1. Parcial 3 Serna

Question

Q1. What means that an aircraft has 60 min ETOPS?

Answer 1

That 60 minutes after take-off, one engine will flame out.

Answer 2

60 minutes is the maximum endurance of the aircraft

Answer 3

That the aircraft can keep flying 60 minutes without an engine.

Answer 4

The time necessary to start the engines up is 60 minutes.

Answer 5

Extended-range Twin-engine Operational Performance Standards.

Answer 6

Extended-range Twin-engine Of Pitot Saturation

Answer 7

Engine Taking Off Performances Standards.

Answer 8

Extended-range Twin-engine Of Pilot Specialization.

Answer 9

a) Air temperature

Answer 10

b) All parameters in relation with the Pitot Static System

Answer 11

c) A and B are correct

Answer 12

d) The temperature of the engine.

Answer 13

a) Equal to SAT (Static Air Temperature)

Answer 14

b) Equal to SAT (Static Air Temperature) + RAM rise.

Answer 15

c) Less than SAT (Static Air Temperature)

Answer 16

d) None of above

Answer 17

a) A thermistor thermometer

Answer 18

b) Direct Reading Thermometer

Answer 19

c) Optical Pyrometers

Answer 20

d) None of above

Answer 21

The pitot-tube must has a drain hole

Answer 22

The pitot-tube must has a system that prevent ice formation

Answer 23

In large aircraft is a system that used to be redundant

Answer 24

All of above are correct.

Answer 25

The pitot-tube must has a drain hole

Answer 26

The pitot-tube must has a system that prevent ice formation

Answer 27

In large aircraft is a system that used to be redundant

Answer 28

All of above are correct.

Answer 29

a) Because it is cool

Answer 30

b) In order to ensure the right measurement at different aircraft attitudes

Answer 31

c) To do it a redundant system.

Answer 32

d) B and C are correct.

Answer 33

Temperature is calculated by the average of two measurements.

Answer 34

In order to do the measurement is needed a reference temperature that never changes.

Answer 35

It is built by two direct reading thermometers

Answer 36

All of above are correct

Answer 37

Low precission resistance

Answer 38

Need electrical source

Answer 39

Measurement at large distance

Answer 40

Thin temperature range chaning sensor resistance

Answer 41

Allows any moisture to leak away without affecting sensing pressure

Answer 42

Prevent ice formation

Answer 43

To ensure right measurement at different aircraft attitudes (minimize position error)

Answer 44

Redundancy of the system

Answer 45

A. Static pressure.

Answer 46

B. Total pressure due to the aircraft motion

Answer 47

C. A and B.

Answer 48

D. Pressure inside the cockpit.

Answer 49

A. Static ports place (position error)

Answer 50

B. Blockage of ports and lines

Answer 51

C. Rupture of lines

Answer 52

D. A, B and C are true

Answer 53

Hysteresis

Answer 54

Material aging

Answer 55

Temperature error

Answer 56

The mechanical movement of the capsule is transmitted mechanically

Answer 57

It moves a bar (I-bar) that modifies an electrical signal sent to an electrical motor.

Answer 58

Feedback system must recover the final position of the bars

Answer 59

The solenoid is attached to the I-bar

Answer 60

Pitot-static measurement

Answer 61

Bernouilli ́s principle

Answer 62

Both are true

Answer 63

Both are fase

Answer 64

Instrument errors

Answer 65

Manouvre induced error

Answer 66

Error of the electric signals

Answer 67

HUD(head up display)

Answer 68

Vertical Gyroscope

Answer 69

Suctioning air by venture law

Answer 70

Electrical power with an electrical rotor

Answer 71

Blowing air that have an impact on the surface of it.

Answer 72

All answer are correct

Answer 73

Erection mechanism

Answer 74

Compass controller

Answer 75

Radio-calibrators

Answer 76

Gyroscope principal

Answer 77

Rigid body with one principal moment of inertia much larger than the other two, in high spin around its axis of maximum inertia.

Answer 78

Rigid body with one principal moment of inertia much smaller than the other two, in high spin around its axis of minimum inertia.

Answer 79

Flexible body with one principal moment of inertia much smaller than the other two, in high spin around its axis of minimum inertia.

Answer 80

Flexible body with one principal moment of inertia much larger than the other two, in high spin around its axis of minimum inertia.

Answer 81

A. Rigidity

Answer 82

B. Precession

Answer 83

D. A and B are correct

Answer 84

Rigidity is one of the properties of the gyroscopes to resistance of the spin axis to tilting

Answer 85

Precession is one of the properties of the gyroscopes to resistance of the spin axis to tilting

Answer 86

Both are false

Answer 87

Both are true

Answer 88

None of the above

Answer 89

None of the above

Siguiente

1. Parcial 3 Serna

Descripción

Resumen del Recurso

Pregunta 1

Pregunta 2

Pregunta 3

Pregunta 4

Pregunta 5

Pregunta 6

Pregunta 7

Pregunta 8

Pregunta 9

Pregunta 10

Pregunta 11

Pregunta 12

Pregunta 13

Pregunta 14

Pregunta 15

Pregunta 16

Pregunta 17

Pregunta 18

Pregunta 19

Pregunta 20

Pregunta 21

Pregunta 22

Pregunta 23

Pregunta 24

Pregunta 25

Similar

	Creado por Ismael Vázquez hace alrededor de 6 años