Custom 465 Sheets are high-strength stainless steel sheets known for excellent resistance to corrosion, wear and high-temperature damage. They are made from a precipitation-hardening alloy that keeps its strength and toughness in extreme conditions. Parag Metal supplies top-grade Custom 465 Sheets with consistent performance, high fatigue strength, and long service life, making them a trusted choice across several industries. These sheets are used in places where both high mechanical strength and corrosion resistance are critical.
Custom 465 can also be heat-treated or cold-worked to meet different strength and corrosion resistance needs. Its performance is far better than other common stainless steels. We provide sheets that fulfill the ASTM A240 and ASME SA240 requirements. Thickness ranges from 0.0125″ to 5.00″, while widths range from 1000mm to 3500mm. You can select among tempers such as annealed, 1/4 hard, full hard, and others. Options for hardness include mild, spring hard, and many more.
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These sheets are utilized in the aerospace, oil and gas, medical, and power generation industries. Their strength and corrosion resistance make them ideal for complex, high-temperature, or high-stress applications. Custom 465 Sheets handle saltwater, chemicals, and extreme heat better than 304 or 316. They’re also easy to shape, weld, and machine, which helps save time and cost in production.
Every sheet goes through strict quality checks, including strength, hardness, and surface finish tests. We pack all products carefully to avoid damage during shipping. We deliver Custom 465 Sheets across India and overseas, offering competitive prices and ready stock details. If you’re looking for a trusted Custom 465 Sheet supplier, contact us today for a quick quote.
Very high strength with excellent toughness.
Superior corrosion resistance for aerospace components.
Good fatigue resistance used in the defense industry.
High hardness suitable for industrial tooling applications.
Maintains strength at elevated temperatures for engine parts.
Ideal for aerospace structural components needing high strength and toughness
Used in aircraft fittings, fasteners, and landing gear parts
Applied in rotorcraft and engine components exposed to high stress
Suitable for defense systems, including missile and weapon system parts
Used in high-performance automotive components
Applied in medical instruments and surgical tools due to excellent corrosion resistance
| Standard Specification | ASTM A240 / ASME SA240 |
|---|---|
| Dimensions | ASTM, ASME, and API |
| Sheets Thickness | Range from 0.008″ to 0.0125″ |
| Plates Width | 1000 mm, 1219 mm, 1500 mm, 1800 mm, 2000 mm, 2500 mm, 3000 mm, 3500 mm, etc. |
| Plates Length | 2000 mm, 2440 mm, 3000 mm, 5800 mm, 6000 mm, etc. |
| Tempers | Annealed, 1/4 Hard, 1/2 Hard, 3/4 Hard, Full Hard |
| Hardness | Soft, Hard, Half Hard, Quarter Hard, Spring Hard, etc. |
| Value Added Service | Cladding, Heat Treatment, Annealed, Pickling, Polish, Rolling, Cutting, Bending, Forging, Minor Fabrication, etc. |



| Fe | Cr | Ni | Ti | Mo | |||||
|---|---|---|---|---|---|---|---|---|---|
| 74.35% | 11.75% | 11.0% | 1.65% | 2.05% | |||||
| Mn | Si | C | P | N | |||||
| ≤0.25% | ≤0.25% | ≤0.020% | ≤0.015% | ≤0.010% | |||||
| S | |||||||||
| 0.010% | |||||||||
| Property | Minimum | Maximum | |||||||
|---|---|---|---|---|---|---|---|---|---|
| Yield Strength Range (Rp0.2 Offset) (ksi) | 170 | 270 | |||||||
| Tensile Strength Range (Rm) (ksi) | 190 | 280 | |||||||
| Elongation (AL=5 × Ø) | 2.3% | 14.0% | |||||||
| Brinell Hardness (H) | 271 | 560 | |||||||
| Modulus of Elasticity (ksi) (E): 32000 | |||||||||
| Machineability General Index: Unknown | |||||||||
Size (in mm) | Size (in inches) |
|---|---|
3.40mm | .134″ |
3.18mm | .125″ |
4.75mm | .187″ |
3.96mm | .156″ |
7.92mm | .312″ |
6.35mm | .250″ |
12.7mm | .500″ |
9.53mm | .375″ |
19.1mm | .750″ |
15.9mm | .600″ |
25.4mm | 1″ |
22.2mm | .875″ |
31.8mm | 1.250″ |
28.6mm | 1.125″ |
44.5mm | 1.750″ |
38.1mm | 1.500″ |
63.5mm | 2.500″ |
50.8mm | 2″ |
76.2mm | 3″ |
| Tolerance over and under nominal thickness t (mm) | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| Width w (mm) | 2.5<t <4.5 | 4.5<t <6.0 | 6.0<t <8.0 | 8.0<t <10.0 | 10.0<t <12.5 | 12.5<t <16.0 | 16.0<t <20.0 | 20.0<t <25.0 | 25.0<t <30.0 | 30<t <40.0 |
| w < 1200 | 0.20 | 0.23 | 0.30 | 0.32 | 0.35 | 0.80 | 0.80 | 0.80 | 1.0 | 1.4 |
| 1200< w <1500 | 0.20 | 0.25 | 0.30 | 0.35 | 0.38 | 0.80 | 0.80 | 0.90 | 1.0 | 1.4 |
| 1500< w <1800 | 0.20 | 0.28 | 0.32 | 0.38 | 0.40 | 0.80 | 0.80 | 0.90 | 1.1 | 1.5 |
| 1800< w <2100 | 0.20 | 0.30 | 0.36 | 0.40 | 0.45 | 0.80 | 0.80 | 0.90 | 1.1 | 1.5 |
| 2100< w <2400 | 0.80 | 0.80 | 0.80 | 0.80 | 0.80 | 0.90 | 1.0 | 1.1 | 1.5 | |
| 2400< w <2700 | 0.80 | 0.80 | 0.80 | 0.80 | 0.90 | 1.0 | 1.1 | 1.3 | 1.7 | |
| 2700< w <3000 | 0.80 | 0.90 | 1.0 | 1.0 | 1.0 | 1.1 | 1.3 | 1.4 | 1.8 | |
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