dual central maintenance computers
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dual central maintenance computers
Hello, would anyone be able to help me with this question:
Q) On an aircraft capable of being equipped with dual central maintenance computer systems (CMCS) if only one CMC is available it :-
a) maybe fitted to either system
b) must be fitted to the left system
c) must be fitted to the right system
I would have thought (b), but I can't find the answer in my course notes or searching on the internet.
Thankyou Ben
Q) On an aircraft capable of being equipped with dual central maintenance computer systems (CMCS) if only one CMC is available it :-
a) maybe fitted to either system
b) must be fitted to the left system
c) must be fitted to the right system
I would have thought (b), but I can't find the answer in my course notes or searching on the internet.
Thankyou Ben
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According to Mr Boeings 744 DDG if two CMC's are fitted, either (only one ) may be unserviceable ( no remarks or exceptions ).
Not sure if there are any single CMC installations out there, but if there were, I would guess at a L/H installation.
Maybe our resident 747 expert QAVION can explain further
GR
Not sure if there are any single CMC installations out there, but if there were, I would guess at a L/H installation.
Maybe our resident 747 expert QAVION can explain further
GR
Last edited by Golden Rivet; 30th May 2003 at 02:18.
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According to the AMM 747-400. If you fit a single CMC of a dual
CMC system. It must be fitted on the left side.
The MEL seems to be covering the situation of two fitted, but one is u/s. In this case it doesn't matter which side the servicable one
is on. Maybe the MEL needs to be ammended to cover the situation of a single computer fit.
CMC system. It must be fitted on the left side.
The MEL seems to be covering the situation of two fitted, but one is u/s. In this case it doesn't matter which side the servicable one
is on. Maybe the MEL needs to be ammended to cover the situation of a single computer fit.
