AIRBUS REVERSER IN ELEC FAILURES
Thread Starter
Joined: Jul 2006
Posts: 18
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From: MADRID
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
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
Joined: Jun 2009
Posts: 451
Likes: 0
From: somewhere
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
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
