When MIL-STD-2000A was written, the issue of the SOT's didn't arise
because at that time, Military didn't allow use of non-hermetic ICs
and thus we didn't consider criteria for these parts. I recall as I
chaired the Acceptance Criteria Committee for the DoD for
MIL-STD-2000A and am still having nasty flashbacks!!!! What you see
in 2000A was a general requirement that solder not contact the part
body lead seal for reasons of thermal transfer (4.23.7.5 Lead heel
fillet.); this wasn't a defect as the idea was that the part's
functionality was 100% checked AND solder may wet up to near/abut lead
if the lead is solderable (e.g. gold). The part about not touching
the bottom of the part was in 4.23.7.7 (J-leaded and V-leaded device)
and had to do with solder under the device acting as a stress loading
point during low temp exposure. Remember, we were talking hermetic
(ie. ceramic) devices.
When ANSI/J-STD-001A was being developed (A rev), it was noted,as you
point out, that solder contacting the sides of the part (on SOT/SOICs)
is fairly common and no failures were noted, thus the condition was
allowed in ANSI/J-STD-001A in table 9-2 note 1.
Call if you have questions.
Jim Maguire
Senior Principal Engineer
Boeing Defense & Space Group
PO Box 3999 M/S 3W-97
Seattle, WA 98124-2499
Phone 206-657-9063
FAX 206-657-8903
Email: [log in to unmask]
______________________________ Reply Separator _________________________________
Subject: ASS- X S Solder on SOT-23
Author: [log in to unmask] at esdigate
Date: 4/30/96 2:32 PM
Mail*Link(r) SMTP ASS: X S Solder on SOT-23
Kenny,
Your response of "no response" I find very interesting.
IMO, I would not allow the filling of the strain reliefs in the component
leads for any "serious" Class 3 product. The following are my
concerns/thoughts:
1) With solder against the component body, significant heat has been
transfered through the component lead(s) through the lead and into component
body seal. This could have degraded the adhesive bond between the lead and
plastic body molding compound.
2) Differences of thermal expansion coefficients between the component and
the printed board interconnection substrate during thermal/power cycling/shock
will strain the (assumed weakened) bond between the component lead and
component body. Re-occuring cyclic reverse-stress could lead to component
failure.
3) Mechanical shock/vibration will likewise subject the component lead and
component body to the same type of possible failure mode as in concern/thought
2).
However it may be acceptable, depending on the life-cycle environment (as you
will read, this pun was not intended) for the poroduct. If the component were
mounted on an assembly that was a medical implant, such as a heart pacemaker,
it would probabibly be acceptable, because if the inside of the ol' human body
is subjected to thermal shock/cycling or mechanical shock/vibration to damage
the assembly/component, I think some other part of the 'ol body will
deteriorate functionality before the SOT-23's soldered connection.
Disclaimer - this is my opinion, and would most probably not endorsed by my
employer.
Ralph Hersey
e-mail: [log in to unmask]
--------------------------------------
Date: 4/30/96 7:17 AM
From: Kenny Bloomquist
On Friday, April 26th I wrote:
We are discussing excess solder on a SOT-23 for a critical DOD application
per MIL-STD-2000A. The condition is solder contacting the body of the
component between the PWB and the body, also solder contacts the lead seal.
Per 2000A this "shall not" be done but it is not in Table 1 as requiring
disposition. My real question is, what is the risk for this condition and
does anyone have any supporting data (good, bad or otherwise)?
I was suprised that no one sent a response. I know this is a touchy subject
but any information would be greatly appreciated.
Thank you in advance for all responses.
[log in to unmask]
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Date: Tue, 30 Apr 1996 06:09:41 -0700
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From: [log in to unmask] (Kenny Bloomquist)
Subject: ASS: X S Solder on SOT-23
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