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080 Principles of Flight - 2014.pdf
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Windshear 15

Windshear Encounter during Approach

The power setting and vertical velocity required to maintain the glide slope should be closely monitored. If any windshear is encountered, it may be difficult to stay on the glide path at normal power and descent rates. If there is ever any doubt that you can regain a reasonable rate of descent, and land without abnormal manoeuvres, you should apply full power and go-around or make a missed approach.

Windshear can vary enormously in its impact and effect. Clearly some shears will be more severe and consequently more dangerous than others.

When countering the effects of windshear, it is best to assume ‘worse case’. It is impossible to predict at the first stages of a windshear encounter how severe it will be, and it is good advice to suggest that recovery action should anticipate the worst.

 

 

 

 

WINDSHEAR

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

From

 

To

From

 

To

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Headwind

 

Calm or Tailwind

Tailwind

 

Calm or Headwind

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

INDICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

 

 

15

 

Indicated Airspeed

Decrease

 

Increase

 

 

 

 

 

 

 

 

 

Pitch Attitude

Decrease

 

Increase

 

Windshear

 

 

 

 

 

 

 

 

 

 

Aircraft

Tends to Sink

 

Balloons

 

 

 

 

 

 

 

 

 

 

 

 

 

Ground speed

 

Increase

 

Decrease

 

 

 

 

 

 

 

 

 

 

 

 

 

ACTIONS

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Power

 

Increase

 

Decrease

 

 

 

 

 

 

 

 

 

Fly

Up to Glideslope

Down to Glideslope

 

 

 

 

 

 

 

 

 

Be prepared to

Reduce Power

Increase Power

 

 

 

 

 

 

 

 

 

To Stay on Glide Path

Increase Rate of Descent

Decrease Rate of Descent

 

 

 

(Due to faster ground speed)

(Due to slower ground speed)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Figure 15.2 Indications & recovery actions for windshear encounter during approach

Referring to Figure 15.2, this table gives guidance should you encounter windshear during a stabilized landing approach. Approaches should never be attempted into known windshear conditions.

491

15 Windshear

Effects of Windshear

Windshear 15

The relationship of an aeroplane in a moving air mass to its two reference points must be fully understood. One reference is the air mass itself and the other is the ground.

On passing through a shear line, the change of airspeed will be sudden, but the inertia of the aircraft will at first keep it at its original ground speed. The wind is a form of energy and when it shears, an equivalent amount of energy is lost or gained.

A rapid increase in headwind (or loss of tailwind) are both ‘energy gains’, and will temporarily improve performance, Figure 15.3.

Downdraughts or a sudden drop of headwind (or increase in tailwind) are the main danger at low altitude because they give an ‘energy loss’, Figure 15.4 and 15.5.

'ENERGY GAIN' - Rapid increase in headwind.

60 kt

 

10 kt

 

 

 

 

Vertical Speed:

200 ft/min R.O.C.

Vertical Speed:

700 ft/min R.O.D.

Ground Speed:

130 kt

Ground Speed:

130 kt

IAS:

190 kt

IAS:

140 kt

GLIDE SLOPE

SHEAR

LINE

Figure 15.3 “Energy gain” due to increase in headwind

492

Windshear 15

'ENERGY LOSS' - Effect of downdraught.

10 kt

Vertical Speed:

1500 ft/min R.O.D.

Vertical Speed:

700 ft/min R.O.D.

Ground Speed:

130 kt

 

Ground Speed:

130 kt

GLIDE SLOPE

IAS:

130 kt

 

IAS:

140 kt

 

SHEAR

LINE

Figure 15.4 “Energy loss” due to downdraught

'ENERGY LOSS' - Loss of headwind.

 

 

10 kt

 

Vertical Speed:

1000 ft/min R.O.D.

Vertical Speed:

700 ft/min R.O.D.

Ground Speed:

130 kt

Ground Speed:

130 kt

IAS:

110 kt

IAS:

140 kt

GLIDE SLOPE

20 kt

SHEAR

LINE

Windshear 15

Figure 15.5 “Energy loss” due to loss of headwind

493

15 Windshear

“Typical” Recovery from Windshear

The combination of increasing headwind, followed by downdraught, followed by increasing tailwind should be considered, as this is the sequence which might be encountered in a microburst on the approach, or following take-off.

• The presence of thunderstorms should be known and obvious, so the increase in speed caused by the rising headwind should be seen as the forerunner of a down-burst or microburst; any hope of a stabilized approach should be abandoned and a missed approach carried out

 

as the only safe course of action.

The initial rise in airspeed and rise above the approach path (balloon) should be seen

 

as a bonus and capitalized on. Without hesitation, increase to go-around power, being

 

prepared to go to maximum power if necessary, select a pitch angle consistent with a

 

missed approach, typically about 15°, and hold it against turbulence and buffeting.

The next phase may well see the initial advantages of increased airspeed and rate of climb

 

being rapidly eroded. The downdraught now strikes, airspeed may be lost and the aircraft

 

may start to descend, despite the high power and pitch angle. It will be impossible to

 

gauge the true angle of attack, so there is a possibility that the stick shaker (if fitted) may be

 

triggered; only then should the attempt to hold the pitch angle normally be relaxed.

• the point at which a downdraught begins to change to increasing tailwind may well be the

 

most critical period. The rate of descent may lessen, but the airspeed may still continue to

15

fall; the height loss may have cut seriously into ground obstacle clearance margins. Given

that maximum thrust is already applied, as an extreme measure if the risk of striking the

 

Windshear

ground or an obstacle still exists, it may be necessary to increase the pitch angle further

the pitch control to try and hold this higher pitch angle, until the situation eases with the

 

and deliberately raise the nose until stick shaker is felt, then decrease back-pressure on

aircraft beginning to escape from the effects of the microburst.

When there is an indefinite risk of shear, it may be possible to use a longer runway, or one that points away from an area of potential threat. It may also be an option to rotate at a slightly higher speed, provided this does not cause undue tyre stress or any handling problems. The high power setting and high pitch angle after rotate already put the aircraft into a good configuration should a microburst then be encountered. The aircraft is, however, very low, there is little safety margin and the ride can be rough. If there is still extra power available, it should be used without hesitation. Ignore noise abatement procedures and maintain the high pitch angle, watching out for stick shaker indications as a signal to decrease backpressure on the pitch control.

In both approach and take-off cases, vital actions are:

Use the maximum power available as soon as possible.

Adopt a pitch angle of around 15° and try and hold that attitude. Do not chase airspeed.

Be guided by stick shaker indications when holding or increasing pitch attitude, easing the back-pressure as required to attain and hold a slightly lower attitude.

494

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