•   0091-22-66157017
  •   info@torqbolt.com
  • Home

    A286 Mechanical Properties

    A286 Specifications

    • AECMA PrEn2171
    • AECMA PrEN2119
    • AECMA PrEN2172
    • AECMA PrEN2173
    • AECMA PrEN2174
    • AECMA PrEN2303
    • AECMA PrEN2304
    • AECMA PrEN2398
    • AECMA PrEN2399
    • AECMA PrEN3510
    • ASME SA 891 (Type 1, 2)
    • ASME SA 638 (Grade 660 Type 1, 2)
    • ASME SA 453 (Grade 660 Class A, B, C, D)
    • BS HR 51
    • BS HR 52
    • GE C50TF78
    • GE C50TF27
    • GE C50TF20
    • GE B50T1181C
    • UNS S66286
    • SAE J467-A286
    • SPS M-118
    • Fairchild MS 301
    • 314 Elliott Turbine MS 618 Weatherford WS-881
    • Cameron MS-003030
    • EN 2399
    • PWA-LCS
    • GE-S400/1000
    • RR SABRe Edition 2
    • EN 1.4944
    • EN 1.4943
    • EN 1.4980

    A286 Mechanical Properties Across Specifications

    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 Mechanical Properties, Tensile, Creep, Stress-Rupture

    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.

    A286 Tensile Properties, Yield, Ultimate, Elongation at RT to 700 °C

    Test Temperature0.2 % Yield (MPa)UTS (MPa)Elongation (%)Reduction of Area (%)
    21 °C (RT)6558951518
    425 °C5958101725
    540 °C5807701928
    650 °C5406852135
    700 °C4855802542

    A286 Stress-Rupture Strength, 1000-Hour Life at Temperature

    Stress to cause rupture in 1000 hours at temperature (typical, AMS 5732 condition):

    A286 Hardness, Modulus of Elasticity & Density

    A286 Charpy V-Notch Impact & Cryogenic Toughness

    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 at 540-700 °C

    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.

    A286 Mechanical Properties vs Alternative Alloys

    For engineers selecting A286 against alternative precipitation-hardening alloys, the relevant mechanical-property comparisons:

    A286 Mechanical Properties by Specification

    Mechanical property requirements differ by specification, full per-spec property tables on the dedicated pages: