Ottima considerazione Nabbo.
Ho fatto una ricerca su molti filmati dell'incidente e dal:
https://www.youtube.com/watch?annota...&v=HsHSWvzPibI
risulta che dal momento in cui sbucano le luci dell'aereo dalle nubi al crash trascorrono 5". Ipotizzando un ceiling a 1800 ft (lo dichiara pił volte il controllore di torre nella registrazione delle comunicazioni T/B/T:
https://www.youtube.com/watch?featur...&v=-4m0FcsLnEg 'Ceiling 630 meters', se ne deduce un variometro medio di cica 20.000 - 22.000 ft/min. Non mi sembra un rateo di discesa che vediamo spesso
"At 15.22:51 (6 seconds after initiating Go Around) engine power reached 83% N1. By 15.23:11 pitch angle increased to more than 25 degrees, and the first "push" movement of the yoke was registered. At that moment airplane was at 2000', climbing 4000'/min. During next 5 seconds pitch decreased from 25 degrees to nearly normal horizontal flight condition and continued to decrease. Plane stopped climbing at 2300'. G-force = 0,5g. At 15.23:16 the second "push" movement of the yoke was registered. As a result of it, pitch changed to -20 degrees, speed to -5000'/min, G-force =0g, speed 140 kt, increasing 10kt/s. At 15.23:21 the third "push" movement of the yoke was registered. As a result of it, G-force changed to -0.9g, pitch angle to -60 degrees. At 15.23:28 airplane collided with the ground close to runway with an airspeed 245kt and pitch angle -75 degrees."
17.11.2013, Tatarstan 363, Kazan.
Quando si dice 'i buchi del groviera cominciano ad allinearsi':
- Nominativo del volo: Sky Dubai
981
- QFE
981
- 'Cleared 900 meters
height'
- QNH 99
8