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Old 3rd Sep 2009, 07:39   #1 (permalink)
Probationary PPRuNer
 
Join Date: Jul 2008
Location: australia
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Where doe the Integrated Standby Instruments System (ISIS) derived its power from?

hey guys need help with deriving the power source of the
Integrated Standby Instruments System (ISIS) in the airbus a330 200 series

is there any website which gives the perfect definition and source information???
rionthai is offline   Reply
Old 3rd Sep 2009, 10:06   #2 (permalink)
 
Join Date: Oct 1999
Location: N.Ireland
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DC Ess Bus generally, back up power Hot Bus 1. FCOM 1, 1.34.25 ISIS, Architecture.

Last edited by Torque2; 3rd Sep 2009 at 10:24.
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Old 7th Sep 2009, 00:30   #3 (permalink)
 
Join Date: Aug 2008
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Sorry to be a pain mate but do you have a direct link to the source need it for referencing. Cheers
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Old 7th Sep 2009, 08:38   #4 (permalink)
 
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nice try rionthai
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Old 7th Sep 2009, 09:48   #5 (permalink)
 
Join Date: Feb 2009
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Just thinking about it logically - you should be able to come up with the right answer with a basic knowledge of the elec system . . .
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Old 7th Sep 2009, 09:54   #6 (permalink)
 
Join Date: Oct 1999
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You can probably find it on http://www.****************.com/
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Old 7th Sep 2009, 10:26   #7 (permalink)
 
Join Date: May 2002
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While it is in the FCOM 1.34.20 P1, also try looking at the AAIB report (2/2008) of G-EUOB and the electrical failure it suffered. In the descriptive text, there is a good explanation of the power sources of the ISIS. In short, it says that the ISIS has two power sources - Ess DC and HBB with prior standby horizons just being Ess DC powered unless modified to the ISIS state.
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Old 7th Sep 2009, 12:18   #8 (permalink)
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ISIS

Swinburne avionics assignment??
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Old 7th Sep 2009, 16:12   #9 (permalink)
 
Join Date: Sep 2004
Location: London
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Yeah I think so as I am after the same information!
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