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Standard

Aircraft Tube Bending Methods, Techniques and Tooling

2022-05-04
CURRENT
AIR5378A
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.
Standard

Aircraft Tube Bending Methods, Techniques and Tooling

2013-01-02
HISTORICAL
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.
Standard

Couplings, Clamp, Grooved, V-Band

2006-02-28
HISTORICAL
AS5355A
This SAE Aerospace Standard (AS) establishes the requirements for a V-band grooved clamp couplings that are intended for use on fluid-line tubing joints, tailpipe joints, and accessory mount joints, on flight vehicles or other attachments. The semi-rigid coupling joint assemblies, hereafter referred to as “the joint”, shall operate within the temperature ranges specified in their applicable part standards.
Standard

Fittings and Bosses, Pipe Threaded, Fluid Connection

2015-06-30
HISTORICAL
AS4842
This SAE Aerospace Standard (AS) establishes the requirements for 37° flared tube or machined cone fluid connection fittings (see Section 6) for use in all types of fluid systems.
Standard

Fluid Couplings for Spacecraft Servicing, Preparation of Specification for, Metric

2015-08-21
CURRENT
MAP2261
This SAE Metric Aerospace Recommended Practice (MAP) establishes the requirements for preparing a specification for fluid couplings for spacecraft servicing. The objective of this document is to provide design, development, verification, storage, and delivery requirement guidelines for the preparation of specifications for fluid couplings and the ancillary hardware for use with serviceable spacecraft designed for use in the space environment. The couplings shall be capable of resupplying storable propellants, cryogenic liquids, and gases to a variety of spacecrafts.
Standard

Hole Contour, Fluid Passage, Tube Fitting

2013-08-15
CURRENT
AS4266
This SAE Aerospace Standard (AS) provides required contours and limits of size of the surfaces of the internal fluid passages of tube fittings for the portions that are not already defined by the fitting end design standard drawings.
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