AECMA PREN 3347-1988
Aerospace Series Aluminium Alloy (2024) Solution Treated, Stretched and Artificially Aged (T8511) Extruded Bars and Sections (a or D) Less Than or Equal to 150mm with Peripheral Coarse Grain Control Issue P 1

Standard No.

AECMA PREN 3347-1988

Release Date

1988

Published By

European Association of Aerospace Industries

Status

Withdraw

Replace By

AECMA PREN 3347-1998

Latest

AECMA PREN 3347-2003

Scope

This standard specifies for the aerospace application, the mechanical properties for extruded bar and section, (a or D)≤ 150 mm, solution treated, stretched and artificially aged (T8511), in aluminium alloy(2024).

AECMA PREN 3347-1988 history

• 2003 AECMA PREN 3347-2003 Aerospace Series Aluminium Alloy AL-P2024-T8511 Extruded Bar and Section a or D Less Than or Equal to 150 mm with Peripheral Coarse Grain Control Edition P 3
• 1998 AECMA PREN 3347-1998 Aerospace Series Aluminium Alloy AL-P2024-T8511 Extruded Bar and Section a or D Less Than or Equal to 150 mm with Peripheral Coarse Grain Control Edition P2
• 1988 AECMA PREN 3347-1988 Aerospace Series Aluminium Alloy (2024) Solution Treated, Stretched and Artificially Aged (T8511) Extruded Bars and Sections (a or D) Less Than or Equal to 150mm with Peripheral Coarse Grain Control Issue P 1