Standard

SAE MA2250

Aug 2015 Published

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Abstract

This Aerospace Specification establishes the requirements for a threaded flexible coupling assembly, hereafter referred to as the assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel, vent, or other systems. This coupling assembly is designed for use from -54 to 93 °C and at 862 kPa peak working pressure. AS coupling components referenced herein have been qualified to AS1710. Ferrule referenced herein are inch ferrules adapted to metric tubing.

Document information

Standard from SAE International
Published: 21 August 2015
Document type: IS
Pages
ISBN:

Publisher SAE International
Distributor SAE International

Product Relations

Referred by: SAE MA2251A
Refers: SAE MA2251
Refers: SAE AS1712
Refers: SAE AS1713
Refers: SAE AS1718
Refers: SAE AS1719
Refers: SAE AS1720
Refers: SAE AS568
Refers: SAE AS567

SAE MA2250

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