MIL-DTL-48360A (AR)
2.3 Order of precedence. Unless otherwise noted herein or in the contract, in the event of
a conflict between the text of this document and the references cited herein, the text of this
document takes precedence. Nothing in this document, however, supersedes applicable laws and
regulations unless a specific exemption has been obtained.
3. REQUIREMENTS
3.1 Required inspections.
3.1.1 First article. When specified, (see 6.2) a sample shall be subjected to first article
inspection in accordance with 4.2.
3.1.2 Conformance. A sample shall be subject to conformance inspection in accordance
with 4.3 when applicable.
3.2 Propelling charge assembly.
3.2.1 Body. Body shall be in accordance with 9281867.
3.2.2 Laminated lead cloth. Laminated lead cloth shall be in accordance with 12913756.
3.2.3 Body and liner assembly. Body and liner assembly shall be in accordance with
9282044.
3.2.4 Charge, propelling, M200 assembly. Charge, propelling, M200 assembly shall be in
accordance with 9282042.
3.3 Propellant weight. The net weight of the propellant shall not differ by more than the
0.07 ounce from that specified in the loading authorization.
3.3.1 Minimum propellant weight. The minimum propellant weight shall not be less than
3.8 oz. from that specified in the loading authorization.
3.4 Proving ground. The propelling charge, shall be fired in the M119 Howitzer and with
the weight of projectile (33 lbs ± 0.10 lbs)
3.4.1 Permissible Individual Maximum Pressure (+145ºF). The propellant charge, at
recommended charge weight, shall not produce a Permissible Individual Maximum Pressure
(PIMP) greater than 57,000 psi at +145ºF when fired in a M119 Howitzer.
3.4.2 Average pressure (+145ºF). The propelling charge, at recommended charge weight,
shall not produce an average chamber pressure greater than 54,000 psi at +145ºF when fired in a
M119 Howitzer.
3
For Parts Inquires submit RFQ to Parts Hangar, Inc.
© Copyright 2015 Integrated Publishing, Inc.
A Service Disabled Veteran Owned Small Business