SAE AMS2510F
Current
The latest, up-to-date edition.
ENGINE GRAY FINISHING LOW BAKING
Hardcopy , PDF
English
20-09-2017
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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 AMS2475G | PROTECTIVE TREATMENTS, MAGNESIUM ALLOYS |
| SAE AMS3125H | ENAMEL, GLYCERYL PHTHALATE, ENGINE GRAY BAKING |
| SAE AMS2350BA | Standards and Test Methods |
| MIL-STD-794 Revision E:1982 | PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF |
| SAE AMS2400X | PLATING, CADMIUM |
| SAE AMS2480H | PHOSPHATE TREATMENT PAINT BASE |
| SAE AMS3110K | PRIMER, ZINC CHROMATE |
| SAE AMS2471H | ANODIC TREATMENT OF ALUMINUM ALLOYS SULFURIC ACID PROCESS, UNDYED COATING |
| SAE AMS2470N | ANODIC TREATMENT OF ALUMINUM ALLOYS, CHROMIC ACID PROCESS |
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