Kachno, ty mě chceš zničit...
přečti si o tom případě něco, dá se toho najít celkem dost a v zjednodušený, stále ale pravdivý podobě i na Wikipedii
Protože mi zjevně nevěříš, postnu sem výcuc událostí poté, co došlo k závadě RA
The throttles were pulled back to idle thrust, but the autothrottle unexpectedly reverted to "retard" mode, which is designed to automatically decrease thrust shortly before touching down on the runway at 27 feet (8.2 m) above runway height. At 144 kt, the pilots manually increased thrust to sustain that speed, but the autothrottle immediately returned the thrust lever to idle power because the first officer did not hold the throttle lever in position. The throttles remained at idle for about 100 seconds while the aircraft slowed to 83 kt, some 40 kt (75 km/h) below reference speed as the aircraft descended below the required height to stay on the glideslope. The stick-shaker activated at about 150 metres (490 ft) above the ground, indicating an imminent stall, the autothrottle advanced, and the captain attempted to apply full power. The engines responded, but there was not enough altitude or forward airspeed to recover; the aircraft hit the ground tail-first at 95 knots (176 km/h; 109 mph).
Tenhle případ s autolandem NEMÁ nic společného! |
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