AIRBUS REVERSER IN ELEC FAILURES
Hola:
Can anyone help me out on the following ?
Why do AB acft loose its respective reverse when loosing the related AC BUS.
e,g. A330 CFM ( pneumatic rvrs) loss of AC1 = loss of REV 1. ( idem AC2)
340 Rolls Royce , exactly same situation.
In both cases none of the several computers involved in REV Operations ( FMGC, EIU, FADECīS, TLA position, ADR; PRIM 1or3,) are lost.
Any idea ?
gracias,
LUPA