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 |
Actuator still requires electrical power to operate.
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Originally Posted by LUPA93
(Post 9307003)
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 |
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