1、AECMA PRENZLB 80 -m 1r012311 ooo2_ew 7 m - - - - I A.E.C.M.A. STANDARD DRAFT Edition 1 October 1980 NORME A.E.G.M.A. A. E.C.M.A. NORM pr E N 231 8 ENGLISH VERSION ALUMINIUM ALLOY 2024-T35 or T35fl BARS AND SECTIONS 1,s mm 10 Wo 460 , 460 2 480 12 4 a 11 5) 2. 10 10 - I I 1 1 - - - -. I- I I I -I Har
2、dness I 120 (for information) - Shear Strength Bendlng Im e I Ruptura ElonQetlon nt ruptum A Notor Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,- AEC
3、MA PREN2318 AO W L01231l 0002874 O W 1 , r!. *.: 1 Electrical conductivity I, 1. . -. , dotan rypical use 2 3 4 5 6 7 17 100 mm r I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
