7178 — wrought aluminum alloy

An older high-strength alloy with more zinc and copper than 7075. You meet it on older airframes, mostly as a material to identify and to replace correctly.

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7178 at a glance

Where to buy
7178 schematic
Schematic

Designation

ItemValue
Designation7178
ClassAluminum
Typewrought aluminum alloy

Composition

ElementLimit
Si0.40
Fe0.50
Cu1.6–2.4
Mn0.30
Mg2.4–3.1
Cr0.18–0.28
Zn6.3–7.3
Ti0.20
AlRemainder

A single number is a maximum. Other elements: 0.05 each, 0.15 total, except where the Teal Sheets say otherwise. Source: Aluminum Association Teal Sheets (Aug 2018).

Properties

PropertyValueSource
Density0.102 lb/in³ (2.83 g/cm³)Teal Sheets
AllowablesNone in Section 3.7MIL-HDBK-5J Table 3.1.1
Named inComparison with 7050 T76 in stress corrosionMIL-HDBK-5J 3.7.4.0
Bend radius, 7178-OSee table belowFAA-H-8083-31B Chart 204
Replacement7178-T6 and clad are in a substitution figureFAA-H-8083-31B Figure 4-168

No strength value is given here because none of the sources used by this site prints one.

Minimum bend radius, inches (AMT Handbook Chart 204)

Alloy and temper0.020"0.032"0.040"0.063"0.125"0.190"
7178-O, 2024-O, 5052-H34, 6061-T4, 7075-O.03.03.06.09.25.38

Selected thicknesses from FAA-H-8083-31B Chart 204, p. 4-61. Chart 204 and AC Table 4-6 do not agree everywhere: where they differ, use the larger radius or the SRM.

Notes from the guide

  • Not a source of design allowables. Values are for reference. MMPDS and the SRM govern a repair.
  • Not a substitution approval. A different alloy or temper needs approved data.

Where to buy

AmericaDistributor coming soonOur partner for this region is on its way
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Distributors coming soon.

Sources

Educational reference only. not approved data. Always consult the applicable SRM, AMM, or AC 43.13-1B and your certifying authority.
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