Aluminium
Downloaded from http://www.everyspec.com MI1-HDBK-694A(MR] 15 December 1966 MIUTARY STANDARDIZATION HANDBOOK ALUMINUM
Views 205 Downloads 10 File size 5MB
Recommend stories
- Author / Uploaded
- xaaabbb_550464353
Citation preview
Downloaded from http://www.everyspec.com
MI1-HDBK-694A(MR] 15 December 1966
MIUTARY STANDARDIZATION HANDBOOK
ALUMINUM AND ALUMINUM ALLOYS
n
MISC
Downloaded from http://www.everyspec.com
DEPARTMENT
OF
WASHINGTON
DEFENSE 25,
D. C.
MIL-HDBK-694A(MR) Aluminum and Aluminum Alloys 15 December 1966 1. This standardization with established procedure. 2, This publication military standardization
handbook
was developed
by the Department
was approved on .15 December handbook series.
1%6
of Defense
for printing
in accordance
and inclusion
in the
3. This document provides basic and fundamental information on alu”minum and aluminum alloys for the guidance of engineers and designers of military materiel. The handbook is not intended to be referenced in purchase specifications ezcepl /or inforrnutiond purposes, nor shall it supersede my speci[icalion reyuirerneqts. 4, Every effort has been made to reflect the latest information on aluminum and aluminum alloys. It is the intent to review this handbook periodically to insure its completeness and Users of this document are encouraged to report any errors discovered and any recurrency. commendations for changes or inclusions to the Commanding Officer, U. S. Army Materials Research
Agency,
Watertown,
Mass.,
02172.
Attn: AMXMR-TMS.
..
Downloaded from http://www.everyspec.com
MlL=ttDBK=694A[ Mll] 15 December 1966
Preface
This is one. of a group of handbooks covering design and construction of military equipment.
metallic
and nonmetallic
materials
used
in the
form, technical information and data The purpose of this handbook is to provide, in condensed of direct usefulness to design engineers. The data, especially selected from a very large number of industrial and government publications, have been checked for suitability for use in design. Wherever practicab~e the various types, classes, and grades of materials are identified with applicable government specifications. The corresponding technical society specifications and commercial designations are shown for information. The numerical values for properties listed in this handbook, which duplicate specification requirements, are in agreement with the values in issues of the specifications in effect at the date of this handbook. Because of revisions or amendments to specifications taking place after publication, differ from those shown in current specifications. In connection the values may, in some instances, with procurement, it should be understood that the governing requirements are those of the specifications of the issue listed in the contract. Wherever specifications are referred to in this handbook, the basic designation only is shown, omitting any revision or amendment symbols. This is done for purposes of simplification and to avoid the necessity for making numerous changes in the handbook whenever specifications are revised or amended. Current “Department
issues of specifications should of Defense Index of Specifications
The material into four sections: Section Section Section Section Comments Army Materials
1 II III IV
in the text
-
is based
be determined and Standards.
on the literature
by consulting ”
listed
the
latest
in the bibliography.
issue
of the
It is subdivided
Aluminum in Engineering Design Standardization Documents Typical Properties of Aluminum and Aluminum A11OYS Specification Requirements.
on this handbook are invited, Research Agency, Watertown,
They should Mass. 02172.
.,.
111
be addressed to Commanding Attn: AMXMR-TMS.
Officer, U. S.
Downloaded from http://www.everyspec.com
Downloaded from http://www.everyspec.com
MILHDBK=694A[MR] 15 December 1966 .-
Contents
Page
Paragraph Preface
. . . . . .
Section
I.
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DESIGN
ALUMINUM IN ENGINEERING
. . . . . . . . . . . . . .s
. . .
. ..
111
1
. . . . . . . . . . . . . . . . . . . . .. GENERAL . . . . . . . . . . . . .. 1. Characteristics . . . . . . . . . . . . . . . . . . . . . . i.,,. ,0. . . . . . . . . . . . . . . . .. 2. Economic Considerations . . . ,,
1 1 2
CLASSES OF ALUMINUM 3. Types Available . 4. “Pure’’ Aluminum . S. Casting Alloy s....... 6. Wrought Alloys .
2 2 2 2 2
AND ALUMINUM ALLOYS . . . . . . .........”.’” . . . . . . .....00.’.occ.c. ..,.,...”””. . . . . . . .,,...,sc”’”..’”
. . . . . . . . . . . . . . . “.-+ 000”...”. +“-s
PROPERTIES OF ALUMINUM . . . . . . . . . ...”.”.. 7. Physical Properties . . . . . . . . . . . ...’””. 8. Mechanical Properties . . . . . . . . . . . ...”!
3 3 3
““” “’.””’ .“”””
TEMPER DESIGN ATION SYSTEM. . . . . . . . . . . . . . .. . . . . . . . . . 9. Temper Designation . . . . . . ., . . . . . . ...””’. .“”.
5 5
HEAT TREATMENT . . . . . . . 10. Effects of Heat Treatment. 11. Effects of Quenching . . . .
““+” ...”” .“..””
8 8 8
‘ .
8 8
~ ~
9 9
FORMABIL,ITY 12. Factors
. . . . . . ...”””” . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . ...c.””.’ Affecting Formability . . . . . . .
.
MACHINABILITY . . . . . . . . . . . . . 13. Factors Affecting Machinability . . . . . . , . JOINING . . . . . . . . 14, Joining Methods . 15. Riveting . . . . 16, Welding . . . . . 17, Brazing . . . . . 18. Soldering . . . . 19. Adhesive Bonding
. . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . .
. . . . . .
.“’ .””’ . . . . . . ...’. ...,..,..”” .,....”.”. . . . . . . . ...” . . . . . . . ...-” . .,..,...”-”
. .
. . ~
“.’ ~ ~ ~
“ “.’ ‘.7 1.7
ALLOYS
.
0.05
0.10
0.05
0.03
0.30
1.0-1.5
1.3-1.8 0.02 1.2-1.8 0.05, 0.8-1.3 0.8-1.3 0.05
0.10 0.10 0.10 0.10 0.10
1.7-2.3 1.7-2.3
0.25 0.25 0.25 0.25 0.25
0.9-1.2 0.10 0.25 0.25 0.10
0.10 0.10
0.10
0.50- 1.3
0.15
0.25 0.25 0.10 0.10 0.20
~
0.04-0.10 0.02-0.10 0.15
0.20
0.06-0.20
0.03 0.15 0.15
0.10
).03 ).05 ).03(18) ).02 ).05(11)
0:15
),05(18) ).05 ).05 ).05 ).05
0.15 0.15 0.15 0.15 0.15
).05 1.05(20) 1.05 ).05 ~.05(181
0.15 0.15 0.15 0.15 0.15
99.00 99.30 99.30 99.35 99.45 99.45 99.60 99.75 Remainder Remainder Remainder Remainder Remainder Remainder Remainder Remainder Remainder Remainder Remainder
j.05(181 3.05 3.05(181 3.05 D.05
0.15 0.15 0.15 0.15 0.15
Remainder Remainder Remainddr Remainder Remainder
D.05(181 D.05{181 0.03 0.05(181
0.15 0.15 0.10 0.15 0.15
Remainder Remainder Remainder Remainder Remainder
0.15 0.15 0.15 0.15 0.15
Remainder Remainder Remainder Remainder Remainder
0,.15 0.05 0.10 0.10 0.05
Remainder Remainder Remainder Remainder Remainder
0.15 0.15 0.10 0.10 0.15
Remainder. Remainder Remainder Remainder Remaimier
):05(181 ).05 ).05 ).05
0,135(161 D.05(113) 0.05 0.05 0.05(16 0.05(16’ 0.05 0.02 0.03 0.03 0.02 0.05 0.05 0.03(19 0.03(19 0.05
0.15 .J
Downloaded from http://www.everyspec.com
TABLE Designation
Silicon
Ill
CHEMICAL
(Continued).
Copper
Iron
Manganese
COMPOSITION
LIMITS
Magnesium
Chromium
0.6-1.2 0.45- 0.8 0.40-0.08 1.1-1.4 1.0- 1.5
0.30 0.15-0.35
OF
WROUGHT
ALUMINUM ritan iurn
~ickel
Zinc
0.20
0.20 0.15
0.15-0.35 0.15-0.35
1.5 0.25 0.20 0.10 1.6-2.4
ALLOYS Others
(3)
Total
0.05 0.05 0.05 0.05 0.05
0.15 0.15 0.15 0.15 0.15
Remainder
Remainder Remainder
0.6-I. Z 0.6-1. Z 0.20-0.50 (t7) (17)
1.0 1.0 0.6 0.35 0.50
0.40-0.9 0.35 0.15-0.40 0.10 0.10
0.8 0.20 0.10
6061 6Z62 6063 6463
0.40-0.8 6.40-0.8 0.20-0.6 0.20-0.6
0.7 0.7 0.35 0.15
0.15-0.40 0.15-0.40 0.10 0.20
0.15 0.15 0.10 0.05
0.8-1.2 0.8-1.2 0.45-0.9 0.45-0.9
0.15-0.35 0.04-0.14 0.10
0.Z5 0.Z5 0.10
0.15 0.15 0.10
0.05 0.05(5) 0.05 0.05
0.15 0.15 0.15 0.15
6066 7001 7039 7072(16)
0.9- 1.8 0.35 0.30 Si 0.7 0.50
0.50 0.40 0.40 Fe 0.7
0.7- 1.2 l. b-. ?.k 0.10 0.10 1.2-2.0
0.6- 1.1 0.20 0.10-0.40 0.10 0.30
0.8-1.4 2.6-3.4 2.3-3.3 0.10 2.1-2.9
0.40 0.)8-0.40 0.15-0.25
0.20 0.20 0.10
0.i8-O.40
0.25 6.8-8.0 3.5-4.5 0.8-1.3 5.1 -6.1
0.20
0.05 0.05 0.05 0.05 0.05
0.15 0.15 0.15 0.15 0.15
0.6 0.7 0.7 0.40 0.40
0.30- 1.0 0.8-i.7 1.6-2.4 0.40- 0.8 0.!0
0.30-0.8
1.2-2.0 1.7-2.3 2.4-3.1 2.9- 3.7 2.0-3.8
0.18-0.35 0.18-0.40 0.10-0.25 0.25
7.0- 8.0 3.7-4.3 6.3-7.3 3.8-4.8 3.5-5.0
0.20 0.10 O.zo 0.10 0.10
0.05 0.05 0.05 0.05 0.05
0.15 0.15 0.15 0.15 0.15
6011 6151 6951 6053 6Z53(
5)
7075 7076 7Z77 7178 7079 ~1 Zn Mg. 413_.-A-45225@
0.40 0.50 0.50 0.30 0.30
0.30 0.10-0.30 0.10-0.70
~
Each
Remainder Remainder Remainder Remainder
Remainder Remainder Remainder Remainder Remainder Remainder Remainder
Remainc3er Remainder Remainder Remainder Remainder + 0.20 Zirconium
w
WI NOTES: (1)
(2)
(3)
(4)
Composition as a range.
in percent
maximum
unless
shown
For purposes of determining conformance to these limits, an observed value or a calculated value obtained from analysis is rounded off to the nearest unit In the last right-hand place of figures used in expressing the specified limit. Analysis is regularly made only [or the elements for which spec>fic limits are shown. except fur unalloyed aluminum. U, however, the presence of other elements is suspected, or indicated in the course of routine analysis, further analysls is Inade to determine that these other elements are not in excess of the amount specified. The aluminum content for unalloyed aluminum not made by a refining process is the tfifference hetwee” 100.000 percent and the sum OF all other metallic elern?nts present in amounts of 0.010 perto the second cent or more each, expressed decimal.
(5)
Also
(6)
Electric
contains
[7)
Reflector
(8)
Cladding
(9)
Foil.
0.40-0.7
percent
each of lead
and bismuth.
conductor. sheet. on alclad
20Z4.
(10)
Cladding
(11)
Also
(12)
Brazing
(13)
Bus conductor
(14)
Cladding
on alclad
ZO14.
(15)
Cladding
on alclad
5056.
(16)
Cladding on alclad 2219. 7075, 7178 and 7079.
(17)
Silicon
(18)
Beryllium wire only.
(19)
Boron,
(20)
Vanadium
on clad
contains
1100 and clad
0.20 -0.6 percent
3003 reflector each of lead
sheet. and bismuth.
aIloy
d
45 to 65 percent 0.0008
UI 3003,
of magnesium
maximm
0.06 percent 0.05-0.15;
3004.
for welding
5050,
6061,
content. electrode
maximum. zirconium
5155,
O.lO-O. Z5.
and filler
Downloaded from http://www.everyspec.com
TABLE
COmme rcial Alloy Designation
Plate Sheet
1100(1) 2011 2014 Alclad 2014 2017 2018 2020 202-4 Alclad 2024 2025 2117 2218 2219 Z618 3003 4032 5052 5056 5083 5086 5454 5456 6011 6053 6061 6063 6066 6151 7075 Alclad 7075 klclad one side 7075 7076 7079 7178 Alclad 7178 7277 X8280
NOTE (1)
WROUGHT
Bar. Rod Shapes and Tube Extruded
QQ-A-25011
ALLOYS
- CROSS
Bar, Rod, Wire or Special Shapes Rolled, Drawn or Cold Finished QO-A-225/l QQ-A-22513 QQ-A-22514
QO-A-20012
REFERENCE
(ALLOY
Drawn Seamless Tube
TO FORM)
Forgings
WW-T-700/l
Impact Ext rus ions MIL-A-12545
QQ-A-367
Rivet Heading Wire QQ-A-430
MIL-A-12545
QQ-A-250/3 QQ-A-367 QQ.A-3A7
QQ-A-22515 QO-A-250J16 QQ-A-25014 QQ-A-2S0/5
QQ-A-20013
QQ-A-225/6
QQ-A-430
WW-T-700J3
QQ-A-430 QQ-A-367 QO-A-430 QQ-A-367 QQ-A-367 QQ-A-367
QQ-A-250/2
QQ-A-200J
1
QQ-A-2Z512
WW-T-700/2
QC3-A-430 QQ-A-367
QQ-A-22517
QQ-A-25018 OQ-A-Z5016 OQ-A-250/7 QO-A-250110 QQ-A-Z50/9
OQ-A-20014 QCJ-A-200/ QQ-A-20016 QO-A-200/7
WW-T-700/4
QQ-A-430 QQ-A-430 QQ-A-367
ww-T-7oof5
5
MIL-A-1254S QQ-A-20018 QO-A-2oo/9 QQ-A-200110
QQ-A-22518
QQ-A-250/12 C2Q-A-250/13 QQ-A-250118
QQ-A-200111
QO-A-22519
QQ-A-250/17 QQ-A-250114 QQ-A-250115
QQ-A-200/12
QQ-A-250111
WW-T-70016
QQ-A-430 QQ-A-430
QQ-A-367 W-A-367 QQ-A-367 QQ-A-367
MU-A-12545 MIL-A-12545
QQ-A-430
QQ-A-367 QQ-A-367
MIL:R-1222 MIL-A-11267
: M.IL-A-
IV.
148-Aluminum
Foil
Downloaded from http://www.everyspec.com
M1141DBK-694A[MR] 15 December 1966 .—
TABLEV.
WROUWTALLOYS
Alloy
I
t060
-CROSS
REFERENCE
I
ASTM
Government
B209, B211, B221,
I
I
B245,
B21O,
(ALLOY
SAE AA106O
B234
QQ-A-225/l
B211
AA
QO-A-250/l QQ-A-430 QQ-A-O0435 WW-T-700/1 MIL-A-14E MIL-A-12545 MIL-R-5674
B209 B316 B209 B234,
AA11OO AA I1OO AA IIOO
2011 2014
1100
Alcld
2014
I
2017
100
B316
AA]
100
QQ-A-225/3
B211
AA2011
QQ-A-2oo/2 QQ-A-225/4 QQ-A-367 MIL-A-12545 MIL-T - 15089 MIL-A-22771 MIL-A-25994
B221 B211 B247
AA2014 AA2014 AA2014
B221 B24? B221
AA2014 AA2014 AA2014
B210
B209
j
AA2014
QQ-A-22515 OQ-A-430
B211
I
AA2017 AA2017
2020
CX2-A-250/16 MIL-A-8882
2024
QQ-A-200/3 QQ-A-225/6
B316
m B247
QQ-A-250/4 QO-A-430 WW-T-700/3
B316 B316 B234,
]
==-1-=B221
B247
I
QQ-A-430 MIL-R-5674
B316
2218
I
QQ-A-367
2219
I
MIL-A-8920
2618
I
3003
QQ-A-250/2 QQ-A-430 QQ-A-00434 WW-T-70C!/2 MIL-R-l 150 MIL-M17999 MIL-P-25995 I
WW-P-402
4032
I
C3Q-A-36
4003
-1 4062
AA2018
I
4153 4121 4134,4135
4028,
4029,4014
I
I
4146
I 4152,4164,4165 4112,4119,4120 4033, 4035, 4037 4086,
4087,4088,
4099,4103,
4104,
4097,
4098,
4105,
4106
AA2024 AA2024
AA2024
‘--l-+-
1
I
AA2117 AA2117
23247
I
AA2218
4142
I
B209
I
AA2219
4031
I
B316
QQ-A-367 QQ-A-2oo/l QQ-A-225/2
3004
4003
7220 4001,
I
QQ-A-367
2117
4180
AA2024
B209
MIL-S-781
4102,
4001,
-.
C3Q-A-250/3
QQ-A-367
2025
I1OO
AAl
2018
TO SPECl FlCATlON)
4132
1AA3003 AA3003 AA3003
B221 B211 B209
B210, 316
B234
AA3003 AA3003
B241,
B345
AA3003 I
I 4006,
4008
4065,
4067
AA3004
B247
AA4032
4145
B211 B209 B316
AA5052 AA5052 AA5052 AA5052 AA5052 AA5052
4114 4015,4016,4017
B210, B234, B307
37
4069,
4070,
4071
Downloaded from http://www.everyspec.com
MI1-HDBK-694AIMR) 15 December 1966 TABLE
V (Continued).
WROUGNT
ALLOYS
- CROSS REFERENCE
(ALLOY
Alloy
Government
ASTM
5056
QQ-A-430 MIL-R-5674C
B316 B316
5083
QQ-A-2oo/4 QQ-A-250/6 MIL-Ji-45225 MIL-A-46027 MIL-A-46083
B221, 345 B209
5086
QQ-A-200/5 QQ-A-250/7 WW-T-700/5 MIL-A-21579
B221 B209 B21O
AA5086 AA5086 AA5086 AA5086
5154
MIL-P-25995
B241, B234
AA5154
5254
MIL-P-25993
B241
5454
QQ-A-200/6 QQ-A-250/JO MIL-P-25995
B22 1 B209 B241
AA5454 AA5454 AA5454
5456
QQ-A-250/9 MIL-A-25994 MIL-A-25995 MIL-A-45225 MIL-A-46027 MIL-A-46083
B209
AA5456 AA5456 AA5456 AA5456 AA5456 AA5456
6053
WW-P-402 QQ-A-430 MIL-P1150
6061
QQ-A-200/8 C)Q-A-225/8 QQ-A-250/11 QQ-A-367 WW-P-402 QQ-A-430 WW-T-700/6 MIL-R-1150 MIL-T-7081 MIL-T-10794 MIL-A-12545 MIL-F17132 MIL-M - 17999 MIL-A-22771 MIL-A-25994 MIL-A-25995
AMs
SAE .
AA5083 AA5083 AA5083 AA5083 AA5083
.
B241, B345 B209
4182
4056, 4057, 4058, 4059
B316 B316 4150,4160,4161 4115,4116,4117 4025, 4026, 4027, 4053 4127, 4146
B247 B22 1 B241, B345
.AA6061 AA6061 AA6061 AA6061 AA6061 AA6061 AA6061 AA6061 AA606 1 AA6061 AA6061 AA6061 AA6061 AA6061 AA606 I AA6061
B22J B241, B345
AA6063 AA6063
4156
B247
AA6151 AA6151
4125
AA7075 AA7075 AA7075 AA7075 AA7075 AA7075 AA7075
4154, 4168, 4169, 4!70 4122,4123 4030 4139, 4141, 4044, 4045
B221 B211 B209 B247 B3 1.6 B2 10, B234 B316 B345 B345 B209
6063
QQ-A-200/9 MIL-P-25995
6066
QQ-A-2oo/lo QQ-A-367 MIL-A-25994
6070
MIL-A-12545 MIL-A-46104
6151
QQ-A-367 MIL-A-12545
7001
MIL-A-52242
7075
QQ-A-2oo/11 QQ-A-225/9 QQ-A-250/12 QQ-A-367 QQ-A-430 MIL-A - 18545 MIL-A-22771
B22 1 B211 B209 B247 B316
7075
QQ-A-250/13 MIL-S-7811
B209
Alclad 7075 One Side
QQ-A-250/18
B204
Alclad
TO SPECIFICATION)
B247
AA7075 AA7075
4079, 4080, 4081, 4082, 4083
4170 4039,4047,4048,
4049
4046 I
38
Downloaded from http://www.everyspec.com
MI1-HDBK=694A[MR] 15 December 1966 WROUGHT ,
Alloy
Government
7076
QQ.
7079
00-A-200/12 OQ-A-250/l QCJ-A-367
ALLOYS
- CROSS
REFERENCE
7079
7178
Alclad
XB2!30 Al,
Zn, Mg
AMS 4137
B22 I B209
AA7079 AA7079 AA7079 AA7079
MIL-A-8923
B209
AA7079
QQ-A-200/13 QQ-A-350/14
B22 1 B209
AA7178 AA7178
7
MIL-R-
12221
MIL-A-
11267
4171 4024 4138,4136
4158
4051,
B209
W3-A-250/15
7178
7277
TO SPECIFICATION)
SAE
ASTM
A-367
MIL-A-22771 Alclad
(ALLOY
4052
AA7277
B316
MIL-A-452.25 MIL-A-46063 MIL-A-46083
TABLE
VI.
TYPICAL
PHYSICAL
PROPERTIES Thermal
Alloy Density, lb per Type
iand
Deal
gnatien
Temper
cu
In
Conduc tiv]ty, CGS (1)
OF
E1ectrlcal -
Resist
lvlty
ALUMINUM
ALLOYS Melt!ng
Coef. Lmea
r
Point,
‘F
Therm. Expan.
Eng.
% MC-S
(2)
[3)
uilcm {4)
37
4.660
10-6, n. I,n.
Solidus
L1quidus
(5)
Cast -F
43
C30-A-601)
0.097
0.34
990
0.097
356 -T51 - T6 - T7
0.40 0.36 0.37
1160 1045 1070
43 39 40
4.010 4.421 4.310
12.3
1065
1170
11.9
1035
1135
1190
0.102
0.33
960
35
4.926
12.7
970
214
0.096
0.33
960
35
4.926
13.4
1110
1185
142
0.102
12,6
990
1175
12.4
965
1155
12.4
970
1160
12.3
965
1100
12.4
1015
1170
13.7
840
1120
13.7
1105
1195
11.9
960
1120
11.9
960
1135
13.1
IJ05
1195
1030
1175
195
- -J-4
-T21 -T571
-T61
44 34
3.9 5.1
0.31
900
33
5.225
0.29
840
31
5.562
0.29
840
30
5.747
0.40 0.34
1160
43
990
36
+.010 4.789
0.21
610
21
8.210
0.33
960
35
4.926
0.26
750
27
6.4
0.24
695
26
6.6
0.)1
960
35
4.9
0.101
108 -F
0.106
113 -F
0.098
355 -T51 - Tb 220
0.093 - T4
40E
0.100 -T5
AIJcast
0.101 -F
X-8
0.096 -F
TenzaJoy
0.100
A6J2
0.102 -F
TernalJoy
5
Ternalloy
7
Almag
1160 930
0.107
122
Red
0.40 0.32
().100
35
0.095 -F
B214
23
7.5
38
4.5
0.096 -F
0.35
IOJ5
1020
J170
J 3.0
1020
1165
J2.7
1090
1170
Downloaded from http://www.everyspec.com
MI1-HDBK=694A[MR] 15 December 1966 TABLE
VI (Continued),
TYPICAL
PHYSICAL
Alloy
~esignation
Type
ermanent old
Temper
13emit y, lb per cu in.
The rmal Conduc tivity,
Electrical Resistivity 7
CGS (1}
Eng. (2)
& (3)
p flcm (4)
0.106
113 -F
Cant
)Q-A-596)
PROPERTIES
0.29
840
30
5.747
0.32
930
34
5.071
0.32 0.31
930 900
34 33
5.071 5.224
0.31
33
0.31
900 900
33
5.224 5,224
0.34
990
37
4.660
0.107
122 -F 142
0.102 -T571 -T61 0.101
B195 - T4 - T6
-F 355
0.098 -T51 - T6
43
0.40 0.34
1160 990
43 36
4.010 4.789
0.34
990
37
4.660
0.36
1045
39
4.421
0.37
1070
40
4.310
0.28
810
29
5.945
0,26
750
27
6.386
0,097 -F
356
0.097 - T6 - T7 0.098 -T551
-F
Melti Point, VF
Solidu6
Liquidu
%5
1160
12.4
965
1155
12.6
990
1175
12,4
970
1170
970
1135
11.9 12.4
1015
1150
12.3
1065
1170
11.9
1035
1135
11.0
1000
1050
960
1120
613
1100
1185
5
603
1105
1180
7
607
Temzaloy Ternalloy
0.104
750 - T5
0.44
1275
0.095
IL-A-10935
0.096
13
e Cant
0.29
841
J085
1165
13.0
435
1200
47
3.668
23
7.496
13.0
1020
1165
31
5,561
11.5
1065
1080
0.096
A13 43 218 B214
0.096
0,34
990
37
4.660
12.3
1065
1170
0.093
0.23
670
24
7.184
13.3
995
1150
0.096
0.35
1015
38
4.537
12.7 1100
0.098
0;24
695
25
6.896
11.7
1000
380
0.098
0.23
670
23
7,496
11.6
1000
1100
360
0.095
C!.27
785
28
11.6
1035
1105
0.095
0.29
841
30
5.747
11.8
1035
1105
0.098
0.23
670
23
7.496
11.3
960
)080
13,1
1195
1215
13,1
1190
1215
12.7
995
1190
12,8
950
1180
13.2
950
1200
A380
A360 384
ought
ALLOYS
12.3
11.9
0.101
319
Q-A-591)
Coef. Linear Therm. E an. 10- 8 in.lin. (5)
0.101
A108
Ternalloy
OF ALUMINUM
1060
.0
0,098
6.158
0.56
1 625
62
2 .8
0.53
1 540
61
2 .8
0.53 0.52
1 540 1 510
59 57
2 .9 3 .0
0.34
990
36
4 .8
-o
0.46
- T4
0,29
1 340 840
50 30
3 .4 5 .7
0.37
1 070
40
4 .3
-o
0.41
11 90
45
3 ,8
- T4
0.29
840
30
5 .7
-HI 8 1100
0.098 -o -H]
2011
8 0.102
- T3 2014
0.101
- T6 2017
0.099
40
—
Downloaded from http://www.everyspec.com
MIL-HDBK-694A[MR] 15 December 1966 TABLE
VI
(Continued),
TYPICAL
All Oy
Type
tVrought (Cont. }
Designation
Temper
2018
Density lb per cu In.
PROPERTIES
The rmal Conduc tivlty, CGS (1)
Eng. (2)
0.37
Electrical Resist lvlty
~&
~*cm
(3)
(4)
1070
40
4.3
0.45 0.29
1310 840
50 30
3.4 5.7
0,37
1070
40
‘4. 3
0.37
1070
40
4.3
0.37
1070
40
4.3
0.41 0.27 0.30
1190 780 870
44 28 30
4.3 3.4 5.1
0.46
1340
50
3.4
42
4.1
0.101 -T61 0.100
2024 -o -T4 2025
0,101 - Tb
2117
0,099 - T4 0.102
2218 -T72 2219
0.103 -o -T31, T37 -T62,T81,T87
3003
0.099 -o
3004
PHYSICAL
-H12
0.39
-H18
0.37
4070
40
4.3
0.39
)130
42
4. J
All
0.098
1130
0.097
4032 - T6
0.33
960
35
4.9
OF ALIJMINUM
Coef. Linear The rm. lo%%%
ALLOYS
Meltin $. Point,
Sol,d”s
Liquidu
(5) 12.4
948
1180
12.9
935
1180
12.6
970
1185
13.2
950
1200
12,4
940
1175
12.4
1010
1190
12.9
1190
1210
13,3
1165
1205
10.8
990
1160
4043
-o
0.097
0.39
1130
42
4.1
1065
1170
5005
All
0.098
0.48
1390
52
3.3
13.2
1170
1205
5050
All
0.097
0.46
1340
50
3.4
13.2
1160
1205
13.2
1100
J200
13.4
1055
1180
5052
0.097 All
5056
-0
0.33
960
35
4.9
0.28 0.26
810 750
29 27
5.9 6.4
0.095
.-H38 5083
-o
0.096
0.28
810
29
5.9
13.2
1060
1180
5086
All
0,096
0.30
870
31
5.5
13.2
1084
1184
5154
All
0.096
0.30
870
32
5,3
13.3
1100
1190
525.2
All
0,097
0.33
960
35
4.9
13.2
J1OO
1200
5254
All
0,096
0,30
870
32
5.3
13.3
1100
1190
5357
All
0.098
0.40
1 160
43
3.9
13.2
1165
1210
13,1
1115
1195
0,097
5454 -o -H38
0.32 0,32
930 930
34 34
5.1 5.1
0.28
810
29
5.9
13.3
1060
1180 1215
-o
0.096
5557
All
0.098
0,45
1310
49
3.5
13,1
1180
5657
All
0.098
0,33
960
35
4.9
13,1
1180
1215
12.8
1070
1205
13.1
1080
1200
5456
6053
0.097 - T6
0.37
1070
40
0.41 0.37
I 190 10 70
4 53 404
4.3
0.098
6061 -o - T4
41
.8 .3
Downloaded from http://www.everyspec.com
.
i
W14iDBK-694A[MRJ 15 December 1966 TABLE
VI
(Continued).
TYPICAL
PHYSICAL
PROPERTIES
OF ALUMINUM
ALLOYS
# Electrical Resistivity
Thermal Uc -
Alloy
remper
Designation
Type
-%-
per
Eng. (2)
cu. in.
0.41
- T6 -T42
0.46
-o - T6
0.37
( 4)
1390 1340
53 50
3.3 3.4
1070 1010
40 37
4,3 4.7
0.35
1510 1540 1510 1570
57 59 ::
3.0 2.9 3.0 2.9
54 42 45
3.2 4.1 3. II
0.098
61o1 -T6 -T61 - T62 -T’64
0.52 0.53 0.52 0.54
0.098
6151 -o - T4 - T6
Meltin }= Point,
Solidus
Jlq uidus
13.0
1)40
1205
12.9
1050
1200
13.0
1140
1205
13.0
1140
1205
,o%l:;~n. (5)
0.41
1420 1130 1190
6262
- T9
0.098
0.41
1190
44
3.9
13.0
1100
1205
7001
- T6
0.J02
0,29
840
31
5.5
13.0
890
1160
7072
-o
0.098
0.53
1540
59
2.9
13.1
0.49 0.39
0.101
7075 - T6 - T6
7178
0.102
7079
0.29
840
30
5,7
0.30
870
31
5.6
0.29
840
31
5.5
0.099 - T6
NOTES
p J_lcm
( 3)
0.098
6066
(1)
fAcs
0.098
6063
f,
Therm.
Density. lb
Coe Linear
:
CGS - callcmlcm210Cls.ec units
- btrdin.
(2)
English
(3)
IACS
- international
(4)
uocm
- microhm
(5)
Average
Change
at 77° F }ft2/OFlhour
Annealed - centimeter
in length
per
at 77°F
Copper
Standard
- equal
at 68°F ‘F
from
68°F
42
to 212°F
volume
1)95
1215
13.1
890
1180
13,0
890
1165
13,1
900
1180
Downloaded from http://www.everyspec.com
MI1=HDBK-694A[MR] 15 December 1966 TABLE
VII. EFFECT
OF TEMPERATURE
ON THERMAL ~EFFICIENT Average
Type
Sand Cast (QQ-A-601)
Die Cast (QQ-A-591)
Wrought
10 ‘6 in, /in. /0F Range,
‘F 68to
572
-58 to +68
68 to 212
68 to 392
43 356 195 214
11.4 11.0 11.7 12.3
12,3 1J,9 12.7 13.4
12.9 12.5 13,2 13.9
13,4 12.9 J3.8 14.5
142 122 108 113
11.6 11.5 11.5 11,3
12.6 12.4 12.4 12.3
13.1 12.9 13,0 12.9
13.6 13,4 13.4 13.3
355 220 40E All cast
11.5 12.6
12.4 13.7 13.7 11.9
13.0 14.2
13.7 14.8
12.4
12.7
13.6
Designation
11,0
12.0 11.8
11.9 13.1 13.3 13,0 12.7
14.2 13.3
14.2 14,4 14.8 13.8
113 122 142 B195
11.3 11.5 11.6 11,4
12.3 12.4 12.6 12.4
12.9 12.9 13.1 13,0
13.3 13.4 13.6 13.4
A108 355 43 356
11,1 11,5 11.4 11.0
11,9 12.4 12.3 11.9
12,5 13.0 12.9 12.5
12.9 13,7 13.4 12.9
A132 319 750
10.3 11.0 12.0
11.0 11.9 13.0
11.5 12.4 13.5
12.0 12.7
13 43 2i0 B214
10.7 11.4 12.4 11.8
11.5 12.3 13.3 12.7
12,0 12.9 14.0 13.3
12.6 13.4 14.3 13.8
A380 380 360 A 360 384
10,8 10.7 10.8 10.9 10.5
11.7 11.6 11.6 11.8 11.3
J2.2 12,1 12.2 12.4 11.8
12.6 12.5 12,7 12.8 12.3
1100 2011 2014 2017
12.2 11.9 12.0 12.1
13.1 12.8 12.3 12.7
13.7 13.4 13,1 13,3
14.2 13.9 13.6 13.9
2018 2024 2025 2117
11.7 11.9 12. J 12.1
12.4 12.6 12.6 13.0
12,9 13.2 13. J 13.6
13.4 13.7 13.6 14.0
2218 3003 4032 5052
11.7 12.0 10.3 12.3
12.4 J2.9 10.8 13.2
13,0 13.5 11,3 13. B
13.5 13,9 11.7 14.3
5056 6053 6061
12.5 12. ) 12.1
13.4 12.8 13.0
14.0 13,4 13.5
14.5 14.0 14.1
6063 6151 7075
12.1 12.1 12.1
13,0 12.8 12.9
13.6 J3.4 13,5
J4.2 13.9 14,4
Red X-8 A612 Ternalloy 7 Almag 35 B214
Pe cmanent Mold Ca@t (QQ-A-596)
Coefficient, Temperature
Alloy
OF LlNEAREXPANSlON
12.1
Downloaded from http://www.everyspec.com
MI1-HDBK=694A[MRJ 15 December 1966 TABLE WII.
TYPICAL
EFFECT
OF TEMPERATURE
Alloy Type
Sand Cast (QQ-A-601)
Permanent Mold Cast (QQ-A - 596)
Designation
356
of Ultimate
Temper
-320F
-11OF
20 F
+75F’
-T51 - T6
126
108
104
100
212F
Strenl 300F
$TRENGTII
!h at 75°F 4001
500 F
600F t700F
92 90
83 70
48 36
30 23
16 12
:
- T4 -T6
95 94
8b 78
46 42
28 25
12 11
8 7
214
-F
94
88
72
52
36
20
142
-T21 -T5’il
100
;:
67 81
44 41
28 25
16
122
-T61
90
80
55
37
18
11
355
-T51 - T6 - T7 -T71
100 100 97 97
86 94 55 86
:; 34 49
34 27 20 27
21 17 12 17
12 10 E 10
118 116
105 106
101 103
122
-T551
92
81
68
49
24
14
142
-T571
99
92
70
33
20
12
-T6
88
72
42
18
9
6
-T51 - T6 -T71
93 ;:
77 76 80
50 30 53
32 1? 26
20 10 17
12 7 10
- ‘3’6 -T7
79 84
55 66
32 38
20 22
10 12
7 8
97
86
72
50
28
14
13 43 218 360
86 85 89 94
74 67 71 74
56 48 47 47
30 27 29 26
16 15 19 15
10 11 11 10
A360 380 A380 384
93 94
74
;:
:; 26 30
:; 13 15
:
;: 81
46 50 49 55
1:
355
356 A132
Wrought
Percent
TENSILE
195
B195
Die Cast [Q()-A-591)
ON ULTIMATE
133
107
103
-T551
1100
-o -H18
189 144
115 109
104 104
77 92
65 75
46 25
31 17
19 10
16 8
3003
-o -H] 4 -H18
206 164 143
122 109 110
107 103 104
;; 90
69 82 79
53 64 48
38 34 26
25 18 14
19 14 10
-o -H34 -H38
158 144 141
106 106 105
101 101 101
100 10Q 98
86 02 81
64 60 55
43 x
27 20 18
18 13 12
-o
141
105
101
100
68
52
36
25
14
5052
5083
4
—
Downloaded from http://www.everyspec.com
MIL-HDBK=694A[MIIJ 15 Oecernber 1966 TABLE
Vlll(Centinued).
TYPICAL EFFECT OF TEMPERATURE TENSILE STRENGTH
ON ULTIMATE
— AIIoy Type Wrought (Cont. )
Percent DeaignatiOn
-3ZOF
-J JOF
2011
- T3
2014
- T6
120
J04
2017
- T4
128
2018
-T61
2024
-T3 - T4 -T81 -T86
-20F
+75F
+212F
Strength
at 75°F
+300F +400F +500F +600F +700F
85
51
29
12
6
4
103
89
57
23
13
9
6
104
J03
90
64
36
19
10
7
118
104
J03
92
74
31
16
9
7
127
106
io4
94 94 9+ 93
;: 79 73
41 40 41 27
17 18 17 16
11 12 11 11
8 8 8 7
2117
-T4
84
?0
37
17
10
7
2218
-T61
95
70
37
17
9
7
4032
- T6
91
67
24
14
9
6
6053
- T6
86
68
35
15
11
8
6061
. T6
133
110
105
93
76
42
17
10
7
-T42 - T5 - T6
153 138 135
I 20 108 I09
108 105 103
100 89 89
95 ::
4J 33 26
20 17 13
14 1) 9
11 9 7
615J
- Tb
125
107
104
88
56
25
14
10
8
7075
- T6
J23
105
103
80
30
17
J3
10
8
7079
- T6
86
44
20
14
10
6
~ 6063
.—
Temper
of Ultimate
119
J05
102
-
—. 45
Downloaded from http://www.everyspec.com
M11411DBK-694A[MR] 15 December 1966 TABLE IX.
A, Type
TYPICAL
EFFECT
OF TEMPERATURE
Percent
Y Dee igna tion
Temper
356
-T51 - T6
195
- T4 - T6
Sand Cast (QQ-A-601)
-320F
108
Vrought
at 75°F’ 1400F +500 I
im im
-20F
+75F
.2)2F
102
100
100
98 96
84 79
48 37
25 21
12 12
8 8
::
86 83
46 37
28 25
12 12
:
214
-F
100
100
I00
67
33
17
142
-T21 -T571
100
83 93
61 70
28 27
17 13
10
95
88
42
23
12
6
96 100 93 96
83 100 81 90
43 38 26 45
22 20 14 17“
13 12 8 10
9 8 6 7
122
-T61
355
-T51 - T6 - T7 -T71
122
109
104
107
100
100
122
-T551
93
78
57
34
15
7
142
-T571
99
97
65
24
12
9
B195
- T6
88
87
42
15
10
b
355
-T51 - T6 -T71
100 100 94
83 93 84
42 35 42
21 19 16
12 11 10
8 7 6
356
- T6 -T7
93 96
63 71
31 35
18 19
11 12
7 8
89.
78
54
36
14 —.
11
13 43 218 360
95 100 92 100
90 94 78 96
71 75 56 56
43 38 33 30
21 22 17 18
12 16 9 12
A360 380 A380 384
100 100 100 100
96 92 91 96
54 67 65 72
27 33 30 36
17 17 1? 16
10 10 11 10
A132
lie Cast DC)-A-591)
of Yield Streneth
-11OF
.— Permanent !dold Cast :C.V2-A-596)
ON YIELD STRENGTH
119
107
103
-T551
1100
-o -H18
123
10?
103
100 82
90 64
70 18
40 9
30 7
20 4
3003
-o -H14 -H18
145 120 122
116 104 107
105 101 103
92 90 78
83
-76
75 43 33
58 19 15
42 12 9
33 10 7
59
J
46
.
Downloaded from http://www.everyspec.com
M11=IUIBK=694A[MR] 15December 1966 -.
TABLE
1X (Continued).
TYPICAL
EFFECT
Percent
A11oY Type Vrought Cont. )
OF TEMPERATURE
5052
Temper
-320F
-11OF
-20F
-o - H34 -H38
121 118 116
100 103 101
100 100 100
ON YIELD STRENGTH
of Yield Strength
at 75°F 700F
300F
400F
500F
600F
100 97 100
100 87 78
85 48 40
62. 26 22
38 16 14
T 10 8
100
82
77
50
34
20
79
44
26
9
5
4
5083
-o
2011
-T3
2014
-Tb
113
103
102
93
58
2.2
12
8
6
2017
- T4
132
104
101
92
75
42
24
12
9
2018
-T61
110
103
101
94
87
28
14
6
5
2024
-T3 -7-4 -T81 - T’86
133
106
101
96 96 95 94
92 77 78 73
44 43 34 23
18 19 14 13
12 13 9 9
8 : 6
2117
- T4
88
71
50
23
15
8
2218
-T61
95
80
36
14
‘7
6
4032
- T6
96
72
20
12
6
4 6
103
88
75
38
12
8 I
103
95
78
38
12
6
5
119 105 106
110 104 102
108 95 90
115 86 64
50 31 21
26 17 11
19 12 8
16 10 6
115
106
104
91
58
22
13
10
8
124
105
102
85
29
16
12
9
6
.98
44
19
12
9
6
6053
- T6
6061
- T6
116
105
6063
- T42 -T5 - T6
126 116 116
6151
- T6
7075
- T6
7079
- T6
. ...
1O(J
100
I
I
47
1
Downloaded from http://www.everyspec.com
MILHDBK=694A[MR] 15 December 1966 TABLE X.
TYPICAL
EFFECT
OF TEMPERATURE
ON ELONGATION —
Percent
Alloy ‘rypc
;and Cast QQ-A-601)
Designation
356
Wrought
-11OF
-20F
+75F
+212F
+300F
+400F +500F
.+600F +700F
3.5
4
5
15
30
60
75
- T4 - T6
8.5 5
5
9 5
20 15
25 25
80 75
100
214
-F
9
9
7
9
12
17
35
142
-T21 -T571
1 0.5
1 0,5
1 0.5
3 1
8 8
20 20
40
122
-T61
0.5
0,5
1
2
6
14
30
355
-T51 - T6 - T7 -T71
1.5 3
2 2
3 1,5
8 8
16 16
36 36
50 50
1.5
2
3
8
16
36
50
1
3
10
25
1.2
1.5
1.5
122
-T551
0.5
142
-T571
J
1
1
2
15
j5
60
B195
- T6
5
5
5
15
25
75
100
355
-T51 - T6 -T71
2 4 3
3 5 4
4 10 8
19 20 20
33 40 40
38 50 50
60 60 60
356
- T6 -T?
i
6 10
10 20
30 40
55 55
70 70
80 80
-T551
0.5
J
1
2
5
10
45
13
2.5
5
8
15
30
35
40
43
9
9
10
25
30
35
35
218 36o A360
8 3 5
; 3
25 4 5
40 8 14
45 20 30
45 35 45
45 40 45
380 A380 384
3 4 1
4 5 1
5 JO 2
8 )5 6
20 30 25
30 45 45
35 45 45
45 15
45 15
55 20
65 65
75 75
80 80
85 85
43 16 10
40 16 10
47 16 11
60 20 18
65 60 60
70 70 70
70 70 70
A132
Die Cast (QQ-A-591)
-320F
-T51 -T6
195
Permanent Mold Cast (QQ-A-596)
Temper
Elongation
1100
-o -H18
3003
-o -H14 -H18
49 32
45 18
44 16
43
0.5
0.5
Downloaded from http://www.everyspec.com
MLHDBK=694A[MRl 15 December 1966 TABLE
X (Continued).
Alloy Type
Nrought ( Cont. )
TYPICAL
EFFECT
OF TEMPERATURE
Percent
!
Designatim
5052
ON ELONGATION
ElongatlOn
Temper
-320F
-I IOF
-20F
+75F
,212F
-o -H32 -H38
30
21
la
30 14 8
35 16 9
45 * 25 20
65 40 40
+300 F +400F +500F
+600F
+7001
80 80 80
100 100 100
120 120 120
5083
-o
25
35
45
60
70
95
120
2011
-T3
15
16
25
35
45
90
125
2014
-T6
13
14
15
35
45
65
70
2017
- T4
22
18
16
28
45
95
100
2018
-T61
12
12
12
25
40
60
100
2024
-T3 - T4 -T81 -T86
17 19 7 5
16 19 8 6
11 17 11 11
23 27 23 28
55 55 55 55
75 75 75 75
100 100 100 100
2117
-T4
27
16
20
35
55
80
110
2218
-T61
13
14
17
30
70
85
100
4032
-T6
9
9
9
30
50
70
90
6053
- T6
13
13
13
25
70
80
90
6061
-T6
17
18
20
28
60
85
90
6063
- T42 - T5 - T6
33 22 !8
18 18 15
20 20 20
40 40 40
75 75 75
80 80 80
105 105 105
6151
- T6
17
19
22
40
50
50
50
7075
-T6
11
15
30
60
65
80
65
7079
-T6
13
18
37
60
100
175
175
25
20
19
49
Downloaded from http://www.everyspec.com
MI1-HDBK-694AIMR) 15 Oocamber 1986 TABLE
Type
Xl.
TYPICAL
MODULII OF ELASTICITY
“eBi’nmL-l ‘“l%”’
Sand Cant (c2Q-A-6ol
(TENSILE)
Designation
psi
Type
Alloy
43 356 195 2J4
JO.3 10.5 10.0 JO.3
Wrought
2017 20J8 2024 Alclad 2024
142 J22 355 220
JO.3 10.7 10.2 9.5
Permanent Mold Cast (C2Q-A-596)
All
Die Cast (QQ-A-591)
All
JO.3 10.7 9.7 JO.3 10.3
5 7
10.3
1L -!i-E_ I
other
than 75° F refer
to the following
table:
MULTIPLIERS FOR OTHER TEMPERATURES Percent of MOrJUlOUK at 75 ~
Temperature ‘F
I
psi
-%5 10.6
10.6
2025 2117 2218 3003
10.4 JO.3 10.8 10.0
4032 5052 5056 5083
)0.3 10.2 10.3 10.3
6053 6061 6063 6066
10,0 10.0 10.0 10.0
6151 7075 7079
10.2 10.4 10.4
JO.3
Wrought
temperatures
ModuJua
106
Alloy
40 E Allcaat A612 Ternalloy T.ernalloy
NOTE : ( 1) For
AT 75° F
-320 -112 -18
112 107 102
+75
100
+212 +300 +400 +500
98 95 90 80
I
50
I
,
Downloaded from http://www.everyspec.com
MIL.HDBK-694A[MOJ 15 December f966 TABLE
XII,
TYPICAL
FATIGUE
STRENGTHS-WROUGHT
Repeated
Flexure
Fatigue
PRODUCTS
Strength
[1)
, ksi
Designation Million Alloy
Temper
1100
-o -H16
3003
--
10.5
to Failure
1.0
10
6.5 11.5
5.5 10
5 9
8 10 11.5
7.5 9 10.5
7 9 10
0.1
14
Cvcles
100
500 5 8
-o -H14’ -H18
:;
9 12 14
5052
-o -H34 -H38
23,5 26 29.5
19.5 20.5 24
17.5 19 22.5
16.5 18 21
16 18 20
2011
-T3
35
26.5
22.5
19.5
18
2014
-T’6
39
30
24
19
j~
2017
-T4
42
34
27
22
20
2018
-T61
42
29
23
19,5
17
2024
- T4
43
31
24
21
20
4032
- T6
37
30
23.5
18
lb
6061
- T6
31
23
1?
1+.5
13.5
6063
- T42 -T5 -T6
19.5 20,5 23.5
16 15.5 16,5
13.5 12 13.5
11 10.5 II
9.5 9.5 9.5
6151
-T6
30
22
17
13
12
7075
- T6
40
29
24
22
22
Designation
Fatig”e 75%
Temper
Alloy
300”F 7.5
Strength(l),
ks,
400°F
500”F
3003
-H18
10
5
3.5
2014
- T6
18
12
8
5
2024
-T4
20
14
9
6
5052
-H36
18.5
12.5
9.5
6
6061
-T6
16
II
7.5
4.5
7075
-T6
22
12
6.5
7
NOTE (1)
:
Reversed
Flexural
Stress
(R. R.
Moore
Rotating
--
51
Beam Test)
Downloaded from http://www.everyspec.com
MIL=HDBK0694A[MR] 15 December 1966 TABLE
XIII.
TYPICAL
Ult, TS ksi
T;~
13 16
35 12 9 :“
45
Alloy
Temper
1100
-o -H12 -H14 -H16 -H18
;; 24
5 15 17 20 22
2011
-T3 - T8
55 59
43 45
2014
-o -T4, -T451 -T6, -T651
27
Clad 2014
-o - T3 -T4, -T451 -T6, -T651
MECHANICALP ROPERTIESO
FWROUGHTALLOYS
Ult. EL% l/16-in. thick
ksi
Hard nees BHN
l/2-in. dia.
Shear Str ha i
Fatigue End. Limil t ksi
;: 17 15
23 28 32 38 44
9 10 11 12 13
.
15 12
95 100
32 35
18 18
14
.
18
45
18
13
62
42
.
20
105
38
20
70
60
.
13
135
42
18
25 63
10 40’
21 20
. -
.
18 37
-
61
37
22
.
.
37
10
-
.
41
68
60
‘
2 ; 9
-o -T-4, -T451
26
10
22
45
18
13
62
40.
22
105
38
18
2018
-T61
61
46
.
12
120
39
17
2020
-o - T6 -T651 -F
-. 70 :: 59 No Req uirements
10 2 6
. . .
-o -T3 -T4, -T351 -T36
27 70
11 50
20 18
22 .
47 120
18 41
13 20
68 72
47 57
20 13
19 .
120 130
41 42
20 18
26 65
11 45
20 18
. .
. .
18 40
42 53
/?
. .
-
H
40 41
65 70
60 66
. .
.
40 42
2017 ‘
2024
Clad 2024
-o - T3 -T4, -T351 -T36 -T.81, -T851 -T86.
35
“’
6 6
2025
- T6
58
37
2117
- T4
43
24
.
27
2218
- T72
48
37
.
11
2219
- T6
58
38
8
-
.
19
35
18
70
28
14
95
30
llo
‘.-
.-
. 1
Downloaded from http://www.everyspec.com
MILHDBK-694A[MR] 15 December 1966 TABLE
X111(Continued).
TYPICAL
MECHANICAL
Alloy
Temper
Ult. TS kei
2616
-T61
58
48
4
3003
-0 -H12 -H14 -H16 -H18
16 19 22 26 29
6 18 21 25 27
30 10 8 5 4
4032
- T6
55
46
5052
-o -H32 -H34 -H36 -H38
28 33 38 40 42
13 28 31 35 37
5056
-o -H18 -H38
42 63 60
22 59 50
5083
-o -H113
42 46
21 33
22 16
-o -Hill
;:
14 21
14 12
-o -Hill -H112
41 42 41
19 26 19
14 12 12
-o -HI 12 -H311
45 45 47
23 24 33
24 22 18
-F - T6
35 50
32 42
%6
;!
3:
6061
-o
18
8
25
6063
-o - T4 - T5 -T6 - T42 - T83 -T831 -T832
13 25 27 35 22 37 30 42
7 13 21 31 13 35 27 39
22 12 12 20 9 10 12
5086
5454
5456
6011
Ten. Ys ksi
Ult. l/16-in. thick
25 12 10 8 7
6053
PROPERTIES
EL v, l/2-in. dia.
OF WROUGHT ALLOYS
Herdnea a BHN
Shear Str kei
Fatigue End. Limi ksi -
40 20 16 14 10
28 35 40 47 55
J1 12 14 15 16
7 8 9 10 10
9
120
38
16
30 18 14 10 8
47 60 68 73 7-I
18 20 21 23 24
16 17 18 19 20
35 10 15
65 105 100
26 34 32
20 22 22
25 23
-
. 3 7
70 95
35 13
26 00
11 23
8 13
30
30
12
9
25 . 60 73 42 82 70 95
10
8
17 22 14 22 18 27
10 10 9
.-
.
Downloaded from http://www.everyspec.com
15 December 1966 TABLE
Xlll (Continued).
Ult. TS ke i
TYPICAL
Ten. Ys ksi
l/16-in. thick
\lloy
Temper
6066
-o -T4, -T451 -T6, -T651
22
12
52
30
57
52
6151
- T6
48
43
7075
-0 - T6 -T651O -T6511
40{ 1)
z4( 1 )
1( 78 81
MECHANICAL
.
10
-T651 -F
22(1) 21(1)” 40( 1) 74 6; 77 66 77 66 No Requirements
7076
-T61
70
60
7079
-T6, -T651
78
68
-o
40( 1 ) 40(1 )
2](1) .
- T6
84 73 84 73 84 73 No Req uirements
8 -
10
-T651 -F
36( 1) 20(1) 40( ~) 78 6; 84 ’73 73 84 No Req uirementa
7277
- T4
60
X82 80
-H12
18
-T651 -F Al clad one side 7075
7178
-o - T6
-T651 -F -o
Alclad 7178
- T’6
NOTE
:
( 1) Specification
Shear Str ks i
Fatigue End. Limit ksi
18
43
14
-
18
90
30
-
12
120
34
16
17
100
32
11 -
.
-
7 . 10
8 . -
-
i 6
10
.
i i 6
-
10
14
145
. 10
-
45 -
-
i 6
10 8 6 6
4
15 maximum
Hard ness BHN
.
7 . 10
- T6
OF WROUGHT ALLOY$
10
20( 1 ) 36(1) 40( 1) i’z 6; 77 66 77 66 No Req uirernent 6
-o
Mclad 7075
Ult. EL% 1I 2-in. dia.
-
70 73
PROPERTIES
requirement
54
.
-
.
35
23
Downloaded from http://www.everyspec.com
Mll+iDBK-694A[MR] 15 December 1966 ?’ABLE XIV.
r
TYPICAL
1 QQ-A-601
, Ten. Ys ksl
-F
19
8
- T4 -T51 - T6
,35(1) 25 33
16 20 24
195
- T4 - T6 - T62 -T7
32 36 41 z9(1)
214
-F
142
122
Temper
43 356
..T..
1 Ult. El. 7a
OF SAND CAST ALLOYS
Hard ness BiiN
1 Comp. Ys ka I
r Shear Str ks I
Fatigue End. Limit ksi
8
40
9
14
8
3(1) 2 3.5
65 60 70
21 25
20 26
8 8.5
16 24 32 19
8,5 5 2 ,(1)
60 75 90 7’0
17 25 34
26 30 33
7 7.5 8
25
12
9
50
12
20
7
-T21 -T571
27 32
18 30
1 0.5
70 85
18 34
21 26
8 11
- T2 -T61
27 41
20 40
/2)
80 115
43
32
14
2.5
55 75
)5
17
11
,. F -T55
108
PROPERTIES
1
Ult. TS ks>
Alloy
-.
Mechanical
:;(1)
8.5
113
-F
24
15
1.5
70
lb
20
9
355
-T51 - T6 - T7 -T71
28 35 3B 35
23 25 3b 29
1.5 3 0.5 1.5
65 Ho 85 75
24 26 38 30
22 28 28 26
8 9 lG 10
220
- T4
48
26
16
75
27
34
8
40E
-T5
35
26
5
75
14
28
9
Allcast
-F -T6
27 36
18 24
2 L
70 80
19 25
22 29
10 II
Red X-8
-F - T6
30 39
21 30
1.5 1.5
60 85
T]
-T5
30(1)
22
‘1(l)
65
Tenzaloy
-T5
34
25
4.5
A612
-T5
35
.?5
5
75 —. 75
25
26
8
19
5(1) 1.5
Te rnalloy
5
-T5
30( 1)
Ternalloy
7
-T5
37
27
-F - T4
40 35(1)
21 l&l(l)
-F
20
13
Almag
35
B214 NOTES
has
minimum
65 ...— 85
—.
10
70 1:(1) 2
:
( 1) Specification (2)
-----
requirement
than O. 5 percent
55
50
14
17
8.5
Downloaded from http://www.everyspec.com
MILliDBK-694A[MR] 15 December 1966 TABLE
XV.
TYPICAL
MECHANICAL
PROPERTIES
OF PERMANENT
AND SEMI-PERMANENT
MOLD CASTING ALLOYS
Temper
Ult. TS ksi
Ten. Ys ksi
Ult, EL %
Comp. Ys ksi
Shear Str ksi
113
-F
28
19
2
70
20
22
9.5
122
-T551 -T65
37 48
35 36
0, 5 0.5
115 140
40 36
30 36
8.5 9
142
-T571 -T61
40 47
34 42
1 0.5
105 110
34 44
30 35
10, 5 9, 5
- T4 -T6 - T7
x 39
19 26 20
9 5 4.5
;: 80
20 26 20
30 32 30
9.5 10 9
-F
28
16
2
70
17
22
13
-T51 -T6 -T62 -T71
30 42 45 36
24 27 40 31
2 4 1.5 3
75 90 105 85
24 27 40 31
24 34 36 27
10 10 10
-F
23
9
10
45
9
16
8
-T6 - T7
38 32
27 24
5 6
80 70
27 24
30 25
13 11
-T551 -T65
36 47
28 43
0.5 0.5
105 125
28 43
28 36
13.5
-F - T6
34 40
19 27
2, 5 3
19
24
10
;;
-T5
33
22
4
11
15
9
CX2-A-596 Class
B195
AI08 355
43 356
A132
319
Tenzaloy
(6 13)
Hard ness BHN
Ternalloy
5 (6o3)
-T5
37
21
10
70
Ternalloy
7 (6o7)
- T5 - T7
47 53
29 43
4 3
95 95
-T5
23
10
12
45
-F
2.2
2, 5
-F -T5 - T6 -T7
28 30 35 31
.
- T6
45
3.0
A750
-T5
18
6.0
B750
- T5
27
3.0
F132
-T5
31
-
C355
-T61
40
3.0
A356
-T61
37
5.0
750 A214 333
357
56
Fatigue End Limi ksi
_
Downloaded from http://www.everyspec.com
MLHDBK0694A[MRJ 15 December 1966 TABLE
QQ-A-591 Alloy
No.
XVI.
TYPICAL
MECHANICAL
Tens]le Strength ks]
PROPERTIES
Yield strength at O. 2% offset ksi
OF DIE CASTING ALLOYS
Elongation 2 inches %
Fatigue End. L]mit ksl
Shear
]n
Str
ks]
13 A13 43 .218
43 42 33 45
21 19 14 27
2.5 3.5 9.0 8.0
25 25 19 29
;:
A360 360
46 44
24 25
3.5 2.5
26 28
!8 20
A380 380
47 46
$:
3.5 2.5
27 28
20 20
SC1 1-1A
48
24
2.5
TABLE
XVII.
APPROXIMATE
RADII FOR 90-DEGREE
I DeslgnatlOn
Radius
Requ]red
19 19
COLD BEND OF WROUGHT
on terms
Of sheet th]ckness,
ALLOYS
t)
7
L
Alloy
Temper
t= l/64
t. 1/32
t= l/16
1100
-o -H14 -H18
0 o o-1
0 0 0.5 - 1.5
0 0 1-2
-0 .H!4 -H18
0 o
t= l/8
t= 3/16
t,l/q
I
t=31b
t=llz 1-2 2-3 3-6
—
-= 3003
5052
-o -H34 -H38
0.5-
1,5
1.5-
i,5
0 0 1-2
0 o-) 1.53
5083
-o
2014 Clad
-o -T3 - T4 -T6
1:2 1-2 2-4
20~4
-o -T3 -T4 -T81
0 1.5 - 3 1.5 - 3 3.55
5456
-o -H321
6061
-o -T4 -T6
0 o-1 o-1
7075
-0 - T6
0 2-4
1.5-
0 0 1-2
0 o 0.5-
0 0
0 0 3
3
0 0-1 2-4 0 0.51.5 2-4
0 0-1 2-4
0 0-: 2 --1
0 0-) 3-5
0 0-1 3-5
0 : - + 1,5 4-6
0 1 -2.5 4-7
1-2 1.5. 7 5-)3 —
0-1 1-2 3-5
0-1 1.53 -I-6
0.51,5 2-3 .?-7
1-2 2,5 - 3,5 S-*
0.5 - 1.s
1.5 - 2
1.5 - 2.5 3-5 5.5 - 8 5.5-8 8-11
0 - 0.5
0-1
0-1
0 1,5-3 1.5 - 3 3 -5
0 2-4 2-4 3-5
0 3-5 3-5 4 -0
0-1 4-6 4-6 5-7
0.7 4-6 4-6 b-lo
1.5- 3 5-7 5-7 7-1o
0’ 2 -4 2-4 4. 5-6
0 3-5 3-5 5-7
0 4 -6 4-6 6,5-8
0-1 4-6 4-L 7-9
o-i 5-7 5-7 8-10
1.5-3 6-B 6-8 q-n
0-1 2-3
0.5 - 1 2-3
0.5 - 1 3-4
0.5 - 1,5 3 -4
0 1-2 1.5-3
0-1 1.5 - 3 2-4
o-i 2-4 3-4
0.5 - 2 2.5 - 4 3,5 - 5.5 —— 2.5 - 4 7-1[
J
0 0-1 0.5 - 1,5 0 3-5
0 0.5 - 1.5 1-2 O-i 4-6
0.51.5 5-7
1-2 j-7
1,5-3 6-10
3-5 6-9 6-9 9-12
I
0.5 - 2 3-4
.—
I - 2.5 3-5 4-6 3.5 7-I’2
I
Downloaded from http://www.everyspec.com
MIL=HDBK-694A[MR] 15 December 1966 TABLE XVIII.
FORGING ALLOYS
cold Workability
Alloy
Strength
1100 2011 2014 2014Clad
4-3 2 1 1
3-4
2017 2018 2024 2024Clad
1 1 i
3
1
2117 2218 3003 4032
3 2 4-3 2
5052 5056 5083 5456
3 2 2 2
6061 6063 6151
3-2 3-2 2
3-4 2-3
7075 7075Clad 7079
1 1 1
NOTES
- RELATIVE
Corrosion Resist.
1 -3 3-4 3-4
RATING BY CHARACTERISTICS
Machinability
1 3-4 3 -4
Electric Conductance
4-3 1 2
2 3 3
1
2
3
3-4 3 3-4
2 2 2
4 3 4
4
1
2
4
2
3 3 1 3
3 2 4-3 3
3 -4
1-3
1 -3 1-3 3 3
1 }-3 1 1 -2
4-3 4-3 4-3 4 .-3
Hardness 4-3 2 1-2
1 3
2 2 1
3
3 3 4
2 4-3 2
4 1 3
4
3 -2
: 4
2 2
1 1 2
3 3 3
; 3
3-2 3-2 2
1
4
3
2
4
1
4
4 4
1 3
2 2
4 4
1
3
:
(1)
-
Relative
(2)
-
First nsm-nber in numbered pairs second number is for hardest.
ratings
TABLE
XIX.
are
in decreasing
TYPICAL
order
of merit.
is rating
TENSILE
for
softest
temper;
STRENGTHS OF GAS-WELDED JOINTS
Alloy Type Sand Cast (QC2-A-601)
Wrought
Forga bility
Designation
Temper
Thickness, inch
Tensile Strength ksi
43
-F
0.500
12
214
-F
0.500
12
1100
-H14
0.249
11
3003
-H14
0,249
14
5052
-H34
0,249
27
58
Downloaded from http://www.everyspec.com
MIL-HDBK-694AIMR] 15 Docmnber 1966 TABLE
XX.
TYPICAL
TENSILE
STRENGTHS OF BUTT WELDEDJOINTS Tensile
Designation Filler Metal Alloy
A6 Welded
lJOO
1100
13.5
3003
1100
16
5052
5052
28
Baoe
Temper
Alloy
NOTE (J)
Metal
4043
34
51
6061
- T6
4043
27
43
6063
-T5,
4043
20
-
T6
tungsten
XXI.
arc
or Argon-
TYPICAL
5052
-H32) or .H38) to -T4 ) or -T6 )
-T3 -T6 -T6
(minimum),
pounds
Sheet in Joint,
per spot
inch
0.016
0.020
0.025
0.032
0,040
0.051
0.064
40
55
70
110
150
205
70
100
145
210
300
98
132
175
235
108
140
185
260
I
0.081
0.102
0.125
280
420
520
590
410
565
775
950
1000
310
442
625
865
1200
1625
345
480
690
1050
1535
2120
to
-H12) or -H18) to -o )
-T3
Strength Thinnest
Temper
-H14) -H18)
shielded
SHEAR STRENGTHS OF SPOT WELDS
Shear
3003 3003 5052
2024 Clad 2024 7075 Clad 7075
kei
:
Combination
6061
Weld,
Heat Treatment and Aging
- T6
TABLE
1100
Across After
2014
Using Argon- shielded consumable electrode.
All Oy
Strength
) to ) ) or ) or ) )
.-
59
Downloaded from http://www.everyspec.com
MI1-HDBK-694A[MR] 15 Oecember 1966 TABLE XXII,
WELDABILITY
Relative
Government Designation
Spec.
Arc
Alloy
QC2-A-601 (Sandcast)
Gas Weld
with flux
Suitability Weld with inert gas
for
Welding,
Resistante Weld
43 356 195 214
A B c c
A B c c
A B :
A B c c
142 122 108 113
c B c
c c B c
c c B c
“c c B c
B D B c c
B D B c B
B D B c B
1 2 3 4 5
c c c“ c B
c c c c B
6 -1 8 9 15
B A B B D
355 220 Allcast A612 B214 Spec.
RATINGS FOR CAST AND WROUGHT PRODUCTS Brazing, PFes cure Weld
a,nd Solde;ing
Soldering
Brazing
D
D D D D
:
D D D D
D D D c
D II D D
B D B c c
D D D D D
D D D c D
c D D A D
c c c c B
c c c c B
D D D D D
c D D D D
D D D D D
B A B B ,D
B A B B D
B A B B B
D P D D D
D D D D D
c c c D D
A D D
A D B
A D B
B D B
A D D
A D D
A D D
D
B
B
A
c
D
D
.C
‘D ,;
c c
Class
QQ-A-596
(Permanent and 5emi-per manent Mold cast)
Spec.
Alloy 110-0 2011 2014 2014Clad
(Wrought) (See tabie V for cOrresponding spec. nos)
2017 2018 2024 2024‘Clad
D D D
B B B
B B B
B B B
D D c
D D D
D D D
D
B
B
A
c
D
D
3003 4032 5052 6061
A D A A
A B A A
A B A A
AiB c A-B A
A c A-B c
A D c B
A D c A
6151 7075
A D
A D
A D
A B
c D
B D
,B D
NOTES :
(1) -
Ratings are defined as follows: A - Generally weldable by all commercial procedure6 and methods. B - Weldable by special technique.
60
C - Weldability limited because of crack Beneitivity or 10ss of properties. D - No common” methods have been developed.
Downloaded from http://www.everyspec.com
i
TABLE
XXIII . CASTING ALLOYS – RELATIVE
Four
Designation P&SP
Sand “QQ-A-601 Alloy
Mold
QQ-A-596 class
43
Die Q-A-591 Alloy
45
Pattern shrinkage Allowance (2) 5132
7 356
51 Jt 1?
195 214 )42
5132
122
5132
51 )2 5/32
108 113
513,? I
355
51 JZ 6
1/;0
220 40 E Allcast 319
3/16 5/ 32 5/32 II
Red X-8 T1 Tenzaloy
5132 3/16 12
A612 Ternalloy
3/16 3/)6
5 13
Ternalloy A1mag 35 B214
7
3/10 14 41L-A-10935 B214 4 5 4
10 15 13 A13 43 A380 3no 360 A 360 218 SCI 14A
?.esistance to f~ot Cracking (3]
RATING By CHARACTERISTICS
Y Characteristics
‘r Fs sure ightness
Fluidity (4)
—.—
olidifl cation shrinkage Tendancy (5)
1 1 1 I 4 5 } 4 3 4 2 3 ) I 1 5 3 z 2 .2 1
1 2
5 5 5 5 5 5 5 3 3 4 1 I I
J 4 3 3 4 3 4 5 4 1 .? ~
4 5 4 4 5 -f 5 5 4 3 3 J 3
1 1 2
z .?
I 1 1 1 4 4 4 4 3 4 z 5 \ 1 1 i ; 2 2 .? I
z 2 1 1 5 2
2 4
3 2 z 1 1 5 2
Notes
:
(1)
Rating: I through 5 are relative ratings w!th 1 and 5 the lowest )n each type indicating the highest nf casting.
(2)
Not applicable to permanent mold Ings. Allowances are for average Shrinkage requirements WIII vary O( design and dimensions.
(3)
Ability of alloy to withstand contraction stresses while cool, ng through hot-short or br, ttlc temperature range.
(4)
Ability of liquid fill thin sections.
(5)
Decrease In volume accompanying freezing of alloy and measure of amount uf compen~atmg feed metal requu red In form of risers.
(6)
f3ased cm alloy {ASTM 33117).
(7)
Composite rating based on ease of cutting, chip characteri~tics, quality of finishing, and tool Ratings, in the case of heat treatable alloys, life. based on T6 temper. C3ther tempers, particularly the annealed temper, may have lower rating.
(8)
Composite polishlng poltsh:ng
(9)
Ability applied
(lo)
Rated
alloy
and die cast sand castings. with intricacy
to flOW readily
resistance
in 5% salt
in mOld and
spray
test
rat, ng based on ● ase and speed of and quallty of f!nish provided by typical procedure.
o{ casting by present
to take and hold an electroplate standard methods.
on lightness of color, anmfizcd roatang
ity of clear
●lectrolyte.
brightness. and uniformapplied ,n sulfuric acid
(11)
Rated on combined alloy to corrosion.
(12)
Rating Lased on Iens#le and yteld strrngths at te#tl perature up to 500 F. after prolonged heating at test>ng temperatures.
(13)
Based on ability of material f]ller rod of same alloy.
(14)
Refers to suitability of a310y 10 withstand temperatures without excessive distortion
(15)
t401 recommended exceeding 200 F.
(16)
Stress
resistance
of coating
to be Iusion
and base
welded
with ●
relief
anneal
for service at 250
brazing or melting.
at temperatures F or less.
Downloaded from http://www.everyspec.com
d
TABLE
XX-II! (Continued).
CASTING ALLOYS - RELATIVE
Desknation
Other
Die X2-A- 591 Auoy 43
43 7
yes
356
yes
8
yea
195 214 14Z
no
yes 3
yes
2
yes yes
1
no no no
IZ2 108 113
yes ye e ye9 w=d yen yes yes yes aged aged aged aged aged aged ye. yes
355 6 220 40E A31cast 319 11 Red X-8 T1 Tenzaley lz A61Z Ternalloy 5
3 3 z z 3 1 4 4 4
no no
13
Ternalloy 7 14 Alrrmg 35 M3L-A- 1093’ BZ14 4
B214
13 A13 43 A380 380 36o A360 218 SCI 14A
(16) no ye e no yes yea aged no no no no no no no no no
: : 3 3
OIJY
only ody on3y O~Y only O~Y
Only
RATING BY CHARACTERISTICS
Characteristics )
Normally Heat Treated
: 3 3 3 3 z 2 2 2 2 z z I i * 3 3 3 3 3 2 5 5 3 3 1 5
5 5 4 3 2 1 z 2 1 1 3 2 z 3 3 1 1 3 3 3 4 1 1 1 1 1 1 1 1 1 z 3 3 4 4 1 3 4 5 3 3 3 3 1 3
d-
us
‘olishing
Electroplating
(8)
(9)
Anodize
ippea.ante (10)
SE$l (11)
5 4 5 3 2 1 z z 2 z 3 z z 3 3 1 1 4 4 3 5
2 z 2 1 1 5
5 4 4 4 z 1
: 1
: 3 3 3 3 3 4 4 1 z 4 4 4 4
1 1 1 1 1 1 1 1 z z 3 5 5
2 2 z 3 3 3 3 5 4 1 2 4 3
z 1 z 2 1 z 1 ; 3 4 5 5
i z 3 2 2 2 2 ! 1 2 3 2 2
5 5 4 3 3 3 3 1 3
i 3 2 1 1 1 I 5 2
5 5 4 3 3 3 3 1 4
i 3 3 5 5 3 3 1 4
: 2 2 1 2 4 2 2 z z 2
2 2 2 z 3 1 4 3 4 4 3 4 4 z 2 : 3 3 3 2
Strength
at
Elevated remperaturea (12) 4 4 3 3 32 1 1 1
1 3 3
(:5) 5 3 3 3 2
5 5 5 5 5 3 3 2 : 2 i 3 5 2 z 2 2 4 2
Weldlng Suitability
Brazing 5u3tability
(13)
(14)
1 1
limited limited no no no no no no no no no no no no no no ye 6
$ 3 4 : 4 4 2 3 4 2 2 5 4 2 z 2 2 4 4 4 4 4 4 4 4 4 4 z 2 z 4 no no no no no no no no no
no no no no yes yes yes yes yes yen yes no no no no no no no ro no no no no no no no
d -
OY
Downloaded from http://www.everyspec.com
I
TABLE
XXIV.
(QQ-A-596)(2)
ALLOYS
43, 195, 108, 40 E Allcast T1,356 355, Red X-8 Tenzaloy A612 Ternalloy 5, Ternalloy 7, Precedent 71A
43, 356 195,113, 355. Precedent
43, 356, 214, 355, 220, Almag 35, B214
142, 355,
1,4,5,6, 7,8,11,12, 13, 14, 16, 17,18
5,6,7,8, 9,10,11,13, 14
7,8, 12, 13.14,1H Almag )5 Ml L-A- 10’+3
ear]ngs 20-l> earings —-
35
—
360, A360 384
—.—
High Temp. Strength
—
..— 13, AIJ, 43, 380, A380
Die (QQ-A-591)(’~
FOR CASTING
Corrosion Resistance
General Purpose
Casting
Permanent & Semi-Permanent Mold
APPLICATIONS
Pressure Tight
Type of
Sand (c3Q-A-6ol)~l)
TYPICAL
——
—-.
— —.
BZ14,
Z18
.—.
——
—
———
NOTES : (1)
Alloy
designation
(z)
Class
designation
d
co a9
..
Downloaded from http://www.everyspec.com
MIL41DBK=694A[MR] 154ocombor TABLE
Alloy
1966
XXV.
PRINCIPAL
CHARACTERISTICS
Outstanding
AND USES OF WROUGHT ALUMINUM ALLOYS
Recommended
Characteristics
Non-heat-treatable
Use
Alloys
Very good formability, weldability, resistance to corrosion. Relatively strength but high ductility.
3003
Good formability and weldability, very good resistance to corrosion. Appreciably higher strength than 1100.
General purpose material for drawing and stamping. Miscel laneous parts where higher strength is needed than that provided by 1100.
5052
Moderate mechanical properties, stronger Fairly and harder than 1100 and 3003. good formability. Readily weldable. Excellent resistance to corrosion by salt water.
General purpose’ alloy where fairly high strength is required. For marine and outside applications, fuel and hydraulic lines, and tanks.
Heat-treatable
and low
Gene ral purpose material for drawing and stamping, and for a miscellany of parts where high etrength is not required,
1100
Alloys Stock for screw-machine products. Bolts, nuts, screws, and a g rest diversity of parts made on autOmatic screw machines,
2011
Excellent free-machining Fairly high mechanical
2014
High mechanical properties including yield and tensile strength, fatigue, and Fair formability and forging hardnees. qualities. Readily machinable.
Most commonly used alloy where high strength is required. General structural applications, heavy duty forgings, and strong fittings.
Clad 2014
A sheet product which combines the high mechanical properties of 2014 with the good corrosion resistance of 6053.
For structures requiring high unit strength together with good resistato various corrosive environnce ments.
2017
A bar, rod, and wire alloy having relatively high strength, and good ining qualities.
Screw-machine products, fittings, and structural applications where relatively high strength is required, Now largely superseded by newer alloys
well
qualities. properties.
mach-
Forged pistons and cylinder head for internal -combustion engines. Suitable for various types of high temperature services, Forged cylinder heads and pistons.
2018 2218
Both retain strength temperatures.
at elevated
2024
A high strength alloy with mechanical properties intermediate between 2014 and 6061.
64
purpose material for General various structural applications where good strength is required. Fittings and screw-machine products.
Downloaded from http://www.everyspec.com
M11+ID$K0694A[MII] 15 Docombtr 1966 TABLE
XXV (Continued).
PRINCIPAL
CHARACTERISTICS
AND USES
OF WROUGHT ALUMINUM ALLOYS
Outstanding
Alloy
Recommended
Characteristic
Use
w Heat-treatable
Alloys I
..-
For structural applications re quiring good strength together with resistance to corroeion.
Clad 2024
A sheet product which combines the mechanical propertied of 2024 with the corros]on resistance of 1230 aluminum allc.y.
2025
Fairly forging
4032
Retains strength temperatures
6151
Fairly good mechanical properties. Excellent forging qualities. Good resistance to corrosion.
General purpose material for ordinary forgings. Small press forgings and intricate pieces that are difficult to forge in the harder alloys.
6061
Good mechamcal properties. Superior brazing and welding qualities. Good forming characteristics, workability, and resistance to corroe~on,
General structural purposes. Marine and outside work. Transportation equipment. Many small Various extrueion forged parts. applications.
7075
Affords limit, forging
Structual application requiring maximum yield and tensile strength. Section thickness limited to 3 inches.
Clad 7075
A sheet product which combines the mechanical properties of 7075 with improved corrosion resistance.
high mechanical qualities,
maximum Not readily quallties.
well
propert~es.
Good
at elevated
strength formed.
Specialty forging alloy. Applica tiotm mostly confined to propel lers for superchargers and engineu. Forged pistons for combustion engines.
and endurance Poorest
-. 65
internal-
Structural applications where the highest strength together with maximum corrosion reslntance is necessary.
Downloaded from http://www.everyspec.com
Downloaded from http://www.everyspec.com
MI1-HDBK-694A[MR] 15 D@cambar 1966
Section Specification
IV Requirements
This section contains tabulations of the chemical composition and mechanical property requireThe data are arranged according to the ments for wrought aluminum alloys used by the Government. numerical commercial de.4ignations of the alloys. Each tabulation of chemical composition shows the maximum allowable percentage of the alloying element, or if a range is indicated, the minimum and the maximum allowable percentages of the elethe minimum values that can be ment. The mechanical property tabulation, when given, indicates expected unless otherwise noted. In the tables, footnotes
are
the following ..—
reference is made to explanatory footnotes t in many of the tables, they are omitted
repeate:
(numerals in parentheses). Since these from the tabulations and are included in
listing.
If, however, the presence of other shall regularly be made only for the elements listed. is indicated in the course of routine analysis, further analysis shall be made to determine conformance with the limits specified for other elements.
(1)
Analysis elements
(2)
Not required
(3)
For rounds (rod) maximum diameter is 8.000 inches; for square, rectangular, gonal bar maximum thickness is 4.000 inches, and maximum cross-sectional
(4)
Direction of specimen: P - P aralle 1 to forging flow lines NP - Not parallel to forging flow lines - Longitudinal L LT - Long Transverse ST - Short Transverse
(5)
Maximum heat treat
(6)
Test
(7)
Identification
(8)
Applicable
to flat sheet
(9)
for wire of less than 0.125 inch diameter.
section
hexagonal, or octaarea is 36 inches.
thickness.
coupon. classification
number. only.
Applicable
to plate
(lo)
Applicable
to plate heat treated
and coiled
(11)
These properties are those of the core alloy since machined from the plate.
(12)
For bar, maximum cross-sectional
( 13)
Applicable
to plate
(14)
Applicable
to flat sheet
and coiled
sheet
and to flat sheet
heat treated
by the user.
by user.
area is 50 square sheet
and plate
only.
only. 67
the tests inches.
are made on a round specimen
Downloaded from http://www.everyspec.com
MIL-HDBK-694A[MR] 15 December 1986 (15)
Applicable
(16)
Not required
(17)
For rounds (rods) maximum diameter
(18)
Cutout specimen.
(19)
Tensile and yield strength test requirements may be waived for material in any direction in which the dimension is less than 2 inches because of th’e difficulty to obtain a tension test specimen suitable for routine control.
(20)
For cross sectional areas the time of heat treatment,
(21)
Non-heat
(22)
For cross-sectional areas the time of heat treatment,
to sheet
and plate heat treated
for material
treatable
% inch
or less
by user.
in width.
is 6.500 inches
- see note (3) for other requirements.
greater than 144 square inches, or thickness grester than 4 inches at the properties shall be as specified in the contract or purchase order.
alloys. greater than 72 square inches, or thicknesses greater than 6 inches at the properties shall be as specified in the contract or purchase order.
68
Downloaded from http://www.everyspec.com
WIDBK-694A[MR] .15 December1866
CHEMICAL Specification
Cu
Si & Fe
Mg
All(a) below
0.20
l. Omax
-
- see
Zn
Ml-l
0.10,
- percent
1
Ti
Cr
Sn
Ni
Al
-
-
-
-
99,0 min
0.05
II
(a) - Aluminum or lead.
foil
(Spcc.
M2L-A-148)
shall
MECHANICAL
Desigru ati cm — MIL-A-148 Foil Specific
QQ-A-z50/ Plate and Sheet
COMPOSITION
1
Thickness inch
on Temper ——
-0
and
- H22
-f-114 and -H24
-H16 -H26
leas
than O. 01 percent
PROPERTIES
Area Sq. in.
and
J
eaci] Of arsenic,
Tensile Str ksi ——
I
! 1
1 Mullen EL Streng min 70 ;
8
cadmium
11 11 11 11 11
0,017 -0,0J9 0.020-0,031 0.032-0.050 0.051 -0, }13 0.114-0.499 0.500-2.000
14 14 14 14 14 14
0.009-0.012 0,013-0.019 0.020-0.031 0.032-0.050 0.05}-0. 113 0.114-0,499 0.500-1,000
16 16 16 16 i6 16 16 19 -1’J 19 19
--l rz3 31 55
Z2
/
0.006-0.019 0.020-0,031 0.032-0.050 0.051-0.249 0.250-3,000
ursting - psi m ax
11
I
69
each total
I I Yield Str is i
I
0.006-0.019 0.020-0.031 0,032-0,050 0.051-0,162
0.05 0.15
- minimum
O. 0008 0.0010 0.0015 0.0020 0.0030 0.0040 0.0050
Annealed
.1:]2
contain
Other “)
1
40 75 110 140
90 150 220 280
~
I !
3.5 3.5
‘ 11 11 11
91
12 i 2 3 4
. 14 14 14
2 10 1 2 _L-
3 4
J
Downloaded from http://www.everyspec.com
MI1-H06K=694A[MR] 15 December 1966
MECHANICAL
Denignetion Specification Tepper QQ-A-Z5011 Plate and Sheet (Cont. )
PROPERTIES
0.006-0,019 0,020-0,031 0.032-0.050 0.051-0.128
22 22 22 22
-I-3112
0.250-0.499 0.500-2.000 2.001-3.000
13 12 11.5
2.250-6.000 All up to up to up to UD”tO 0:3’?5 All
WW-T-700/l Tube, Seamless, Round, Square, Rectangular, and Other Shapes
-o -HA2 -H14 -H16 -H18 -F
All All AU All AU’
MIL-A- 12545 Impact Extrusion
-F
QQ-A-430 Rod and Wire for Rivets and Cold Heading
-o
QQ-A-225/3
~ . . .
15.5 max :: 19 22 - No requirement
-.
I
I
1-
-H14
CHEMICAL Specification
-
15.5 max 14 16 19 T 22 - NO requirement 11
0.374 0.374 0.374 0.374 and eve; .
iullen Bursting ;trangth - pe i min max
EL %
9 14 20
requirement
-N
i I
Yield Str ksi
1 2 3 4
-H18 and - H28
-o -H12 .H14 -Hi6 - H18 -F .H12
(Cent).
Tensile Str ksi
Area 5q. in.
Thickness inch
-F Q+ A- 225/1 Bar, Rodj and Wire, Rolled, Drawn, or Cold Finished
- minimum
COMPOSITION
- percent
Cu
Si
Fe
Mg
Zn
Mn
Cr
Sn
Ni
Bi
Pb
Al
5.06.o
0,40
0.7
-
0.30
-
-
-
-
0.200.6
0.200.6
Bal‘ ante
MECHANICAL Designation Specification Temper QQ-A- 225/3 Bar, Rod, and Wire
- T3
- T8
PROPERTIES Area Sq. in.
Thickness inch O. 125 to 1, 500 1.501 to 2.000 2.001 to 3.000 O. 125 to 3.250
70
Other(l) 0.05 0.15
- minipum Tensile ksi
Str
Yield Str kc i
EL %
-
45
38
10
-
43
34
12
-
42
30
14
-.
52
40
10
each total
Downloaded from http://www.everyspec.com
MlL4iDBK=694AlMRJ 15 December 1966 ..
CHEMICAL Specification AU-see
below
Cu 3.95.0
Si
Fe
0.501.2
1.0
COMPOSITION
Mg
Z.
Mn
Ti
c?
0.200,8
0.25
0.401.2
0.15
0.10
MECS-LANICAL Designation Specification QQ-A- 200/2 Bar, Rod, Shapes, and Tube, Extruded
PROPERTIES
Thickness inch
Area Sq, in.
Tensile ks i
-o
All
All
-T4, -T451O, -T4511
All
- T42
Ml
-Tb, -T651O, -T6511
up to 0,499 0.,00. 0.749 0.750 & over 0.750 & over
}.poYo( 3) -T451
0.5008.000(
30 max
18 max
12
All
50
35
12
~ A,,
,0
29
12
~ :
;:
:;
Up thru 25 ‘ Over 25 thru 32
68
60
,7
68
58
~6
AU
60
53
7;
Up thru 25 Over 25 thru 32
60
53
7
60
53
35 max
-
12(3)1
55
32
16
55
32
‘ 16
65
55
8
65
55
8
i
-
QQ-A-367 Die Forgings, Heat Treated
Str
;:
‘
6
:,POYO( 3)
-
0, 5oo8.000(3)
-
( 5) 4 max
(4) 55(P)
(19)-(4) 30( P)
\:)
- T4 - T6
4 max
65( P)
55( P)
10
- T6
4 max
64( NP)
56( P)
-T6( I) (7)
6
; ;; k!)
55(L) 55( LT)
-T6( 11)
(7)
-T6(II117)
-T6( IV17)
I I
~n~t~e!’
! ;
upt03X6 the width
0( ST)
55( ST)
6
~ Up to 16. Lengths up to 3x the width
65( L) 6 3( LT) 6O(ST)
55( L) 55( LT) 55( ST)
6
Over 16 to 36. Lengths upto3x the width
65 ( L) 63 ( LT) 60 ( ST)
Over 16 to 36. Lengthe up to 3x the width
65 (L) 63 (LT) 60 (ST)
6
BHN
70
‘
3)
- T6 -T651
each total
EL
up to 8.000
- T4
0.05 0.15
Yield Str ka i
up to 0.749 0.750 & over 0.750 & over
-o
Other(1)
Al Balante
- minimum
Temper
-T62
QQ-A-225/ 4 Bar, Rod, Wi re and-Special Shapes; Rol led, Drawn, or Cold Finished
- De rcent
71
I
53( L) 53(L3 53( ST)
53( L) 53(LT) 53( ST)
100 I 13
125 1125
1 10
I I
6 3 10 4! 2
19 5 2
9 3 2
;
Downloaded from http://www.everyspec.com
MllwBK-694A[MR] 15 bdc~tifbar 1966
.. MECHANICAL Specification
Des ignati on Temper -T6( v)~l
CK3-A-367 Die l?orginga, Heat T~eated (Cont. )
MIL-A-12545 lrnpact Extrusiom
PROPERTIES
Thickness inch (5) 6
I
a-
Over 36 to 144 Lengths up to 3x the width
62(L) 59(LT) 56( ST)
53(L) 52(LT) 52[STJ
7 2.5 1
- T6( VIIP
6
Over 144
60(L) 58(LT) 55( ST)
52(L) 50(LT) 50( ST)
5 2 1
-F -o
30 max
-
55
32
10
100
- T6
65
55
6
125
3.95.0
0.5” 1,2
1.0 max
Cladding
o, 10
0.35-
6003
max
1.0
0.6 max
Fe
Mg
- percent Othera
“ )
Zn
Mrl
Ti
Cr
0. 20-0.8
0.25 max
0.40: 1,2
0!15 max
0,10 max
0,05 each, 0.15 total
0.81.5
0.20 ma x
0.8 max
0.10 max
0.35 max
0.05 each, 0.15 total
MECHANICAL Designation Specification 3 Sheet
COMPOSITION
Al
I
QQ-A-250/ Plate and
BHN
- T4
Si
Remainder
Teneil c Str Yield Str EL kei ks i (4)— - [19) - (4)- + 62(L) 53(L) 3 59(LT) 52(LT) 1 56( ST) 52( ST)
6
Cu
QQ-A-i?5013 Core 2014
Over 36 to 144 Lengths up to 3x the width
( Cent),
-T6(VI)(7)
CHEMICAL Specification
Area Sqo in.
- minimum
Temper
PROPERTIES
Thickneea inch
Area Sq. in.
w
- minimum
EL %
-o
0.020-0.499 0, 500-1. Ooofl 1,
.T3(8)
0.020-0.039 0.040-0.249
.=4(9)
0,020-0.039 0.040-0.249 0.250-0. 49911) 0.500-1. Ood
55 57 57 58
:“ :::-:”;:)11) -.
57 58
-T42(10)
0.250-0.49911) o. 500-i. Ood
57 58
34 34
15 15
- T6
0.020-0.039 0.040-0.499 0.500-1.0007 1! 001-1. 500(11) 1, 501-2.000 2.001-3.000 1
63 64 67 67 65 63
55 ;; 59 59 57
7 8 6 4 3 2
- T65 1
0.250-0.499 0.500-1.0001 1.001-1. 500(11) 1.501-2.000 1 2.001-3,000
64 67 67 65 63
57 59 59 59 57
8 6 4 3 2
-F
All
-T451
I
55 57
- No requirements
72
,
J6 10
35 36
14 15
32 34 36 36
14 15 15 15
~ ;:
I
-
15 15
Downloaded from http://www.everyspec.com
MIL=HDBK=694A[MR] 15 December 1966
CHEM3CAL Specification All - see below
Ctl
Mg
3. 5-4.5
0. 20-0.8
COMPOSITION
Mn 0. 40-1.0
Si
Fe
Zn
Cr
Other(’)
0.8
1.0
0.25
0.10
0.05 each, 0.15 total
MECHANICAL Designation Specification Temper QQ-A-225/ 5 Bar, Rod, and Wire (Rolled or Drawn)
Tnickness inch
1
-o
- percent
PROPERTIES Area Sq. in.
- T4
up to 8.000~’2)
-
55
32
Up to 8.000( ’2)
-
55
32
QQ-A- 367 Forgings, Heat ,Tr’eated
- T4
4 max($)
55(P)(4)
30(19)
QQ-A-430 Rod and Wire for Rivets and Coid Heading
-o
diameter 0.501 and over
-
-H13
Up thru 0,500
-
- T4
0:063-0,615
Specification
Cu
QQ-A-367
3.54.5
Si 0.9
Designation Specification
COMPOSITION
Mn
Mg
1.0
0.20
0, 450.9
QQ-A- 367 Forgings, Heat Treated
-T61
Specification QQ-A-250/
16
12
16(6)
Zn
Area Sq. in.
4 max(’)
-
Cr 0.10
33
Ni
Other(’)
1.72.3
0,05 each, 0, 15 total
Al
Str
Yield Str ksi(j9)
EL
q.
BHN
40(P14’
1d6’
100
55(P)(4)
- percent
Cd
Mn
Cu
Fe
Si
ME
Z.
T]
Othcr( ‘ )
0.91.7
0.100.35
0.300.8
4.05.0
0,40
0.40
0.03
0.25
0.10
0.05 each o,15 total
MECHANICAL
PROPERTIES
Al Balance
- minimum
Area Sq. in.
Thicknena inch
Balance
- minimum Tenailc ksi
COMPOSITION
;6
Li
Designation Specification Temper
100
- percent
0.25
Thickness inch
CHEMICAL
‘
32(19)
PROPERTIES
Tensile kei
Str
EL %
Yield Str ksi 1
QQ-A-250/ 16 Plate and Sheet
-o
0,040-2.000
-
- T6
0.040-0.249 0.250-0.499 0! 500-1.000 1.001-2.000
-
0.250-0.499 0.500-1.000 1.001-1.500 1.501-2.000 2.001-3.000
.
-T651
..-F
All
,
.— 73
BHN
12
30
Fe
Temper
I
35 max 55
MECHANICAL
Shear Str kai
lb
-T451
CHEMICAL
{
EL %
Yield Str kai
35 max
~
Balance
- minimum
Tensile Str ks i
UP to 8.000
Al
~
35 max
-
75. 75
;; 70 70
4 3 2 1.5
57 59 59 59 51
8 6 4 3 2
~;:i
64 :; 65 63
I
- No requirements
\
I -
10
Downloaded from http://www.everyspec.com
Ml14iDBK-694A[MR] 15 December 1966
CHEMICAL Specification All - see below
Cu
Mg
3.8-4.9
1.2-1.8
Mn 0. 30-0.9
COMPOSITION
0.50
MECHANICAL Designation Specification Temper QQ-A - 250/4 Plate and Sheet
Si
Fe
0.50
PROPERTIES
- percent Zn
Cr
0.25
0.10
0.05 each 0, 15 total
Al Balan{
- minimum Tene ile Str ksi
Area Sq. in.
Tbickneea inch
Other(’)
Yield Str ksi
EL ( 16%) 12
-o
0,010-0.499 0.500-1.750
All All
32 max 32 -X
14 max -
-T3(8)
0.008-0.009 0.010-0.020 0.021-0,249
All All All
63 64 64
42 42 42
10 12 15
-T4(13)
0,010-0.020 0,021-0.249 0, 250-0.499 0, 500-1.000 1.001-1.500 1.501-2.000 2.001-3.000
All All All All All AU All
62 62 64 62 1: 56
40 40 40 40 40 40 40
12 15 12 8 7 6 4
0.020-0.062 0.063-0.499 0.500 0,020-0.062 0.063-0.249 0,.250-0.500 0.020-0.062 0.063-0.249 0, 250-0.500 0:063-0.249 0.250-0.499 0.500
- width 30 & under 30 & under 30 & under over 30 thru over 30 thru over 30 thru over 48 thru over 48 thru over 48 thru over 60 rover 60 over 60
69 69 69 69 69 69 67 68 67 67 66 66
52 52 52 52 52 52 50 51 50 50 49 49
8 9 10 8 9 10 8 9 10 8 9 10
62 62 64 62 60 60 56
38 38 30 38 38 38 38
12 15 12 8 7 6 4
64 62 60 60 56
40 40 40 40 40
12 8 7 6 4
-T3fJ14)
-T42(15)
48 48 48 60 60 60
0.010-0.020 0.021-0.249 0.250-0.499 0.500-1.000 1.001-1.500 1,501-2,000 2.001-3.000
All All AH
0.250-0.499 0.500-1.000 1.001 -1.”500 1, 501-2.000 2.001-3,000
All
-T6(15)
0.012-0.499 0.500 & over
AU
64 63
50 50
5 5
-T8~(14)
0.010-0.499” 0.500-1.000
All
67 66
58 58
5 5
.T86(14)
0.020-0.062 0.063-0.249 0,250-0.500 0.020-0.062 0.063-0.249 0.250-0,500 0.ozo-0,062 0.063-0.249 0.250-0.500 0.063-0.249 0.250-0.500
- width 30 & under 30 k under 30 & under over 30 thru over 30 thru over 30 thru over 48 thru over 48 thru over 48 thru over 60 over 60
72 72 72 72 72 71 70 71 70 71 70
66 68 6-1 66 67 66 62 67 65 2:
3 4 4 3 4 4 3 4 4 4 4
0.250-0.499 0.500-1.000
AU AU
67 66
58 58
5 5
A31
- No requirements
-T351
-T851 -F
H All All
All All
All
74
48 48 48 60 60 60
-
Downloaded from http://www.everyspec.com
MI1-HDBK=694AIMR) 15 Docellhr
MECHANICAL
DeaignatlOn Specification Ternper 2Q-A- 200/3 Bar, Rod, 3hapea, ! and rube, Ext rbded
PROPERTIES
Thickness Inch
-o
Al 1
Al 1
loll-lax
12
42 44 46
12( 10 for tube’ 12(10 for tube) 10
70
52 ( 48
10
32
68
for tube) 48( 46 for tube )
up to 0.749 O“ 750-1.499 1.500 & over 1.500 & over
Al 1 All Up thru 25 Oter 25 thru 32
57 57 57 57
38 38 38 38
12 10 10 8
-T81,
0.050-0,249
-T8511
1.500 & over
::
56 58 58
4
0.250-1.499
Al 1 All Up thru 32
64
-T851O,
35 max
-
:: 62 66
40 50 58
10 10 5 5
32 max
15 max
-
;: 64 64
42 42 42 42
;O( 18) ,.( 18) , Z( 18)
40 40 40 40
;.(18) ,.(18) , *( 18)
:;;:;:’
:“;;:-:”;;:
>Q-A-225/6 hr, Rbd, nd Wire, 1011ed, Drawn, ,r Gold ~ini8hed
-o - T351 -T4 - T6 -TS51
rW- T-700/3 ‘ube, Round, quare, Rect. ngular, and tier Shapes, *awn, Seam!as
-o
All All Al 1 Up thru 25
inc]
-T3
& over
: !“:!: !i5?:?~Ti 7) Up to 6: 500( 17) 0.500 m 6.500( 17) wall thickness All 0.018-0,024 0.025-0.049 0.050-0.259 0.260-0.500
‘:
.
H
-o
35 max
-
-H13
up thru 0.500
32
-
c.
QQ-A-250/5 Core 2024
3.8-4.9 0,10
Mg
Mn
1. 2-1.8 -
0. 30-0.9 0.05
Designation Temper Specification -o
-d’)
Thickness inch width 0.008-0.009 0.010-0.062 0.063-0.499 0.500-1.750 0.008-0.009 0.010-0.020 0,021-0.062 0.063-0.249
(#
-
- diameter 0,501 & over
Specification
8
5 5
40
0.018 -O.024 0.025-0.049 0.050-0.259 0.250-0.500
- T4
ME C~NICAL
*
::
Over 25 thru
CHEMICAL
QQ-A-250/5 Plate and Sheet
EL %
35 rnax
Up to 0.249
-T42
1230
Yield Str ks i
57
.1’4,
1.500
Cladding
( Cont. )
Tensile St r ka i
Area Sq. in.
1. 500-& ”Over
Q-A-430 Od and Wire; or Rivets and old Heading
- minimum
1986
64 64
COMPOSITION
- percent
Fe
Si
Cr
Zn
0.5
0.50
0,10
0.25
FekSi
0.7
PROPERTIES
-
0.05 each 0.15 total 0.05 each
0.10
Al Balance 99.3 mln
- minimum
Area Sq. in.
Tensile ksi
All All All All
30 30 32 32
All All All All
58 59 59 62
75
Others(])
max max max max
Str
Yield Str ks i
EL 76
14 max 14 max 14 max
10 12 12 12
39 39 39 40
10 12 15 15
Downloaded from http://www.everyspec.com
M11=HBBK=694A[MR] 15 December 1966
MECHANICAL
PROPERTIES
- minimum
( Cont. )
.—
I
Decimation SpecificationTemper QQ-A-250/5 Plate and Sheet ( Cent)
Area Sq. in.
Thickness inch
-T4(13)
0,010-0.020 0.021-0.062 0,063-0.128 0,250-0.499 0,500-1. 000( 1.001-1.500( 1.50i-z. 000( 2.001-3.000(
-T36( 14)
0.020-0.062 0.063-0.499 0.500(11) 0.020-0.062 0.063-0, 499 0.500(11) 0.063-0.499 0.500(11)
.T42(15)
0,008-0.009 0.010-0.020 0,021-0.062 0.063-0.249 0.250-0.499 0,500.1.000(11) 1.001-1.500(11) 1.50 J-2.000(1’) 2.001-3.000(1’)
All AH All All All All All All
~:;;:;:;~[j;] /
Str
Yield ksi
Str
EL ?’0
58 58 61 62 62 60 60 56
37 37 38 40 40 40 40 40
12 15 15 12 8 7 6 4
62 66 69 61 65 67 64 66
48 50 52 47 49 50 48 49
8 9 10 8 9 10 9 10
AU All All All All All All All All
55 56 56 59 62 62 60 60 56
34 34 34 36 38 38 38 38 38
10 12 15 15 12 8 7 6 4
All All All All All
62 62 60 60 56
40 40 40 40 40
J2 8 7 6 4
48 and under 48 and under 48 and under over 48 thru 60 over 48 thru 60 over 48 thru 60 over 60 over 60
- T351
1:501=2:000(11 2.001-3,000(11
Teneile ks i
-T6(I
)
0.010-0.062 0.063-0,499
All All
60 62
47 49
5 5
-T8J(
4)
0.010-0.062 0.063-0.499 0,500-1.000(1
All All All
;: 66
54 56 58
5 5 5
30 and under 30 and under 30 and under 30 and under over 30 thru over 30 thru over 30 thru over 30 thru over 48 thru over 48 thru over 48 thru over 48 thru over 60 over 60 over 60
66 70 70 72 66 70 69 71 64 69 68 70 69 68 70
62 66 65 67
:: 63 65 64 62 64
3 4 4 4 3 4 4 4 3 4 4 4 4 4 4
56 58
5 5
-T86(
-T851 -F
4)
0,020-0.062 0.063-0.249 0,250-0.499 0.500(11) 0,020-0,062 0.063-0.249 0.2’50-0.499 0,500(11) 0.020-0.062 0.063-0.249 0.250-0.499 0, 500(11) 0.063-0.249 0.250-0.499 0,500(11)
)
48 48 48 48 60 60 60 60
:; 64 66
0.250-0.499 0.500-1.000(1’)
All AU
65 66
All
All
- No requirements
76
-
Downloaded from http://www.everyspec.com
15 Docomhir
CHEMICAL Specification QQ-A- 367
Si
Cu
Fe
j 3.9-5 .0j0,50-1,2:1.
I
I
.
O I
COMPOSITION
Mn . . .. 0. 40-1.2
MECHANICAL
Mg
Zn
Cr
0.25
0.10
I
Area
Ti
Other(’) 0,05
i
Tensile
Cu
Specification QQ-A-430
2. 2-3.0
“-”--$:’-
12’-’”2
CHEMICAL
COMPOSITION
Mn 0.20
Mg 0.20-0.50
J
Yield Str(’9)
Str
MECHANICAL Deslgnaticm Temper Speclflcation QQ-A-430 Rod and Wire; for R]vets and Cold Head,ng
‘$+’
Si
Fe
0.8
1!0
PROPERTIES
“i
and over
EL 16(6) %
- percent Cr
Zn
0.10
0.25
Others(’) 0.05 0.15
each total
Al Balance
- mlnlmum
Area Sq, m,
Diameter
I
- minimum
33(P)(4) =-
Al Balance
each 0, 15 total
0.15
I
PROPERTIES
Thickness
Designation
- percent
0.05
I
1
196ti
Tensile ks]
-o
0.501
-
25 max
-H15
Up thru O. 500
-
28
-T4
0.063-0,615
-
38
Str
Yield Str kn >
EL %
Shear Str kai
418
18
26
,: Em I
CHEMICAL Specification
Cu
QQ-A- 361
3. 5-4.5
COMPOSITION
Si
Fe
Mn
Mg
0.9
1.0
0.20
1. 2-1.8
- percent
Zn X25
I
Cr
Ti
0.10
-
— MECHAMCAL
PROPERTIES
Other~’)
N] 1. 7-2.3
0.05 each 0, 15 total
—..
- minimum .——
Specification
Temper
QQ-A - 367
-Tbl
Forgings, Heat Treated
Area
Thickness
Designation
‘
inch 4(5)
Sq. in. 1 1-
Tensile ksi 55(P)(4)
Str
Yield Str(’9) ksi 40(P)(4)
EL %
Bf-2N
10(6)
100
Al Balance
Downloaded from http://www.everyspec.com
Mll+iDBK=694A[MR] 15 December 1966 —
CHEMICAL Specification QQ-A- 361 a - Vanadium
I
Gu
Si 0, 20
5.8-6.8 O. 05-0.15
Fe 0.30
COMPOSITION
Mn 0.20-0.40
and Zirconium
- T6
Zn
Cr
0.10
-
PROPERTIES
Tbicknecs inch
- T6
QQ-A - 367 Forgings, Heat Treated
Mg 0.02
(4, 19) Tensile Str ks i
Area Sq. in.
Al Balance
yield
s{:.
19)
EL
kai
%
.
58( P)
38(P)
-
58( NP)
38(NP)
58( L) 55(LT) 53( ST)
40( L) 37( LT) 35( ST)
6 4 2
61(L) 58(LT) 56( ST)
43(L) 40( LT) 38( ST)
6 4 2
65( L) ;:;;L;
47(L) 44( LT) 40( ST)
6 4 2
.
CHEMICAL
COMPOSITION
c.
Si
Fe
Mn
Mg
Zn
Cr
Ti
Ni
1.9-2.7
0.25
0.9-1.3
-
1. 3-1.8
-
-
0.04-0.10
0. 9-1.2
PROPERTIES
Other(l) 0.05 each 0.15 tobl
- minimum
Area Sq. in.
J6)
I
QQ-A- 367
MECHANICAL
~(6)
- percent
Specification
rensile Str(4, ‘9) ksi
-T61
4(5}
58(P)
48(P)
-T61
4(5} ‘
55(NP)
45(NP)
4(6)
-T61 (Clase
I)
-T61 (Class
13)
-T61 (Class
III)
——
4(5, 20)
16 and under
58(L) 55(LT) 52(ST)
48(L) 45(LT) 42( ST)
7 5 4
4(5, 20)
Over 16 to 36
57(L) 55(LT) 52(ST)
47( L) 45(LT) 42(ST)
7 5 4
4(5, 20)
Over 36 to 144
56( L) 53(LT) 51( ST)
46(L) 40(LT) 39( ST)
7 4 4 .
78
Al Balance
— Yield Str(4,19) ksi
EL % — 6(6)
Thicknes] inch
Designation Temper Specification QQ-A-367 Forgings, Heat Treated
‘a
0.05 each 0.15 total
4(5)
~(5, 20)
-T’87
Oier(l
4(5)
4(5, 20)
-T852
-
- minimum
4(5, 20)
- T6
Ni
Ti 0.02-0.10
O. 10-0.25
MECHANICAL Designation Temper Specification
- percent
BHN 115
I
Downloaded from http://www.everyspec.com
MlLJmBK=694A[MRj 15 December 1966
CHEMICAL Specification
Fe
Mn
All - see below
1.0-1.5
0.7
QQ-A-250t 2 Plate and Sheet
Temper
-o
-H12 or -H22
-H14 or -H24
-H16 or -H26
-H18 or -H28
QQ-A-20011 Bar, Rod,
and Tube truded
QQ-A-22512
Zn
c. 0.20
0.6
0.10
PROPERTIES
Thickne8s inch
Area Sq. in.
0,006-0.007 0.008-0.012 0.013-0.031 0.032-0.050 0.051-0.249 0.250-3.000
-
0.017-0,019” 0.020-0,031 0.032-0.050 0.051-0. 113 0.114-0.161 0.162-0.249 0.250-0.499 0.500-2.000
-
-
0,009-0.012 0.013-0.019 0.020-0.031 0.032-0.050 0.051-0.113 0.114-0.161 0.162-0.249 0.250-0.499 0.500-1.000
-
-
0,006-0,019 0.020-0.031 0.032-0.050 0.051-0.128
Al
each total
Balance
- minimum Tensile ksi
Str
Yield Str ksi
(16) 14 18 20 23 25 23
14 14 14 14 14 14
3 4
17 17 17 17 17 17 17 17
: 7 8 9 10 1 2 3 4
-
1 2 3 4
-
27 27 27 27
; 3 4
17 15 1..
8 12 18
-
-F
O, 250-6.
-
No requirements
All
19 max
All
14
-F
All
- No requirements
-o
- diameter All sizes
-H, lz
EL %
24 24 24 24
-
0.250-0.4$’9 0.500-2.000 2.001-3.000 OUO
tier(’) 0.05 0.15
: 7 8 10
: -
0,006-0.019 0.020-0.031 0.032-0,050 0.051-0, 162
- percent
20 20 20 20 20 20 20 20 20
-
-HI 12
-o
Shapes, Ex-
,
Si
MECHANICAL Designation Specification
COMPOSITION
25
-
15 max
25
14
-H12
up to 0.374
-H14
up to 0.374
16
-H16
up to 0.374
19
-H18
up to 0.374
22
-HI 12
All e izee
11
-
Downloaded from http://www.everyspec.com
MI1-HDBK=694A[MRJ 15 December 1966 —MECHANICAL PROPERTIES Specification
I
WW-T-700/2 Tube, Round, Square,. Rec. tangular, and Other Shaper., Drawn, Seamleas
Temper
-H12
Al 1
-H14
Ail
20
-H16
All
24
-H18
All
Si
0.50- 1.3
11.0 -13.5
COMPOSITION
1-
- percent
4
Mg
Zn
Cr
Ti
-
0.8-1.3
0.25
0.{0
-
1.0
PROPERTIES
Ni
Al
Other(’)
0. 50-1.3
0.05 each o.15t0tal
Balance
- minimum
Area Sq. in.
Thickness inch
Tensile koj
4(5)
- T’b
27”
Mn
MECHANICAL
QQ-A- 367 Forgings,
19rnflx
I
Fe
Designation Temper Specification
I
17
CHEMICAL
QQ-A-367
ka i
- wall thickness All
Cu
EL %
Yieid Str
-o
r Specification
- minimum (Cont. )
Thickness inch
Designation
Str
52( Pf14)
Yield
Str kni
(19)
EL BHN
% 5(6)
42(P)(4)
115
Heat Treated
CHEMfCAL Specification AU- sec
below
Mg
Fe
COMPOSITION
Si
0.45
2,2-2,8
I
&
Cr
0.15-0.35
MECHANICAL
I
Designation Srrecification ‘3’emDer
I
QQ-A-250/8 Plate and Sheet
-H32 -H22
or
M.
Z.
0.10
0.10
0.10
PROPERTIES
Thickneae
inch 0,006-0.007 0,008-0.019 0,020-0,031 0.032-0.249 0.250-3.000
-o
- percent Cu
Arc& Sq. in.
- n~inilttum
Others 0.05 each O. 15 total
Ai
Salance
.—— YIt,lrl Str hill -—. —
EL ‘%
(lb) .. 15 18 20 la
0.017-0.019 0.020-0.050 0,051-0.113 0.114-0.249 0, 250-0.499 0, 500-2.000
; 11 12
4 5
-H34 -H24
or
0,009-0.019 0.020-0.050 0.051-0.113 0.114-0,249 0.250-1.000
3 4 6 7 10
-H36 -H26
or
0.006-0,007 0,008-0.031 0,032-0.162
-. 3 4
Downloaded from http://www.everyspec.com
MIL=HDBK=694A[MR] 15 December1966
MECHANICAL Des ignation Specification Ternper QQ-A-25018 Plate and Sheet (Cent )
QQ-A-22517 Bar, Rod, and Wire; Rolled, Drawn, or Cold Fimshed
WW-T-700/4 Tube, Round, Square, Rectanguiar, and Other Shapes, Drawn, Seamless
-—
QQ-A-430 Rod and Wire; For Rivets and Cold Heading
PROPERTIES
QQ-A-430
)
Area Sq. in.
Tensile ksi
-H38 or -1-128
0.006-0.007 0.008-0.031 0.032-0.128
-
39 39 39
EL Yo -3 4
-HI 12
0.250-0.499 0.500-2.000 2.001-3,000
-
28 25 25
7 12 16
-
- No requirements
-F
0.250-6.000
-0
- diameter All sizes
-H32
up
-H34
up
,-
Yield Str ksi
Str
-
32 max
(2) 25
to 0.374
31
--
to o, 374
34
--
-
-1-136
up
to 0.374
37
--
-H38
up to 0.374
39
--
-o
wall thickness All
-H32
All
31
-H34
“All
34
35 max
-H36
All
37
-H38
All
39
-F
All
- No requir ements
-o
- diameter 0. 501 and over
-
32 max
-H32
Up thru O. 500
-
31
Mn
Mg 4. 5-5.6
0,05-0,20
Designation Temper Specification %-o - H32
COMPOSITION
Cr
c.
0.05-0.20
MECHANICAL
QQ-A-430 Rod and Wire; For Rivets and Cold Heading
( Cont.
Thickness inch
CHEMICAL Specification
- minimum
0.10
Thickness inch
- percent
S1
Fe
Zn
Ti
0.30
0.40
0.10
-
PROPERTIES Area Sq. in.
Tensile kei
-
46 max
Up thru O. 500
-
44
81
Others(’) 0,05 0.15
each
Al Balance
total
- minimum
- diameter 0,501 and over
*
-
Str
Yield Str kei
EL %
Downloaded from http://www.everyspec.com
MI1-HD6K 694A[MR] 15 Decembe
1966 - —.—
-“
CHEMICAL Specification
COMPOSITION
- percent
Si
Fe
Cu
Mg
Cr
Zn
*i
Ni
QQ-A-250/ 6 md QQ-A-200/4
0.40
0.40
0.10
0.30- 1.0
4.0-4.9
0.05-0.25
0.25
0.15
-
0.05 each o.15 total
Balance
DQ-A-367
0.40
0.40
0.10
0. 30-1.0
4.0-4.9
-
0.25
-
-
0,05 each 0.15 total
Balance
PROPERTIES
- minimum
Mn
MECHANICAL Designation Specification Temper QQ-A-250/6 Plate and Sheet
Q~A-200/
Bar, Rod, Shape*; and Tube,
Yield Str ke i
Tensile Str kai
Area
Sq. in.
Al
EL
%
0,051-1,500
-
40
18
(16) 16
1.501-3.000
-
39
17
16
- H32
0,051-0.125 0.126-0.249
-
45 45
34 34
8 10
-H34
0.051-0,125 0.126-0,”249
-
50 50
39 39
6 8
-H113
0, 188-2.000
-
-o
Upthru
-Hill
Up thru 5.000
-o
4
Thickness inch
Other(’)
5.000
44
31
12
Up tbru 32
39
16
14
Up tttru 32
40
24
12
Extruded QQ-A- 367 Forgings,
-Hill
-H112
Heat
Treated
-Hill -H112
(4-19) 42(P)
w
;12K:;
;
-H112 .
CHEMICAL Specification
Si
Fe
Gu
Mn
0,40
0.50
0.10
0.7
1.
I I
COMPOSITION
MECHANICAL Deaigna SDecificatiOn QQ-A-250/7 Plate and Sheet
on
Temper
jtl
40(P)
-23111
All - see below
(4-19) ;;~P/
Mg 3.5-4.5
22(NP) la(m)
14(6) lb(b)
42(L) 39(LT)
22( L) 20(LT)
16 14
40(L) 39(LT)
18(L) 16(LT)
16 14
- percent Cr
Ti
0.05-0.25
0.15
PROPERTIES
Thickness inch
42(NP) 40(NP)
Area Sq. in,
Zn
Others(l)
0.25
M
0.05 ~aeh 0.15 total
Balance
1 minimum Tensile Str ksi
Yield Str ksi
EL %
-o
0.020-0.050 0.051-0.249 0,250-2.000
35 35 35
14 14 14
(16) 15 18 14
-H32
0,020-0,050 0.051-0.249 0.250-2,000
40 40 40
28 28 28
6 8 12
-H34
0.020-0.050 0.051-0.249 0.250-2.000
44 44 44
34 34 34
f? 10
.
-,H36
0,020-0.050 0.051-0.162
47 47
38 38
4 6
-H112
0.188-0, 499 0.500-1.000 1,001-2.000 2.001-3.000
36 35 35 34
18 16 14 14
8 10 14
82
14
Downloaded from http://www.everyspec.com
MIL-HIIBK-694A[MR) 15 December 1966 .—
MECHANICAL Designation Specification Temper
PROPERTIES
‘Thickness inch
- minimum
Area Sq. in.
(Cont.
Tensile ksi
)
Str
Yield Str kai
EL %
QQ-A-200/5 Bar, Rods, S~apes, and Tube Extruded
-o
Up thru 5.000
Up thru 32
35 max
14
14
-Hill
Up thru 5.000
Up thru 32
3b
21
12
WW-T-700/5 Tube, Round, Squqre, Rec tangular, and Other Shapes, Drawn, Seamless
-0
All
35
14
14
-H32
0,010-0.050 0.051-0,450
-
40 40
28 28
6 8
-H34
0.010-0.050 0.051-0.450
-
44 44
34 34
5 6
-H36
0.010-0.050 0.051-0.450
-
47 47
38 38
4 5
-F
- No requirements
-
-wall
thicknesss]zes
mm At
CHEMICAL Cr
Mn
Ti
Cu
Zn
2. 4-3.0
0.05-0.20
0. 50-1.0
0.20
0.10
0.25
MECHANICAL Desiimation SpecificatiOnQQ-A-250/:o Plate and Sheet
—
QQ-A-ZOOJ6 Bar, Rod, Shapes, and Tube, Ex truded
PROPERTIES
Thickness Tempt r -o
... —.
inch
—.—
—
Fe & S1 Other 0.50
Balance
- minimum
Area Sq. in.
Tensile ksi
Str
Yield Str ksi
.—
31 31 31 31
12 12 12 12
-H32
0.020-0.050 0,051-0.249 0.250-2.000
36 36 36
26 26 26
- H34
0.020-0.050 0.051-0.161 0, 162-0.249 0.250-1, 000
39 39 39 39
29 29 29 29
32 12 31
18 11
0.250-0.499 0, 500-2.000 2.001-3.000
—— *,
(l)”-
0.05 each 0. 15 total
0.020-0.031 0.032-0.050 0.051-0.113 0.114-3.000
-H112
I
- percent
Mg
Specification All - nee below
COMPOSITION
31
12 T
—-—
EL 74
I (16) iz I
14 16 1s
I ~ 11 {
; 7
10 8
11 15
-o
Up thru 5.000
Up thru 32
41
-Hill
Up thru 5.000
Up thru 32
42
26
12
-H112
Up thru 5.000
Up thru 32
41
19
12
I
—.
+
14
Downloaded from http://www.everyspec.com
MI1-HINIK-694A[MR) 15 December 1966
CHEMICAL COMPOSITION - percent Mg
Specification
Cr
4.7-5.5
All - aee below
Ti
Mn
0. 50-1.0
0,05-0.20
0.20
Gu
Zn
0.10
0.25
MECHANICAL PROPERTIES
- minimum
0.051-1.500 1,501-3.000 3.001-5.000 5.001-7.000 7,001-8,000
42 41 40 39 38
19 18
. H24
0,051-0.249
51
39
9
-H112
0.250-1.500 1,501-3.000
42 41
19 18
12 12
-H321
0.051-0,624 0.625-1, 250 J.2S)-1 ,500 1.501-3.000
46 46 44 41
33 33 31 29
12 12 12 12
-H323
0.051-0.125 0.126-0.249
46 48
36 36
6 8
-H343
0.051-0,125 0.126-0.249
53 53
41 41
6 8
-o
Up thru
5.000
Up thru
32
31
12
14
-Hill
Up thr.
5.000
Up thru
32
33
19
)2
-H112
Up thru
5.000
Up thru 32
31
12
12
QQ-A- 250/9 Plate and Sheet
-o
Mg
Si
0. 6-1.2
0. 6-1.2
Cu 0. 40-0.9
Araa Sq. in.
Thickness inch
CHEMICAL
MIL-A-12545
COMPOSITION Mn
Zn
Fe
Ti
0.8
1.5
1.0
0.20
Thickness
Area
inch
Sq. in,
(16) 16
16 14 14 12
16
15
- percent
MECHANICAL PROPERTIES Designation Temper Specification
EL %
17
Cr
Ni
Others(’)
Al
0.30
0.20
0, 05 each 0.15 total
Balance
,
i
Balance
Yield Str kei
Temper
Specification
Al
0.05 each .15 total
0.40
Tensile Str ksi
Designation
Spticif ication
E
Fe& Si others(’)
1
t
- minimum Tensile
Str
Yield Str
EL
ksi
ksi
%
BH N
MJL-A-12545
-F
35
32
3
70
1 m~act
- T6
50
42
7
95
Ex-
b CHEMICAL Specification
Si
Fe
QO-A-430
-a-
0.35
a - 45 to 65 percent
1
of magneaium
w +2”5
-
percent
Cu
Mn
Mg
0.10
-
1. 1-1.4
0.15-0.35
PROPERTIES
- minimum
Zn
Ti
Othere( 1)
Al
0, 10
-
0.05 each 0.15 total
Balance
Cr
I
content.
MECHANICAL Designation
COMPOSITION
Area Sq. in.
Thickness inch - diameter 0.501 and over
, -
Up thru O. 500
I
0.063-0.615
1-
-
84
I
Tensile ksi
I
19 max
[
30
1191
Str
I
I I
Yield Str kni
-120
EL 70
i I
14
Downloaded from http://www.everyspec.com
MIL-HDBK-694A[MR] 15 December 1966
CHEMICAL Mg
Specification All . aee
below
0.8-1.2
Si
0.15-0.35
MECHANICAL
QQ-A-250/11 Plate and Sheet
-o
- T4
and
‘Ube’
‘Xtruded
QQ-A.22518 Bar, Rod, Wire and Special 6hapeo; Rolled,
WW-T-70016 Tube, Round,
Square, Rectangular, and Other .!%apen, Drawn, Seam Iese
0.15
PROPERTIES Area Sq. in.
Thickneaa inch
0.010-0,020 0.021-0.128 0.129-0.499 0.500-1.000 1.001-3.000
- minimu Tensile ksi
-
0.010-0.020 0,021-0.249 0,250-1,000 1.001-3.000
.
EL % (16) 14 16 18’ 18 16
30 30 30 30
:: 16 16
16 18 16
30 30
16 16
18 16
max max max ma.x max
14
0.010-0.020 0.021-0.499 0.500-1.000 1.001-2.000 2.001-3.000 3.001-4.000 4.001-5.000
42 42 42 42 42 42 40
35 35 35 35 35 35 35
8 10 9 8 6 6 6
-T651
0,250-0.499 0.500-1.000 1.001-2.000 2,001-3.000 3, 001-4, 000 4, 001-5.000
42 42 42 42 42 40
35 35 35 35 35 35
10 9
D. 250-6,
-
-
000
-o
22 ma.
-T4, -T451O, -T451 1
26
16
-T6, -T651O, -T6511
38
{
18
4L
!5
10
4L
!5
10
22 ma.
14max
-
-t-
(18) 15
- T4
).025 }. 050 1,260
to 0,049 to 0,259 to O. 500
30 30 30
16 16 16
14 16 18
-T6
1.025 1.050 1.260
to 0,049 to 0.259 to 0.500
42 42 42
35 35 35
8 10 12
I
Others
(1)
0.05 each 0, 15 total
*1 Balance
. Yield Stl ka i
Str (19)
12 max 12 max 12 max .. .
22 22 22 22 22
.
0.25
0.15
-T6
--L Drawn or Cold Finished
0.15-0.40
2n
Mn
0.250-1.000 1.001-3.000
-F
Shapes,
Ti
-T451 I
00-A-200/8 Bar, Rod,
0.7
- percent Gu
Fe
Gr
0. 40-0.8
Deaignaticm SDeciflcation lTemper
COMPOSITION
-
BHN
Shear ksi
Str
Downloaded from http://www.everyspec.com
MIL-HDBK-694A[MR] 15 December 1966
-
id
Designation 1Temper Specification
XUNICAL
PR(
Thickness Inch
PERTIES Area ~q. in.
I QQ-A-367
rensile Str ksi
I Cont.
)
Yield Str ka i
I -1-b
4(5)
(4) 38(P)
(4) 35(P)
. Tb
4(5)
38(NP)
35(NP]
I -T’6
up
38(L) 38(LT) 37(ST) 37(L)” 37(LT) 35( ST)
35(L) 35(LT) 33(ST) 34(L) 34(LT) 32( ST)
Forgings, Heat Treated
up to 144
to 4
I Over
4 10 M
Up to 256
--——— QQ-A-430 Rod and W Ire; For Rivets and Cold Heading
- minimum
-0 -H)J - T6
- d]ameter 0. 501 and Up lhru
ovc
EL %
9HN
IO(6I
80
5(6)
80
Shear Str ksi
10 .8 5 : 4
22 max 22
O. 500
42
0.063-0.615
86
35
10
25
Downloaded from http://www.everyspec.com
MIL=HDBK=694A[MR] 15 December 1966 ..
CHEMICAL COMPOSITION - percent Specification
Si
Mg 0.45-0.9
QQ-A-ZOO19
0.20-
0.6
Fe
Cu
Ti
0.35
0.10
0.10
Mn 0.10
Zn
Cr
0.10
0.10
others(’) 0.05
Al
Balance
each
0.15 total ROPERTIES
MECHANICAL
Designation Specification ITempe r
Thickness inch
-o OGA-2oO19 Bar, Rod. Shapes, - T* and Tube, Extruded - T42
in.
Str
Yield Str ksi
I i
EL
I
18
I
14 14
%
All
19 max
Up thru O. 500 0.501-1.000
19 18
10
Up thru O. 500 0.501-1.000
17 16
9 8
- T5
Up thru O. 500 0,501-1,000
22 21
16 15
8 8
- T6
UPthrtr O. 124 0.125-1.000
30 30
25 26
a 10
Si
Mg
specification below
Tens ile ks i
Area
Sq.
CHEM3CAL
Ml - see
- minimum
0. 9-1.8
0.8-1,4
COMPOSITION Mn
Cu
0. 6-1,1
0.7-1.2
MECHANICAL PROPERTIES , Th)cknearn
De mignation Temper
QQ-A-200/10 Bar, Rod, Shapes, and Tube Extruded
-o -=4 .T4~*o .T4~J]
Cr
Fe
0.40
0,50
Tensile Str ks ]
in.
-
Al
0.05 0.15
each
Balance
total
Y]eld Str ksl
EL %
29 max
18 max
16
40
25
14
40
24
14
-
50
45
8
BHN
‘
4(5)
T6
0.20
-
-T62 QQ-A-367
Others
Ti
al
0,25
- mimmum
-T42 -T6, -T651O, -T6511
12 12
- percent
Area Sq.
mch
SpecificattOn
9
50
42
50(P)(4)
45(P)(4)
8 ]2(6)
100
Forgings, Heat Treated
CHEMl CAL COMPOSI T1ON - percent Cu
Specification All
- see
0.35
below
Si 0,6-1.2
Fe
1.0
MECHANICAL Denigration Specification
QQ-A-367 Forgingo, Heat Treated
Temper
Thicknes~ inch
Mn 0.20
Mg 0.45-0.8
PROPERTIES Area Sq. in.
Zn
Cr
0.25
0.15-0.35
Ti 0.15
Others 0.05 0.15
Al
each total
Balance
- mirnmum Tensile ka>
Str
Yield Str ka I
EL % (:J
-T6
(5) 4
(4) 44(P)
(4) 37(P)
- T6
4
44(NP)
37(NP)
L4
37
BHN
90 6
90
10
90
●
MIL-A.12545 Impact Extrtmionc
- T6
87
Downloaded from http://www.everyspec.com
M11=HDBK9694A[MR] 15 December 1966
CHEMICAL Mg
Zn
Specification
5. 1-6.1
All - see below
2. 1-2.9
QQ-A-250112 Plate and 5heet
2Q-A-200/Jl Bar, Rod, ;hapea, and hbe, Ex,rudecl
Thickness inch 0.015-0.499 0.500-2.000
-o -T6
0.015-0.039 0.040-0.499 0.500-1.000 1.001-2, 000 ,2.001-2.500 2.501-3, 000 3.001-3.500 3.501-4.000
-T651
0.250-0.499 0.500-1.000 1.001-2.000 2, 001-2.500 2.501-3.000 3.001-3,500 3.501-4.000
Cr
1.2-2.0
MECHANICAL. Designation specification Temper
COMPOSITION
Gu
0,.18-0.40
PROPERTIES Area Sq, in,
Fe
Si
0.30
0,7
0,50
.
Othero(’) 0.05 each 0, 15 total
Str
Yield Str ka i
EL %
21 max -
76 77 77 77 73 70
65 66 66 66 62 60
R
2;
: 4 3 3 3 2
77 77 77 73 70 70 67
66 66 66 62 60 57 53
8 6 4 3 3 3 2
7
All
- No requir ements
All sizes
40 max
24 ma%
-T6, -T651O, -T651 1
up to 0,250 0.500 3.000
78 81 81
70 73 72
7 7 7
Up to 20 sq, in. Over 20 to 32
81 78
71 70
7 6
&oT”tO 5.000 Up to 32 sq. in,
76
68
6
(2)
f~)
-0
Bar, Rod, wire, and
- T6
up
-T651 special jhapes: Roll Cd >rawn, or Cold Finiehed
to 2.999
10
to 4.499
40 max
-
up to 4.000
77
66
7
0, 500 to 4, 000
77
66
7
to 8.000
- T6
3
(19,4) 75(P)
(19,4) 65(P)
- T6
3
71(NP)
62(NP)
3(7)
- T6 (class
3
Up t: 16 Lengths up to 3 Y.. the width
75(L) 75(LT) 72( ST)
64(L) 63(LT) 63(ST)
: 2
Up to 16 Lengths over 3 times the width
75(JJ 73(LT) 70(ST)
63(L) 61 (LT) 61(ST)
9 4 2
61(L) 60(LT) 60(ST)
7
60(L) 59(LT) 59( ST)
7 3 2
(5)
1)
BHN
(16) 10 10
40 max 40” max
-F
0Q-A-367 Forgings, -teat rreated
- percent Mn
]o(6)
;
135 135
Shear St! koi
Downloaded from http://www.everyspec.com
MI1=HDBK-694A[MR] 15 December 1966
Blmn MECHANICAL
- T6
-T6 (Class VI)
[ Cent)
Tensile ksi
4
69(LT) 66(ST)
59( L) 57(LT) 57(ST)
2 1
70(L) 67(LT) 64( ST)
58(L) 56(LT) 56(ST)
4 2 1
65
5
66
7
3
Over 36 to 144 Lengths up to 3 times the width
71(L)
66(ST)
to 256
EL q,
Stz
4 2
71(L) 69(LT)
144
Yield ksi 60(L) 58(LT) 58( ST)
Over 36 to 144 Lengths up to 3 times the width
Over
I
Str
3
(Claaa v)
Treated ( Cent)
- minimum
Area Sq. in.
Thickness inch
Designation Specification [ Temper
QQ-A- 367 Forging s,. Heat
PROPERTIES
BHN
Shear ksi
1
40 max
+ QQ-A-430 Rod and Wire; For Rivets
-0 -H13
Cold
- T6
and
75
I
1
-diamcter0, 501 and over Up thru
135
40 ma. 36
O. 500
77
0.063-0.615
42
Heading
mm CHEMICAL Zn
Specification QQ-A-250/13 Core (7075) Cladding (7072)
5. 1-6.1 0,8
Mg 2. 1-2.9 0, 10
-1.3
COMPOSITION
Cu 1. 2-2.0
Cr 0.18-0.40
0.10
X-L4N2CAL
1-
De.sig
Specification
QQ-A-250/ 13 Plate and Sheet
tion Temper
PRC
Thickness inch
- percent
Mn
Fe
Si
Ti
0.30
0.7
0.50
0.20
0.10
Fe k Si10.7
CR TIES
Area Sq. in.
Others(l)
-
Tensile kai
Str
- T6
0,008-0.011 0.012-0.039 0.040-0.062 0.063-0.187 0.188-0.499 0, 500-1.000 1.001-2.000 2.001-2.500 2.501-3.000 3.001-3.500 3.501-4.000
68 70 72 73 75 77 77 1 73(11) 70 70 67 1
58 60 62 63 64 66
75 77 77
64 66 66 \ 62 60(11)
-3?
0.250-6.000
0.05 0.15
Balance
ksi
36 36 38 39 40
0.250-0.499 0.500-1.000 1.001-2.000 2.001-2.500 2.501-3.000 3.001-3,500 3.501-4.000
Balance
Yield Str
0.008-0,014 0.015-0.062 0.063-0.087 0.188-0.499 0.500-1.000
- T651
0.05 each 0. 15 total each total
minimum
-o
.
Al
max max max max mzx( 11 )
\
,.j I ,.(ll) 70 67
J
20 20 20 21 -
max max max max
)
8 6 4 3 3 3 2
57 53 J
- NO requirements
9 10 10 10 10 5 7 8 8 8 6 4 3 3 3 2
66 1 62(11) 60 57 53
EL %
-
(16)
Str
Downloaded from http://www.everyspec.com
MIL=HDBK=694A[MRJ 15
December 1966
CHEMICAL
2Q-A-250/ 18 Core (7075) Cladding (7072)
Mg
c.
2. 1-2.9
1. 2-2.0
Zn
specification
5. 1-6.1
0.10
0. 8-1.3
COMPOSITION Cr 0.18-0.40
0.10
MECHANICAL Designation Temper Specification -o
QQ-A-250/18 Plate and Sheet
- T6
QQ-A-367
Thickness inch
QQ-A-367 Forgings, Heat Treated L
0.50
0.20
0.10
Fe & SYO.7
Tensile ksi
Si
Fe 0.6
Mn
Thickness inch 4(5)
Yield Str ksi
Balance
EL 70 10
73 74 75 76 77(11) 77(11)
62 64 64 65 66(11) 66(1 1)
7 8 8 8 6 4
76 77(11) 77(11)
65 66(11) 66(11)
8 6 4
requirements
-
- percent
Mg
Zn
Cr
Ti
Ni
7.0-8,0
-
0.20
-
Area Sq, in.
Balance
10 10 10
1.2-2.0
PROPERTIES
each total each total
21 mah 21 max
- No
0. 30-0.8
Al
21 ma>
-
0.40
-
38 ma> 39 max
,-
COMPOSITION
0.05 0.15 0.05 O. 15
Str
062 187 499 000
Others(’)
- minimum
39 ma> 40 ma>
All
-T61
0.7
-
-F
Temper
0.30
Area Sq. in.
MECHANICAL
Specification
Ti
0.188-0.499 0.50 U-1.000 0.015-0.039 0, 040-0, 0.063-0. 0.188-0, 0, 500-1, 1.001-2.000
Designation
Si
-
0.250-0.499 0.500-1,000 1.001-2.000
1,0
Fe
0,015-0.062 .0.063 -0.187
-T651
Cu 0,30-
bin
PROPERTIES
CHEMICAL Specification
- percent
Others(’)
Al
0, 05 each 0, 15 total
Balat]ce
- minimum Ten~ile ksi 70(P) 67(NP)
s:;)
~ic,d
s~:)
ksi 60(P) 5X(NP)
~J()) 70
BHN
1I !
140 1-10
Downloaded from http://www.everyspec.com
MIL-HDBK-694A[MR] 15 December 1966
CHEMICAL specification All - nee below
Mg
Zn 3. 8-4.8
0. 40-0.8
MECHANICAL
QQ-A”-250117 Plate
- T6 -T6 and -T651
-F
-T6 and -T651
0, 10-0.30
0,10-0.25
PROPERTIES
Thickness inch (Long traveree 0.040-0.249
- percent
Area Sq, in,
Tensile ksi
mechanical
properties) 72
Ti 0.10
Str
62
(16) 8
63 63 63 63 62 60 58 5a 57 56
8 8 7 6 6 5 5 5 4 4
0.250-6.000
- No requirements
73 73 73 73 71
capabilities
each total
EL %
:: 68 67 66
(Mechanical 3.001-4.000
Others(’) 0.05 0.15
Yield Str ksi
0.250-1.000 1.001-1.500 1.501-2.000 2. OOJ-2.500 2.501-3.000 3.001-4.000 4, 001-4.500 4.501-5.000 5.001-5, 500 5.501-6.000
:! 68 63 68 63 67 62 66 61
5.001-5.500 5.501-6.000
6 2 6 2 5 2 4 2 4 2
60 56 58 54 58 54 5-I 53 56 52
All
42 tnax
24 max
-T6
Up thru O. 249
Up thru 20
75
67
7
-T6510
0,250-0.499
Up thru 20
77
68
7
.-T6511
0, 500-1.499 1, 500-2.999 3.000-4, 499
‘?8 79 79 77 76 78 76 78 76 76 74
70 70 70 70 68 68
7 7 7 7 7
:: 68 66 64
(22, 4) 72(P)
(19, 4) 62(P)
70(NP) 71(L) 69(LT) 65(ST)
60(NP) 62(L) 58(LT) 54(ST)
4.500-5,
All
000
5, 001-5.999 6.000-6.999
-T6
6(5)
- T6
6(5) UP to 6
BHN
-
-o
Up Up Up Over Over Up Over Up Over Up over
Al Balance
properties)
4.501-5.000
M-A-367 Forgingn, Heat Treated
Si 0.30
- minimum
4.001-4.500
QQ-A-250/12 Plate and Sheet
Fe 0.40
Mn
Cr
c.
2. 9-3.7
Designation Specification Temper
COMPOSITION
thru 20 thru 20 thru 20 20 thru 32 thru thru 38 38 thru thru 38 38 thru thru 50 50 thru
Up to 72(22)
32 50 60 60 60
10
: 6 6 6 4 10(6)
3(6) ; 4
135 135
Downloaded from http://www.everyspec.com
M1l-tlDEIK-694AlMR] 15 December 1966
CHEMICAL Specification
Zn
QQ-A-250/
14
Mg
6. 3-7.3
COMPOSITION Cr
Cu
2.4-3.1
1. 6-2,4
0.18-0.40
MECHANICAL Des ignation Specification 1 Temper QQ-A-250/ Plate and
14 Sheet
~+l.cll)ng
6.3-7,
0.20
0.05 0.15
- minimum
Area Sq. in.
Tensile ksi
.
40 max 40 max
21 max --
83
Str
Yield Str ksi
EL To
(16) 10 10
84 84 84 80
73 73 73 70
8 4 4 3
- No requirements
All
COMPOSITION
Cu 1. 6-2.4
Cr 0.18-0.40
0.10
- percent Mn
Fe
Si
Ti
0.30
0.7
0.50
0.20
0,10
Fe & Si10.7
PROPERTIES
Thickness inch
-
Others(’) 0.05 0.15 0.05 0. 15
-
Area Sq. in.
Tensile ksi
Str
Yield Str ksl
0.015-0,499 0, 500(11)
36 ma-x 40 max
20 max --
-T6
0.015-0,044 0.045-0.499 0.500-1,000(11) 1,001-1.500(11) 1. 501-2.000(11)
: -
76 78 84 84 80
66 68 73 73 70
0.250-0.499 0.500 -1,000(J1) 1.001-1,500(11) 1.501-2,000(11)
: -
78 84 84 80
68 73 73 70
All
- No requirements
92
each total each total
Al Balance Balance
- minimum
-o
-F
Balance
0.250-0.499 0.500-1.000 1.001-1.500 1.501-2,000
0.10
-T651
each
total
7 8 6 4 3
Temper
15
0.50
72 73 73 73 70
Designation
QQ-A-250/
0,7
Al
84 84 84 80
MECHANICAL
Specification
0.30
Other.(’)
0.015-0.044 0,045-0.499 0.500-1.000 1.001-1.500 1.501-2.000
2,4-3,1
0,8-1.3
Ti
- T6
M% 3
Si
0.015-0.499 0.500
CHEMICAL Zn
Fe
PROPERTIES
Thickness inch
-F
>Q-A-250] 15 Core (7178)
Mn
-o
-T651
pacification
- percent
EL % (16) 10 10 7 : 4 3
.
-
8 6 4 3
Downloaded from http://www.everyspec.com
MILHDBK=69411[MR) 15 Decemlter 1966
I
CHEMICAL
CO,MPOSITIOh’
- percent
I
P
‘Specification
Si
AIIL-R-12Z21
Fe
0.50
0.7
c.
Mn
0. 8-1.7
-
Mg
MECHANICAL Designation Temper Specification
Ni
Cr
1 .7-2.3
0.1/+-0.35
-
PROPERTIES
3
Others(’)
0! 10
Al Balance
each 0.15 total
0.05
- m]nirnum
Area Sq. in.
Thickness inch
Ti
Zn 3.7-4.
Tensile ksi
Str
EL
Yield Str ksi
’10
MI L- R-i2221 Ri\.et, Solid, Tempered
CHEMICAL Specification
Sn
MIL-A- 11267
5. 5-7.0
c.
N1
0. 7-1.3
0,20- 0.7
MECHANICAL Designation Temper Specification MIL-A - 11267 Sheet (For Recoil Mechanism Cup Rings)
>-
COMPOSITION
-H12
s]
Fc
Mn
1.0-2.0
0.7
0.10
PROPERTIES
I
- percent Ti
Otherso)
0.10
0,05 each 0. 15 total
~Al
—
B,ila!lce ,
- minimum ~
Thickness inch
Area Sq. in
Tensile ksi In
Str
Yield Str ksi
EL %
15
-1 *
I
Downloaded from http://www.everyspec.com
Downloaded from http://www.everyspec.com
M11=HDBK=694A[MR) 15 December 1966
Biblio~raphy
Only a small are listed
.
in this
number of references, selected from the extensive literature of aluminum metallurgy, bibliography. The object is to provide the designer with citations to the latest availAfew basic papers are included which may be most useful and also readily obtained.
able information together with certain
references
that
1. Alcoa Aluminum
Handbook,
1959, Aluminum
contain
good bibliographies. Company
of America.
2. Alcoa
Aluminum
Impact
3.
Alcoa
Aluminum
in Automatic
4.
Alcoa Structural
5,
“Aluminum
Alloy Castings,
6.
“Aluminum
Alloys
7.
“Aluminum and Aluminum Alloy s,” L.W. Kempf and K.R. Van Horn, American Metals Handbook, 1948, pp. 761-840.
1948, Aluminum
Extrusions,
Handbook,
Screw Machines,
1958, Aluminum Company ” F.A. Lewis,
The Aluminum Data Book,
9.
Aluminum
Extrusionsj
10.
Aluminum
Forming,
11.
Aluminum Heat Treating,
1961, Reynolds
Designing
wi~,
1961, Reynolds
and Methods,
12. The Aluminum Symposium,
1951, Engineer
An Appraisal Construction,
14.
Brazing
Alcoa Aluminum,
15.
Casting
Alcoa Alloys,
16.
“Creep and Stress-Rupture Investigations T. E. Tietz, American Society for Testing
17.
“The Creep Properties Materials, Proceedings,
18.
Cross-index of Chemically Equivalent ferrous Alloys), MIL-HDBK-HI.
58, pp. 484-489. Society
for Metals,
Metals
Company.
Company. Research Alloys
Company
1953, Aluminum Company
and Development for Supersonic
Laboratories,
Aircraft
Fort Belvoir.
and Guided Missile
of America.
of America.
on Some Aiuminum Alloy Sheet Metals, ” J. E. Dorn and Materials, Proceedings, 1949, vol. 49, pp. 815-831.
of Some Forged and Cast Aluminum 1949, vol. 49, pp. %4-976.
Design Details for Aluminum,
vol.
Metal Company.
of the Usefulness of Aluminum 1948, The Rand Corporation. 1959, Aluminum
1950,
Metal Company.
Metals
13.
1948, vol. 27, pp. 89-104.
Metal Progress,
1958, Reynolds
1958, Reynolds
of America.
of America.
Materials
- 1940 to 1950, ” E,H. Dix, Jr.,
8.
19.
Company
1949, Aluminum Company of America.
Specifications
1944, Aluminum
Alloy s,”
American
and Identification
Society
Code (Ferrous
for Testing and Non-
Company of America.
1949 Aluminum
Company of America.
20,
Designing
for Alcoa Die Castings,
21.
Designing
for Alcoa Forgings,
22.
Development 444 National
of Cast Aluminum Alloy for Elevated Advisory Committee for Aeronautics.
23.
Die Casting,
H.H. Doehier,
24.
Effects of Design Details on the Fatigue Strength of 355T6 Sand Cast Aluminum AlioY, 1951, Technical Note No. 2, 394, National Advisory Committee for Aeronautics.
25.
“Effect of Grain Direction 21, pp 126-130.
1950, Aluminum Company of America.
1951, McGraw-Hill
,on Fatigue
Temperature
Service,
1948,
Technical
Note No. 1,
Book Company.
Properties
vol.
95
of Aluminum Alloy s,”
Product
Engineering,
1950,
Downloaded from http://www.everyspec.com
!$
MILHI)BK=694A[MR] 15December 1966 26.
The Elastic Constants of Wrought Aluminum Alloys, Advisory Committee for Aeronautics.
27.
“Engineering for Aluminum-Alloy 1948, VOL 70, pp. 505-514.
Castings,
28.
Fastening
Methods
1951,
‘ 29.
“Fatigue
Properties
.,30,
F~
31,
for Aluminum,
1945, Technical
” T,R. Gauthier
Reynolds
and W.J. Rowe, Mechanical
uieeririg,
,” R, V. Vanden Berg, Product
32,
Forming
33.
High Strength Nonheat-Treated Aluminum Casting American Foundrymen’s Society, Annual Meeting,
Alcoa Aluminum,
Alloys, 1952.
Preprint
‘(Hot Forming Machining
Alcoa Aluminum,
36.
Machining
Aluminum,
37.
Mechanical and Corrosion Tests of Spot-Welded Aluminum Alloys, 538, National Advisory Committee for Aeronautics.
38.
Metals Handbook, for Metals.
39.
“Metals
40.
Review of Information on Mechanical Technical Note No. 2, 082, National
41.
Riveting
42.
Standards
43.
Strength
44.
Alloy s,”
M.P* Meinel, Metals
Vol. 1, 8th edition,
En4neeting,
1951, VOI 23, PP. 163-165.
Company.
Properties
ASME Handbook,
and Selection
1954, American
1951, Technical
of Metals,
Society
Note No. 2,
1961, Americsrr Society
of Mechanical
Engineers.
Properties of Aluminum Alloys at Low Temperatures, Advisory Committee for Aeronautics.
1950,
1954, Aluminum Company of America.
for Wrought Aluminum Mill Products, of Metal Aircraft
Product
No. 52-44, W. Bonsack,
1952, Aluminum Company of America.
1958, Reynolds
Alcoa Aluminum,
1951, vol. 22,
1953, Aluminum Company of America.
35.
Properties,”
1952, vol. 23, pp. 119-U3.
Engineering,
34.
Aluminum
Engineerirr~,
“Metals Company.
of Cast Aluminum ~&q&!! .. .. —.Xlihiinurn;~%2, Reynolds Metals Company.
“Finishes for Aluminum Products pp. 179-186.
Note No. 966, National
Elements,
Bulletin
Third Revision,
1%2, Aluminum Association.
ANC-5, 1951, Munitions
Board Aircraft
Committee.
Stress Rupture and Creep Tests on Alurninum-Alioy Sheet at Elevated Technical Publication 2, 033, Inst. Metals Div. AIMME.
Temperatures,
1946,
45.
hrvey of Available Information on the Behavior of Aircraft Materials Repeaterj Load, Report No. M-653, 1954, War Metallurgy Committee.
and Stmctures
46.
Tensile, deg. F.,
Fatigue, and Creep Properties of For~ed Aluminum 1958, Technical Note No. 1, 469, N afional Advisory
47.
“Tolerances Mechanical
48.
“Trends Progress,
49.
Welding Alcoa Aluminwp,
50.
“Wrought
under
uP to 8°0 for Aeronautics.
A11OYS at Temperatures
Committee
arr~ Specifications for Aluminum and Magnesium Casings, ” W.D. Stewart, Engipeeri~g, 1953, vol. 75, pp. 450-455. in High Strength Wrought Aluminum MIOYS, ” W.B.F. Mackay and R.L. Dowdell, 1949, vol. 56, pp. 331-336, 404, 406.
Metal
1958, Aluminum Company of America.
Aluminum A]]oys, ‘‘ ~. C)’Keefe,
Materials
96
and Methods,
1951, vol. 33, pp. 90-104.
— Downloaded from http://www.everyspec.com
INSTRUCTIONS: submitting
-.
In a continuing
effort to make our standardization
comrnenta and snggeationr for improvemerh
docurnsnti
better, the DoD provides thb form for uae in
AU wan of military atandardizatkm
documents
are invited to provide
_tioM. ~~ form MSY be de~cbed, folded ~ons the lines indicated, taped along the loons edge (DO NOT STAPLE), and mailed. In block 5, be aa specific as pasible about particular problem arena such u wordhg which required interpretation, war too rigid, rwtrictive, loons, ambiguous, or wsa incompatible, and give proposed wording changea wMcb would alleviate the If block 7 is filled out, art problems. Enter in block 6 any remarks not related to a specific paragraph of the document. acknowledgement will be mailed to you within 80 days to let you know thst your “knrnentc were received and are being considered, NOTE: Thin form may not be used to request copies of documents, nor to request waivera, deviati~, specification reqrdrementi on current contmcta. Comments submitted on thie form do not constitute to waive any portion of the referenced document(s) or to amend contractuni requirements.
or clarification of or imply authorization
(Foid don# thb line)
(Fold along thk line) DEPARTMENT
OF THE ARMY
111111 I
OFFICIAL PENALTY
BUSINE~ FOR PRIVATE
USE S3~
u
BUSINESS REPLY MAIL ‘FIRST CLASS
PERMIT NO 12062
WASHINGTON D. C
POSTAGE WILL SE PAID BY THE DEPARTMENT
Director US Army Materials and DRXMR-SSS ATTN : Watertown, MA 02172
Mechanics
OF THE ARMY
Research
Center
NO POSTAGE I NECESS~RY IF MAILEO IN THE UNITEO STATES
Downloaded from http://www.everyspec.com
I
I
STANDARDIZATION DOCUMENT IMPROVEMENT PROPOSAL (See Itswibctwns - ilpwk Side)
I
I
1. DOCUMENT
t
h. NAME OF SUBMITTING
2. DOCUMENT TITLE
NUMBER
L TYPE OF ORGANIZATION
ORGANIZATION
❑
I I I I
D b. ADCtftE&%@tmet, CllY,8tde,ZIPCud4
❑
(Mark one)
vENDOR
USE R
MANUFACTURER
❑
OTHEti ,S@cci,y,:
,,
I
I
5. PROBLEM AREAS a ParograptINurnbor ●nd Wordktg:
I
b. t?ocommondedWordhg:
c. Rmsonllhtlonah
for Rocomrnsndation:
;. REMARKS
to. NAME OF SUBMITTER
&f,
b. WORK TELEPHONE Co&) - Optlonol
Fjmt, Ml) - optl~d
. MAILING AODRESS (Strwr, City, Stotc, ZIP Code) - Optlond
0. DATE OF SUBMISSION (YYMMDD)
1
DD
FORM 82 MAR
1426
PREVIOUS EO1710N IS O~SOLETE.
NUMBER (lneht& Ama