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Fuel systems Control systems Finishing Commercial aircraft G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

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Standard

Flexure Fatigue Strength of Tube Fitting Joints
2013-01-02
HISTORICAL
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.
Standard

FLEXURE FATIGUE STRENGTH OF TUBE FITTING JOINTS
2011-08-09
HISTORICAL
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.
Standard

Flexure Fatigue Strength of Tube Fitting Joints
2020-05-06
CURRENT
AIR1418B
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.
Standard

U.S. Government Document Retention Status and Non-Government Document Replacement - Aerospace Couplings, Fittings, Hoses, and Tube Supports
2007-09-26
HISTORICAL
AIR5478
This SAE Aerospace Information Report (AIR) is intended to document the status of U.S. Government Specifications and Part Standards used by SAE G-3 Committee. The contents are based on information provided by the Standard Preparing Activities of the U.S. Air Force, Army, Navy, and DSCC in support of Military Standards Reform. The data has been tabulated to show the current government status, the applicable superseding documents, and the G-3 committee document replacement decision.
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

Fitting, Plug-in Union, Ring Locked, 24 Degree Cone, Fluid Connection, 5080 psi (35 000 kPa), Specification for
2010-07-07
HISTORICAL
AS5000C
This SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone AS5827 or EN 6123 flareless Ring locked fitting assemblies per AS5550 and AS5865, for use in aircraft fluid systems at nominal operating pressure of 5080 psi (35 000 kPa) maximum and operating temperature range of -65 to +275 °F (-54 to +135 °C). The general requirements shall be for, but not limited to, commercial aircraft hydraulic components per AS4941, using port configuration as specified in AS5551.
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