ASTM A194 Grade 8MNA specifies premium austenitic stainless steel nuts manufactured from AISI Type 316N. This highly versatile grade takes the excellent chloride-pitting resistance of standard Grade 8M (Type 316) and significantly boosts its mechanical capabilities through the precise metallurgical addition of Nitrogen (N). Nitrogen acts as a powerful solid-solution strengthening agent, substantially increasing the material's yield strength while maintaining robust corrosion resistance.
What sets Grade 8MNA apart from its standard counterpart is the crucial "A" designation. This mandates that the fasteners undergo a final Carbide Solution Treatment (full annealing) after all forging, machining, and thread-tapping operations are completed. This vital thermal process eliminates any residual cold-work stresses introduced during manufacturing, ensuring a fully softened, strictly non-magnetic state (60-90 HRB). This restoration of the matrix maximizes resistance to Stress Corrosion Cracking (SCC) in highly aggressive chemical and marine applications.
| Material Classification | Nitrogen-Strengthened Austenitic Stainless Steel (Type 316N - Annealed) |
|---|---|
| UNS Designation | S31651 |
| Microstructure | Austenitic (Nitrogen-Stabilized, Post-Annealed) |
| Magnetic State | Strictly Non-Magnetic (Annealed post-machining) |
| Density | ~8.00 g/cm³ (0.289 lb/in³) |
| Size Range | Metric: M6 to M100 | Imperial: 1/4" to 4" |
| Strengthening Method | Nitrogen Strengthening & Full Solution Annealing After Machining |
Contains detailed proof load thresholds, dimensional tolerances for ASME B18.2.2 standard and heavy hex profiles, and precise galling-prevention torque values for A193 B8MNA assemblies.
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The 8MNA designation relies on a targeted addition of Molybdenum (2.00-3.00%) for robust defense against chloride pitting and crevice corrosion. A standard carbon limit is maintained, but any risk of residual stress is entirely negated by the mandatory post-machining annealing process.
| Carbon (C) | Manganese (Mn) | Chromium (Cr) | Nickel (Ni) | Molybdenum (Mo) | Phosphorus (P) | Sulfur (S) | Silicon (Si) |
|---|---|---|---|---|---|---|---|
| 0.08 Max | 2.00 Max | 16.0 – 18.0 | 10.0 – 13.0 | 2.00 – 3.00 | 0.045 Max | 0.030 Max | 1.00 Max |
Because Grade 8MNA is explicitly annealed after all machining to remove localized cold-work hardening, ASTM tightly controls the hardness range to guarantee the matrix remains fully softened and stress-free.
| Mechanical Property | Grade 8MNA (Annealed) Limits |
|---|---|
| Hardness Limit (Rockwell) | 60 - 90 HRB Maximum |
| Proof Load | Dependent on Size |
| Standard / System | Designation |
|---|---|
| ASME Standard | SA194 Grade 8MNA |
| Common Trade Name | Type 316N Stainless Nuts (Annealed), Nitrogen-Strengthened 316 |
| European Equivalent | EN 1.4406 / X2CrNiMoN17-11-2 (Approximate) |
| Internal Threads (A194 Gr 8MNA) | Mating Bolts (A193 Gr B8MNA) | Mating Studs (A193 Gr B8MNA) |
|---|---|---|
| Grade 8MNA Heavy Hex Nuts | ASTM A193 Grade B8MNA Hex Bolts | A193 Grade B8MNA Fully Threaded Studs |
Due to the fully softened, austenitic nature of 8MNA, severe thread galling is a prominent risk under high clamping loads. Premium high-temperature anti-seize lubrication (such as nickel-based paste) is absolutely mandatory for safe installation and future unbolting.
| Nominal Diameter | Threads Per Inch (UNC) | Target Torque — Lubricated (ft-lbs) |
|---|---|---|
| 1/2" | 13 | 30 |
| 5/8" | 11 | 60 |
| 3/4" | 10 | 100 |
| 1" | 8 | 250 |
The "A" indicates that the component has been Annealed after all manufacturing and machining processes are complete. This removes all internal cold-work stresses generated during machining, ensuring the part is fully softened and strictly non-magnetic to maximize resistance against Stress Corrosion Cracking.
While both share the exact same chemical composition (Molybdenum and Nitrogen enhanced), standard Grade 8MN may retain residual stress and slight magnetism from the manufacturing process. Grade 8MNA guarantees that these stresses are completely removed through post-machining full solution annealing.
Because the "A" specification is designed to eliminate internal stress through annealing, the hardness is restricted between 60 and 90 HRB. If a nut measures harder than 90 HRB, it strongly indicates that residual cold-work stress remains from the machining or threading process, meaning the part is not fully annealed and fails the specification.