Samra: Radio Communication And Nav Aids Flashcards
Time to NDB in minutes formula
Time in seconds / relative bearing change
Distance to NDB formula
(Ground speed in knots x time to NDB in minutes) / 60
Bearing to station
MH+RB
Vor range formula
- 23 X square root altitude above station
- 23
- 23x square root height of station plus height of terrain around station
An ILS Localizer provides valid and reliable signal coverage out to 10 nm at a spay of how many degrees per side?
35
Certified airport, aircraft following the on slope signal PA PI are provided with safe obstruction clearance to a minimum of
6° on either side of the extended runway centreline out to 7.5 km from the runway threshold
VLF radio range
3 to 30 kHz
What is CPDLC?
Controller Pilot data link communications, text message communication
VHF
ACARS
Aircraft communications addressing and reporting system, receives update messages of weather conditions along with Plan and route, and send messages about the conditions of onboard equipment. ACARS transmissions are made via VHF & HF and supported by satellite communications in oceanic areas
GPS position is accurate
 horizontally 6 m vertically 8 m 95% of the time
RNAV definition
Method of navigation permitting aircraft operation on any desired flight path within the coverage of station-referenced NAVAIDs or within the limits of the capability of self contained navaids or a combination of these
Wave length sizes
The higher the frequency the smaller the wavelength. Small wave length is 10 cm for a UHF, and the bigger is 10 km for the LF
Multilateration Is technology used to accurately locate the aircraft by measuring its distance from ground stations placed in strategic locations around an aerodrome
MLAT  uses ground stations that interrogate and receive replies from aircraft transponders, aircraft are located by principle known as time difference arrival, aircraft using MLAT must have mode E, C, or S transponders or ADS-B and some MLAT systems are directly linked to ADS-B
FMS system is comprised of what?
FMS system is comprised of an automatic flight control system or automatic flight guidance system, flight management computer, navigation sensors (IRS or radio navigation), A control display unit and a primary flight display and or multifunction display