This content is not included in your SAE MOBILUS subscription, or you are not logged in.
The Pre-Treatment and Protection of Steel Items of Specified Maximum Tensile Strength Exceeding 1450 MPa
- Aerospace Material Specification
- AMS03_4
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This SAE Standard specifies the special treatments and precautions that are to be observed when protective and other surface treatments are applied to items, including springs, made from steel of specified maximum tensile strength exceeding 1450 MPa. The requirements of this Standard qualify those in process specifications and override the latter where there is conflict. The Standard also gives advice on design, manufacture, and preparation of items prior to cleaning and protection.
Rationale
This Standard is a direct replacement for DEF STAN 03-4 and has been reproduced by SAE International under the Open Government Licensing Agreement. The technical content remains unchanged from Issue 6 of the Defence Standard it supersedes. Any queries should be referred via the link shown in the feedback box at the bottom of this page.
Recommended Content
| Aerospace Material Specification | The Pre-Treatment and Protection of Steel Items of Specified Maximum Tensile Strength Exceeding 1450 MPa |
| Aerospace Material Specification | Steel, Corrosion and Heat-Resistant, Welded Tubing 18Cr – 10.5Ni – 0.40Ti (321) Solution Heat Treated |
| Aerospace Material Specification | Copper-Nickel-Tin Alloy, Bars and Rods 77Cu - 15Ni - 8Sn Solution Annealed, Cold Finished and Spinodal Hardened (TX TS) |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| [Unnamed Dataset 1] | ||
| Table 1 | Tensile strength criteria | |
| [Unnamed Dataset 3] | ||
| Table 2 | Baking treatments to be given to items after protective processing |
Issuing Committee
AMS B Finishes Processes and Fluids Committee
The committee of Finishes, Processes, and Fluids, AMS Committee B, shall prepare, coordinate, and revise documents related to processing technology, such as plating, brazing, coatings and compounds, through the participation of process suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace processes.
Reference
| Number | Title |
|---|---|
| AMD03_14 | This document is not part of the subscrption. |
| AMS03_11A | Phosphate Treatment of Iron and Steel |
| AMS03_17A | Electro-Deposition of Gold |
| AMS03_19A | Electro-Deposition of Cadmium |
| AMS03_2C | Cleaning and Preparation of Metal Surfaces |
| AMS03_20A | Electro-Deposition of Zinc |
| AMS03_27A | Electro-Deposition of Nickel for Engineering Purposes |
| AMS03_28 | This document is not part of the subscrption. |
| AMS03_9A | Electro-Deposition of Silver |
| ASTMF519 | This document is not part of the subscrption. |
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.