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    A286 Tie Rod

    A286 tie rod is A286 threaded rod specifically designed for tension-loaded structural and machinery applications, tying two structural members together against a tensile load. Distinguished from general-purpose threaded rod by intended use (tie rod = primary tension-load-carrying member with engineered end fittings; threaded rod = general all-thread material). TorqBolt manufactures A286 tie rod to ASTM A453 grade 660, AMS 5731 / 5732, DIN 976, and custom drawing standards in M12-M64 metric and 1/2 inch to 2-1/2 inch sizes. End geometries include threaded for clevis-pin termination, threaded for eye-end fitting, threaded for jam-nut + plate termination, and machined-shoulder for shoulder-eye fitting. Heat-treated to deliver 130 ksi tensile / 95 ksi yield, retained mechanical properties to 700 °C continuous service. See parent A286 rods, sister variants threaded rod, hex rod, and the canonical chemical composition, heat treatment.

    About A286 Tie Rod

    A286 tie rod (UNS S66286), tension-loaded threaded rod with end fittings

    A286 tie rod design centres on tension-load capability rather than length flexibility. Each tie rod is machined to drawing, typically from A286 round bar input, with the central shank turned to specified diameter, threads rolled or cut at each end to engage matching clevis / eye / jam-nut fittings, and surface-passivated per ASTM A967 Type II. Critical design feature: the shank cross-section determines tension capacity (tensile area × yield stress = pull capacity); the threads concentrate stress at the root, so thread-root cross-section is typically 60-70 % of shank cross-section. For aerospace fail-safe design, redundant tie-rod pairs or backup retention is specified, a single A286 tie rod failing under tension can be catastrophic. Heat-treated per AMS 5732 for 130 ksi tensile, 95 ksi yield. Surface finish typically cold-drawn or peeled; centerless-ground for precision applications.

    A286 Tie Rod Configurations & End Fittings

    TorqBolt produces A286 tie rod in five primary end-fitting configurations:

    • Threaded both ends (jam-nut termination), Most common, threaded both ends for jam-nut + plate or jam-nut + frame termination. Tension transferred through the jam-nut + plate into the structural frame.
    • Threaded both ends (clevis-pin termination), Threaded both ends; clevis fitting + cross-pin transfers tension through the clevis ears into the structural frame. Used in adjustable-length tie applications.
    • Threaded one end + machined eye end, Threaded one end + integral eye-end machined as a single piece, eye accepts a clevis pin for direct frame attachment. Eliminates separate eye fitting.
    • Threaded both ends + turnbuckle center, Tie rod with reverse-thread directions at each end + central turnbuckle body that adjusts overall length under load. Used in bracing and rigging applications.
    • Custom shoulder eye + threaded shank, Tie rod with machined shoulder + integral eye at one end + threaded shank at the other, used in aerospace control-linkage and engine-mount applications.

    A286 Tie Rod Sizes & Tension Capacity

    Shank diameterThreadStandard lengthTensile area mm²Min. tension (kN)Working tension (kN, 75% yield)
    12 mmM12 × 1.75200-2000 mm84.375.555.2
    16 mmM16 × 2.0200-2500 mm157140103
    20 mmM20 × 2.5300-3000 mm245219160
    24 mmM24 × 3.0300-3000 mm353316231
    30 mmM30 × 3.5300-3000 mm561502367
    36 mmM36 × 4.0300-3000 mm817731535
    48 mmM48 × 5.0300-3000 mm14731318964
    64 mmM64 × 6.0300-3000 mm267623951751

    A286 Tie Rod Manufacturing Process

    Every a286 tie rod TorqBolt ships traces back to a vacuum-induction-melted plus vacuum-arc-remelted (VIM-VAR) ingot meeting AMS 5731 / 5732 chemistry. Process route:

    1. VIM-VAR round bar input: AMS 5731 / 5732 round bar drawn or peeled to shank-blank diameter ≈ shank ⌀ + 0.5-1 mm machining allowance.
    2. Shank turning: CNC lathe turns shank to drawing diameter, typically smooth turned + rolled finish or centerless-ground for precision applications.
    3. End-fitting machining: Both ends machined to specified geometry: threading for jam-nut termination, machined eye for direct clevis attachment, or shoulder + thread for shoulder-eye fittings.
    4. Thread rolling (preferred) or cutting: Threads rolled (Class 6g / 4g6g) for fatigue performance; cutting only for sizes > M64. Roll-formed threads provide 30-40 % higher fatigue strength.
    5. Solution treatment: Vacuum or atmosphere furnace 1650 °F (AMS 5737) or 1800 °F (AMS 5732 alt). 1 h per inch of section, oil-quench.
    6. Precipitation aging: 1325 °F for 16 hours, air-cool. Hardness 29-32 HRC.
    7. Surface finish: Pickle + passivate per ASTM A967 Type II. Optional silver / nickel anti-galling for above-540 °C service.
    8. Tensile pull-test (sampling): Sample from each heat tested in tensile-pull fixture per ASTM E8, confirms guaranteed minimum tensile strength.
    9. Marking + label: Tie rod end-stamped 'A286' + lot. Heat-traceability label attached. AS9102 first-article on aerospace lots.

    A286 Tie Rod Inspection & Certification

    Each lot ships with a signed inspection certificate. Aerospace orders default to AS9100D first-article reporting per AS9102. Industrial orders default to EN 10204 type 3.1; sour-service and offshore step up to type 3.2 with third-party witness. Inspection scope:

    • Shank diameter verified by snap gauge per drawing tolerance (typically ±0.05-0.10 mm).
    • Thread gauge GO/NO-GO at both ends per ISO 1502 (commercial) or MIL-S-8879 (aerospace).
    • End-fitting geometry verified by CMM or fixed-gauge inspection.
    • Tensile pull-test (sampling per heat) per ASTM E8, confirms minimum tensile strength.
    • Hardness traverse 4-point Vickers per heat-treat batch per ASTM E384.
    • Magnetic permeability < 1.005 per ASTM A342 on every aerospace heat.
    • LPI per ASTM E1417 on aerospace lots, full surface inspection.
    • AS9102 first-article on aerospace lots per AS9100D AQMS.

    A286 Tie Rod Installation & Service Notes

    Tie rod is tension-loaded, apply preload to shank by tightening jam nuts at both ends to specified torque, then verify tension by elongation measurement (Δlength / original length × A286 modulus 199 GPa). Working tension typically 50-65 % of yield (vs 75 % for cycling joints) due to fatigue considerations. For aerospace tie rods, redundant retention or backup tie-rod pairs are typically specified for fail-safe design. Above 540 °C apply nickel anti-seize at thread + jam-nut interfaces. For long tie rods, account for thermal expansion: A286 coefficient is 17.0 µm/m·°C, a 2 m tie rod expands ~9 mm from 20 °C to 700 °C; spring-mount termination required to accommodate.

    A286 Tie Rod Applications by Industry

    A286 tie rod serves tension-loaded structural and machinery applications:

    • Aerospace control-linkage tension members: A286 tie rods as control-rod tension members in flight-control linkages, spoiler actuators, flap-deployment mechanisms. Non-magnetic + 700 °C ceiling.
    • Industrial gas turbine combustor tie-rods: Tie rods spanning combustor liner-to-casing structural attach, tension-loaded against combustion-pressure load + thermal-cycling differential expansion. A286 gas turbine applications.
    • Pressure-vessel internal tie-rods: A286 tie rods in nuclear and petrochemical pressure vessels, internal structural reinforcement against pressure-loading. ASTM A453 grade 660 / ASME III. A286 nuclear applications.
    • Aerospace engine mount tie-rods: Engine-mount tension members on jet-engine pylons, helicopter engine support structures, missile-launcher attach. Single-piece machined tie rods.
    • Turnbuckle bracing systems: Adjustable-length A286 tie rods with central turnbuckle for high-temperature bracing, gas-turbine, kiln, and process-furnace structural support.
    • Cryogenic LNG tank internal bracing: Tie rods spanning LNG tank internal frame supports, A286 retains 85 % toughness at -196 °C. Hydrogen-storage internal bracing.

    Governing Standards & Material Specifications

    Every A286 rod product is released against the applicable industry standard. EN 10204 type 3.1 mill certificates ship with every order. See A286 AMS / ASTM specifications hub for full spec scope.

    AuthoritySpecificationCoverage
    ASTMA453 grade 660 Cl. A/B/C/DHigh-temperature bolting material
    AMS5731Bar / forging, solution-treated
    AMS5732Bar / forging, solution-treated and aged
    AMS5853Welding wire (matching A286)
    UNSS66286Material designation
    DIN1.4980 / X5NiCrTiMoVB25-15-2European designation
    EN10204 3.1 / 3.2Mill / third-party-witness certification

    A286 Tie Rod vs Alternative Materials

    Engineers compare A286 against three alternatives: A286 vs Inconel 718, A286 vs 17-4 PH, and A286 vs Waspaloy. See A286 equivalent grades.

    How to Specify A286 Tie Rod

    A complete a286 tie rod callout should include all relevant elements. Example callout:

    A286 tie rod, ASTM A453 grade 660 Class A, sol-treated and aged, shank ⌀ 16 mm × M16 × 2.0 thread both ends × 1500 mm overall length, jam-nut termination, MIL-S-8879 thread tolerance if aerospace, EN 10204 3.1, tensile-pull-tested.

    A286 Tie Rod, Frequently Asked Questions

    What's the difference between A286 tie rod and A286 threaded rod?

    Tie rod: tension-loaded structural member with engineered end fittings (jam-nut, clevis, eye, turnbuckle). Threaded rod: general-purpose all-thread material supplied in standard 1-3 m lengths for customer cut-to-size. Tie rods are pre-engineered and pre-cut to drawing; threaded rods are general stock.

    How is A286 tie rod tension capacity calculated?

    Tension capacity = tensile area × yield stress. For A286 grade 660 Class A: yield = 655 MPa (95 ksi). M16 tie rod tensile area = 157 mm², so theoretical pull capacity = 103 kN at yield. Working preload typically 50-65 % of yield for fatigue (cycling) or 75 % for static. Always design for the smaller of shank cross-section or thread-root cross-section.

    Are A286 tie rods threaded both ends?

    Standard configurations: threaded both ends with jam-nut termination (most common), threaded both ends with clevis termination, threaded one end + integral eye-end at the other, or shoulder-eye + threaded shank for aerospace control linkages.

    What's the maximum length of A286 tie rod?

    Standard production: 3 m. Custom-drawing: up to 6 m for shaft sizes ≥ M30. Beyond 6 m, custom production with end-to-end welding (TIG) or splice-coupling required.

    Are A286 tie rods magnetic?

    No. Magnetic permeability < 1.005 verified per ASTM A342 on aerospace lots. Critical for non-magnetic structural assemblies in instrumentation, MRI, and aerospace electromagnetic-sensitive applications.

    Can A286 tie rods be used in cryogenic applications?

    Yes, A286 retains 85 % of room-temperature toughness at -196 °C. Used for LNG storage-vessel internal bracing, hydrogen-storage tank tie members. Confirm Charpy V-notch ≥ 27 J at service temperature.

    What's the typical end-fitting for an A286 tie rod?

    Jam-nut termination: thread + nut + plate, transfers tension through plate to frame. Clevis termination: thread + clevis fitting + cross-pin, transfers tension through clevis ears. Aerospace: machined shoulder-eye + threaded shank in single piece.

    Can A286 tie rods be used in rotating service?

    Generally no, tie rods are tension-loaded static members, not rotating drive shafts. For rotating applications use A286 hex rod or A286 round bar machined to a shaft. Tie rods may have rotational vibration but not continuous rotation.

    Is A286 tie rod NACE MR0175 sour-service compliant?

    Yes, when supplied with hardness ≤ HRC 35 per NACE MR0175 / ISO 15156-3. Each heat receives Vickers traverse before release for sour-service applications.

    Why TorqBolt for A286 Tie Rod

    Three reasons aerospace and industrial OEMs place a286 tie rod orders with us:

    • Vertically integrated supply, VIM-VAR melt sourcing from approved AMS-conforming mills, in-house drawing + thread rolling + vacuum heat-treatment.
    • Aerospace AQMS, AS9100D-certified factory in Mumbai with published quality manual.
    • Lead time discipline, 4-6 weeks for ASTM A453 grade 660 standard sizes, 8-12 weeks for custom-drawing aerospace parts.

    30+ years of fastener-manufacturing track record. Active certifications: ISO 9001:2015, AS9100D AQMS, PED 2014/68/EU and NORSOK M-650 QTR.

    Recent A286 Tie Rod Order Patterns

    Active tie rod orders cover M16 / M20 jam-nut-terminated for industrial gas-turbine combustor liner-to-casing tie members, custom shoulder-eye + threaded-shank for aerospace engine-mount tension members, M24 / M30 turnbuckle-style for high-temperature kiln structural bracing, and M36 / M48 for nuclear pressure-vessel internal reinforcement.