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| MIL-W-81752A(AS)
27 FEBRUARY 1987
SUPERSEDES
MIL-W-81752(AS)
23 April 1970
MILITARY SPECIFICATION
WINDSHIELD SYSTEMS, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR
This specification is approved for use within the Naval Air Systems
Command, Department of the Navy, and is available for use by all
Departments and Agencies of the Department of Defense.
SCOPE
1.
1.1 Scope - This specification establishes the general
requirements for the design, performances, installations and acceptance
of windshield systems in fixed wing aircraft,
APPLICABLE
DOCUMENTS -
2.
2.1 Government
documents -
2.1.1 Specifications, standards, and handbooks. The following
specifications, standards, and handbooks form a part of this
specification to the extent specified herein. Unless otherwise
specified, the issues of these documents shall be those listed in the
issue of the Department of Defense Index of Specifications and
Standards (DODISS) and supplement thereto, cited in the solicitation.
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