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7049/7149-T73 Die forging: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form7049/7149 / T73 / Die forging
SpecificationsAMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771
HandbookMIL-HDBK-5J, 31 January 2003, section 3.7.3.0, Table 3.7.3.0(c) (pdf page 307 of the chapter file)
Dimension bands5
Density0.103 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 band0–1 in1.001–2.000 in2.001–3.000 in3.001–4.000 in4.001–5.000 in
SpecificationAMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771
BasisABABABABAB
Ftu, ksiL71747073697268716770
LT71…70…70…70…68…
ST…………………………
Fty, ksiL60645963586157605559
LT61…60…60…60…58…
ST…………………………
Fcy, ksiL62666165606359625761
LT…………………………
ST56605559545753565155
Fsu, ksiL40413941394038403739
LT40…39…39…38…37…
ST40413941394038403739
Fbru (e/D = 1.5), ksiL1001059910398102961009599
LT100…99…98…96…95…
ST1001059910398102961009599
Fbru (e/D = 2.0), ksiL132138130136128134126132125130
LT132…130…128…126…125…
ST132138130136128134126132125130
Fbry (e/D = 1.5), ksiL82827580747873767075
LT82…75…74…73…70…
ST82827580747873767075
Fbry (e/D = 2.0), ksiL99999197909488938591
LT99…91…90…88…85…
ST99999197909488938591
e, %L7777777777
LT3…3…3…2…2…
ST…………………………
E, Msi10.210.210.210.210.210.210.210.210.210.2
Ec, Msi10.710.710.710.710.710.710.710.710.710.7
G, Msi3.93.93.93.93.93.93.93.93.93.9
ν0.330.330.330.330.330.330.330.330.330.33
ρ, lb/in30.1030.1030.1030.1030.1030.1030.1030.1030.1030.103

Effect of Temperature

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

Other 7049/7149 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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.