Fitting, Tee, Internal Straight Thread Port

Standard:
Revised:
  • 2008-11-05
 
  • HISTORICAL Access the latest revision: AS5192D
Publisher:
  • SAE International
Pages:
5
Scope:

Scope unavailable.

Rationale:

1. THIS STANDARD IS BEING REVISED TO REDUCE THE OPERATING PRESSURES FOR ALUMINUM, SIZES -10 AND ABOVE. THIS WAS PROMPTED BY MS20819/AS5176 WHICH ELIMINATED ALUMINUM AS AN OPTIONAL METAL. AND AS A RESULT, THE OPERATING PRESSURES FOR MANY OTHER MIL-F-5509/AS4841 AS4842/AS4843/AS4875 FLARED FITTING PARTS, THAT USED ALUMINUM, WERE REDUCED, FOR SIZES -10 AND ABOVE.

2. UPDATED NADCAP NOTE PER AEROSPACE STYLE MANUAL. SEE /4/

3. ADDED CADMIUM WARNING NOTE PER AEROSPACE STYLE MANUAL.

4. ADDED TITANIUM NOTE /17/ . LEGACY FROM AN938

5. INCLUDED CADMIUM IN TITANIUM NOTE /17/. FROM COMMENT AND LEGACY FROM AN938.

6. REDUCED WEIGHTS BY 10%. FROM COMMENT.

7. ADDED IVD FINISH AND FLAG NOTE /18/ TO PIN FOR "V" FINISH OPTION FOR ALUMINUM. FROM COMMENT.

8. ADDED CRES 347 AND INACTICATIVATED IT TO CRES 321 CODE R. LEGACY FROM AN938 AND COMMENT.

History:
Standard Published Revision Status
AS5192D 2014-04-22 Latest Revised
2008-11-05 Historical Revised
2005-06-24 Historical Revised
2005-01-20 Historical Revised
2000-07-01 Historical Issued
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