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SAE AS 196:2008-02-16
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SAE AS 196:2008-02-16
THERMO-SENSITIVE ELEMENT (IRON - CONSTANTAN)More info
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.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 2008-02-16 |
| ICS | 49.090 : On-board equipment and instruments
|
| Number of pages | 1 |
| Set | AEROPAKS10U-10 |
| Year | 2008 |
| Document history | |
| Country | USA |
| Keyword | SAE 196;SAE AS196;SAE AS196;SAE AS 196 |