All Papers

Radio Navigation — Sample Paper 3

50 questions · pass mark 70% · answer at your own pace, then submit for the full key.

Q1.

GPS orbital height:

Q2.

VOR frequency band:

Q3.

In order to Tune, Identify and Monitor N0NA1A NDB emissions the BFO should be used as follows:

Q4.

AWR colour — weakest precipitation:

Q5.

UK VFR conspicuity squawk:

Q6.

Primary radar PRF = 450 pps. Maximum range (ignoring PW and flyback):

Q7.

Selectable overlays available in MAP mode include:

Q8.

Navigation and system data message transmitted through:

Q9.

The maximum range an aircraft at 2500 ft can communicate with a VHF station at 196 ft is:

Q10.

Maximum range determined by:

Q11.

DME ident interval:

Q12.

SBAS geostationary orbit altitude:

Q13.

Mode S data link direction:

Q14.

ILS LOC beam width adjusted to give:

Q15.

VOR variation should be applied at:

Q16.

NAVSTAR/GPS operates in the ___ band; receiver determines position by ___:

Q17.

GPS constellation: total operational SVs:

Q18.

A ground DME transponder becomes saturated at approximately:

Q19.

Primary radar cannot determine:

Q20.

GPS horizontal accuracy (SPS, 95%):

Q21.

MLS channels:

Q22.

VORTAC: civil aircraft uses:

Q23.

The minimum angle at which a false glide path is likely to be encountered on a 3° glide path is:

Q24.

Due to 'Doppler' effect an apparent decrease in the transmitted frequency, which is proportional to the transmitter's velocity, will occur when:

Q25.

Earth model used for NAVSTAR/GPS:

Q26.

GPS RAIM — SVs for fault detection only:

Q27.

GPS ephemeris — sub-frames:

Q28.

The coverage of the Microwave Landing System in the UK extends to ___ up to a height of ___ and ___ either side of the on-course line.

Q29.

Mode S ICAO address size:

Q30.

The magnitude of the error in position lines derived from ADF bearings that are affected by coastal refraction may be reduced by:

Q31.

GNSS availability — definition:

Q32.

The DME frequency band is:

Q33.

Wavelength of 375 kHz NDB signal:

Q34.

Which of the following is NOT a waypoint definition format for the CDU:

Q35.

Aircraft on 152° radial. OBS set to 329° (TO). CDI indication:

Q36.

Pulse width 2 µs. Minimum range:

Q37.

PRN codes are used to determine range by:

Q38.

Correct format to input position 50°N 005°27'E to the CDU:

Q39.

AWR antenna is stabilised:

Q40.

TAR maximum range:

Q41.

The DME interrogator pulse rate in the SEARCH phase is approximately:

Q42.

Mode C P1–P3 spacing:

Q43.

VOR variation applied at:

Q44.

VOR ident transmission interval:

Q45.

Mode C altitude referenced to:

Q46.

Echo time is 1720 µs. Range of target:

Q47.

To double the range of a primary radar requires power to be increased by a factor of:

Q48.

DME number of channels:

Q49.

AWR HOLD function:

Q50.

Quadrantal error in ADF caused by:

0/50 answered