ENGINE GRAY FINISHING LOW BAKING

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

20-09-2017

Publisher

SAE International

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

This specification covers the engineering requirements for finishing aircraft parts and assemblies with an engine gray enamel.

Committee	AMS-B
DocumentType	Standard
Pages	4
PublisherName	SAE International
Status	Current
Supersedes	SAE AMS 2510 : 2013

SAE AMS 2475H : 2009	PROTECTIVE TREATMENTS, MAGNESIUM ALLOYS
SAE AMS 3125 : 2012	ENAMEL, GLYCERYL PHTHALATE, ENGINE GRAY BAKING
SAE AMS 2350 : 1989	STANDARDS AND TEST METHODS
MIL-STD-794 Revision E:1982	PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF
SAE AMS 2400 : 2013	PLATING, CADMIUM
SAE AMS 2480 : 2013	PHOSPHATE TREATMENT PAINT BASE
SAE AMS 3110 : 2013	PRIMER, ZINC CHROMATE
SAE AMS 2471 : 2014	ANODIC TREATMENT OF ALUMINUM ALLOYS SULFURIC ACID PROCESS, UNDYED COATING
SAE AMS 2470 : 2013	ANODIC TREATMENT OF ALUMINUM ALLOYS, CHROMIC ACID PROCESS