108-1740
Rev D 2 of 5
3.3. Ratings
!
Current : Si gnal appli c ation only, .5 amper e maximum per c ontact . Continuous current r ati ng for
individual c ontact s cannot be applied dir ec tl y to the number of cont ac ts as they ar e
dependent on t her mal and physi c al properti es of t he materi als. Sy stem desi gn shal l
ensure that c onti nuous curr ent rat ing does not create i nternal hot spots that ex c eed
temperature designated by connector speci fi c ation dur ing steady state or t r ansi ent
conditions.
!
Temperature: -65 to 105
/
C unless limi ted by temper ature rati ng of c able used
3.4. Perfor manc e and Test Descripti on
Product i s designed t o meet the elect r ical, mechanical and envi r onmental per formance r equirement s
specified in Figure 1. Unless otherwise specifi ed, al l tests shall be perfor med at ambient environment al
condi ti ons per T est S pec ificat ion 109-1.|
3.5. Test Requirement s and Proc edur es Summary
Test Description Requir ement Procedur e
Exami nation of product. Meets requirement s of product
drawing and Appli c ati on|Specification 114-40056.
Vi sual , di mensi onal and functi onal
per appl icable quality inspection
plan.
ELECTRICAL
Termination resistance. 30 milliohm s max im um. AMP Spec 109-6-1.
Subj ec t mated c ontacts assembl ed
in housi ng to 50 mv maximum
open ci r c uit at 100 ma m aximum.
See Figure 3.
Insulat ion resistance. 1000 m egohms m ini mum. AMP Spec 109-28-4.
Test bet ween adjac ent cont ac ts
within a row and contacts in
adjac ent row of unmated and
unterminat ed samples.
Dielectric withstanding voltage. 200 v olt s DC at sea l evel.
1 m inut e hold wit h no br eak down or
flashover.
AMP Spec 109-29-1.
Test bet ween adjac ent cont ac ts
within a row and contacts in
adjac ent row of unmated and
unterminat ed samples.
MECHANICAL
Vi br ati on, random. No discont inuities of 1 micr osecond
or l onger dur ati on.
See Note.
AMP Spec 109-21-7.
Subj ec t wired and mat ed samples
to 3. 13 G's rms between 5-500 Hz.
15 m inut es i n eac h of 3 mutuall y
perpendi c ular planes.
See Figure 4.
Figure 1 (c ont)