MIL-S-26716A (USAF)
5 October 1982
SUPERSEDING
MIL-S-26716
31 December 1956
MILITARY SPECIFICATION
STAND, TEST, AIRCRAFT HYDRAULIC SYSTEMS, NON-PORTABLE
This specification is approved for use by the Department
of the Air Force, and is available for use by all Depart-
ments and Agencies of the Department of Defense.
1.
SCOPE
1.1 Scope. This specification covers the general requirements for test
stands for aircraft hydraulic systems and components and shall become a part
of a detail specification by attachment or reference.
2.
APPLICABLE DOCUMENTS
*
2.1 Government documents.
Unless otherwise specified (see 6.2),
2.1.1 Specifications and standards.
the following specifictions and standards 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.
SPECIFICATIONS
FEDERAL
CC-M-1807
Motor Alternating Current, Fractional and Integral
Horsepower (500 HP and Smaller)
MILITARY
MIL-C-104
Crate, Wood, Lumber and Plywood Sheathed, Nailed and
Bolted
MIL-P-116
Preservation, Methods of
MIL-A-5498
Accumulators , Aircraft Hydropneumatic Pressure
MIL-H-5606
Hydraulic Fluid, Petroleum Base, Aircraft, Missile,
and Ordnance
MIL-P-6808
Primer Coating, Zinc Chromate, Process For Applica-
tion of
Window Observation
MIL-W-10434
Beneficial comments (recommendations, additions, deletions) and any perti-
nent data which may be of use in improving this document should be
addressed to the Engineering Division, San Antonio Air Logistics Center,
Kelly AFB, Texas, 78241 by using the self-addressed Standardization Document
`Proposal (DD Form 1426) appearing at the end of this document or by letter.
FSC 4920
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