SAE ARP1524A PDF

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Surface Preparation and Priming of Aluminum Alloy Parts for High Durability Structural Adhesive Bonding

Category: ARP Tags: Adhesives and sealants, Aluminum alloys, Assembling, Hazardous materials, Humidity, Nozzles, Parts, Production control, Titanium alloys

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Description

This Aerospace Recommended Practice (ARP) describes the processing system and techniques for the surface preparation and priming of aluminum alloy parts for structural adhesive bonding to achieve optimum bondline durability, corrosion resistance, and manufacturing producibility.

History

ARP1524A	2013-07-19	Latest	Reaffirmed
ARP1524	1978-04-01	Historical	Issued

ISSUING COMMITTEE	AMS P17 Polymer Matrix Composites Committee
DATE	2013-07-19
DOI	https://doi.org/10.4271/ARP1524A
ISCURRENT	Current
PAGE	10
PUBLISHER	SAE International
REVISED	REAFFIRMED