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    A286 Nuts

    A286 Fasteners being an austenitic age-hardenable iron based super alloy stainless steel that is melted as AOD + ESR, AOD + VAR, or VIM + VAR is manufactured at TorqBolt. Cres-A286 fasteners have excellent strength even at high temperatures up to 1500 Degrees Fahrenheit. Alloy A286 Stainless Fasteners has excellent creep resistance making it excellent for critical high temperature applications such as jet engine components. A286 Fastener Strength conforming to the ASTM A453 Grade 660 Class D specification (with a guaranteed yield strength minimum of 105,000 PSI), but with stress rupture tests carried out to also conform to ASTM A453 Grade 660 Class A. These provide a tensile strength of 895 MPa (minimum), 0.2% offset yield strength of 725 MPa (minimum), elongation of 15% and reduction of area of 18%. Hardness is in the range 29-35 HRC.

    In general, we also supply ASTM A453 GR 660 heat-treated and tested to conform to grade B. This provides a tensile strength of 895 MPa (minimum), a lower 0.2 offset yield strength of 585 MPa (minimum), elongation of 15% and reduction of area of 18%. Hardness is in the range 24-37 HRC.

    A286 Nut Variants, Browse by Type

    TorqBolt manufactures Alloy A286 nuts in standard, heavy and self-locking variants:

    • A286 Hex Nuts, DIN 934 / ISO 4032 (Type 1 standard), ISO 4033 (Type 2 heavy), ASME B18.2.2 in M5-M64 / 1/4"-2-1/2". Default mate for A286 hex bolts and stud bolts.
    • A286 Self-Locking Nuts, Nylon-insert (DIN 985), all-metal prevailing-torque (IFI-100), and aerospace MS 21043 / NAS 1291 self-locking variants for cycling joints.
    • A286 Lock Nuts, Jam nut (DIN 936 / ISO 4035) and pellet-lock variants for static joints with vibration risk.

    All A286 nuts are upset-forged from A286 hex bar (AMS 5731), tapped, then solution-treated and precipitation-aged per ASTM A453 grade 660. See the canonical A286 chemical composition and A286 mechanical properties pages.

    About A286 Nuts

    A286 Nuts, UNS S66286 manufacturer and supplier

    TorqBolt produces Alloy A286 (UNS S66286 / DIN 1.4980) nuts in hex, jam, all-metal lock, K-lock, flange, castle and slotted patterns from M5 to M64 / 1/4" to 2-1/2". A286 nuts are solution-treated and aged per ASTM A453 grade 660, AMS 5731 / 5732 stock, and certified to EN 10204 type 3.1 or 3.2 inspection, supplying the high-temperature retention required for aerospace fasteners, gas-turbine assembly, exhaust manifolds and cryogenic LNG service down to −196 °C.

    A286 Nut Patterns & Locking Mechanisms

    Alloy A286 nuts are produced from cold-drawn, solution-treated bar (AMS 5731 / 5732), broached or tapped after heading, then aged at 720 °C for 16 hours to develop full strength. Nut height is controlled so the thread strips at ≥ 1.0 × mating-bolt UTS, ensuring the nut is never the failure mode.

    • Standard hex nut, DIN 934 / ISO 4032 / ASME B18.2.2.
    • Heavy hex nut, ASME B18.2.2, used on heavy-hex bolting for ASME B16.5 high-pressure flanges.
    • Jam nut (thin), DIN 439 / ISO 4035, 0.6 × standard height; used as a locking jam-nut.
    • Prevailing-torque all-metal lock nut, DIN 980V / IFI-100, deformed-thread crown, > 5 re-use cycles per IFI-101.
    • K-lock (Kep nut), integrally captive serrated washer; one-piece installation, single-use.
    • Flange-serrated nut, DIN 6923 / IFI-145, integral washer that bites the joint surface.
    • Castle / slotted nut, DIN 935 / ASME B18.2.2, slotted to receive a cotter pin.
    • Acorn / cap nut, DIN 1587, closed dome that protects exposed thread from corrosion.

    A286 Nut Mating & Thread Class

    A286 nuts mate with A286 bolts using ASME B1.13M class 6H/6g (metric), UNC/UNF class 2A/2B (inch standard fit), or 3A/3B (precision aerospace fit). Tap-then-age sequence holds tighter tolerance than nut-rolled threads. Lubricant on the nut bearing face (nickel anti-seize) reduces torque-tension scatter from ± 25 % to ± 8 % per ASME PCC-1 Appendix K.

    A286 Nut Application Areas

    • Jet-engine and gas-turbine matched-pair bolting (one heat per assembly drawing).
    • Exhaust manifold & turbocharger flange retention, vibration plus 540-700 °C cycling.
    • Cryogenic valve and pump bonnet retention down to -196 °C.
    • NACE MR0175 / ISO 15156 sour service when nut hardness verified ≤ HRC 35.

    Alloy A286 Nuts , Specification Overview

    An A286 nut is engineered to outlast its mating bolt. By controlling the nut height, thread engagement and aging cycle so the through-thread shear strength exceeds 1.0 × the bolt’s tensile strength, the assembly’s failure mode is locked to bolt fracture, never thread strip. That is why A286 nuts dominate jet-engine matched-pair bolting, where loss of clamp at temperature would be catastrophic.

    The locking strategy , free-spinning hex with separate lock washer, prevailing-torque all-metal lock, K-lock with captive washer, castle with cotter pin, or flange-serrated bearing face, is selected based on vibration severity, temperature, and re-use cycles. TorqBolt produces every locking pattern listed in DIN, ISO, ASME, NAS and MIL-DTL, plus customer-drawing variants.

    A286 Nuts Governing Standards & Specifications

    TorqBolt manufactures every a286 nuts to the applicable industry standard. The matrix below lists the principal specifications , material, dimensional, inspection, that a286 nuts are released against. EN 10204 type 3.1 mill certificates ship with every order; type 3.2 third-party-witnessed inspection is available for nuclear, offshore and customer-mandated source-surveillance contracts.

    Authority Specification Coverage
    ASTMA453 grade 660 Class A/B/C/DHigh-temperature nut material
    AMS5731 / 5732 / 5737Bar stock for nut manufacture
    ASMEB18.2.2 / B18.6.9 / B18.16.1Hex / acorn / lock-nut dimensions
    DIN934 / 439 / 980 / 985 / 935 / 6923 / 1587Metric hex / jam / lock / castle / flange / cap
    ISO4032 / 4035 / 7040 / 7042 / 4759-1Metric hex / jam / nylon-insert / all-metal lock
    NAS1801 / 21072 / 21076Aerospace self-locking nuts
    MIL-N25027 / MS21042 / MS21044Self-locking nuts for aerospace
    IFI100 / 145Prevailing-torque all-metal lock; flange-serrated
    EN10204 3.1 / 3.2Mill / third-party-witness cert
    NACEMR0175 / ISO 15156-3Sour service ≤ HRC 35
    ASMEPCC-1 Appendix KLubricated nut bearing-face friction

    A286 Nuts Sizes & Available Patterns

    A286 nuts are produced from cold-drawn solution-treated bar (AMS 5731), broached or tapped after upsetting, then aged at 720 °C for 16 hours. Nut height is controlled so the thread strips at ≥ 1.0 × mating-bolt UTS , the nut is never the failure mode.

    Pattern Standard Metric range Inch range Locking
    Hex nutDIN 934 / ISO 4032 / ASME B18.2.2M3, M64#4 , 2-1/2"None (free-spinning)
    Heavy hex nutASME B18.2.2M12, M641/2" , 2-1/2"None (free-spinning)
    Jam (thin) nutDIN 439 / ISO 4035M3, M64#4 , 2-1/2"Lock as second nut
    Prevailing-torque (all-metal)DIN 980V / IFI-100M5, M481/4" , 2"Deformed-thread crown
    K-lock (Kep) nutDIN 6923 base + serrated washerM3, M16#4 , 5/8"Captive serrated washer
    Flange-serratedDIN 6923 / IFI-145M5, M301/4" , 1-1/4"Bearing-face teeth bite work
    Castle (slotted)DIN 935 / ASME B18.2.2M6, M481/4" , 1-1/2"Cotter pin lock
    Acorn / capDIN 1587 / ASME B18.6.9M3, M30#4 , 1-1/4"Closed dome (decorative)

    A286 Nuts Manufacturing Process

    Every a286 nuts TorqBolt ships traces back to a vacuum-induction-melted plus vacuum-arc-remelted (VIM-VAR) ingot meeting AMS 5731 / 5732 chemistry. The complete manufacturing route is:

    1. Melt: VIM-VAR / VIM-ESR ingot to AMS 5731 chemistry.
    2. Bar production: hot-rolled to bar, peeled, centerless-ground for cold-heading feedstock.
    3. Cold heading: 4-station or 5-station header upsets the hex blank from solid bar; hex form is forged, not machined, for grain-flow continuity.
    4. Tapping or broaching: threads cut after heading. Tapped nuts hold a tighter pitch tolerance than rolled-thread bolts, so the bolt-nut assembly always fits.
    5. Solution treatment: 980 °C, oil-quench, preserves the finished thread profile because no further plastic deformation follows.
    6. Precipitation aging: 720 °C / 16 h, air-cool. Hardness 277-302 HBW (30-32 HRC).
    7. Lock-feature finishing: for prevailing-torque nuts, the deforming operation that creates the locking element is performed before aging so the deformation is ‘locked in’ by precipitation.
    8. Surface finish: passivation per ASTM A967, or silver / cadmium / dry-film lubricant per drawing.
    9. Inspection: proof-load test on every lot per ASTM F606, hardness verification per NACE MR0175 (if invoked), gauge-mate check, NDT to drawing.

    Lot traceability is maintained from VIM-VAR heat number through finished-part inspection. Customer-witness sampling, NDT (LPI / UT / RT), and radiographic certification are available on contracts that invoke AS9100D, NORSOK M-650 QTR or nuclear ASME III subsection NB.

    A286 Nut Inspection Process

    Nut inspection focuses on three failure modes that bolts don't share: thread-strip strength, prevailing-torque retention, and bearing-face flatness. Our standard release sequence is:

    • Proof-load test per ASTM F606 , every lot, sample size per Z1.4 normal inspection level II.
    • Prevailing-torque verification on every all-metal lock-nut lot, first-installation, fifth-installation, and removal-torque traces recorded per IFI-100/107.
    • Thread profile gauged with optical comparator at 50× magnification on first piece, plate gauges on full lot.
    • Hardness verification per heat , Vickers HV 280 to 320 corresponds to the ASTM A453 grade 660 Class A range.
    • Magnetic permeability spot-check at one nut per 500 to confirm austenitic structure (must read < 1.005 µᵣ).
    • Bearing-face flatness check, TIR < 0.05 mm per ASME B18.16.6 to ensure even preload distribution.

    EN 10204 type 3.1 mill cert is standard. Customer-mandated source-surveillance contracts (typical on offshore Adnoc, Saudi Aramco and Petrobras orders) drive type 3.2 with NACE MR0175 hardness witnessing.

    A286 Nut Applications by Industry

    Aerospace matched-pair bolting

    Every A286 nut on a jet-engine compressor wheel, turbine disc or augmentor case is heat-locked to a single melt heat. AMS / NAS / MIL drawings call out matched-pair traceability so the nut and bolt have identical chemistry, identical aging cycle, and predictable thermal-expansion behaviour through the engine’s thermal cycles.

    Exhaust manifold and turbocharger

    540-700 °C cyclic service with high vibration. K-lock and prevailing-torque nuts are the dominant patterns, retained on the bolt thread by frictional grip even when bolt elongation reduces the nominal preload.

    Cryogenic LNG valves and pumps

    A286 retains 85 % of room-temperature toughness at −196 °C; its austenitic structure stays ductile where ferritic-stainless nuts (304L, 316L) suffer brittle cleavage at LNG temperatures.

    Sour-service oil & gas

    NACE MR0175 / ISO 15156-3 limits A286 nut hardness to ≤ HRC 35 (HV 327) for use in H₂S environments. Verified by Vickers traverse on every heat per the standard.

    Nuclear pressure-vessel hand-hole studs

    A453 grade 660 nuts are listed in ASME III NB-2000 for primary-pressure-boundary bolting; matched to A453 grade 660 stud bolts on PWR steam-generator hand-hole closures.

    A286 Nuts vs Alternative Materials

    Nut material follows the bolt almost without exception. A286 nuts are paired with A453 grade 660 stud bolts; A194 grade 2H nuts pair with A193 B7 bolts; Inconel 718 nuts pair with AMS 5662 bolts. The choice cascades from the joint's service envelope.

    Property A286 nut (S66286) A194 grade 2H Inconel 718 A194 grade 8MA
    Mating-bolt gradeA453 660A193 B7AMS 5662A193 B8M
    Service ceiling700 °C450 °C700 °C425 °C
    Hardness windowHRC 30-32HRC 24-38HRC 36-44HRC 28-32
    Sour service ≤ HRC 35YesRestrictedRestrictedYes
    Cost index1.0×0.2×3.0×0.6×

    A286 is the sweet-spot fastener material when service temperature exceeds 315 °C (the 17-7 PH ceiling) but the application can’t justify a 3× cost jump to Inconel 718. Roughly 70 % of all jet-engine and industrial-gas-turbine bolting falls in this 540-700 °C envelope, which is why A286 is the highest-volume aerospace superalloy fastener material in the world.

    How to Specify an A286 Nut

    1. Material spec: ASTM A453 grade 660 Class A (or AMS 5731 for aerospace).
    2. Pattern: hex / heavy hex / jam / castle / lock-nut type / flange-serrated / acorn.
    3. Dimensional standard: DIN 934 / ISO 4032 (metric standard hex), ASME B18.2.2 (inch heavy hex), MS21042 (aerospace self-locking), DIN 6923 (flange).
    4. Thread: internal thread class 6H (metric) or 2B / 3B (inch).
    5. Locking element: none / nylon insert (capped at 121 °C , never on A286 over 121 °C) / all-metal deformed thread / serrated washer / cotter pin.
    6. Coating: passivated per ASTM A967, silver-plate per AMS 2410, or dry-film lubricant.
    7. Inspection certificate: EN 10204 3.1 default, 3.2 if invoked.

    Example: “Hex nut, ASTM A453 grade 660 Class A, ST+A, DIN 934, M16, 6H, passivated, EN 10204 3.1, NACE MR0175 hardness verified.”

    Why TorqBolt for A286 Nuts

    Buying A286 nuts loose-from-stock is a commodity decision; buying matched-pair to a specific bolt heat is the strategic one. We do both, but the matched-pair side is where we differentiate:

    • Same-heat matched pairs: cut from the same VIM-VAR ingot as the mating bolt; identical thermal-expansion behaviour through the engine's thermal cycles.
    • Locking patterns to drawing: prevailing-torque, K-lock, castellated, flange-serrated. Whatever the OEM specs, we produce.
    • Proof-load record per lot: EN 10204 cert ships with proof-load test data for every released batch.

    30-plus years of fastener manufacture; ISO 9001:2015 + AS9100D + PED 2014/68/EU certified; NORSOK M-650 QTR maintained; NACE MR0175 hardness verification on every heat. No MOQ on stocked patterns.

    A286 Nut Demand Profile

    The nut orders we ship break roughly into three categories. About half are matched-pair industrial flange bolting (paired with our A286 stud-bolt SKUs). Roughly a third are aerospace prevailing-torque self-locking nuts (DIN 980V and MS21042 patterns) released under AS9100D. The remainder are speciality patterns: K-lock for assembly-line work, castle nuts for shaft retention with cotter pins, and flange-serrated for engine-mount vibration service.

    From the QA bench: we keep two rejection bins for A286 nuts, one for hardness drift, one for thread gauge. The thread bin almost always wins, mostly from over-aggressive tap re-grinds on small-batch runs. We replaced the smaller-than-M10 tap inventory in 2023 and the gauge-rejection rate dropped from 0.8 % to 0.05 %.