Ken -- That's correct -- Section 22 is planned to be included in a Rev
scheduled for review at the end of 2008 --- that information was
presented to SAE AE2 (who produce Section 22 for RTCA DO 160) by the Air
Force representative to Mil 461 -- according to him, the reason there is
no lightning testing included at this time is that the Navy and Air
Force couldn't agree on pin injection testing -- apparently that was
resolved during 2007 and they expect a draft of a new revision to Mil
461 to be available by the end of 2008... 




Michael Hopkins 
Thermo Fisher Scientific
One Lowell Research Center 
Lowell, MA 01852 
Tel: +1 978 275 0800 ext. 334 
Fax: +1 978 275 0850
mobile: +1 603 765 3736
[email protected] 


From: [email protected] [mailto:[email protected]] On Behalf Of Ken
Javor
Sent: Friday, December 14, 2007 11:01 AM
To: [email protected]
Subject: Re: FAA TSO requirements

MIL-STD-461F does not have lightning requirements included.
 
Ken Javor

Phone: (256) 650-5261


> From: "Hopkins, Michael J." <[email protected]>
> Date: Fri, 14 Dec 2007 10:41:51 -0500
> To: <[email protected]>, <[email protected]>
> Conversation: FAA TSO requirements
> Subject: RE: FAA TSO requirements
> 
> Actually, DO-160E is now current (issued December 9, 2004) and 
> Revision F has been approved by RTCA for publication. Quite a lot of 
> changes appear throughout the documents.
> 
> RTCA SC-135 has been given approval to begin work on the next revision

> and this will start in March 2008.
> 
> Lots going on based on composite airframes --
> 
> Also, it is expected that Mil 461 will pick up and include Section 22 
> of DO 160 (Lightning) in a revision expected to be available for 
> comment by December 2008.
> 
> Hope this is helpful...
> 
> 
> Michael Hopkins
> Thermo Fisher Scientific
> One Lowell Research Center
> Lowell, MA 01852
> Tel: +1 978 275 0800 ext. 334
> Fax: +1 978 275 0850
> mobile: +1 603 765 3736
> [email protected]
> 
> -----Original Message-----
> From: [email protected] [mailto:[email protected]] On Behalf Of 
> [email protected]
> Sent: Friday, December 14, 2007 9:30 AM
> To: [email protected]
> Subject: Re: FAA TSO requirements
> 
> I have only a basic understanding of EMC for avionics and I hope that 
> another forum member can provide more information, but I am willing to

> contribute what I know.
> 
> First, I thought that RTCA/DO-160D superseded revision C about 10 
> years ago.  Revision D updated the susceptibility testing, in 
> particular the RF susceptibility test methods.  Avionics tested to the

> older standard might not meet the new standard.
> 
> Second, there have almost certainly been changes over the past 10 
> years that would significantly affect the EMC performance of any 
> electronic device.  One problem I have frequently encountered has been

> die shrinks from the semiconductor manufacturers.  As the 
> semiconductor manufacturers move their highest performance parts to 
> lines with smaller features, they are left with older fabrication 
> lines with excess capacity.  They often migrate all of their 
> components to smaller feature sizes.  It lets them get more dies out 
> of a single wafer and increases profit.  Often, everything is shrunk 
> without changing the relative dimensions of the gates.  This can 
> affect susceptibility, and it can sharpen the edges increasing the 
> broadband noise in emissions.  The smaller gates and conductors can
also be much more susceptible to EMC.
> 
> In short, I would think it quite reasonable to requalify a design that

> is at least 10 years old.
> 
> Ted Eckert
> American Power Conversion/MGE
> http://www.apc.com/
> 
> The items contained in this e-mail reflect the personal opinions of 
> the writer and are only provided for the assistance of the reader. The

> writer is not speaking in an official capacity for APC-MGE or 
> Schneider Electric.
> The speaker does not represent APC-MGE's or Schneider Electric's 
> official position on any matter.
> 
> 
>  
> 
>              Ken Javor
> 
>              <ken.javor@emccom
> 
>              pliance.com>
> To 
>              Sent by:                  <[email protected]>
> 
>              [email protected]
> cc
>  
> 
>  
> Subject 
>              12/13/2007 10:18          FAA TSO requirements
> 
>              PM
> 
>  
> 
>  
> 
>  
> 
>  
> 
>  
> 
> 
> 
> 
> 
> Forum members,
> 
> Lend me your ears.
> 
> I am reviewing RTCA/DO-160C qualification data for some aircraft 
> engine monitor gauges (rpm, temperature at various points). These 
> devices date back ten years, plus they were qualified by similarity to

> an earlier design - how much earlier is not stated.
> 
> My question is whether any forum members have a feel for how tight 
> this TSO process really is.  It is hard for me to imagine that every 
> part in these gauges is built exactly like it was ten years ago, or 
> more.  I can see where the individual component part numbers would 
> need to be the same, but is there any guarantee that the dc/dc 
> converter manufacturer is building his product the same way, even if 
> he uses the same part number? What about integrated circuits in 
> general over such a span of years?
> 
> Thanks in advance,
> 
> Ken Javor
> 
> Phone: (256) 650-5261
> 
> -
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