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A320 MEL Ignition System A

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A320 MEL Ignition System A

Old 8th Nov 2019, 09:31
  #1 (permalink)  
Thread Starter
Join Date: Jun 2013
Location: south korea
Age: 30
Posts: 14
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

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igniter a.pdf (102.8 KB, 42 views)
kikwon is offline  
Old 9th Nov 2019, 02:47
  #2 (permalink)  
Join Date: Jan 2013
Location: Seattle Area
Posts: 150
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.
Dave Therhino is offline  

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