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5086-H112 Sheet and plate: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form5086 / H112 / Sheet and plate
SpecificationsAMS-QQ-A-250/7
HandbookMIL-HDBK-5J, 31 January 2003, section 3.5.3.0, Table 3.5.3.0(b) (pdf page 238 of the chapter file)
Dimension bands4
Density0.096 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 band0.188–0.499 in0.500–1.000 in1.001–2.000 in2.001–3.000 in
SpecificationAMS-QQ-A-250/7AMS-QQ-A-250/7AMS-QQ-A-250/7AMS-QQ-A-250/7
BasisSSSS
Ftu, ksiL36353534
LT36353534
Fty, ksiL18161414
LT17161414
Fcy, ksiL17151414
LT18161414
Fsu, ksiL22212120
LT22212120
Fbru (e/D = 1.5), ksiL54525251
LT54525251
Fbru (e/D = 2.0), ksiL72707068
LT72707068
Fbry (e/D = 1.5), ksiL25242424
LT25242424
Fbry (e/D = 2.0), ksiL31282828
LT31282828
e, %L8101414
LT…………
E, Msi10.210.210.210.2
Ec, Msi10.410.410.410.4
G, Msi3.853.853.853.85
ρ, lb/in30.0960.0960.0960.096

Effect of Temperature

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

Other 5086 Tables

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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.