabin air humidifiers in an aircraft air conditioning system?

    At high altitudes at all times

  • 10

    Hydraulic fluid has which of the following properties ?

    Is is almost incompressible

  • 11

    When comparing the properties of pneumatic vs hydraulic systems?

    Pneumatics do not require return lines but hydraulic systems do

  • 12

    In what way does the extension of leading edge devices such as flaps and slats effect the co efficient of lift and drag, and the nose pitching moment ?

    Increase in lift and drag coefficients, and a nose up pitch moment

  • 13

    Assuming the same degree of trailing edge flap deflection, which answer best describes the primary advantage of slotted flaps, compared to fowler flaps

    Improved boundary layer airflow over flaps

  • 14

    Assuming the aircraft is within the various radio altitude envelope bands, in which of the following scenarios will the flight crew receive a warning

    When an unsafe radio height is reached, with the aircraft NOT in the landing configuration

  • 15

    Assuming a constant speed drive is disconnected in flight when, and under what circumstance can it be reconnected ?

    Mechanically, when the aircraft is on the ground

  • 16

    Which of the following best describes how an APU speed is controlled ?

    By a governor

  • 17

    The device that controls the direction of movement of a hydraulic actuating unit, is called the ?

    Selector valve

  • 18

    Which of the following switches must be closed before a generator can be connected to the synchronising bus?

    The bus tie breaker switch

  • 19

    Which answer best describes the disadvantage of a turboprop engine, compared to a turbojet engine ?

    Lower propulsive efficiencies at high subsonic mach numbers

  • 20

    The auto land status annunciator

    Monitors only autopilot and autopilot support system integrity

  • 21

    A swept wing transport turbojet is cruising at higher than normal operating altitude, at normal cruise mach number, in non turbulent conditions. If it experiences buffet, which statement is correct ?

    It could be high or low speed buffet, as it is difficult to tell at high altitude

  • 22

    Shockwaves can form at a true mach number below Mach 1.0 , this is because?

    Curved surfaces in various parts of the aircraft accelerate the air to greater than free stream mach number

  • 23

    A control tab that is moved by the main control linkage, such that the hinge moments cause a deflection of the primary control surface. This device is called a ?

    Servo tab

  • 24

    High flying air transport aircraft have a fuel tank venting system, this is to?

    Ensure the tank walls do NOT rupture when in turbulence or during manoeuvres

  • 25

    What is the reason why the hydraulic reservoir is pressurised in high flying aircraft ?

    To prevent the fluid from foaming due to low ambient pressures at high altitudes

  • 26

    An aircraft is fitted with TCAS and GPWS. Which statement is most correct ?

    Both TA's and RA's are inhibited by GPWS warnings

  • 27

    The B767 incorporates a typical autopilot flight director systems (AFDS). When an ILS is being flown, with the Altitude Hold and Approach modes selected, which statement best represents the actions that follow ?

    The system is armed to capture the glideslope and altitude hold will automatically cancel when this occurs

  • 28

    The manoeuvre envelop defines?

    The speed/load factor limits within which the aircraft is to be operated

  • 29

    Manual reversion is provided?

    On aircraft that do not have triple hydraulic system redundancy

  • 30

    An aircraft accelerated beyond Mcrit, if not corrected by the Mach Trimmer, it can display a nose down tendency. This is due to ?

    The rearward movement of the centre of pressure and reduced tailplane down load

  • 31

    On large transport aircraft, the effect of a failure of leading edge high lift devices to extend is to ?

    Require a lower than normal attitude, and a higher airspeed on approach

  • 32

    With an increase in altitude, and same equivalent airspeed (EAS) spiral stability ?

    Increases

  • 33

    Which statement is most correct?

    The primary function of ground spoilers is to reduce lift and increase braking effectiveness

  • 34

    AS the sped of a large transport aircraft increases from low speed stall to Mmo, the power requirements during this phase can be best described as ?

    Decrease than increase

  • 35

    The primary reason for fitting leading and trailing edge flaps is to ?

    Reduce the landing and takeoff speeds and distances needed

  • 36

    A number of swept wing jet transport aircraft have a limitation such that flap extension at high altitudes (typically above FL200) is prohibited. This is because ?

    Stall warning and flap fatigue life may be compromised

  • 37

    With increasing altitude up to max cruise level ?

    Low, and high speed stall buffet speed IAS values become closer together

  • 38

    An excessively aft CoG when on approach to land will cause?

    Light elevator control forces and decreased pitch stability

  • 39

    The CoG is near its forward envelope limit, Which statement is most correct ?

    Greater elevator force is required to change the pitch attitude than with an aft CoG

  • 40

    as altitude is gained , how is the low speed stall value effected ?

    Both IAS and EAS values increase, EAS will always be equal to or less than IAS value

  • 41

    A Trip Free circuit breaker can be reset ?

    When the bi metalic strips have cooled

  • 42

    The ZFW limit imposed on some aircraft is to ensure the spar is not overstressed and is ?

    Relevant at takeoff weight only

  • 43

    During a climb at a constant mach number, the angle of attack will ?

    Increase

  • 44

    In stable asymmetric flight ?

    Bank and rudder are used in coordination to counteract the yaw produced by the live engine

  • 45

    Greater rearward wing sweep?

    Reduces trailing edge flap effectiveness

  • 46

    Which of the answers is incorrect about factors assisting lateral static stability

    Inboard flaps

  • 47

    An aircraft fitted with two EADI and 2 EHSI . what is the minimum number of symbol generators required for all screens to be operational ?

    2

  • 48

    Which answer listed is correct regarding aircraft system warnings whilst the aircraft is taking off ?

    Cautions are automatically inhibited from 80kts to 400ft RA or 20 seconds after lift off, whichever occurs first

  • 49

    Which does not effect hydroplanning speed ?

    Tyre Size

  • 50

    Which RPM range will produce the greatest variation in thrust for a given movement of the power lever ?

    The upper end of the rpm range

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    問題一覧

  • 1

    What is the primary advantage of AC over DC electrical generation types?

    Saving in space and weight

  • 2

    An aircraft is fitted with NiCad batteries, the crew get a high battery temp warning light. This situation is probably caused by?

    The rate of charging was too high

  • 3

    After a 'wet start' in a turbine engine, what precautions should be taken to prevent a future engine malfunction ?

    Motor over to prevent torching when re starting

  • 4

    With increasing airspeed up to and beyond Mach 1.0, the co-efficient of drag and a constant angle of attack will?

    Initially increase, then decrease

  • 5

    The purpose of a cabin pressure relief valve is to automatically open when ?

    Cabin differential pressure reaches a pre set value

  • 6

    The valve that controls the air pressure in a cabin pressurisation system is known as?

    The outflow valve

  • 7

    Which of the following correctly names the component in a pneumatic system that will automatically shut off the air supply to non-essential services, when system pressure reduces below a certain predetermined value?

    Pressure maintaining valve

  • 8

    In what way is the SG of Avtur effected by changes in ambient temperature ?

    SG decreases with temperature rise

  • 9

    Under which of the following conditions is it necessary to incorporate cabin air humidifiers in an aircraft air conditioning system?

    At high altitudes at all times

  • 10

    Hydraulic fluid has which of the following properties ?

    Is is almost incompressible

  • 11

    When comparing the properties of pneumatic vs hydraulic systems?

    Pneumatics do not require return lines but hydraulic systems do

  • 12

    In what way does the extension of leading edge devices such as flaps and slats effect the co efficient of lift and drag, and the nose pitching moment ?

    Increase in lift and drag coefficients, and a nose up pitch moment

  • 13

    Assuming the same degree of trailing edge flap deflection, which answer best describes the primary advantage of slotted flaps, compared to fowler flaps

    Improved boundary layer airflow over flaps

  • 14

    Assuming the aircraft is within the various radio altitude envelope bands, in which of the following scenarios will the flight crew receive a warning

    When an unsafe radio height is reached, with the aircraft NOT in the landing configuration

  • 15

    Assuming a constant speed drive is disconnected in flight when, and under what circumstance can it be reconnected ?

    Mechanically, when the aircraft is on the ground

  • 16

    Which of the following best describes how an APU speed is controlled ?

    By a governor

  • 17

    The device that controls the direction of movement of a hydraulic actuating unit, is called the ?

    Selector valve

  • 18

    Which of the following switches must be closed before a generator can be connected to the synchronising bus?

    The bus tie breaker switch

  • 19

    Which answer best describes the disadvantage of a turboprop engine, compared to a turbojet engine ?

    Lower propulsive efficiencies at high subsonic mach numbers

  • 20

    The auto land status annunciator

    Monitors only autopilot and autopilot support system integrity

  • 21

    A swept wing transport turbojet is cruising at higher than normal operating altitude, at normal cruise mach number, in non turbulent conditions. If it experiences buffet, which statement is correct ?

    It could be high or low speed buffet, as it is difficult to tell at high altitude

  • 22

    Shockwaves can form at a true mach number below Mach 1.0 , this is because?

    Curved surfaces in various parts of the aircraft accelerate the air to greater than free stream mach number

  • 23

    A control tab that is moved by the main control linkage, such that the hinge moments cause a deflection of the primary control surface. This device is called a ?

    Servo tab

  • 24

    High flying air transport aircraft have a fuel tank venting system, this is to?

    Ensure the tank walls do NOT rupture when in turbulence or during manoeuvres

  • 25

    What is the reason why the hydraulic reservoir is pressurised in high flying aircraft ?

    To prevent the fluid from foaming due to low ambient pressures at high altitudes

  • 26

    An aircraft is fitted with TCAS and GPWS. Which statement is most correct ?

    Both TA's and RA's are inhibited by GPWS warnings

  • 27

    The B767 incorporates a typical autopilot flight director systems (AFDS). When an ILS is being flown, with the Altitude Hold and Approach modes selected, which statement best represents the actions that follow ?

    The system is armed to capture the glideslope and altitude hold will automatically cancel when this occurs

  • 28

    The manoeuvre envelop defines?

    The speed/load factor limits within which the aircraft is to be operated

  • 29

    Manual reversion is provided?

    On aircraft that do not have triple hydraulic system redundancy

  • 30

    An aircraft accelerated beyond Mcrit, if not corrected by the Mach Trimmer, it can display a nose down tendency. This is due to ?

    The rearward movement of the centre of pressure and reduced tailplane down load

  • 31

    On large transport aircraft, the effect of a failure of leading edge high lift devices to extend is to ?

    Require a lower than normal attitude, and a higher airspeed on approach

  • 32

    With an increase in altitude, and same equivalent airspeed (EAS) spiral stability ?

    Increases

  • 33

    Which statement is most correct?

    The primary function of ground spoilers is to reduce lift and increase braking effectiveness

  • 34

    AS the sped of a large transport aircraft increases from low speed stall to Mmo, the power requirements during this phase can be best described as ?

    Decrease than increase

  • 35

    The primary reason for fitting leading and trailing edge flaps is to ?

    Reduce the landing and takeoff speeds and distances needed

  • 36

    A number of swept wing jet transport aircraft have a limitation such that flap extension at high altitudes (typically above FL200) is prohibited. This is because ?

    Stall warning and flap fatigue life may be compromised

  • 37

    With increasing altitude up to max cruise level ?

    Low, and high speed stall buffet speed IAS values become closer together

  • 38

    An excessively aft CoG when on approach to land will cause?

    Light elevator control forces and decreased pitch stability

  • 39

    The CoG is near its forward envelope limit, Which statement is most correct ?

    Greater elevator force is required to change the pitch attitude than with an aft CoG

  • 40

    as altitude is gained , how is the low speed stall value effected ?

    Both IAS and EAS values increase, EAS will always be equal to or less than IAS value

  • 41

    A Trip Free circuit breaker can be reset ?

    When the bi metalic strips have cooled

  • 42

    The ZFW limit imposed on some aircraft is to ensure the spar is not overstressed and is ?

    Relevant at takeoff weight only

  • 43

    During a climb at a constant mach number, the angle of attack will ?

    Increase

  • 44

    In stable asymmetric flight ?

    Bank and rudder are used in coordination to counteract the yaw produced by the live engine

  • 45

    Greater rearward wing sweep?

    Reduces trailing edge flap effectiveness

  • 46

    Which of the answers is incorrect about factors assisting lateral static stability

    Inboard flaps

  • 47

    An aircraft fitted with two EADI and 2 EHSI . what is the minimum number of symbol generators required for all screens to be operational ?

    2

  • 48

    Which answer listed is correct regarding aircraft system warnings whilst the aircraft is taking off ?

    Cautions are automatically inhibited from 80kts to 400ft RA or 20 seconds after lift off, whichever occurs first

  • 49

    Which does not effect hydroplanning speed ?

    Tyre Size

  • 50

    Which RPM range will produce the greatest variation in thrust for a given movement of the power lever ?

    The upper end of the rpm range