MIL-V-19068A (ASG)
30 APRIL 1957
Superseding
MIL-V-19068(Aer)
20 August 1955
MILITARY SPECIFICATION
VALVES, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE II SYSTEMS
This specification has been approved by the Departments
of the Air Force and by the Navy Bureau of Aeronautics.
1.
SCOPE
1.1 Scope. - This specification covers hydraulic shuttle valves for use in type
II aircraft hydraulic systems conforming to and as defined in Specification MIL-H-5440
The complete specification for these valves consists of Specification MIL-H-8775, which
covers general requirements common to all aircraft hydraulic components, and this speci-
fication, which includes additional requirements specifically applicable to shuttle
valves.
Classification. Shuttle valves shall be furnished in accordance with the
folloowig standards as specified, (see 6.3).
Standard MS28766 Direct mounting.
Standard MS28767 Internal tube thread.
2.
APPLICABLE DOCUMENTS
2.1 The following specifications and standards, of the issue in effect on date
of invitation for bids, form a part of this specification to the extent specified herein:
SPECIFICATIONS
Military
MIL-H-5440
MIL-V-5529
MIL-H-8775
Hydraulic Systems
Design, Installation and Tests
of Aircraft (General Specification for)
Valves
}
Hydraulic Directional Control
Hydraulic System Components Aircraft, General
Specification for
STANDARDS
Military
MS28766
Valve Hydraulic Shuttle, 3,00 PSI, Direct Mounting
(Type II Systems)
MS28767
Valve - Hydraulic Shuttle, 3,000 PSI, Internal Thd.
Tube Fitting Outlet: (Type II Systems)
(Copies of specifications, standards, drawings, and publications required by con-
tractors in connection with specific procurement functions should be obtained from the
procuring activity or as directed by the contracting officer.)
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