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GASKET - COPPER, TUBE CONNECTION, PLAIN
- Aerospace Standard
Published May 03, 2006 by SAE International in United States
Downloadable datasets availableAnnotation ability available
THIS DOCUMENT HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE 5-YEAR REVIEW POLICY.
MATERIAL: COPPER AMS 4500.
HEAT TREATMENT: GASKETS SHALL BE ANNEALED AFTER FABRICATION.
SURFACE TEXTURE: SYMBOLS PER ANSI Y14.36-1978; REQUIREMENTS PER ANSI B46.1-1978.
DIMENSIONING AND TOLERANCING: ANSI Y14.5-1973.
BREAK SHARP EDGES .003 - .015 (0.08 - 0.38).
DIMENSIONS IN INCHES (MILLIMETRES). METRIC CONVERSIONS ARE INTERNATIONAL SYSTEMS UNTTS (SI).
IDENTIFICATION: APPLY MARKING SYMBOL PER AS478-29. SYMBOLS MAY BE SINGLE OR MULTIPLE.
IF MULTIPLE: PORTIONS OF THE SYMBOL MAY BE INCOMPLETE. MARK PART NUMBER AND MANUFACTURERS IDENTIFICATION ON CONTAINER.
THICKNESS TO BE UNIFORM WITHIN .002 (0.05).
DO NOT USE UNASSIGNED PART NUMBERS.
|Aerospace Material Specification||Identification Welding Wire, Tab Marking Method|
|Aerospace Standard||GASKET - 37° FLARED TUBE FITTING, NICKEL, AMS5553|
Data Sets - Support Documents
|Unnamed Dataset 1|
E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
|AMS4500||Copper, Sheet, Strip, and Plate, Soft Annealed|
|ANSI/ASME/B46.1||This document is not part of the subscrption.|
|ANSI/Y14.36||This document is not part of the subscrption.|
|ANSI/Y14.5||This document is not part of the subscrption.|
|AS478||Identification Marking Methods|
|AS478J||Eddy Current Inspection of Circular Holes in Nonferrous Metallic Aircraft Engine Hardware|
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