Tools › Materials › Aluminum › 2026-T3511 Extrusions

2026-T3511 Extrusions: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form2026 / T3511 / Extrusions
SpecificationsAMS 4338
HandbookMIL-HDBK-5J, 31 January 2003, section 3.2.5.0, Table 3.2.5.0(b) (pdf page 153 of the chapter file)
Dimension bands5
Density0.1 lb/in3

Design Mechanical and Physical Properties (room temperature)

As printed in the handbook table. Bases: A and B are statistical minimums (99 % and 90 % probability at 95 % confidence), S the specification minimum. Grain directions: L longitudinal, LT long transverse, ST short transverse.

Dimension band0.000–0.249 in0.250–0.499 in0.500–1.499 in1.500–2.249 in2.250–3.250 in
SpecificationAMS 4338AMS 4338AMS 4338AMS 4338AMS 4338
BasisABABABABS
Ftu, ksiL666970727275737673
LT586162646667646761
Fty, ksiL485152535356545754
LT414445464648444942
Fcy, ksiL434546474747495250
LT424546464649454743
Fsu, ksiL373937383233323332
LT373937383233323332
Fbru (e/D = 1.5), ksiL909492958790858985
LT909492958790858985
Fbru (e/D = 2.0), ksiL112117113117109114108112105
LT112117113117109114108112105
Fbry (e/D = 1.5), ksiL626666676164616461
LT626666676164616461
Fbry (e/D = 2.0), ksiL768181837681768076
LT768181837681768076
e, %L111112121111111110
LT…………88888
E, Msi10.710.710.710.710.710.710.710.710.7
Ec, Msi10.910.910.910.910.910.910.910.910.9
G, Msi444444444
ν0.330.330.330.330.330.330.330.330.33
ρ, lb/in30.10.10.10.10.10.10.10.10.1

Effect of Temperature

The handbook maps no temperature-effect figure to this table.

Source and Use

U.S. Department of Defense (2003). Metallic Materials and Elements for Aerospace Vehicle Structures. MIL-HDBK-5J, 31 January 2003 (public domain). The values are the handbook's design allowables as extracted from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ. No warranty is given.