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|  MIL-A-85116(AS)
4.3.4 Test equipment. All test equipment shall be calibrated and main-
tained in accordance with the provisions of MIL-C-45662. All reports of
preproduction and quality conformance tests and inspections shall include
certification to this effect (see 6.2.2).
4.4 Test methods.
4.4.1 Functional tests.
No-fire current test. A test current of 28 2 tide shall be
4.4.1.1
the control circuit for a period of not less than 1 hour. This
applied to
be conducted at temperatures of -43 and +57C. The actuator
test shall
the requirements of 3.2.1.1.
shall meet
All-fire current test. A test current of 0.300 0.005 Adc shall
4.4.1.2
to the control circuit for a period not to exceed 10 ms. This
be applied
test shall
be conducted at temperatures of -43 and +57C. The actuator
the requirements of 3.2.1.2 and 3.2.1.3.
shall meet
4.401.3 Exhibited force. The piston shall be mounted in an instrumented
test fixture devised to measure the time and force of movement of the piston
upon initiation of the actuator as specified in 4.4.1.2. The actuator may
by mounted perpendicular to the direction in which gravity would aid passing
of the test. The actuator shall meet the requirements of 3.2.1.3.
4.4.2 Physical examination and test.
4.4.2.1 Visual and mechanical inspection. The actuator shall be inspected
to verify that the dimensions, materials, marking, finish, construction, and
workmanship are in conformance with the requirements of 3.2.2.1, 3.3.3 and
3.5 without disassembly.
4.4.2.2 Terminal strength. The actuator shall be tested in accordance
with MIL-STD-202, Test Method 211, Test Condition A, except that the applied
force shall be 3 pounds minimum for a period of 30 seconds minimum. The
actuator shall meet the requirements of 3.2.2.2.
4.4.2.3 Lead-to-lead resistance. This test shall be performed in accord-
ance with MIL-STD-202, Test Method 303, with a test current of 1.1 milli-
amperes maximum. The actuator shall meet the requirements of 3.2.2.3.
4.4.2.4 Insulation resistance, pre-fired condition and post-fired con-
dition. This test shall be performed in accordance with MIL-STD-202. Test
Method 302. The test potential shall be 50 5 volts dc applied between the
lead wires shunted together and the case. The actuator shall meet the re-
quirements of 3.2.2.4,
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