• AS196

• 2008-02-16

• 1948-03-01

• A-4 Aircraft Instruments Committee

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.

• SAE AS 196

• Aerospace

• Avionics
• Aircraft instruments
• Aircraft displays
• Flight control systems
• Flight management systems
• Interiors, Cabins and Cockpits
• Displays
• Smoke detection
• Instrument panels
• Parts
• Safety
• Fire detection
• Tests and Testing