SAE AS196
Thermo-Sensitive Element (Iron - Constantan)
Month of publication: 1948-03-01
Date reaffirmed: February 2008
Developed by committee: A-4 Aircraft Instruments Committee
Annotation and contents
Source of this annotation and contents: SAE.
This specification defines the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft air systems. The rigid coupling joint assembly, hereafter referred to as "the joint", shall operate within the temperature range of -65 degrees Fahrenheit to +800 degrees Fahrenheit.
