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MIL-S-1399E(AR)
Tracer extinction and star initiation
interval over max (see 3.5.8)
Major
Detached composition burning time over
max (see 3.5.9)
Major
4.4.3.3.1 Two hundred forty (240) signal assemblies selected
and tested in accordance with 4.4.3.2.1 shall be function tested in
accordance with 4.5.3.  The lot shall be rejected if a Critical
defect occurs or if eight (8) or more defects are found during the
test (see Table IV).
4.4.3.3.2 The eighty (80) signal assemblies selected and tested
in accordance with 4.4.3.2.2 shall be tested for functioning in
accordance with 4.5.3. " The lot shall be rejected if a Critical
defect occurs or if four (4) or more Major defects are found during
the test (see Table IV).
4.4.3.4 Air leakage test (see 3.6).  This test shall be
performed 100 percent in accordance with the procedure specified in
4.5.4*  All assemblies that fail to comply with the requirement
shall be classed defective and removed from the lot.
4.4.3.5 Static test of star and tracer assemblies (see dwgs.
8847448 and 8847453).  The star assembly and tracer assembly shall
each be tested and observed for the following defects as classified
in Table V.
TABLE V
Classification
Defect
Major
Assembly fails to ignite
Major
Candlepower under min.
Major
Color value under min.
4.4.3.5.1 First three (3) lots.  Beginning with the first lot
produced and continuing until three (3) consecutive lots have
complied with the acceptance criteria specified, eighty (80) star
assemblies shall be selected from each lot for test in accordance
with the procedure specified in 4.5.5.  The lot shall be rejected if
five (5) or more defects are found during the test.
4.4.3.5.2 After three (3) consecutive lots. After three
consecutive lots have complied with the acceptance criteria of
4.4.3.5.1, thirty-two (32) star assemblies of each color and
thirty-two (32) tracer assemblies of each color shall be selected
from each lot. for test.  The lot shall be rejected if, during the
test, three (3) or more assemblies exhibit any of the defects as
listed in Table V.
28

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