2. Parcial 3 Ser

Question

Q9. What does RIC/GMC mean?

Answer 1

Remote Indicating Compass / Gyro Magnetic Compass

Answer 2

Remote Indicating Compass / Gravity Measurements Compass

Answer 3

Range of Internal Calibration / Gyro Magnetic Calibration

Answer 4

Remote Internal Calibration / Gyro Magnetic Calibration

Answer 5

Where aircraft magnetic perturbations are greater

Answer 6

Where the instruments have more air cooler flow

Answer 7

Where aircraft magnetic perturbations are not important

Answer 8

All of the above are correct

Answer 9

Turn indicator displays the rate of, and direction of turn, using gyroscopic principles.

Answer 10

Balance indicator shows if the plane performs balanced or unbalanced turn (skidding or sideslipping)

Answer 11

In general, the instrument show how the aircraft change the pitch.

Answer 12

Balance indicator has a black ball in a liquid filled glass tube.

Answer 13

The velocity and position of the aircraft is obtained by measuring its acceleration and integrating it twice.

Answer 14

A disadvantage is that we have to measure the acceleration vector, in module and direction, and perform integrals

Answer 15

An advantage is that it is not necessary a good precision of the system alignment with True North, because the quality information not depends on that.

Answer 16

Classification: Gimballed INS and Strapdown INS.

Answer 17

Inertial Navigation Unit

Answer 18

Mode Selector Unit

Answer 19

Control Display Unit

Answer 20

All of the above are correct

Answer 21

Inertial Reference System

Answer 22

Internal Resistance Source

Answer 23

Inertial Refuse System

Answer 24

Internal Reducing Sound

Answer 25

A. Typically triangular but other shapes are possible

Answer 26

B. Low stable (with temperature) material to avoid undesired dilatations/contractions.

Answer 27

C. He+Ne mixture at low pressure

Answer 28

D. A and C are correct.

Answer 29

High reliability (no moving parts)

Answer 30

Very high G sensitivity

Answer 31

Digital input

Answer 32

Warm-up time

Answer 33

Excessive descent rate

Answer 34

Excessive lateral deviation from localizer

Answer 35

Height lost during an approach or go around

Answer 36

Excessive downward deviation from glide path

Answer 37

Too low terrain

Answer 38

All of them

Answer 39

Set QNE (1013 mb) to the QNH of the aerodrome

Answer 40

Provide aural and visual warnings of an aircraft reaching, or deviating from a preselected altitude by using an output from a pressure altimeter or ADC

Answer 41

Warn when there is a fuel loss

Answer 42

None of them

Answer 43

Level A: Warning

Answer 44

Level B : Caution

Answer 45

Level C: Advisory

Answer 46

All are right

Answer 47

To reduce the traffic collisions

Answer 48

To avoid stall conditions

Answer 49

To avoid overspeed conditions

Answer 50

To reduce controlled flight in to terrain accidents

Answer 51

World terrain data base

Answer 52

Inertial position system in order to improve the precision

Answer 53

High precision positioning system

Answer 54

Airstrip database

Answer 55

A. Warning in rapid change of velocity ( 25 kts)

Answer 56

B. It is not compulsory

Answer 57

C. Warning in change of R0C/ROD ( greater than 500 fpm)

Answer 58

D. B and C are correct

Answer 59

A. Altimeter

Answer 60

B. Alerting unit

Answer 61

C. A and B are true

Answer 62

D. A and B are false

Answer 63

A. Control panel

Answer 64

B. Display

Answer 65

C. Mode S transponder

Answer 66

D. A, B and C are correct

Answer 67

From 15 to 100 NM

Answer 68

From 5 to 40 NM

Answer 69

From 8 to 31 NM

Answer 70

None of the above

Answer 71

Aneroid capsules

Answer 72

Smackdown tube

Answer 73

Bourdon tube

Answer 74

Capacitive

Answer 75

Piezoelectric

Answer 76

All of the above

Answer 77

Fuel and oil pressures

Answer 78

A. White indicates certain limitations

Answer 79

B. Green indicates normal operation values

Answer 80

C. A and B are correct

Answer 81

D. A is not correct and B is correct

Answer 82

It is not used

Answer 83

Take off, caution, or exceptional values

Answer 84

Landing gear is not down under 6500 feet altitude

Answer 85

None of the above

Answer 86

D. B and C are correct

Nächster

2. Parcial 3 Ser

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