IS 733:1983 is the Indian Standard (BIS) for wrought aluminium and aluminium alloy plate, sheet and strip for general engineering purposes - specification. This standard specifies the chemical composition, mechanical properties, and dimensional tolerances for wrought aluminium and aluminium alloy bars, rods, and sections used in general engineering. Engineers use it to procure, specify, and test aluminium extrusions and solid sections to ensure adequate strength, purity, and appropriate temper conditions.
Covers the requirements for wrought aluminium and aluminium alloy plate, sheet, and strip used for general engineering purposes.
Alloy/temper and the property that governs façade design.
| Reference | Value | Clause |
|---|---|---|
| Architectural alloy | 6xxx (Al-Mg-Si, e.g. 63400/6063) | Alloy |
| Temper | T5 / T6 — sets proof & ultimate strength | Temper |
| Modulus of elasticity | ≈ 70 GPa (~⅓ of steel) | Property |
| Design governed by | Deflection (stiffness), not yield | Design |
| Thermal expansion | ≈ 2 × steel — provide movement joints | Detail |
| Isolation | Isolate from steel/concrete (galvanic/alkaline) | Detail |
| Finish | Anodise (IS 1868) / powder coat — durability | Finish |
IS 733:1983 specifies wrought aluminium and aluminium alloy bars, rods and sections (extruded) for general engineering purposes — the extruded aluminium stock behind window/door framing, curtain-wall mullions, louvres, handrails, partitions and architectural metalwork. It defines the alloy designations, tempers and mechanical properties you select an extrusion by.
*(Note: the code-database title for this entry reads 'Plate, Sheet and Strip'; IS 733's established scope is bars, rods and (extruded) sections — flat-rolled aluminium plate/sheet/strip is covered by separate standards such as IS 737. The discrepancy has been flagged for correction; this note addresses extruded bars/rods/sections.)*
It is read with the architectural-metal stack:
Aluminium structural/architectural extrusions are specified by alloy + temper, which together fix strength, corrosion resistance and extrudability:
A correct specification states alloy *and* temper (e.g. '63400-T6'), the section, and the finish (anodised/powder-coated) — not just 'aluminium section'.
Brief: an aluminium mullion spanning floor-to-floor (~3.6 m) carrying wind on the glazed bay.
Step 1 — wind load: design wind pressure to IS 875 Part 3 × the mullion's tributary width → a line load on the mullion.
Step 2 — alloy/temper: choose a 6xxx architectural alloy in a T6 temper (e.g. 63400-T6) for adequate proof strength and good anodising.
Step 3 — deflection governs: size the section so mid-span deflection under wind ≤ the serviceability limit (commonly ~ span/175 or a fixed cap for glazed systems) — because E ≈ 70 GPa, this almost always governs over the strength check.
Step 4 — strength check: bending stress ≤ the allowable for the alloy/temper from IS 733 (with the relevant safety factor).
Step 5 — movement & isolation: detail thermal-movement provision (≈2× steel expansion) and isolate aluminium from steel/concrete to prevent bimetallic/alkaline corrosion. Select the lightest section that passes the deflection limit.
1. Specifying 'aluminium section' without alloy + temper. Strength varies several-fold between tempers; an unspecified extrusion can be a soft T4 where a T6 was assumed.
2. Designing for strength, not deflection. With E ≈ ⅓ of steel, slender mullions/spans are almost always deflection-governed — a strength-only check gives a flimsy, oil-canning façade.
3. Ignoring thermal movement. Aluminium expands ~2× steel; no movement joints → buckling, sealant failure and glass stress.
4. Bimetallic / alkaline contact. Aluminium in contact with steel, or cast into concrete/mortar, corrodes — isolate with gaskets/coatings.
5. No finish specified. Bare aluminium pits in coastal/polluted air — specify the anodising class (IS 1868) or powder-coat system; finish is a durability requirement, not cosmetics.
IS 733 is reaffirmed and remains the procurement reference for extruded architectural aluminium, with the alloy/temper system broadly aligned to the international 6xxx designations system suppliers quote. The page/database title for this entry appears mis-described (it lists plate/sheet/strip) — for flat product use IS 737; this note covers IS 733's true subject, extruded bars, rods and sections, and the discrepancy is flagged for correction.
The engineering message for façade and architectural work is consistent: aluminium design is governed by stiffness and movement, not yield strength. Specify alloy + temper + finish explicitly, size sections on the deflection limit for the glazing system, detail generous thermal movement, and electrically/chemically isolate aluminium from steel, concrete and mortar. Façade failures attributed to 'weak sections' are almost always deflection, thermal movement or galvanic-corrosion detailing errors — not the alloy.
| Parameter | IS Value | International | Source |
|---|---|---|---|
| Alloy Designation Equivalent | 65032 | 6061 | ASTM B209 |
| Chemical Composition (Silicon, Alloy 65032/6061) | 0.40 - 0.8% | 0.40 - 0.8% | ASTM B209 |
| Chemical Composition (Magnesium, Alloy 65032/6061) | 0.8 - 1.2% | 0.8 - 1.2% | ASTM B209 |
| Min. Tensile Strength (Alloy 65032-WP / 6061-T6, <6.3mm thick) | 295 MPa | 290 MPa (42 ksi) | ASTM B209 |
| Min. 0.2% Proof Stress (Alloy 65032-WP / 6061-T6, <6.3mm thick) | 255 MPa | 240 MPa (35 ksi) | ASTM B209 |
| Min. Elongation % (Alloy 65032-WP / 6061-T6, ~3mm thick) | 8% | 10% | ASTM B209 |
| Definition of 'Plate' thickness | Over 6 mm | Over 6.3 mm (0.250 in) | EN 485-1 |
| Thickness Tolerance (2mm thick sheet, 1000-1250mm wide) | ±0.15 mm | ±0.14 mm to ±0.16 mm (depending on exact thickness range) | EN 485-4 |