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
AMS 5895 is the SAE Aerospace Material Specification covering A286 (UNS S66286) sheet and strip in solution-treated and precipitation-aged condition. Material ships at full A286 mechanical properties (130 ksi tensile / 95 ksi yield) — ready for use without further heat-treatment. Distinguished from AMS 5525 (sol-treated only) by aging condition: AMS 5895 ships aged; AMS 5525 ships sol-treated for downstream aging or forming. AMS 5895 is used as direct-use input for stamped aerospace components, electrical bus-bar applications requiring full A286 strength, and sheet-metal aerospace structural panels. See parent A286 AMS specifications hub, related A286 sheet, flat washers, sister spec AMS 5525.
AMS 5895 covers A286 sheet and strip in solution-treated and precipitation-aged condition. VIM-VAR melted, cold-rolled or hot-rolled to thickness ≤ 6 mm, solution-treated 1650 °F + oil-quench, precipitation-aged 1325 °F × 16 hours + air-cool. Final hardness 29-32 HRC; tensile ≥ 895 MPa; yield ≥ 655 MPa. Used as direct-use input for aerospace stamped components, electrical bus-bar, structural panels.
| Element | Min % | Max % | Notes |
|---|---|---|---|
| Iron (Fe) | Balance | Balance | ~53 % typical |
| Nickel (Ni) | 24.0 | 27.0 | Solid-solution stabilizer |
| Chromium (Cr) | 13.5 | 16.0 | Corrosion + oxidation resistance |
| Titanium (Ti) | 1.90 | 2.35 | Gamma-prime former (Ni3Ti) |
| Molybdenum (Mo) | 1.00 | 1.50 | Solid-solution strengthener |
| Vanadium (V) | 0.10 | 0.50 | Carbide stabilizer |
| Aluminium (Al) | 0 | 0.35 | Gamma-prime former (Ni3Al) |
| Boron (B) | 0.001 | 0.010 | Grain-boundary strengthening |
| Carbon (C) | 0 | 0.08 | Per ASTM A453 |
| Manganese (Mn) | 0 | 2.00 | Per ASTM A453 |
| Silicon (Si) | 0 | 1.00 | Per ASTM A453 |
| Phosphorus (P) | 0 | 0.025 | Trace impurity |
| Sulphur (S) | 0 | 0.015 | Trace impurity |
| Property | AMS 5895 requirement | Notes |
|---|---|---|
| Form | Sheet (cold-rolled), strip | ≤ 6 mm thickness |
| Heat treatment | Sol 1650 °F + aged 1325 °F × 16 h | Mill-aged |
| Tensile strength | ≥ 895 MPa (130 ksi) | Aged condition |
| Yield strength (0.2 %) | ≥ 655 MPa (95 ksi) | Aged condition |
| Hardness | 29-32 HRC | Aged |
| Surface finish | No. 2D matte or No. 4 brushed | Per drawing |
| Thickness range | 0.5-6 mm | Aerospace standard |
| Magnetic permeability | < 1.005 | Per ASTM A342 |
SAE / AMS spec covering A286 (UNS S66286) sheet and strip in solution-treated and precipitation-aged condition. Mill-aged aerospace sheet — material ships at full A286 mechanical properties, ready for use.
AMS 5895: sol-treated AND aged from mill, ready for use, hardness 29-32 HRC. AMS 5525: sol-treated only, soft (24-28 HRC), suitable for cold-forming. Choose AMS 5895 for direct use; AMS 5525 for forming or downstream aging.
0.5-6 mm sheet/strip per AMS 5895. For thicker plate, specify AMS 5525 (covers up to 100 mm plate).
Limited — aged condition has reduced ductility. Bend radius ≥ 4 × thickness for aged AMS 5895 vs 2 × for sol-treated AMS 5525. For cold-forming, use AMS 5525 sol-treated then age after forming.
Standard sizes 0.5-6 mm thickness × up to 1500 × 6000 mm: 8-12 weeks from heat release. Aerospace AS9102 first-article: add 1-2 weeks.
No. Magnetic permeability < 1.005 verified per ASTM A342. Critical for non-magnetic stamped components and electrical bus-bar applications.
Yes — TIG / GTAW with matching A286 welding rod (AMS 5853). Aged condition requires post-weld solution-treatment + aging for weld zone strength recovery — for welded fabrications, sol-treated AMS 5525 is preferred starting condition.
No. 2D matte or No. 4 brushed per ASTM A480 — depending on application. Aerospace lots may specify additional passivation per ASTM A967 Type II.
Yes — when supplied with hardness ≤ HRC 35 per NACE MR0175 / ISO 15156-3 for sour-service. Specify on PO; each heat receives Vickers traverse before release.
| Property | Min value (mill-aged) | Notes |
|---|---|---|
| Tensile strength (MPa) | ≥ 895 | Aged |
| Yield strength 0.2 % (MPa) | ≥ 655 | Aged |
| Elongation (%) | ≥ 15 | In 50 mm gauge |
| Hardness HRC | 29-32 | Aged target |
TorqBolt manufactures the following A286 products to this specification:
Common mating and related A286 specifications used alongside this spec:
A286 sheet, AMS 5895, sol-treated and aged, 2.0 mm thickness × 1000 mm × 3000 mm, pickled passivated, hardness 29-32 HRC, EN 10204 3.1.
Other A286 specifications: AMS / ASTM hub · AMS 5525 · AMS 5731 · AMS 5732 · AMS 5737 · AMS 5853 · AMS 5895 · ASTM A453 grade 660 · ASTM A638 grade 660 · ASTM B637 · DIN 1.4980 · UNS S66286.
Canonical A286 reference: A286 chemical composition · A286 mechanical properties · A286 heat treatment · alloy comparisons (vs Inconel 718 · vs Waspaloy).