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Viewing 1 to 30 of 1863
CURRENT
1993-03-01
Standard
AIR1973A
This index of trademarks of current and former manufacturers of aerospace fittings, couplings, hose, and tube support devices is within the scope of activities of the SAE G-3 Committee and available at the time of publication. Suggestions for additional entries may be sent to the SAE in Warrendale, PA.
HISTORICAL
1987-01-01
Standard
AIR1973
Listings are current and former manufacturers of aerospace fittings, couplings, hose and tube support devices that are within the scope of activities of the SAE G-3 Committee and available at the time of publication. Suggestions for additional listings may be sent to the SAE in Warrendale, PA.
CURRENT
1999-12-01
Standard
AIR5378
This SAE Aerospace Information Report (AIR) is intended to assist tube bending facilities dedicated to aerospace/aircraft applications. It describes in part the principles, methods, tool selection, and tool set-up requirements to achieve tube bends with aircraft quality.
CURRENT
2001-08-01
Standard
AIR5426
This SAE Aerospace Information Report (AIR) includes the selection, installation, inspection, and maintenance of tube fittings and tube fitting assemblies used in aerospace plumbing applications. The user must determine the suitability of selected designs to meet the performance requirements of the system for which it is intended to be installed. Only fittings for which industry or government standards have been published are described in Section 3 of this Aerospace Information Report. A variety of these tube fittings are shown in AIR310. Illustrations of some non-published proprietary designs are shown in Section 7.
CURRENT
1990-12-06
Standard
AIR310A
This Aerospace Information Report (AIR) is written as an aid for locating and identifying various fitting designs and configurations that are designated as standard parts.
HISTORICAL
1994-06-01
Standard
AIR310
This Aerospace Information Report (AIR) is written as an aid for locating and identifying various fitting designs and configurations that are designated as standard parts.
HISTORICAL
1972-11-01
Standard
AIR1228
This SAE Aerospace Information Report (AIR) establishes the part numbers and/or description of the critical components and operational guidelines for the standard hydraulic impulse machine for testing hydraulic hose assemblies, tubing, coils, and fittings and may be used for similar fluid system components, if desired. The standard impulse machine is established for the following purposes: As referee in the event of conflicting data from two or more nonstandard impulse machines. Such a referee machine might be built by an impartial testing activity. A design guide for future machines being built by manufacturers and users, or the upgrading of present machines. A design guide for higher pressure machines or special purpose machines being designed. It is not the intention of this document to obsolete present machines.
CURRENT
2009-01-07
Standard
AIR1228A
This SAE Aerospace Information Report (AIR) establishes the specifications and descriptions of the critical components and operational guidelines for the standard hydraulic impulse machine for testing hydraulic hose assemblies, tubing, coils, fittings and similar fluid system components. This revision to the AIR1228 provides a description of a system that meets the requirements for specifications including: AS603, AS4265, and ARP1383. This impulse system utilizes closed loop servo control with specifically generated command signal waveforms. Data accuracy and integrity are emphasized in this revision. Knowing the uncertainty of the pressure measurement is important whether using a resonator tube system, as described in the original release of this document, or a closed-loop systems as described in this release. The accuracy of the data measurement system and consistency of the pressure waveform are fundamental to test validity, regardless of the system type.
HISTORICAL
1978-10-01
Standard
AIR1358
This AIR indicates those dimensions,d eemed critical by the manufacturer, which are required to be adhered to so that proper mating of the disconnect hose fitting with the correct disconnect be accomplished. The dimensions are critical, but not necessarily complete, in defining these fittings since there are other criteria which must also be met.
HISTORICAL
2009-08-27
Standard
AIR1358B
This Aerospace Information Report (AIR) indicates those dimensions, deemed critical by the manufacturer to assure proper mating of disconnect hose fittings. The dimensions are critical, but not necessarily complete, in defining these fittings since there are other criteria which must also be met.
HISTORICAL
2000-10-01
Standard
AIR1358A
This AIR indicates those dimensions, deemed critical by the manufacturer, which are required to be adhered to so that proper mating of the disconnect hose fitting with the correct disconnect be accomplished. The dimensions are critical, but not necessarily complete, in defining these fittings since there are other criteria which must also be met.
CURRENT
2014-12-31
Standard
AIR1358C
This Aerospace Information Report (AIR) indicates those dimensions, deemed critical by the manufacturer to assure proper mating of disconnect hose fittings. The dimensions are critical, but not necessarily complete, in defining these fittings since there are other criteria which must also be met.
HISTORICAL
1985-07-01
Standard
AIR1160B
HISTORICAL
1973-11-30
Standard
AIR1160A
CURRENT
1999-10-01
Standard
AIR1160C
This document defines features that require interface definitions between aircraft engines and accessory drives and flanges and summarizes various aerospace standard dimensional performance data.
HISTORICAL
1977-07-01
Standard
AIR853
CURRENT
1999-10-01
Standard
AIR853A
This document defines the functional requirements of basic types of disconnect devices used in airborne accessory installations.
CURRENT
1994-08-01
Standard
AIR4918
To present a summary of the guidelines and practices presently being used by the aerospace industry for the selection of coiled tubes, flexible hoses, swivel fittings, and extension fittings in aircraft fluid systems.
CURRENT
1996-08-01
Standard
AIR1418A
This SAE Aerospace Information Report (AIR) presents flexure fatigue strength of tube fitting joints in the form of graphs showing applied deflection D and total calculated axial stress S versus number of cycles to failure N. The graphs have been prepared from data obtained by actual testing conducted in accordance with ARP1185.
HISTORICAL
1993-04-01
Standard
AIR1418
This information report presents flexure fatigue strength of tube fitting joints in the form of graphs showing applied deflection D and total calculated axial stress S vs. number of cycles to failure N. The graphs have been prepared from data obtained by actual testing conducted in accordance with ARP 1185.
CURRENT
2013-04-12
Standard
AMSP5510A
This specification covers requirements for the material, design, testing and packaging of straight thread tube fitting boss O-rings. O-rings covered by this specification are acrylonitrile-butadiene rubber.
HISTORICAL
1998-03-01
Standard
AMSP5510
This specification covers requirements for the material, design, testing and packaging of straight thread tube fitting boss packings.
CURRENT
2016-06-09
Standard
AMSP29609A
This specification covers basic characteristics required for porous polyimide materials intended for use as instrument and thin section ball bearing retainers (cages), and methods of determining these characteristics.
HISTORICAL
1985-09-01
Standard
ARP603F
This Aerospace Recommended Practice (ARP) establishes the requirements and procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace hydraulic systems of 8000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
CURRENT
2008-06-19
Standard
ARP603G
This Aerospace Recommended Practice (ARP) establishes the requirements and procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace systems of 8000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
HISTORICAL
1963-09-01
Standard
ARP603A
This Aerospace Recommended Practice (ARP) establishes the requirements and procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace systems of 8000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
HISTORICAL
1975-07-15
Standard
ARP603C
This Aerospace Recommended Practice (ARP) establishes the requirements and procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace systems of 8000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
HISTORICAL
1979-08-01
Standard
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.
HISTORICAL
1977-10-01
Standard
ARP603D
This Aerospace Recommended Practice (ARP) establishes the requirements and procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace systems of 8000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
CURRENT
1999-09-01
Standard
ARP600B
This SAE Aerospace Recommended Practice (ARP) defines a method for determining a torque value (range) for threaded fluid connections.
Viewing 1 to 30 of 1863

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