AMS6459G is the latest revision released by SAE International in December 2023, replacing AMS6459F, which was confirmed in 2007. This specification targets low-alloy steel welding wire with a composition of 1.0Cr-1.0Mo-0.12V (0.18-0.23C), corresponding to the UNS K22720 alloy system, and is primarily used in critical weld joints in the aviation industry.
| Element | Minimum Value(%) | Maximum Value(%) | Test Method |
|---|---|---|---|
| Carbon (C) | 0.18 | 0.23 | ASTM A751 |
| Chromium (Cr) | 0.80 | 1.20 | |
| Molybdenum (Mo) | 0.80 | 1.20 | |
| Vanadium (V) | 0.08 | 0.15 | Regular finished product testing |
| Hydrogen (H) | - | 0.0010 | ASTM D2650 |
Main updates to the 2023 edition: Strengthening the control of interstitial elements such as oxygen (≤100ppm), nitrogen (≤50ppm), and hydrogen (≤10ppm), requiring periodic gas element testing of finished steel wire.
The steel wire was used for GTAW welding of the high-pressure casing of an aircraft engine. After post-weld heat treatment, the strength of the weld joint reached 98% of the parent material, meeting the requirements of AMS6415 for base material.
| Test Type | Test Item | Implementation Standard | Frequency |
|---|---|---|---|
| Acceptance Test | Chemical Composition/Dimensions | AMS2259 | Per Heat/Batch |
| Periodic Test | Weldability | ARP1876 | Manufacturer Specific |
| Special Test | Alloy Verification | ARP4926 | Per Reel/Pack |
Packaging and labeling requirements: AMS2814 high-quality packaging methods must be used, and 203mm of length must be retained at both ends of each coil of steel wire for alloy verification.

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Update:
Mon, 18 May 2026 19:10:06 +0000