50 questions · pass mark 70% · answer at your own pace, then submit for the full key.
Q1.
ILS false glideslope strongest at:
Q2.
Max beacon spacing for airway with ±5 NM half-width, VOR error 5°:
Q3.
When flying over the sea and using an inland NDB to fix position with a series of position lines, the plotted position in relation to the aircraft's actual position will be:
Q4.
DME accuracy standard (en-route) is:
Q5.
ILS CAT IIIB minima:
Q6.
Best action to insert accurate IRS position using POS INIT page (Appendix A):
Q7.
GPS L1 frequency:
Q8.
Frequency band and scan rate of Airfield Surface Movement radars:
Q9.
Class 'B' VHF DF bearings are accurate to within:
Q10.
The BFO facility on ADF equipment should be used as follows when an NDB having N0NA1A type emission is to be used:
Q11.
The main advantage of continuous wave (CW) radars is:
Q12.
An aircraft is intending to track from NDB 'A' to NDB 'B' on a track of 050°(T), heading 060°(T). If the RBI shows the relative bearing of 'A' to be 180° and the relative bearing of 'B' to be 330° then the aircraft is:
Q13.
ILS receivers showing predominant 90 Hz on both localizer and glide slope; runway QDM 264°. Aircraft is:
Q14.
Two NDBs — 20 NM from coast vs 50 NM inland. Greatest coastal refraction error?
Q15.
Positions input to FMC using maximum 5 alphanumerics:
Q16.
4D RNAV adds to 3D capability:
Q17.
DME transponder offset:
Q18.
The upper and lower limits of an ILS glide path transmitter having a 3.5° glide slope are:
Q19.
SSR transponder receives on ___, replies on ___:
Q20.
Radial resolution improved by:
Q21.
ILS outer marker: tone and light:
Q22.
An aircraft on a heading of 235°(M) shows an RMI reading of 090° with respect to an NDB. Any quadrantal error which is affecting the accuracy of this bearing is likely to be:
Q23.
VORTAC provides:
Q24.
When a DME is operating in the TRACKING phase, it interrogates at approximately:
Q25.
Aircraft on radial 270°, heading 090° inbound to VOR, OBS set to 090°. TO/FROM indicator shows:
Q26.
Squawk 7700:
Q27.
The principal propagation path employed in an NDB/ADF system is:
Q28.
Most significant ADF error:
Q29.
ILS CAT IIIC minima:
Q30.
Middle marker approximately:
Q31.
DME frequency band:
Q32.
GPS time accuracy (SPS, 95%):
Q33.
PDOP (Position Dilution of Precision) — best geometry:
Q34.
The frequency band containing the frequency corresponding to 29.1 cm is:
Q35.
A category II ILS installation in the UK:
Q36.
A radio wave is:
Q37.
VORTAC differs from VOR/DME in that:
Q38.
ILS glidepath accuracy requirement:
Q39.
The range promulgated in the AIP and flight guides for all NDBs in the UK is the range:
Q40.
ELS (Elementary Surveillance) provides:
Q41.
RAIM — what does it detect?
Q42.
The phenomenon of coastal refraction which affects the accuracy of ADF bearings:
Q43.
The DOC of a VOR is valid:
Q44.
GLONASS orbital period:
Q45.
ADF action for bearing — which aerials?
Q46.
VOR scalloping caused by:
Q47.
A VOR/DME pairing applies in a TMA when the equipment is within: