SAE AMS 2510 : 2017
Current
The latest, up-to-date edition.
ENGINE GRAY FINISHING LOW BAKING
Hardcopy , PDF
English
20-09-2017
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 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 |
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