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Old 21st Apr 2014, 06:48
  #800 (permalink)  
HazelNuts39
 
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Originally Posted by CONF iture
Not differently that the FCOM :
"It represents the speed corresponding to the maximum angle of attack that the aircraft can attain in pitch normal law."
How does that differ from the definition of Vs1g?

P.S.

The special conditions for certification of the A320 (and associated guidance material) define Vs1g as the minimum speed (corrected to 1g and zero thrust) obtained in the following maneuver:

- forward center of gravity
- idle thrust
- normal law except deactivated alpha-floor
- decelerate at 1 kt/sec until sidestick reaches aft stop
- maintain sidestick on aft stop for 2 seconds or until pitch attitude does not increase further, whichever occurs later
- recover

Last edited by HazelNuts39; 21st Apr 2014 at 11:38. Reason: P.S.
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