A320 MEL Ignition System A
Thread Starter
Joined: Jun 2013
Posts: 14
Likes: 0
From: south korea
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
Joined: Jan 2013
Posts: 263
Likes: 0
From: Seattle Area
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.
