Speed, Position Reference And Altimetry Flashcards

1
Q

Define knot

A

Nautical mile per hour. 1 knot is equal to 1 minute of latitude

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2
Q

Define ground speed, indicated airspeed, calibrated, equivalent and true airspeed.

A

GS - TAS of aircraft corrected for headwind/tailwind
IAS - on ASI, amount of air molecules moving through the wings
CAS - IAS after correcting for position and instrument errors
EAS - CAS after corrected for compressibility error. Exists when TAS > 250kts
TAS - EAS after correct density error or actual airspeed of aircraft through the air.

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3
Q

Explain how TAS is affected by changes in pressure altitude, air temp and density.

A

Pressure:
- Difference between TAS & IAS as pressure changes, as altitude increase, pressure decreases then the gap between IAS and TAS increases.

With a constant TAS and a gain in altitude, IAS will decrease.
With a constant IAS and a gain in altitude, TAS will increase.

Temperature:
- warm air less dense, flying through warm air will give an increase in TAS if IAS remains constant.

Density - the higher you fly the higher the difference between TAS and IAS due to reduction in density.

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4
Q

Speed provided by GNSS and intertial system is what?

A

INS (Inertial reference system) receives GPS data. Blends GPS data with INS data to receive optimum position. Vertically and horizontally.

Speed provide = GS

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5
Q

Define waypoint and what are the two types.

A

Location/fix which can be entered into a GPS

A specified geographical location used to define an area navigation route or the flight path of an aircraft employing area navigation (IFR).

Fly-by waypoint: a waypoint which requires turn anticipation to allow a tangential interception of the next segment of a route or procedure

Flyover waypoint: a waypoint at which a turn is initiated in order to join the next segment of a route or procedure.

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6
Q

Describe and apply position reference methods:

Place/bearing/distance

Latitude and longitude

A

Place - e.g overhead NZCH, object bears 170R at 32nm

Lat/long - s43 29 22 E172 32 04

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7
Q

Locate a position on a chart from NDB given magnetic direction to and distance from and the three types:

A

ADF points to an NDB

3 types
Fixed card- north always at top.
Rotatable card - Like a DI, always what you set
RMI - aligns to your heading

HDG + RB = BRG TO

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8
Q

From VOR given radial & DME distance, locate a position on chart

A

Radials:

Originate at the VOR
Magnetic direction away from the VOR
360º for each VOR

DME
Consists of DME ground station and airborne component, straight line distance (slant range) - use Pythagoras

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9
Q

Define Indicated altitude, True altitude, Pressure altitude, flight level, QNE, density altitude, transition level/layer/altitude, QNH and QFE

A

Indicated altitude - altitude on altimeter, corrected for position, instrument error, set by QNH
True - indicated altitude corrected for temp error, for airspace not ground
Pressure altitude - altitude where pressure is located according to ISA
Flight level - FL16
QNE - vertical distance when 1013hPa set on altimeter
Density altitude - PA corrected by density, DA = PA + 120 x (OAT - ISA)
Transition layer - when descending through Transition level set QNH on sub-scale, when climbing through Transition altitude, set 1013 on sub-scale
QNH - local mean sea level
QFE - vertical distance from specified datum height above that level

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10
Q

Explain and apply the VFR table of cursing levels below and above transition

A

NOSE: North = 270-089ºM South = 090 - 269ºM

Below transition layer: Fly an altitude (QNH)
Above transition layer: Flight at flight level (QNE)

Lowest causing level is 3000ft, always add 1000ft above highest terrain. And 500ft for VFR levels and 1000ft for IFR.

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11
Q

Explain how true altitude and indicated altitudes are affected by changes in air pressure and air temperature.

A

Altimeter is calibrated with ISA conditions, but atmosphere varies with pressure and temperature. Depends on what pressure is set on subscale.

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12
Q

Explain how true and indicated altitude are related when using flight levels.

A

When flying on a lower then 1013.2 day altimeter will over read.

Flying on a higher then 1013.2 day altimeter will under read.

High - low, read high be low
Low to high, read low be high.

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13
Q

Define Local Mean Time (LMT)

A

Actual time on a selected meridian of longitude, set by the sun. All points along a meridian have the same LMT

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14
Q

Calculate the LMT

A

UTC +/- LMT
Add if going East
Subtract if going West

Longitude 
360º = 24 hours
15º = 1 hr
1º = 4min
15’ = 1min
1’ = 4sec
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15
Q

Convert between LMT, UTC, NZST, NZDT

A

LMT - time on a given meridian of longitude
UTC - time at Greenwich, 0º
NZST = UTC +12
NZDT = UTC +13

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