Specifications
Surface Treatments
Certifications
- ISO 9001 - 2015 Certified
- PED 2014/68/EC
- NACE MR0175/ISO 15156-2
- NORSOK M-650
- DFAR
- MERKBLATT AD 2000 W2/W7/W10
A286 mechanical properties (yield strength, tensile strength, hardness, elongation, density) follow the requirements of the applicable specification. Reference pages: AMS 5732 (≥ 895 MPa tensile / ≥ 655 MPa yield) · AMS 5737 (precision-aged) · ASTM A453 grade 660 (Class A/B/C/D variants) · ASTM A638 grade 660 (Type 1/2 forgings).
A286 retains mechanical properties from cryogenic to elevated temperatures. Industry applications relying on these properties: jet engine fasteners · gas turbine · nuclear · aerospace.
Compare against alternative alloys: A286 vs Inconel 718 · A286 vs 17-4 PH · A286 vs Waspaloy · A286 vs Nimonic 80A.
Related canonical A286 reference: A286 chemical composition · A286 heat treatment · A286 machinability · AMS / ASTM specifications hub.
Alloy A286 (UNS S66286) develops its strength through precipitation of gamma-prime Ni₃(Ti,Al) during the 720 °C / 16-hour aging cycle. The values below correspond to ASTM A453 grade 660 Class A (solution-treated 980 °C, oil-quenched, aged 720 °C / 16 h) and represent typical specimen results, certified test reports per heat are available on request.
| Test Temperature | 0.2 % Yield (MPa) | UTS (MPa) | Elongation (%) | Reduction of Area (%) |
|---|---|---|---|---|
| 21 °C (RT) | 655 | 895 | 15 | 18 |
| 425 °C | 595 | 810 | 17 | 25 |
| 540 °C | 580 | 770 | 19 | 28 |
| 650 °C | 540 | 685 | 21 | 35 |
| 700 °C | 485 | 580 | 25 | 42 |
Stress to cause rupture in 1000 hours at temperature (typical, AMS 5732 condition):
Typical Charpy impact energy at 21 °C: 35-45 J. Impact energy at −196 °C (cryogenic): 30-40 J, A286 retains usable toughness down to liquid-nitrogen temperatures, supporting aerospace and LNG cryogenic-service fastener applications.
A286 creep strength is the rate-controlling property for sustained-temperature service. Typical creep rate (1 % deformation in 1000 hours per AMS 5732 condition):
For sustained service above 700 °C with continuous load, A286 creep deformation accumulates beyond useful design margin. Waspaloy retains usable creep resistance to ~870 °C; Nimonic 80A to ~815 °C. For 540-700 °C continuous service A286 is the cost-efficient choice; above this temperature switch to higher-temperature superalloys.
For engineers selecting A286 against alternative precipitation-hardening alloys, the relevant mechanical-property comparisons:
Mechanical property requirements differ by specification, full per-spec property tables on the dedicated pages: