30 August 1983
30 August 1974
TANKS, AIRCRAFT PROPULSION FLUID SYSTEM,
INTERNAL, REMOVABLE, NON-SELF-SEALING
This specification is approved for use by all
Departments and Agencies of the Department of Defense.
1.1 Scope. This specification covers internal removable, non-self-sealing,
propulsion fluid system tanks, including tank fittings, for use on aircraft.
1.2 Classification. The tanks shall be of the following general types, as
specified (see 6.2):
- Nonmetallic, flexible cell construction.
Class A - Continuously supported.
Class B - Continuously supported tear resistant.
Class C - Intermittently supported.
Type III - Nonmetallic, self-supporting cell construction.
2.1.1 Specifications, standards, and handbooks. Unless otherwise specified,
the following specifications, standards, and handbooks of the issue listed in
that issue of the Department of Defense Index of Specifications and Standards
(DoDISS) specified in the solicitation form a part of this specification to the
extent specified herein.
Plating, Cadmium (Electrodeposited)
Standard Test Fluids, Hydrocarbon
Ethyl Alcohol (Ethanol) Denatured Alcohol, and Proprietary
Beneficial comments (recommendations, additions, deletions) and any
pertinent data which may be of use in improving this document should
be addressed to: ASD/ENESS, Wright-Patterson AFB, OH 45433 by using
the self-addressed Standardization Document Improvement Proposal
(DD Form 1426) appearing at the end of this document or by letter.