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SAE International - AS1733F

BODY, COUPLING, RIGID, FIXED CAVITY, THREADED, FERRULE TYPE TUBE ENDS, TYPE II

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Organization: SAE International
Publication Date: 16 December 2019
Status: active

Document History

AS1733F
December 16, 2019
BODY, COUPLING, RIGID, FIXED CAVITY, THREADED, FERRULE TYPE TUBE ENDS, TYPE II
A description is not available for this item.

References

This document references:
AMSQQA200/3 - Aluminum Alloy 2024, Bar, Rod, Shapes, Tube, and Wire, Extruded
Published by SAE International on May 3, 2018
This specification covers the specific requirements for aluminum alloy 2024 bar, rod, shapes, tube, and wire produced by extrusion.
This document references:
AMSQQA225/6 - ALUMINUM ALLOY, 2024, BAR, ROD, AND WIRE; ROLLED, DRAWN, OR COLD FINISHED
Published by SAE International on July 1, 1997
This specification covers the specific requirements for 2024 aluminum alloy bar, rod and wire produced by rolling, drawing or cold finishing.
This document references:
AMSWWT700/3 - Tube, Aluminum Alloy, Drawn, Seamless, 2024
Published by SAE International on July 1, 2001
This specification covers the specific requirements for seamless tube drawn from aluminum alloy 2024.
This document references:
AS1730 - COUPLING, FUEL, RIGID, THREADED TYPE
Published by SAE International on September 1, 1982
This specification defines the requirements for a threaded rigid coupling assembly, which utilizes ferrule type machined tube end fittings, to join tubing and components in aircraft fuel, vent and...
This document references:
AS478 - IDENTIFICATION MARKING OF ITEMS FOR AIRCRAFT POWER PLANTS
Published by SAE International on May 15, 1960
This standard covers permanent marking intended to be easily and accurately read during the normal service life of the item and also covers temporary marking intended to provide legible...
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