Qualification Test
Report 501-341
27Oct09 Rev A
All Paragraphs Revised
.100 Inch Centerline Crimp-Snap Connectors
©2009 Tyco Electronics Corporation
Harrisburg, PA
All International Rights Reserved
* Trademark
| Indicates change 1 of 7
LOC B
1. INTRODUCTION
1.1. Purpose
Testing was performed on the Tyco Electronics .100 Inch Centerline Crimp-Snap Connectors to
determine their conformance to the requirements of Product Specification 108-1328 Revision A.
1.2. Scope
This report covers the electrical, mechanical, and environmental performance of the .100 Inch
Centerline Crimp-Snap Connectors. Testing was performed at the Engineering Assurance Product
Testing Laboratory between July and November 1995. Additional Testing was completed on 10Jul09.
The test file numbers for this testing are ACL1443-003, ACL1443-004, ACL1443-005 and
EA20090472T. This documentation is on file at and available from the Engineering Assurance Product
Testing Laboratory.
1.3. Conclusion
The .100 Inch Centerline Crimp-Snap Connectors listed in paragraph 1.5., conformed to the electrical,
mechanical, and environmental performance requirements of Product Specification 108-1328 Revision
A.
1.4. Product Description
The .100 Inch Centerline Crimp-Snap Connectors are wire-to-board connections consisting of
crimp-snap contacts seated in a housing that mates to .025 inch square post headers on .100 inch
centerline and is designed to be terminated to 22 to 26 AWG wire.
1.5. Test Specimens
Test specimens were representative of normal production lots. Specimens identified with the following
part numbers were used for test:
Test Group Quantity Part Number Description
110 1-770602-0 CST-100, 10 position housing
10 1-641215-0 MTA-100, 10 position .025 inch Au header assembly
1,2,3 260 770601-1 CST-100 Sn contacts with 22 AWG wire
2,3,4 16 2-770602-0 CST-100, 20 position housing
260 770601-1 CST-100 Sn contacts with 26 AWG wire
6 2-640456-0 MTA-100, 20 position .025 inch Sn header assembly
4100 770601-2 CST-100 Au contacts with 22 AWG wire
5 2-641215-0 MTA-100, 20 position .025 inch Au header assembly
5 10 1-640456-0 MTA-100, 10 position .025 inch Sn header assembly
Figure 1 (continued)
501-341
Test Group Quantity Part Number Description
Rev A 2 of 7
625 1375819-1 CST 100 II contact with 22 AWG wire
25 1375819-1 CST 100 II contact with 24 AWG wire
25 1375819-1 CST 100 II contact with 26 AWG wire
Figure 1 (end)
1.6. Environmental Conditions
Unless otherwise stated, the following environmental conditions prevailed during testing:
!Temperature: 15 to 35°C
!Relative Humidity: 25 to 75%
1.7. Qualification Test Sequence
Test or Examination Test Group (a)
123456
Test Sequence (b)
Examination of product 1,9 1,9 1,7 1,5 1,3 1,3
Termination resistance 3,7 2,7 2,4
Insulation resistance 2,5
Dielectric withstanding voltage 3,6
Temperature rise vs current 3,8
Solderability 2
Sinusoidal vibration 5 6(c)
Physical shock 6
Durability 4
Mating force 2
Unmating force 8
Crimp tensile 2
Thermal shock 4
Humidity/temperature cycling 4(d)
Temperature life 5
Mixed flowing gas 3(e)
(a) See paragraph 1.5.
NOTE (b) Numbers indicate sequence in which tests are performed.
(c) Discontinuities shall not be measured. Energize at 18
E
C level for 100%
loadings per Test Specification 109-151.
(d) Precondition specimens with 10 cycles durability.
(e) Gold plated specimens only.
Figure 2
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Rev A 3 of 7
2. SUMMARY OF TESTING
2.1. Examination of Product - All Test Groups
All specimens submitted for testing were representative of normal production lots. Specimens were
inspected and accepted by the Product Assurance Department of the Commercial Products Business
Unit. No evidence of physical damage detrimental to product performance was observed.
2.2. Termination Resistance - Test Groups 1, 2 and 4
All contact termination resistance measurements, taken at 100 milliamperes DC maximum and 50
millivolts DC maximum open circuit voltage were less than 6 milliohms initially and 10 milliohms after
testing.
Test
Group Number of
Data Points Condition Termination Resistance
Min Max Mean
1 100 Initial 2.81 3.54 3.07
After mechanical 2.64 9.82 4.19
260
Initial 2.68 3.34 2.99
After vibration 3.12 8.52 4.52
497
Initial 3.35 5.67 4.22
After mixed flowing gas 3.29 9.22 4.83
All values in milliohms.
NOTE
Figure 3
2.3. Insulation Resistance - Test Group 3
All insulation resistance measurements were greater than 1000 megohms initial and 100 megohms
final.
2.4. Dielectric Withstanding Voltage - Test Group 3
No dielectric breakdown or flashover occurred.
2.5. Temperature Rise vs Current - Test Group 2
All specimens had a temperature rise of less than 30°C above ambient when tested using a baseline
rated current of 5.52 amperes DC.
2.6. Solderability - Test Group 5
The contact leads had a minimum of 95% solder coverage.
2.7. Sinusoidal Vibration - Test Groups 1 and 2
No discontinuities were detected during vibration testing. Following vibration testing, no cracks, breaks,
or loose parts on the specimens were visible.
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2.8. Physical Shock - Test Group 1
No discontinuities were detected during physical shock testing. Following physical shock testing, no
cracks, breaks, or loose parts on the specimens were visible.
2.9. Durability - Test Group 1
No physical damage occurred as a result of manually mating and unmating the specimens 15 times.
2.10. Mating Force - Test Group 1
All mating force measurements were less than 2 pounds per contact.
2.11. Unmating Force - Test Group 1
All unmating force measurements were greater than .80 pound per contact.
2.12. Crimp Tensile - Test Group 6
All crimp tensile measurements were greater than 11 pounds for 22 AWG wire; 10 pounds for 24 AWG
wire and 7 pounds for 26 AWG wire.
2.13. Thermal Shock - Test Group 3
No evidence of physical damage was visible as a result of exposure to thermal shock.
2.14. Humidity/temperature Cycling - Test Group 2
No evidence of physical damage was visible as a result of exposure to humidity/temperature cycling.
2.15. Temperature Life - Test Group 2
No evidence of physical damage was visible as a result of exposure to temperature life.
2.16. Mixed Flowing Gas - Test Group 4
No evidence of physical damage was visible as a result of exposure to the pollutants of mixed flowing
gas.
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Rev A 5 of 7
3. TEST METHODS
3.1. Examination of Product
Specimens were inspected and accepted by the Product Assurance Department of the Commercial
Products Business Unit.
3.2. Termination Resistance
Termination resistance measurements were made using a 4 terminal measuring technique (Figure 4).
The test current was maintained at 100 milliamperes DC maximum with a 50 millivolt DC maximum
open circuit voltage.
All wire resistance was subtracted from the measurements
NOTE
Figure 4
Termination Resistance Measurement Points
3.3. Insulation Resistance
Insulation resistance was measured between adjacent contacts using a test voltage of 500 volts DC
applied for 2 minutes before the resistance was measured.
3.4. Withstanding Voltage
A test potential of 1000 volts AC was applied between adjacent contacts for 1 minute and then returned
to zero.
3.5. Temperature Rise vs Current
Thermocouples were attached to individual contacts to measure their temperature while energized at
5.52 amperes DC. The ambient temperature was then subtracted from this measured temperature to
find the temperature rise. When the temperature rise of 3 consecutive readings taken at 5 minute
intervals did not differ by more than 1°C, the temperature measurement was recorded.
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Rev A 6 of 7
3.6. Solderability
Specimen contact solder tails were immersed in a type R flux for 5 to 10 seconds, allowed to drain for
10 to 20 seconds, then held over molten solder without contact for 2 seconds. The solder tails were then
immersed in the molten solder at a rate of approximately 1 inch per second, held for 5 seconds, then
withdrawn. After cleaning in isopropyl alcohol, the specimens were visually examined for solder
coverage. The solder used for testing was 60/40 tin lead composition and was maintained at a
temperature of 245 ± 5°C.
3.7. Sinusoidal Vibration
Mated specimens were subjected to sinusoidal vibration, having a simple harmonic motion with an
amplitude of .06 inch maximum total excursion. The vibration frequency was varied uniformly between
the limits of 10 and 55 Hz and returned to 10 Hz in 1 minute. This cycle was performed for 2 hours in
each of 3 mutually perpendicular planes. Specimens in test group 1 were monitored for discontinuities
of 1 microsecond or greater using a current of 100 milliamperes DC. Specimens in test group 2 were
energized at 3.5 amperes to produce an 18°C temperature rise, discontinuities were not measured.
3.8. Physical Shock
Mated specimens were subjected to a mechanical shock test having a half-sine waveform of 50 gravity
units (g peak) and a duration of 11 milliseconds. Three shocks in each direction were applied along the
3 mutually perpendicular planes for a total of 18 shocks. Specimens were monitored for discontinuities
of 1 microsecond or greater using a current of 100 milliamperes DC.
3.9. Durability
Specimens were manually mated and unmated 15 times at a maximum rate of 10 cycles per minute.
3.10. Mating Force
The force required to mate individual specimens was measured using a tensile/compression device with
a free floating fixture and a rate of travel of .5 inch per minute. The force per contact was calculated.
3.11. Unmating Force
The force required to unmate individual specimens was measured using a tensile/compression device
with a free floating fixture and a rate of travel of .5 inch per minute. The force per contact was
calculated.
3.12. Crimp Tensile
The force required to pull the wire from the specimens was measured using a tensile/compression
device with a free floating fixture and a rate of travel of 1 inch per minute.
3.13. Thermal Shock
Mated specimens were subjected to 10 cycles of thermal shock with each cycle consisting of 30 minute
dwells at -55 and 105°C and 1 minute transition between temperatures.
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3.14. Humidity/temperature Cycling
Mated specimens were exposed to 10 humidity/temperature cycles. Each cycle lasted 24 hours and
consisted of cycling the temperature between 25 and 65°C twice while maintaining high humidity (Figure
5).
Figure 5
Humidity/Temperature Cycling Profile
3.15. Temperature Life
Mated specimens were exposed to a temperature of 105°C for 792 hours.
3.16. Mixed Flowing Gas, Class IIA
Mated specimens were exposed for 14 days to a mixed flowing gas Class II exposure. Class II exposure
is defined as a temperature of 30°C and a relative humidity of 70% with the pollutants of Cl2 at 10 ppb,
NO2 at 200 ppb and H2S at 10 ppb.