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Standard

Solenoid, Electrical, General Specification For

2000-11-01
CURRENT
AS40401
This specification covers the general requirements for electrical solenoids used to actuate various devices through the conversion of electrical signals into mechanical motion. These solenoids are of the axial stroke type and the rotary stroke type.
Standard

Reducers, Pneumatic Pressure, Missile

1994-12-01
HISTORICAL
AS1297A
The complete specification for a pneumatic pressure reducer for high pressure pneumatic systems used in missiles comprises: (1) this standard, which includes many of the general performance requirements, (2) a detailed procurement specification describing envelope and operating conditions, and (3) the "Pneumatic Components, Aeronautical - General Specification For - MIL-P-8564" which covers general requirements common to all components for use in high pressure pneumatic systems.
Standard

Reducers, Pneumatic Pressure, Missile

2014-10-06
CURRENT
AS1297B
The complete specification for a pneumatic pressure reducer for high pressure pneumatic systems used in missiles comprises: (1) this standard, which includes many of the general performance requirements, (2) a detailed procurement specification describing envelope and operating conditions, and (3) the "Pneumatic Components, Aeronautical - General Specification For - MIL-P-8564" which covers general requirements common to all components for use in high pressure pneumatic systems.
Standard

Recommended Practice for the Design of Tubing Installations for Aerospace Fluid Power Systems

2012-08-22
HISTORICAL
ARP994A
This document provides recommended practices for the design of tubing systems that are used for the transmission of liquid and gasses in fluid power systems for aerospace vehicles such as aircraft, missiles and boosters. The primary emphasis is given to recommended practices for line sizing, tube routing, supports and clamping, stress considerations and permissible defects, and provisions for flexure through the use of flexible hoses, coiled tubes, swivel joints, and expansion glands. The sections regarding tubing materials and fitting types are included for reference, but particular recommendations are purposely avoided since their selection is dependent upon the specific requirements of each particular vehicle system and many other factors.
Standard

Recommended Design and Test Requirements for Quantity Measuring Hydraulic Fuses

2018-11-07
WIP
ARP8450
1. SCOPE This Aerospace Recommended Practice (ARP) provides recommendations for design and test requirements for quantity measuring hydraulic fuses. 1.1 Purpose The recommended requirements contained in this ARP are compiled for inclusion, as applicable, in a Procurement Specification for this type of hydraulic fuse. NOTES: 1. The recommended requirements in this ARP should be reviewed by the procuring activity and only those requirements that are applicable for a specific application should be incorporated in the Procurement Specification. 2.
Standard

RECOMMENDED PRACTICE FOR THE DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE FLUID POWER SYSTEMS

1976-04-01
HISTORICAL
ARP994
This document is a compendium of recommended practices for the design of tubing systems for the transmission of liquid and gasses influid power systems for aerospace vehicles such as aircraft, missiles and boosters, and is considered applicable to the design of future space vehicles and other applications using aircraft technology. Primary emphasis is given to recommended practices for line sizing, tube routing, supports and clamping, stress considerations and permissible defects, and provisions for flexure through the use of flexible hoses, coiled tubes, swivel joints, and expansion glands. Fluid power systems are differentiated from the normal aircraft fuel and oil systems and the various fluid systems used for environmental control and air conditioning systems; however, the practices cited herein will in many cases be applicable to these other systems.
Standard

Pump, Hydraulic, Ram, Hand Driven

2001-11-14
HISTORICAL
AS55151
This specification covers hand driven, hydraulic ram pumps used on type I (-65° to +160°F) aircraft hydraulic systems.
Standard

Pump, Hydraulic, Ram, Hand Driven

2004-08-04
CURRENT
AS55151A
This specification covers hand driven, hydraulic ram pumps used on type I (-65° to +160°F) aircraft hydraulic systems.
Standard

General Requirements for Hydraulic System Reservoirs

2018-06-11
CURRENT
AS5586A
This SAE Aerospace Standard (AS) specifies the general requirements for hydraulic system reservoirs that are installed in commercial and military aircraft and helicopters and also in missile hydraulic systems. This document includes design, test (production and qualification) criteria for various types of reservoirs. Appendix A provides information on hydraulic fluid volume requirements and reservoir sizing. This document also provides a basis for the Procurement Specification to completely define individual reservoir requirements.
Standard

Design of Tubing Installations for Aerospace Hydraulic Systems

2016-11-17
CURRENT
ARP994B
This document provides recommended practices for the design and selection of tube, hose, and fitting systems that are used to transmit hydraulic fluid on aircraft. NOTE: Guidance for the sizing of hydraulic tubing is contained in Appendix A.
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