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|  MIL-D-81347C(AS)
STANDARDS
Military
Standard General Requirements for Electronic Equipment
MIL-STD-454C
15 Oct 1970
Maintainability Program Requirements (for Systems and
MIL-STD-470
Equipment)
21 Mar 1966
MIL-STD-471
Maintainability Demonstration
15 Feb 1966
Preferred and Guidance List of Semiconductor Devices
MIL-STD-701E
30 Dec 1964
Electric Power, Aircraft Characteristics and Utilization of
MIL-STD-704A
9 August 1966
Reliability Tests, Exponential Distribution
MIL-STD-781A
10 Dec 1965
Requirements for Reliability Program (for System and
MIL-STD-785
Equipment)
30 June 1965
Parts and Equipment, Procedures for Packaging and
MIL-STD-794
Packing of
10 Mar 1965
Meter, Time Totalizing, 115Volt -400 Cycle
MS-17322C
Control Panel, Console Type, Aircraft Equipment, Basic
MS-25212C
Dimensions
25 Aug 1960
Control Panel, Aircraft Equipment, Typical Installation
MS-25213A
25 Aug 1960
Color
FED-STD-595
1 Mar 1956
Naval Air Systems Command
Avionics Installation Instructions for Data Analysis Pro-
EI-515A
gramming Group AN/AYA-8B
Availability of Documents -When requesting specifications,
2.1.1
standards, drawings, and publications, refer to both title and number. Copies of this specification
and applicable specifications required by contractors in connection with specific procurement functions
may be obtained upon application to the Commanding Officer, Publications and Forms Center
(NPFC 1032), Code 105, 5801 Tabor Avenue, Philadelphia, Pennsylvania 19120.
REQUIREMENTS
3.
Preproduction - The specification makes provision for prepro-
3.1
duction testing.
Parts and Materials - In the selection of parts and materials,
3.2
fulfillment of major design objectives shall be the prime consideration. In so doing the following shall
govern:
(1) Microelectronic devices shall conform to requirements
specified in WR-101, Part II.
(2) Other parts and materials requirements shall conform to
Specification MIL-E-5400.
(3) Nonrepairable subassemblies, as outlined in Specification
MIL-E-5400, shall be used when practicable. The general size of the subassembly and the amount of
circuitry to be included therein shall be approved by the procuring activity. Nonrepairable subassem-
blies must be reliable.
3
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