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 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.
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.
TorqBolt produces A286 tie rod in five primary end-fitting configurations:
| Shank diameter | Thread | Standard length | Tensile area mm² | Min. tension (kN) | Working tension (kN, 75% yield) |
|---|---|---|---|---|---|
| 12 mm | M12 × 1.75 | 200-2000 mm | 84.3 | 75.5 | 55.2 |
| 16 mm | M16 × 2.0 | 200-2500 mm | 157 | 140 | 103 |
| 20 mm | M20 × 2.5 | 300-3000 mm | 245 | 219 | 160 |
| 24 mm | M24 × 3.0 | 300-3000 mm | 353 | 316 | 231 |
| 30 mm | M30 × 3.5 | 300-3000 mm | 561 | 502 | 367 |
| 36 mm | M36 × 4.0 | 300-3000 mm | 817 | 731 | 535 |
| 48 mm | M48 × 5.0 | 300-3000 mm | 1473 | 1318 | 964 |
| 64 mm | M64 × 6.0 | 300-3000 mm | 2676 | 2395 | 1751 |
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:
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:
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 serves tension-loaded structural and machinery applications:
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.
| Authority | Specification | Coverage |
|---|---|---|
| ASTM | A453 grade 660 Cl. A/B/C/D | High-temperature bolting material |
| AMS | 5731 | Bar / forging — solution-treated |
| AMS | 5732 | Bar / forging — solution-treated and aged |
| AMS | 5853 | Welding wire (matching A286) |
| UNS | S66286 | Material designation |
| DIN | 1.4980 / X5NiCrTiMoVB25-15-2 | European designation |
| EN | 10204 3.1 / 3.2 | Mill / third-party-witness certification |
Engineers compare A286 against three alternatives: A286 vs Inconel 718, A286 vs 17-4 PH, and A286 vs Waspaloy. See A286 equivalent grades.
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.
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.
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.
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.
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.
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.
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.
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.
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.
Yes — when supplied with hardness ≤ HRC 35 per NACE MR0175 / ISO 15156-3. Each heat receives Vickers traverse before release for sour-service applications.
Three reasons aerospace and industrial OEMs place a286 tie rod orders with us:
30+ years of fastener-manufacturing track record. Active certifications: ISO 9001:2015, AS9100D AQMS, PED 2014/68/EU and NORSOK M-650 QTR.
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.