Posible Examen de Navegación Aérea

Question

1. The NAVSTAR/GPS control segment comprises:

Answer 1

a) The space segment the user segment and the ground segment

Answer 2

b) A ground segment and the INMARSAT geostationary satellites

Answer 3

c) A master control station, a back-up control station and five monitoring stations

Answer 4

d) A master control station, a back-up control station, five monitoring station and the INMARSAR geostationary satellites

Answer 5

a) Centre Map

Answer 6

d) Expanded nav

Answer 7

a) Full ILS

Answer 8

b) Full VOR

Answer 9

c) Full nav

Answer 10

d) Full map

Answer 11

a) 0.25 nm

Answer 12

a) Twin DME

Answer 13

b) VOR/DME

Answer 14

c) Twin VOR

Answer 15

d) Any of the above

Answer 16

a) In Pitch, roll and yaw

Answer 17

b) In pitch and roll

Answer 18

c) In pitch and roll but only when 0º tilt has been selected

Answer 19

d) In pitch and roll whether the stabilization is on or off

Answer 20

a) Flying over land with the Land/sea switch in the sea position

Answer 21

b) Flying over mountainous terrain

Answer 22

c) There is cloud and precipitation between the aircraft and a cloud target

Answer 23

d) Attempting to use the mapping beam for mapping in excess of 50nm.

Answer 24

a) Aircraft transmit and receive on different frequencies.

Answer 25

b) Aircraft will only accept unique twin pulses

Answer 26

c) Aircraft reject pulses not synchronized with its own random pulse recurrence rate

Answer 27

d) Each aircraft has its own frequency allocation

Answer 28

a) 3% of rangev

Answer 29

b) 1.25% of range

Answer 30

d) +/-0.25 +/-1.25% of range

Answer 31

a) Utilizes paired pulses transmitted from ground station to the aircraft at a specific spacing

Answer 32

b) Utilizes paired pulses transmitted from the aircraft to a ground station at a specific spacing

Answer 33

c) Utilizes paired pulses transmitted from ground station to the aircraft at a specific frequency

Answer 34

d) Utilizes paired pulses transmitted from the aircraft to a ground station at a specific frequency

Answer 35

a) Provides ground distance from aircraft to the station. By applying a simple formula can also know the slant Range

Answer 36

b) The GS provided by the DME equipment can be consider valid when distance(DME) is minor than the height in thousands of feet 100

Answer 37

c) Above 5000 feet GS can always be considered exact, it doesn’t matter the DME distance.

Answer 38

d) All the options are false.

Answer 39

a) With 1radial anticipation

Answer 40

b) With 4 radial anticipation

Answer 41

c) With 2 radial anticipation

Answer 42

d) No anticipation is needed

Answer 43

a) Aparece banderola Nav

Answer 44

b) Aparece banderola HDG

Answer 45

c) Aparece banderola NDB

Answer 46

d) No hay indicación

Answer 47

a) Consist of a Flight Management Computer(FMC), one or more Control Display Units(CDU), one or more Display Unit(DU), a Data Base and an Emergency Navigation System

Answer 48

b) The FMS utilizes aircraft sensors and navigation database information to compute and display aircraft position, performance data, and navigation information during all phases of flight.

Answer 49

c) Both are correct

Answer 50

d) None are correct

Answer 51

a) Three marker beacons are located along ILS final to “mark” a specific position along the approach course, and are depicted on the terminal chart by the letters OM, MM an IM,. All of them must always be installed for every ILS approach.

Answer 52

b) Minimum are normally reached at or near de MM whereby if an aircraft is on glideslope, it will be at an altitude of approximately 200 feet above the elevation of the touchdown zone. The MM may not be used as the sole method of identifying the MAPt.

Answer 53

c) Inner marker- A marker beacon located between the MM and the OM, transmitting a radiation pattern keyed at six dots per second and indicating to the pilot, both aurally and visually, that he/she is at the designated decision height(DH), normally 100 feet above touchdown zone elevation.

Answer 54

d) Marker beacons are not installed for navigation purposes, but indicate a specific point on the localizer course to provide information of aircraft position in relation to the runway. If it were not possible to install marker beacons would be wishable to have a DME system associated.

Answer 55

a) Two highly directional transmitting systems

Answer 56

b) As many as three marker beacons or compass locators

Answer 57

c) Optional DME transmitters

Answer 58

d) Malfunction indication system

Answer 59

a) An energy wave comprising an electrical field in the same plane as a magnetic field

Answer 60

b) An electrical field alternating with a magnetic field

Answer 61

c) An energy wave where there is an electrical field perpendicular to a magnetic field

Answer 62

d) An energy field with an electrical component

Answer 63

a) 4298 GHz

Answer 64

b) 4,298 GHz

Answer 65

c) 429,8 GHz

Answer 66

d) 42,98 GHz

Answer 67

a) Absortion

Answer 68

b) Diffraction

Answer 69

c) Attenuation

Answer 70

d) ionisation

Answer 71

a) Further from the coast

Answer 72

b) Closer to the coast

Answer 73

c) Co-incident

Answer 74

d) Inaccurate due to the transmitted wave front decelerating

Answer 75

a) Static build up on the airframe and St. Elmo’s Fire

Answer 76

b) The aircraft’s major electrical axis, the fuselage, reflecting and re-radiating the incoming NDB transmissions.

Answer 77

c) Station interference and/or night effect

Answer 78

d) NDB signals speeding up and bending as they cross from a land to water propagation path.

Answer 79

a) Is most marked at night

Answer 80

b) Can be minimized by using beacons situated well inland

Answer 81

c) Can be minimized by taking bearings where the signal crosses the costline at right angles

Answer 82

d) Os most marked one hour before to one hour after sunrise and sunset

Answer 83

a) The DVOR provides DME distance to the station

Answer 84

b) The DVOR is second generation VOR but provides the same signal quality and accuracy as a regular VOR

Answer 85

c) The DVOR is the combination of TACAN and VOR

Answer 86

d) The DVOR avoids errors caused by reflected signals

Answer 87

a) 10º, 35

Answer 88

b) 35º, 10

Answer 89

c) 35º, 17

Answer 90

d) 25º, 25

Answer 91

a) ±8 out to 10nm

Answer 92

b) ±10º out to 8nm

Answer 93

c) ±12º out to 17nm

Answer 94

d) ±35º out to 25nm

Answer 95

a) Will receive false on-course or reverse sense signals

Answer 96

b) Will not normally receive signals

Answer 97

c) Will receive signals without coding

Answer 98

d) Can expect signals to give control indications.

Answer 99

a) 20nm; 20000ft; 40 degrees

Answer 100

b) 35nm; 5000ft; 40 degrees

Answer 101

c) 35nm; 5000ft; 30 degrees

Answer 102

d) 17nm; 2000ft; 35 degrees

Answer 103

a) Black, yellow, green, magenta

Answer 104

b) Black, green, yellow, magenta

Answer 105

c) Grey, green, yellow, red

Answer 106

d) Black, green, yellow, red.

Answer 107

a) Primary 8800Mhz SHF

Answer 108

b) Secondary 9.375Mhz UHF

Answer 109

c) Secondary 9375Mhz SHF

Answer 110

d) Primary 9375 Mhz SHF

Answer 111

a) It causes a momentary distinctive display to appear on the controller’s screen.

Answer 112

b) An identification pulse is automatically and continuously transmitted for 20 seconds, 4.35µ sec before the last framing pulse

Answer 113

c) An identification pulse is automatically and continuously transmitted for 10 seconds, 4.35µ sec after the las framing pulse.

Answer 114

d) An identification pulse is automatically and continuously transmitted for 20 seconds 4.35µ sec after last framing pulse

Answer 115

a) 7700; 7600; 2000; 7500

Answer 116

b) 7700; 7600; 7500; 2000

Answer 117

c) 7600; 7500; 2000; 7700

Answer 118

d) 7500; 7600; 2000; 7700

Answer 119

a) A target which will respond to the interrogation, and this target will always be an aircraft

Answer 120

b) A target which will respond to the interrogation, and this target will always be ground based

Answer 121

c) A target which will respond to the interrogation, and this target may be either an aircraft or a ground based transponder

Answer 122

d) A quiescent target

Answer 123

a) Initiate the required manoeuver immediately

Answer 124

b) Make a note of the details

Answer 125

c) Request a flight clearance deviation from ATC

Answer 126

d) Do nothing until a TA is received

Answer 127

a) Threat, climb; threat, descend

Answer 128

b) Climb left, Climb right, Descend left, Descend right.

Answer 129

c) Climb, descend, increase climb, increase descent

Answer 130

d) Turn left, Turn right, Increase turn, Decrease turn.

Answer 131

a) Has an FM refenrence signal and an AM variable signal

Answer 132

b) Has a 150Hz reference signal and a 90Hz variable signal

Answer 133

c) Has an AM reference signal and a 150Hz variable signal

Answer 134

d) Has an AM reference signal and a FM variable signal

Answer 135

a) 1º 300; 2º 345

Answer 136

b) 1º 120; 2º 165

Answer 137

c) 1º 300; 2º 210

Answer 138

d) 1º 300; 2º 255

Answer 139

a) From the glideslope needle the captain may be receiving false course and reverse sense indications and from the localizer needle intermittent and incorrect indications.

Answer 140

b) The aircraft’s receiver is not detecting any transmissions and the ILS needle OFF flags are visible

Answer 141

c) From the localizer needle the captain may be receiving false course and intermittent indications and from the glideslope needle reverse sense and incorrect indications.

Answer 142

d) From the localizer needle the captain may be receiving false course and reverse sense indications and from the glideslope needle intermittent and incorrect indications.

Answer 143

a) RAs may be disregarded only when the pilot visually identifies the potentially conflicting traffic and decides that no deviation is necessary and has the clearance confirmed by ATC

Answer 144

b) RAs may be disregarded only when the pilot visually identifies the potentially conflicting traffic and decides that no deviation is necessary and has advised ATC of the other aircraft’s proximity

Answer 145

c) RAs mist never be disregarded

Answer 146

d) RAs may be disregarded only when the pilot visually identifies the potentially conflicting traffic and decides that no deviation is necessary.

	Erstellt von Juanan Aroca Balsalobre vor etwa 7 Jahre

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Posible Examen de Navegación Aérea

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