MIL-DTL-48360A (AR)
parts and assemblies listed in 3.2 and the conduct of all test specified in Table II and when
required Table III (see 6.10).
4.2.3 First article rejection. If any item fails to comply with requirements, the first article
sample shall be rejected.
TABLE II. First article inspection.
Number of
Requirement
Inspection Method
Sample
Examination or Test
Conformance Criteria
Paragraph
Reference
Units
Body
15
3.2.1
4.3.2.1
100%
(Dwg. 9281867)
Examination of defects
Laminated lead cloth
15
3.2.2
4.3.2.2
100%
(Dwg. 12913756)
Examination of defects
Body and liner assembly
15
3.2.3
4.3.2.3
100%
(Dwg. 9282044)
Examination of defects
15
3.2.4
4.3.2.4
Charge, propelling, M200, assembly (1/)
100%
(Dwg. 9282042)
Examination of defects
100%
3.2
4.4.2.1
Propellant weight from assembled
100%
propelling charge
1/ Propellant charge assemblies shall be packed in a fiber drum.
The following test program should be used for the initial production test:
TABLE III. Initial production test.
Temperature
No. Test
TECOM
Test Phase
No. Control Rounds
(Deg F)
Rounds
TOP
Propellant
70
10
TOP-4-2-504
Checkout
145
10
TOP-4-2-504
-60
10
TOP-4-2-504
Sequential
145
15
60
TOP-4-2-504
Environmental
-60
15
60
TOP-4-2-504
4.3 Conformance inspection.
4.3.1 Inspection lot formation. Inspection lots shall comply with the lot formation
provisions of MIL-STD-1916 and lot numbering shall comply with MIL-STD-1168. In addition,
inspection lots of propellant shall contain M30 propellant, Type I, from not more than one lot
from one manufacturer. An entire lot of propellant shall be utilized in the formation of one lot of
propelling charges unless otherwise specified in the contract.
6
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