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时间:2011-10-28 17:35来源:蓝天飞行翻译 作者:航空
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APPROACH
If significant ice accretion develops on parts of the wing that have not been deiced, the aircraft speed must be increased (Refer to FCOM/PRO-SUP-30 OPERATIONS IN ICING CONDITIONS).
When the temperature is lower than ISA -10, the target altitudes (provided by the ATC) must be corrected, by adding the values that are indicated in the table below:
Corrections to be Added
Height ISA -10 ISA -20 ISA -30
500 50 70 100
1 000 100 140 190
2 000 200 280 380
3 000 290 420 570
4 000 390 570 760
5 000 490 710 950

These corrections correspond to approximately 4 x ▴ISA x Height (ft)/1000 LANDING
Obviously, landings should be avoided on very slippery runways. However, if it is not possible to avoid such landings, the following factors (linked to operations on contaminated runways) should be considered:
? Braking action
? Directional control.
BRAKING ACTION
The presence of fluid contaminants on the runway has an adverse effect on braking performance, because it reduces the friction between the tires and the surface of the runway. It also creates a
 
SUPPLEMENTARY INFORMATION
ADVERSE WEATHER
 
layer of fluid between the tires and the runway surface, and reduces the contact area. The landing distances, indicated in the QRH, provide a good assessment of the real landing distances for specific levels of contamination.
A firm touchdown should be made and MAX reverse should be selected, as soon as the main landing gear is on ground. Using reversers on a runway that is contaminated with dry snow may reduce visibility, particularly at low speeds. In such cases, reverse thrust should be reduced to idle, if necessary.
The use of MED (4 for A340-500/600) autobrake is recommended, when landing on an evenly
contaminated runway. It is possible that the DECEL light on the AUTO BRK panel will not come on, as the predetermined deceleration may not be achieved. This does not mean that the autobrake is not working.
In the case of uneven contamination on a wet or contaminated runway, the autobrake may laterally destabilize the aircraft. If this occurs, consider deselecting the autobrake.
Typical Landing Distance Factors vs. Runway Conditions
DIRECTIONAL CONTROL
During rollout, the sidestick must be centered. This prevents asymmetric wheel loading, that results in asymmetric braking and increases the weathercock tendency of the aircraft.
The rudder should be used for directional control after touchdown, in the same way as for a normal landing. Use of the tiller must be avoided above taxi speed, because it may result in nosewheel skidding, and lead to a loss of directional control.
When required, differential braking must be applied by completely releasing the pedal on the side that is opposite to the expected direction of the turn. This is because, on a slippery runway, the same braking effect may be produced by a full or half-deflection of the pedal.
 
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