MIL-H-18325B(Aer)
Test Procedures for Aircraft Cabin Pressurizing and
MIL-T-18606(Aer)
Air Conditioning Systems
Thermal Anti-Icing Equipment, Wing and expennage
MIL-T-18607(Aer)
STANDARDS
Colors - Fluid Line Identification
AND-10375
Receptacles - Electrial Connector, Box Mouning
MS-3102
MC-16051(Aer)
Coupling, Ground Cooling, Combat Type Aircraft
Air Inlet Combat Aircraft, Ground Cooling
MS-16052(Aer)
Connector, Receptacle. Electrical, Integral Mounting
MS-33678
PUBLICATIONS
AIR FORCE-NAVY AERONAUTICAL BULLETIN
Specifications
and Standards, Use of
ANA 143
(When requesting specifications, standards, drawings, and publications refer to both
title and number. Copies of this specification and applicable spedicifications may be obtained
upon application to the Commanding Officer U.S. Naval Aviation Supply Depot, 700 Robbins
Avenue, Philadelphia 11, Pennsylvania, Attention Code ODPT).
3. REQUIREMENTS
3.1 Materials - When materials are used which are not specifically designated herein, they
shall be of the best quality, of the lightest possible weight, and fully suitable for the
purpose. The specification to be used for the procurement of the applicable materials and
products shall be in accordance with the policty outlined in ANA Bulletin No. 143.
3.1.1 Dissimilar Metals - The use of dissimilar metals, especially brass~ copper, or steel
in intimate metal-to-metal. contact with aluminum or aluminum alloy shall be avoided except when
absolutely necessary and when used, adequate steps should be taken wherever possible to insulate
the metals from each other to prevent electrolytic corrosion in accordance with the requirements
of specification MIL-F-7179.
Corrosion - When materials are used which are subject to corrosion in salt air, or other
3.1.2
atmospheric conditions likely to occur during service usage, they shall be protected against
such corrosion in accordance with the requirements of Specification MIL-F-7179 and in a manner
which will in no way prevent compliance with the requirements of this specification.
3.1.3 Magnesium Alloy - The use of magnesium alloy is not desired and its use shall be subject
to the approval of the Bureau of Aeronautics.
3-.2 Construction
3.2.1 Ruggedness - The component parts of the heating and ventilating system as specified
herein shall be sufficiently rugged to withstand the mechanical shocks, vibrations and
stresses incident to its use in the airplane in which it is installed,
Assembly - The design and location of the component parts of the heating and ventilating
3.2.2.
system shall be such as to facilitate disassembly and reassembly for the purpose of repair or
replacement of parts, preferably without the use of special tools or movement of other parts.
If special tools. are required for servicing, one complete set of such tools shall be furnished
per installation for inclusion in the airplane tool kit.
Interchangeabilty
3.3
3.3.1 Dimensions - Dimensional limits and tolerance shall be such that all parts built to
the same drawing will be interchangeable so that selective fits will not be necessary.
3
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