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Questions for INDIGO RADIO NAVIGATION

Answer the following questions

1.

What is the minimum level that an aircraft, at a range of 113 NM, must fly in order to contact the tower on R/T for a VDF bearing from an airport sited 169 FT above MSL?

2.

A Category 1 Instrument Landing System (ILS) ground installation provides accurate guidance from coverage limit down to

3.

In which one of the following circumstances is ground direction finding (VDF) likely to be used to fix an aircraft's position?

4.

What is the maximum number of usable Secondary Surveillance Radar (SSR) transponder codes?

5.

In which frequency band do VOR transmitters operate?

6.

The maximum theoretical range at which an aircraft at FL210 may receive signals from a VOR facility sited 340 feet above mean sea level is approximately

7.

ADF bearings by an aeroplane by day within the published protection range should be accurate to within a maximum error of

8.

In an Electronic Flight Instrument System (EFIS) data relating primarily to navigation is provided by

9.

In which frequency band does the Microwave Landing System (MLS) operate?

10.

At what approximate height above the WGS-84 ellipsoid are NAVSTAR/GPS satellites circling the earth?

11.

In relation to radar systems that use pulse technology, the term 'Pulse Recurrence Rate (PRR)' signifies the

12.

In order to indicate an emergency situation, the aircraft Secondary Surveillance Radar (SSR) transponder should be set to

13.

An aircraft DME receiver does not lock on to its own transmissions reflected from the ground because

14.

Ignoring pulse length, the maximum pulse repetition frequency (PRF) that can be used by a primary radar facility to detect targets unambiguously to a range of 200 NM is:(pps = pulses per second)

15.

Which of the following coordinate systems is used by the GPS receiver to determine position (Latitude, longitude and altitude)?

16.

Airborne weather radar systems use a wavelength of approximately 3 cm in order to

17.

The minimum range of a primary radar, using the pulse technique, is determined by the (i)........ , the maximum unambiguous range by the (ii).........

18.

Which of the following is the ICAO allocated frequency band for ADF receivers?

19.

In the NAVSTAR/GPS satellite navigation system, 'Selective Availability' (SA) gives the option to artificially degrade the accuracy by

20.

In relation to Area Navigation Systems (RNAV), which of the following is an Air Data input?

21.

What type of satellite navigation system NAVSTAR/GPS receiver is most suitable for use on board an aircraft?

22.

Where, in relation to the runway, is the ILS localiser transmitting aerial normally situated?

23.

The database of an FMS (Flight Management System) is organised in such a way that the pilot can

24.

A DME in tracking mode subsequently experiences a reduction in signal strength will switch the equipment in the first instance to

25.

The DME (Distance Measuring Equipment) operates within the following frequencies

26.

Given:Magnetic heading 280°VOR radial 090°What bearing should be selected on the omni-bearing selector in order to centralise the VOR deviation needle with a ""TO"" indication?

27.

The ATC transponder system,excluding Mode S, contains

28.

Which one of the following is an advantages of a multi-sensor system using inputs from a global navigation satellite system (GNSS) and an inertial navigational system (INS)?

29.

An RMI indicates aircraft heading. To convert the RMI bearings of NDBs and VORs to true bearings the correct combination for the application of magnetic variation is

30.

The ground Secondary Surveillance Radar (SSR) equipment incorporates a transmitter and receiver respectively operating in the following frequencies: Transmitter Receiver

31.

An aircraft carrying out a 3° glidepath ILS approach experiences a reduction in groundspeed from 150 kt at the outer marker to 120 kt over the threshold. The effect of this change in groundspeed on the aircraft's rate of descent will be a decrease of approximately

32.

The basic elements of the satellite navigation system NAVSTAR/GPS are the

33.

In which situation will speed indications on an airborne Distance Measuring Equipment (DME) most closely represent the groundspeed of an aircraft flying at FL400?

34.

In which frequency bands are the L1 and L2 frequencies used by the satellite navigation system NAVSTAR/GPS for transmission of the navigation message?

35.

An aircraft at FL 100 should be able to receive a VOR groundstation at 100 FT above MSL at an approximate maximum range of

36.

For a conventional DME facility 'Beacon Saturation' will occur whenever the number of simultaneous interrogations exceeds

37.

A DME is located at MSL.An aircraft passing vertically above the station at flight level FL 360 will obtain a DME range of approximately

38.

The selection of code 7600 on an aircraft SSR transponder indicates

39.

GPS satellites transmit on two L-band frequencies with different types of signals. Which of these are generally available for use by civil aviation?

40.

The track-line on the Electronic Horizontal Situation Indicator (EHSI) or Navigation Display of an Electronic Flight Instrument System

41.

An aircraft is required to approach a VOR via the 104° radial. Which of the following settings should be made on the VOR/ILS deviation indicator?

42.

In relation to the satellite navigation system NAVSTAR/GPS, which of the following statements correctly describes the term 'Pseudo Random Noise (PRN)' signal?

43.

In order to obtain an ADF bearing the

44.

In the event of the use of Selective Availability, how does this affect, if at all, the navigation accuracy of the NAVSTAR/GPS satellite navigation system ?

45.

ICAO Annex 11 defines Area Navigation (RNAV) as a method of navigation which permits aircraft operation on any desired flight path

46.

Which combination of characteristics gives best screen picture in a primary search radar?

47.

The aircraft DME receiver cannot lock on to interrogation signals reflected from the ground because

48.

There are two NDBs, one 20 NM inland, and the other 50 NM inland from the coast. Assuming that the error caused by coastal refraction is the same for both propagations, the extent of the error in a position line plotted by an aircraft that is over water will be

49.

What is the approximate angular coverage of reliable navigation information for a 3° ILS glide path out to a distance of 10 NM?1.35° above the horizontal to 5.25° above the horizontal and 8° each side of the localiser centreline

50.

Which frequency band is used by VOR transmissions?