SAE AMS 3144 : 2012

Superseded

View Superseded by

PRIMER, ANODIC ELECTRODEPOSITION FOR AIRCRAFT APPLICATIONS

Available format(s)

Hardcopy , PDF

Superseded date

10-21-2019

Language(s)

English

Published date

01-01-2012

Publisher

SAE International

1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES

Specifies the requirements for a waterborne, corrosion inhibiting, chemical and solvent resistant, anodic electrodeposition epoxy primer capable of curing at 200 to 210 degrees F (93 to 99 degrees C).

Committee	AMS G8
DocumentType	Standard
Pages	17
PublisherName	SAE International
Status	Superseded
SupersededBy	SAE AMS 3144 A : 2019

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