Salt Atmosphere,Temperature Humidity,Mechanical Shock Environmental Stress Testing Results,and FMA of the JG-PP / JCAA Lead Free Soldering Program
The American Competitiveness Institute (ACI) performed a series of Environmental Stress Tests for the Joint Group of
Pollution Prevention / Joint Council of Aging Aircraft (JG-PP / JCAA) Lead Free Soldering Program. The objective was to
determine if Lead Free soldered hardware was equivalent to or better than its Tin Lead (SnPb) counterpart. The program’s
test vehicle was manufactured by BAE Systems in Irvine,Texas. The JG-PP / JCAA test vehicle was soldered with Tin Lead
(SnPb) as a baseline,Tin Silver Copper (95.5Sn3.9Ag0.6Cu or SAC),Tin Silver Copper Bismuth ((92.3Sn3.4Ag1.0Cu3.3Bi
or SACB),and stabilized Tin Copper (99.3Sn0.7Cu0.05Ni).
The Salt Atmosphere test was performed in accordance to ASTM B117 Test Method for 48 hours. The Temperature
Humidity test followed the procedure MIL-STD 810F; Test Method 507.4. In both tests,no failures were found that could be
attributed to the solder joints. Therefore,the Tin Lead and Lead Free soldered hardware can be considered equivalent.
Two types of Mechanical Shock tests were performed. The first Mechanical Shock test was performed using the test
procedure MIL-STD 810F; Method 516.5; Procedure 1. The test was performed on all 3 axes. 2 components soldered with
SACB failed the tests. The balance of the SnPb and Lead Free soldered components passed this mechanical shock test with
no failures.
The second Mechanical Shock test was performed to a modified version of MIL-STD 810F; Method 516.5; Procedure 1,
where the test vehicle was tested in the Z-Direction,at increasing levels to failure. The mechanical shock levels reached in
this test were above those in the first mechanical shock test. Across all test levels and component types,the SnPb soldered
hardware performed comparable or better than the SAC and the SACB soldered hardware.