2759/2 | Ams

Modified with vanadium for improved toughness in airframe structural fittings.

Due to the limited hardenability inherent in ultra-high-strength steel processing, AMS 2759/2 establishes explicit to prevent incomplete martensitic transformation at the core of the part. Critical Process Steps and Thermal Cycle Controls ams 2759/2

When required by the purchase order, tensile testing, impact testing, or metallographic examination may be performed to verify conformance to mechanical property requirements. Modified with vanadium for improved toughness in airframe

If you tell me your specific role (e.g., heat treater, design engineer, auditor), I can narrow down the most useful single paper for you. ams 2759/2