PJ (& others) I have a couple of supplementary Q’s
- If one engine (either one) failed, at what shaft (% RPM) would the associated GEN trip out? And;
- Notwithstanding the above, following a single engine (either one) failure, would AC1 remain energized by the other power plant? If yes;
- Following the inevitable ECAM/s, would ACARS output message/s?
On a similar but different subject, at FL350 & M.82:-
- Following an asymmetric failure (whilst in ALTN 2), how promptly would the PF need to get rudder in to avoid yaw induced roll?
Last edited by ARFOR; 8th Jul 2009 at 08:46.
Reason: typo