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G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies Quality control Tools and equipment

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References, Spacecraft and Spacecraft Servicing, Fluid System Components (Abbreviations, Acronyms, Definitions, Applicable Documents and Environmental Conditions)
2021-04-30
CURRENT
AIR4728A
This SAE Aerospace Information Report (AIR) presents reference information for use in preparing detailed specifications and other documents. The intent is to have a master reference document containing frequently required tabulations of information, such as the meaning of abbreviations, the spelled out wording of acronyms, the definition of terms, etc. so that such tabulations need not be repeated in recommended practice documents describing how to prepare technical documents. This document is intended to provide references in the field of fluid system components for space applications. Space applications include spacecraft, such as satellites, space stations, launch vehicles and space shuttles, and servicing equipment and components used for ground systems and launching and for servicing in space. Fluid system components include couplings, fittings, hose and tubing assemblies.
Standard

IMPULSE TESTING OF HYDRAULIC HOSE ASSEMBLIES, TUBING, AND FITTINGS
1979-08-01
HISTORICAL
ARP603E
This Aerospace Recommended Practice (ARP) establishes the requirements and the procedures for impulse testing of hose assemblies, tubing, and fittings for use in aerospace hydraulic systems of 4000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
Standard

PERMISSIBLE DENT AND CHAFING DAMAGE OF AIRCRAFT HYDRAULIC TUBING
1975-07-01
HISTORICAL
AIR1388
This AIR is intended to assist in evaluating the serviceability of damaged hydraulic tubing lines. The performance requirements are outlined to which the defect samples were tested. Test methods and data are described and summarized to assist in further work toward establishing limits for defects in aircraft hydraulic tubing. Permissible defect limits are listed for 6061T6 aluminum return lines, 3000-psi hydraulic tubing of 21Cr-6Ni-9Mn as well as 304 1/8 hard corrosion resistant steel (CRES), and 3Al-2.5V cold-worked (CW) titanium.
Standard

Adapter - Port Connection, Ring Locked Installation and Removal of
2017-03-01
CURRENT
MA2114B
This SAE Aerospace Standard provides the essential minimum design, installation and removal standard for MA2111, MA2112, MA2113, and MA2119 adapters, and is applicable when specified on engineering drawings or in procurement documents.
Standard

National Aerospace and Defense Contractors Accreditation Program Titanium 3Al-2.5V Alloy, Seamless Hydraulic Tubing Manufacturing Requirements
2013-01-09
HISTORICAL
AS7112/6
This Aerospace Standard (AS) is to be used as a supplement to SAE AS7112. In addition to the requirements specified in AS7112, the requirements specified herein shall apply to suppliers seeking Nadcap Fluid System accreditation for manufacturing titanium 3AI-2.5V alloy, seamless hydraulic tubing. The corresponding PRI Audit Criteria (AC) is to be applied to ensure the tubing is manufactured to the applicable specification(s) and standard(s).
Standard

HOSE CHARACTERISTICS AND SELECTION CHART
1963-09-01
HISTORICAL
AIR797
This report lists military and industry specifications and standards which are used in aerospace systems and for ground servicing equipment. The characteristic limitations of the hose which are of major importance to designers and the sizes in which the hoses are standard, are shown. Revisions and amendments which are current for these specifications and standards are not listed.
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