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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.