A320 MEL Ignition System A
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Join Date: Jun 2013
Location: south korea
Age: 35
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A320 MEL Ignition System A
hey guys, i am a very curious first officer here preparing for another sim session at the end of this year
This is written under this MEL:
it states, system A is considered inop on both engines when the common power supply line from 401XP 115VAC ESS BUS is inop as a result of either a loss of electrical continuity or a short circuit
Does anyone have in depth knowledge in this particular statement?
I have seen this diagram and i can't understand it at all
i will upload it with this thread for all of you to look at
This is written under this MEL:
it states, system A is considered inop on both engines when the common power supply line from 401XP 115VAC ESS BUS is inop as a result of either a loss of electrical continuity or a short circuit
Does anyone have in depth knowledge in this particular statement?
I have seen this diagram and i can't understand it at all
i will upload it with this thread for all of you to look at
Join Date: Jan 2013
Location: Seattle Area
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Maybe I'm missing what's confusing about this, but it seems simple. Ignition system A for both engines is powered by the same electrical bus, so if that electrical bus is inoperative, both ignition systems A on the two engines are inoperative.
