18.40.6 List the factors to be considered when selecting alt

18.40.6 List the factors to be considered when selecting alternate routes and destination
alternates.
Sub Topic Syllabus Item

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(b) describe the method of indicating relief;


Relief on an aeronautical map is shown by colour shading. Areas with low terrain are generally green, where high peaks or points can be a darker shade, possibly brown or red. 

This allows the pilot to quickly distinguish the local terrain without having to read over spot heights or numbers. 

18.16.6 Convert between LMT, UTC, NZST and/or NZDT.

18.16.6 Convert between LMT, UTC, NZST and/or NZDT.
Aeronautical Charts

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(b) true altitude

a

(a) place/ bearing/distance

When making a position report in relation to a bearing and distance, an accurate bearing to or from a position, place or navigation aid; with a distance gives an accurate position report. 

rbearing

18.8.2 Define: (c) indicated airspeed (IAS)


Indicated airspeed (IAS) is the airspeed read directly from the airspeed indicator in the aircraft, displayed in knots.  

It uses the difference between total pressure and static pressure, to calculate a speed through the air

18.4.4 Explain the processes, cautions and limitations deriving track distances and bearings from a chart

18.4.4 Explain the processes, cautions and limitations when deriving track distances and
bearings from a chart.

When measuring track distances on a chart, make sure you measure in the middle of your track, that you measure accurately, and that you use the correct scale of ruler. 

When measuring bearings, make sure you line the protractor up with True North, and that you accurately read off the track line against the bearing. 

NWESBegining (X)Ending (X)Middle (✔)

(c) Rhumb Lines

Following a constant heading creates a track called a Rhumb Line. This is the easiest method of travelling from one point to another.

It is not however the shortest track. The shortest track is following the path of a great circle. To do this a constant change of heading throughout the flight is required.

Rhumb Line

A Rhumb Line cuts each Meridian at a constant angle, this angle will be our heading relative to True North. Over a large distance and as we get closer to the poles, the issue with following this path becomes apparent.

Rhumb Line 45 Rhumb Line Sphere 

To achieve the shortest track, a Great Circle path must be followed, This is more difficult as it requires many constant adjustments to the heading throughout the flight. Modern Flight Computers are perfectly suited to handle this issue

Great Circle Angle Great Circle Globe


Tracking directly along the equator or directly true north creates a path that is both a Rhumb Line and a Great Circle

Wind Triangle

[vfr_{Model p1=”windtriangle” p2=”example=yes”]

Time and Distance to a departure/destination equi-time point (ETP)

(b) time and distance to a departure/destination equi-time point (ETP)

Equi-time Point is important to know when you have a problem you need to know quickly  what to do you go return to your departure point or carry on to your destination.

No wind

In a no-wind situation it is easy it is the halfway point due to your ground speed being the same on the way out as it is on your way back home.


A B No Wind TAS 200kts Distance 400nm <- 200 ETP 200 ->



Things get a whole lot more interesting when you start adding wind in to the situation which we always seem to have.

As you will observe how the Equi-Time Points (ETP) will all moved toward the wind

Head wind

A B TAS 200kts Distance 400nm 40kts Head Wind <-<- <- 240 ETP 160 ->

  Leg  Ture Airspeed   Wind Component   Ground Speed   Distance    Time 
   A to ETP     200kts   -40kts   160kts   160mn      1hr
   ETP to B   200kts   40kts   240kts   240mn    1hr 

Head wind (Example 2)

A B TAS 100kts Distance 400nm 20kts Head Wind <-<- <- 240 ETP 160 ->

  Leg  Ture Airspeed   Wind Component   Ground Speed   Distance    Time 
   A to ETP     100kts   -20kts   80kts   160mn      2hr
   ETP to B   100kts   20kts   120kts   240mn    2hr 

Tail Wind 

A B 40kts Tail Wind ->-> TAS 200kts Distance 400nm <- 160 ETP 240 ->

  Leg  Ture Airspeed   Wind Component   Ground Speed   Distance    Time 
   A to ETP     200kts   40kts   240kts   240mn      1hr
   ETP to B   200kts   -40kts   160kts   160mn    1hr