January

MIL-HDBK-5J, Metallic Materials and Elements for Aerospace Vehicle Structures

Last Updated 29 Oct 2026

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1. PDF page 5

Section		Page
Chapter 1
1.0	General	1-1
1.1	Purpose and Use of Document	1-1
	1.1.1 Introduction	1-1
	1.1.2 Scope of Handbook	1-1
1.2	Nomenclature	1-3
	1.2.1 Symbols and Definitions	1-3
	1.2.2 International Systems of Units (SI)	1-3
1.3	Commonly Used Formulas	1-4
	1.3.1 General	1-4
	1.3.2 Simple Unit Stresses	1-4
	1.3.3 Combined Stresses (see Section 1.5.3.5).	1-4
	1.3.4 Deflections (Axial)	1-4
	1.3.5 Deflections (Bending)	1-4
	1.3.6 Deflections (Torsion)	1-5
	1.3.7 Biaxial Elastic Deformation	1-5
	1.3.8 Basic Column Formula	1-5
	1.3.9 Inelastic Stress-Strain Response	1-6
1.4	Basic Principles	1-7
	1.4.1 General	1-7
	1.4.2 Stress	1-8
	1.4.3 Strain	1-8
	1.4.4 Tensile Properties	1-9
	1.4.5 Compressive Properties	1-11
	1.4.6 Shear Properties	1-11
	1.4.7 Bearing Properties	1-12
	1.4.8 Temperature Effects	1-13
	1.4.9 Fatigue Properties	1-14
	1.4.10 Metallurgical Instability	1-17
	1.4.11 Biaxial Properties	1-17
	1.4.12 Fracture Toughness	1-19
	1.4.13 Fatigue-Crack-Propagation	1-24
1.5	Types of Failures	1-28
	1.5.1 General	1-28
	1.5.2 Material Failures	1-28
	1.5.3 Instability Failures	1-29
1.6	Columns	1-30
	1.6.1 General	1-30
	1.6.2 Primary Instability Failures	1-30
	1.6.3 Local Instability Failure	1-30
	1.6.4 Correction of Column Test Results	1-31
1.7	Thin-Walled and Stiffened Thin-Walled Sections	1-40

2. PDF page 6

Section	Page
References	1-41

3. PDF page 6

2.0	Steel	2-1
2.1	General	2-1
	2.1.1 Alloy Index	2-1
	2.1.2 Material Properties	2-2
	2.1.3 Environmental Considerations	2-5
2.2	Carbon Steels	2-6
	2.2.0 Comments on Carbon Steels	2-6
	2.2.1 AISI 1025	2-7
2.3	Low-Alloy Steels (AISI Grades and Proprietary Grades)	2-10
	2.3.0 Comments on Low-Alloy Steels (AISI and Proprietary Grades)	2-10
	2.3.1 Specific Alloys	2-15
2.4	Intermediate Alloy Steels	2-66
	2.4.0 Comments on Intermediate Alloy Steels	2-66
	2.4.1 5Cr-Mo-V	2-66
	2.4.2 9Ni-4C0-0.20C	2-74
	2.4.3 9Ni-4C0-0.30C	2-79
2.5	High-Alloy Steels	2-91
	2.5.0 Comments on High-Alloy Steels	2-91
	2.5.1 18 Ni Maraging Steels	2-93
	2.5.2 AF1410	2-104
	2.5.3 AerMet 100	2-107
2.6	Precipitation and Transformation-Hardening Steels (Stainless)	2-115
	2.6.0 Comments on Precipitation and Transformation-Hardening Steels (Stainless)	2-115
	2.6.1 AM-350	2-115
	2.6.2 AM-355	2-122
	2.6.3 Custom 450	2-128
	2.6.4 Custom 455	2-140
	2.6.5 Custom 465	2-151
	2.6.6 PH13-8Mo	2-157
	2.6.7 15-5PH	2-167
	2.6.8 PH15-7Mo	2-183
	2.6.9 17-4PH	2-195
	2.6.10 17-7PH	2-213
2.7	Austenitic Stainless Steels	2-220
	2.7.0 Comments on Austenitic Stainless Steel	2-220
	2.7.1 AISI 301 and Related 300 Series Stainless Steels	2-222
2.8	Element Properties	2-237
	2.8.1 Beams	2-237
	2.8.2 Columns	2-237
	2.8.3 Torsion	2-240
References		2-246

4. PDF page 7

Section		Page
Chapter 3
3.0	Aluminum	3-1
3.1	General	3-1
	3.1.1 Aluminum Alloy Index	3-2
	3.1.2 Material Properties	3-2
	3.1.3 Manufacturing Considerations	3-18
3.2	2000 Series Wrought Alloys	3-26
	3.2.1 2014 Alloy	3-26
	3.2.2 2017 Alloy	3-65
	3.2.3 2024 Alloy	3-68
	3.2.4 2025 Alloy	3-150
	3.2.5 2026 Alloy	3-152
	3.2.6 2090 Alloy	3-154
	3.2.7 2124 Alloy	3-157
	3.2.8 2219 Alloy	3-166
	3.2.9 2297 Alloy	3-195
	3.2.10 2424 Alloy	3-199
	3.2.11 2519 Alloy	3-202
	3.2.12 2524 Alloy	3-205
	3.2.13 2618 Alloy	3-209
3.3	3000 Series Wrought Alloys	3-218
3.4	4000 Series Wrought Alloys	3-218
3.5	5000 Series Wrought Alloys	3-218
	3.5.1 5052 Alloy	3-218
	3.5.2 5083 Alloy	3-231
	3.5.3 5086 Alloy	3-237
	3.5.4 5454 Alloy	3-247
	3.5.5 5456 Alloy	3-252
3.6	6000 Series Wrought Alloys	3-258
	3.6.1 6013 Alloy	3-258
	3.6.2 6061 Alloy	3-262
	3.6.3 6151 Alloy	3-290
3.7	7000 Series Wrought Alloys	3-293
	3.7.1 7010 Alloy	3-293
	3.7.2 7040 Alloy	3-302
	3.7.3 7049/7149 Alloy	3-305
	3.7.4 7050 Alloy	3-322
	3.7.5 7055 Alloy	3-363
	3.7.6 7075 Alloy	3-368
	3.7.7 7150 Alloy	3-427
	3.7.8 7175 Alloy	3-439
	3.7.9 7249 Alloy	3-454
	3.7.10 7475 Alloy	3-458
3.8	200.0 Series Cast Alloys	3-486
	3.8.1 A201.0 Alloy	3-486

5. PDF page 8

Section	Page
3.9 300.0 Series Cast Alloys	3-496
3.9.1 354.0 Alloy	3-496
3.9.2 355.0 Alloy	3-498
3.9.3 C355.0 Alloy	3-501
3.9.4 356.0 Alloy	3-503
3.9.5 A356.0 Alloy	3-506
3.9.6 A357.0 Alloy	3-510
3.9.7 D357.0 Alloy	3-513
3.9.8 359.0 Alloy	3-516
3.10 Element Properties	3-518
3.10.1 Beams	3-518
3.10.2 Columns	3-519
3.10.3 Torsion	3-521
References	3-525

6. PDF page 8

4.0	Magnesium Alloys	4-1
4.1	General	4-1
	4.1.1 Alloy Index	4-1
	4.1.2 Material Properties	4-1
	4.1.3 Physical Properties	4-2
	4.1.4 Environmental Considerations	4-2
	4.1.5 Alloy and Temper Designations	4-3
	4.1.6 Joining Methods	4-5
4.2	Magnesium-Wrought Alloys	4-6
	4.2.1 AZ31B	4-6
	4.2.2 AZ61A	4-17
	4.2.3 ZK60A	4-19
4.3	Magnesium Cast Alloys	4-27
	4.3.1 AM100A	4-27
	4.3.2 AZ91C/AZ91E	4-29
	4.3.3 AZ92A	4-33
	4.3.4 EZ33A	4-39
	4.3.5 QE22A	4-44
	4.3.6 ZE41A	4-48
4.4	Element Properties	4-53
	4.4.1 Beams	4-53
	4.4.2 Columns	4-53
	4.4.3 Torsion	4-56
	References	4-57

7. PDF page 8

5.0	Titanium	5-1
5.1	General	5-1
	5.1.1 Titanium Index	5-1

8. PDF page 9

Section		Page
5.1.2	Material Properties	5-1
5.1.3	Manufacturing Considerations	5-2
5.1.4	Environmental Considerations	5-2
5.2	Unalloyed Titanium	5-5
	5.2.1 Commercially Pure Titanium	5-5
5.3	Alpha and Near-Alpha Titanium Alloys	5-15
	5.3.1 Ti-5Al-2.5Sn	5-15
	5.3.2 Ti-8Al-1Mo-1V	5-27
	5.3.3 Ti-6Al-2Sn-4Zr-2Mo	5-43
5.4	Alpha-Beta Titanium Alloys	5-51
	5.4.1 Ti-6Al-4V	5-51
	5.4.2 Ti-6Al-6V-2Sn	5-92
	5.4.3 Ti-4.5Al-3V-2Fe-2Mo	5-110
5.5	Beta, Near-Beta, and Metastable-Beta Titanium Alloys	5-118
	5.5.1 Ti-13V-11Cr-3Al	5-118
	5.5.2 Ti-15V-3Cr-3Sn-3Al (Ti-15-3)	5-135
	5.5.3 Ti-10V-2Fe-3Al (Ti-10-2-3)	5-139
5.6	Element Properties	5-144
	5.6.1 Beams	5-144
References		5-145

9. PDF page 10

Section		Page
Chapter 7
7.0	Miscellaneous Alloys and Hybrid Materials	7-1
7.1	General	7-1
7.2	Beryllium	7-1
	7.2.1 Standard Grade Beryllium	7-1
7.3	Copper and Copper Alloys	7-8
	7.3.0 General	7-8
	7.3.1 Manganese Bronzes	7-9
	7.3.2 Copper Beryllium	7-12
7.4	Multiphase Alloys	7-21
	7.4.0 General	7-21
	7.4.1 MP35N Alloy	7-21
	7.4.2 MP159 Alloy	7-27
7.5	Aluminum Alloy Sheet Laminates	7-32
	7.5.0 General	7-32
	7.5.1 2024-T3 Aramid Fiber Reinforced Sheet Laminate	7-32
	References	7-50

10. PDF page 10

8.0	Structural Joints	8-1
8.1	Mechanically Fastened Joints	8-2
	8.1.1 Introduction and Fastener Indexes	8-2
	8.1.2 Solid Rivets	8-11
	8.1.3 Blind Fasteners	8-37
	8.1.4 Swaged Collar/Upset-Pin Fasteners	8-110
	8.1.5 Threaded Fasteners	8-125
	8.1.6 Special Fasteners	8-147
8.2	Metallurgical Joints	8-150
	8.2.1 Introduction and Definitions	8-150
	8.2.2 Welded Joints	8-150
	8.2.3 Brazing	8-172
8.3	Bearings, Pulleys, and Wire Rope	8-172
	References	8-173

11. PDF page 10

9.0	Index	9-1
9.1	General	9-5
	9.1.1 Introduction	9-5
	9.1.2 Applicability	9-5
	9.1.3 Approval Procedures	9-5
	9.1.4 Documentation Requirements	9-5
	9.1.5 Summary	9-6
	9.1.6 Data Basis	9-8
	9.1.7 Rounding Procedures	9-10
9.2	Material, Specification, Testing, and Data Requirements	9-11

12. PDF page 11

Section		Page
	9.2.1 Material Requirements	9-11
	9.2.2 Specification Requirements	9-11
	9.2.3 Required Test Methods/Procedures	9-11
	9.2.4 Data Requirements	9-24
	9.2.5 Experimental Design	9-40
9.3	Submission of Data	9-50
	9.3.1 Recommended Procedures	9-50
	9.3.2 Computer Software	9-50
	9.3.3 General Data Formats	9-50
9.4	Substantiation of S-Basis Minimum Properties	9-59
9.5	Analysis Procedures for Statistically Computed Minimum Static Properties	9-60
	9.5.1 Specifying the Population	9-60
	9.5.2 Regression Analysis	9-64
	9.5.3 Combinability of Data	9-77
	9.5.4 Determining the Form of Distribution	9-82
	9.5.5 Direct Computation Without Regression	9-94
	9.5.6 Direct Computation by Regression Analysis	9-104
	9.5.7 Indirect Computation without Regression (Reduced Ratios/Derived Properties)	9-106
	9.5.8 Indirect Computation using Regression	9-109
9.6	Analysis Procedures for Dynamic and Time Dependent Properties	9-110
	9.6.1 Load and Strain Control Fatigue Data	9-110
	9.6.2 Fatigue Crack Growth Data	9-130
	9.6.3 Fracture Toughness Data	9-133
	9.6.4 Creep and Creep-Rupture Data	9-135
9.7	Analysis Procedures for Structural Joint Properties	9-142
	9.7.1 Mechanically Fastened Joints	9-142
	9.7.2 Fusion-Welded Joint Data	9-158
9.8	Examples of Data Analysis and Data Presentation for Static Properties	9-162
	9.8.1 Direct Analyses of Mechanical Properties	9-162
	9.8.2 Indirect Analyses of Mechanical Properties	9-175
	9.8.3 Tabular Data Presentation	9-179
	9.8.4 Room Temperature Graphical Mechanical Properties	9-184
	9.8.5 Elevated Temperature Graphical Mechanical Properties	9-202
9.9	Examples of Data for Dynamic and Time Dependent Properties	9-212
	9.9.1 Fatigue	9-212
	9.9.2 Fatigue Crack Growth	9-228
	9.9.3 Fracture Toughness	9-230
	9.9.4 Creep and Creep Rupture	9-234
	9.9.5 Mechanically Fastened Joints	9-240
	9.9.6 Fusion-Welded Joints	9-244
9.10	Statistical Tables	9-247
	9.10.1 One-Sided Tolerance Limit Factors, K, for the Normal Distribution, 0.95 Confidence, and n-1 Degrees of Freedom	9-248
	9.10.2 0.950 Fractiles of the F Distribution Associated with n₁ and n₂ Degrees of Freedom	9-250

13. PDF page 12

Section		Page
9.10.3	0.950 Fractiles of the F Distribution Associated with n₁ and n₂ Degrees of Freedom	9-251
9.10.4	0.95 and 0.975 Fractiles of the t Distribution Associated with df Degrees of Freedom	9-252
9.10.5	Area Under the Normal Curve from -∞ to the Mean +Zp Standard Deviations.	9-253
9.10.6	One-Sided Tolerance-Limit Factors for the Three-Parameter Weibull Acceptability Test with 95 Percent Confidence	9-254
9.10.7	One-Sided Tolerance Factors for the Three-Parameter Weibull Distribution with 95 Percent Confidence	9-255
9.10.8	γ-values for Computing Threshold of Three-Parameter Weibull Distribution	9-261
9.10.9	Ranks, r, of Observations, n, for an Unknown Distribution Having the Probability and Confidence of T99 and T90 Values	9-264
Standards and References		9-266

14. PDF page 12

10.1	Intended Use	10-1
10.2	Subject Term (Key Word) Listing	10-1
10.3	Changes from Previous Issue	10-1

15. PDF page 12

A.0	Glossary	A-1
A.1	Abbreviations	A-1
A.2	Symbols	A-5
A.3	Definitions	A-6
A.4	Conversion of U.S. Units of Measure Used in MIL-HDBK-5 to SI Units	A-17
B.0	Alloy Index	B-1
C.0	Specification Index	C-1
D.0	Subject Index	D-1
E.0	Figure Index	E-1

16. PDF page 52

1.4.3.1	Goodman, S. and Russell, S.B., U.S. Air Force, “Poisson’s Ratio of Aircraft Sheet Materials for Large Strain,” WADC-TR-53-7, 58 pp (June 1953).
1.4.4	“Test Methods of Tension Testing of Metallic Materials,” ASTM E 8.
1.4.5(a)	Hyler, W.S., “An Evaluation of Compression-Testing Techniques for Determining Elevated Temperature Properties of Titanium Sheet,” Titanium Metallurgical Laboratory Report No. 43, Battelle Memorial Institute, 38 pp, Appendix 28 pp (June 8, 1956).
1.4.5(b)	“Compression Testing of Metallic Materials at Room Temperature,” ASTM E 9.
1.4.6	Stange, A.H., Ramberg, W. and Back, G., “Torsion Tests of Tubes,” National Advisory Committee for Aeronautics, Report No. 601, pp 515-535 (Feb. 1937).
1.4.7(a)	Stickley, G.W. and Moore, A.A., “Effects of Lubrication and Pin Surface on Bearing Strengths of Aluminum and Magnesium Alloys,” Materials Research and Standards, 2, (9), pp 747-751 (September 1962).
1.4.7(b)	“Method of Pin-Type Bearing Test of Metallic Materials,” ASTM E 238.
1.4.8.2.1(a)	“Recommended Practice for Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic Materials,” ASTM E 139.
1.4.8.2.1(b)	Rice, Richard, “Reference Document for the Analysis of Creep and Stress Rupture Data in MIL-HDBK-5,” AFWAL-TR-81-4097 (September 1981).
1.4.8.2.1(c)	Aarnes, M.N. and Tuttle, M.M., “Presentation of Creep Data for Design Purposes,” ASD Technical Report 61-216 (June 1961) (MCIC 45114).
1.4.9(a)	“Recommended Practice for Constant Amplitude Axial Fatigue Tests of Metallic Materials,” ASTM E 466.
1.4.9(b)	“Recommended Practice for Constant-Amplitude Low-Cycle Fatigue Testing,” ASTM E 606.
1.4.9.2(a)	Grover, H.J., “Fatigue of Aircraft Structures,” Prepared for Naval Air Systems Command, Department of the Navy, 335 pp (1966).
1.4.9.2(b)	Osgood, C.C., “Fatigue Design,” Wiley-Interscience, A Division of John Wiley and Sons, Inc., 523 pp (1970).
1.4.11	Bert, C.W., Mills, E.J. and Hyler, W.S., “Mechanical Properties of Aerospace Structural Alloys Under Biaxial-Stress Conditions,” AFML-TR-66-229, (August 1966).
1.4.12.2(a)	“Standard Method of Test for Plane-Strain Fracture Toughness of Metallic Materials,” ASTM E 399.
1.4.13.1	“Test Method for Measurements of Fatigue Crack Growth Rates,” ASTM E 647.

17. PDF page 56

Section	Alloy Designation
2.7	Austenitic stainless steels
2.7.1	AISI 301 and Related 300 Series Stainless Steels

18. PDF page 70

Alloy	Sheet, strip, and plate	Bars and forgings	Tubing
	Form
4130	AMS-S-18729, AMS 6350^a, AMS 6351^a	AMS-S-6758^a, AMS 6348^a, AMS 6370^a, AMS 6528^a	AMS-T-6736, AMS 6371^a, AMS 6360, AMS 6361, AMS 6362, AMS 6373, AMS 6374
8630	AMS-S-18728^b, AMS 6350^a	AMS-S-6050, AMS 6280^a	AMS 6281^a
4135	AMS 6352^a		AMS 6372^a, AMS 6365, AMS-T-6735^b
8735	AMS 6357^a	AMS 6320^a	AMS 6282^a
4140	AMS 6395^a	AMS-S-5626^a, AMS 6382^a, AMS 6349^a, AMS 6529^a	AMS 6381^a
4340	AMS 6359^a	AMS-S-5000^a, AMS 6415^a	AMS 6415^a
8740	AMS 6358^a	AMS-S-6049^b, AMS 6327, AMS 6322^a	AMS 6323^a
4330V		AMS 6427^a	AMS 6427^a
4335V	AMS 6433	AMS 6430	AMS 6430

19. PDF page 71

Alloy	AISI 4130		AISI 4135		AISI 8630
Specification [see Tables 2.3.1.0(a) and (b)]	AMS 6360 AMS 6373 AMS 6374 AMS-T-6736 AMS-S-18729		AMS 6365 AMS-T-6735^a		AMS-S-18728^a
Form	Sheet, strip, plate, and tubing		Tubing		Sheet, strip, and plate
Condition	Normalized and tempered, stress relieved^b
Thickness or diameter, in.	≤0.188	>0.188	≤0.188	≤0.188	≤0.188	≤0.188
Basis	S	S	S	S	S	S
Mechanical Properties:
F_tu, ksi	95	90	100	95	95	90
F_ty, ksi	75	70	85	80	75	70
F_cy, ksi	75	70	89	84	75	70
F_su, ksi	57	54	60	57	57	54
F_bru, ksi:
(e/D = 1.5)
(e/D = 2.0)	200	190	190	180	200	190
F_bry, ksi:
(e/D = 1.5)
(e/D = 2.0)	129	120	146	137	129	120
e, percent	See Table 2.3.1.0(d)
E, 10³ ksi	29.0
E_c, 10³ ksi	29.0
G, 10³ ksi	11.0
μ	0.32
Physical Properties:
ω, lb/in.³	0.283
C, K, and α	See Figure 2.3.1.0

20. PDF page 72

Alloy	AISI 4130
Specification [see Tables 2.3.1.0(a) and (b)]	AMS 6361 AMS-T-6736	AMS 6362 AMS-T-6736	AMS-T-6736
Form	Tubing
Condition	Quenched and tempered^a
Thickness or diameter, in.	≤0.188	≤0.188	All Walls
Basis..	S	S	S
Mechanical Properties:
Ftu ksi	125	150	180
Fty, ksi	100	135	165
Fcy, ksi	109	141	173
Fsu, ksi	75	90	108
Fbru, ksi:
(e/D = 1.5)	194	231	277
(e/D = 2.0)	251	285	342
Fbry, ksi:
(e/D = 1.5)	146	210	257
(e/D = 2.0)	175	232	284
e, percent	See Table 2.3.1.0(e)
E, 10³ ksi	29.0
E, 10³ ksi	29.0
G, 10³ ksi	11.0
μ		0.32
Physical Properties:
ω, lb/in.³	0.283
C, K, and α	See Figure 2.3.1.0

21. PDF page 78

Alloy	AISI 4130		AISI 4135		AISI 8630		AISI 8735
Specification [see Tables 2.3.1.0(a) and (b)]	AMS 6350 AMS 6528 AMS-S-6758		AMS 6352 AMS 6372		AMS 6281		AMS 6357
Form	Sheet, strip, plate, bars, and forgings		Sheet, strip, plate, and tubing		Tubing		Sheet, strip, and plate
Condition	Normalized and tempered, stress relieved^a
Thickness or diameter, in.	≤0.188	>0.188	≤0.188	>0.188	≤0.188	>0.188	≤0.188	>0.188
Basis	^b
Mechanical Properties:
F_tu, ksi	95	90	95	90	95	90	95	90
F_ty, ksi	75	70	75	70	75	70	75	70
F_cy, ksi	75	70	75	70	75	70	75	70
F_su, ksi	57	54	57	54	57	54	57	54
F_bru, ksi:
(e/D = 1.5)
(e/D = 2.0)	200	190	200	190	200	190	200	190
F_bry, ksi:
(e/D = 1.5)
(e/D = 2.0)	129	120	129	120	129	120	129	120
e, percent	See Table 2.3.1.0(d)
E, 10³ ksi	29.0
E_c, 10³ ksi	29.0
G, 10³ ksi	11.0
μ	0.32
Physical Properties:
ω, lb/in.³	0.283
C, K, and a	See Figure 2.3.1.0

22. PDF page 171

Specification	AMS 5548
Form	Sheet and strip^a
Condition	SCT 850
Thickness, in.	≤ 0.187
Basis	S
Mechanical Properties:
F_tu, ksi:
L	183
LT	185
F_ty, ksi:
L	147
LT	150
F_cy, ksi:
L	163
LT	…
F_su, ksi:	121
F_bru, ksi:
(e/D = 1.5)	…
(e/D = 2.0)	373
F_bry, ksi:
(e/D = 1.5)	…
(e/D = 2.0)	252
e, percent:
LT	10^b
E, 10³ ksi	29.0
E_c, 10³ ksi	30.0
G, 10³ ksi	11.0
μ	0.32
Physical Properties:
ω, lb/in.³	0.282
C, Btu/(lb)(°F)	0.12 (32 to 212°F)
K and α	See Figure 2.6.1.0

23. PDF page 206

Condition	TYS (T), ksi	K_Iscc, ksi/in.	Remarks
H950	226	68	No cracking
H1000	213	98	No cracking

24. PDF page 206

Specification	Form
AMS 5936	Bars, Wires, and Forgings

25. PDF page 225

Specification	AMS 5400
Form	Investment casting
Condition	H935
Location within casting	Any area
Basis	S
Mechanical Properties:^a
F_tu, ksi	170
F_ty, ksi	150
F_cy, ksi	155
F_su, ksi	107
F_bru^b, ksi:
(e/D = 1.5)	269
(e/D = 2.0)	349
F_bry^b, ksi:
(e/D = 1.5)	209
(e/D = 2.0)	240
e, percent	6
RA, percent	14
E, 10³ ksi	28.5
E_c, 10³ ksi	29.2
G, 10³ ksi	11.2
μ	0.27
Physical Properties:
ω, lb/in.³	0.283
C, Btu/(lb)(°F)
K, and α	See Figure 2.6.7.0

26. PDF page 238

Specification	AMS 5520
Form	Sheet, strip, and plate
Condition	TH1050
Thickness, in	0.0015-0.500
Basis	S
Mechanical Properties:
F_tu, ksi:
L	185
LT	190
F_ty, ksi:
L	165
LT	170
F_cy, ksi:
L	182
LT	188
F_su, ksi	120
F_bru, ksi:
(e/D = 1.5)	327
(e/D = 2.0)	377
F_bry, ksi:
(e/D = 1.5)	259
(e/D = 2.0)	272
e, percent:
LT	a
E, 10³ ksi	29.0
E_c, 10³ ksi	30.0
G, 10³ ksi	11.4
μ	0.28
Physical Properties:
ω, lb/in.³	0.277
C, Btu/(lb)(°F)
K and α	See Figure 2.6.8.0

27. PDF page 239

Thickness, inches	e (LT), percent
0.0015 to 0.0049	2
0.0050 to 0.0099	3
0.010 to 0.019	4
0.020 to 0.1874	5
0.1875 to 0.500	6

28. PDF page 250

Specification	Form
AMS 5604	Sheet, strip, and plate
AMS 5643	Bar, forging, and ring
AMS 5342	Investment casting (H1100)
AMS 5343	Investment casting (H1000)
AMS 5344	Investment casting (H900)

29. PDF page 327

MIL-HDBK-5 Section No.	Alloy	Weldability^b,c
MIL-HDBK-5 Section No.	Alloy	Inert Gas Metal or Tungsten Arc	Resistance Spot
3.8.1	A201.0	C	C
3.9.1	354.0	B	B
3.9.2	355.0	B	B
3.9.3	C355.0	B	B
3.9.4	356.0	A	A
3.9.5	A356.0	A	A
3.9.6	A357.0	A	B
3.9.7	D357.0	A	A
3.9.8	359.0	A	B

30. PDF page 331

Specification	AMS 4028
Form	Sheet				Plate^a
Temper	T62^b
Thickness, in	0.020-0.039		0.040-0.249		0.250-0.499		0.500-1.000
Basis	A	B	A	B	A	B	A	B
Mechanical Properties:
F_tu, ksi:
L	65	67	67	68	65	67	65	67
LT	64	66	66	67	67	69	67	69
F_ty, ksi:
L	58	60	59	60	57	59	57	59
LT	57	59	58	59	59	61	59	61
F_cy, ksi:
L	58	60	59	60	59	61	59	61
LT	59	61	60	61	60	62	60	62
F_su, ksi	39	40	40	41	37	39	37	39
F_bru, ksi:
(e/D = 1.5)	97	100	100	102	100	103	100	103
(e/D = 2.0)	123	127	127	129	127	131	127	131
F_bry, ksi:
(e/D = 1.5)	81	84	83	84	84	87	84	87
(e/D = 2.0)	93	96	95	96	99	103	99	103
e, percent (S-basis):
LT	6	…	7	…	7	…	6	…
E, 10³ ksi	10.5				10.7
E_c, 10³ ksi	10.7				10.9
G, 10³ ksi	4.0				4.0
μ	0.33				0.33
Physical Properties:
ω, lb/in.³	0.101
C, K, and α	See Figure 3.2.1.0

31. PDF page 332

Specification	AMS-QQ-A-250/3
Form	Sheet				Plate
Temper	T6				T651
Thickness, in.	0.020-0.039		0.040-0.249		0.250-0.499		0.500-1.000^b		1.001-2.000^b		2.001-2.500^b		2.501-3.000^b		3.001-4.000^b		4.001-5.000^b		5.001-6.000^b
Basis	A	B	A	B	A	B	A	B	A	B	A	B	A	B	A	B	A	B	A	B
Mechanical Properties:
Ftu, ksi:
L	62	64	65	67	63	65	63	64	63	64	61	62	60	61	58	59	58	59	58	59
LT	61	63	64	66	64	66	64	65	64	65	62	63	60	56	57	56	57	56	57	56
ST													59	60
Fy, ksi:
L	54	56	57	59	58	60	57	58	57	59	56	58	54	55	56	55	56	55	56	55
LT	53	55	56	58	57	59	56	57	56	58	55	57	52	53	54	53	54	53	54	53
ST													54	56
Fcy, ksi:
L	54	56	57	59	56	58	55	56	55	57	54	56	52	53	54	53	54	53	54	53
LT	55	57	58	60	59	61	58	59	58	60	57	59	55	56	57	56	57	56	57	56
ST													59	61
Fsu, ksi	37	38	39	40	38	39	38	38	38	38	37	37	36	36	36	36	36	36	36	36
Fbru, ksi:
(e/D = 1.5)	93	96	97	100	101	104	101	102	101	102	97	99	94	96	94	96	94	96	94	96
(e/D = 2.0)	117	121	123	127	128	132	128	130	128	130	124	126	120	122	120	122	120	122	120	122
Fbry, ksi:
(e/D = 1.5)	76	78	80	83	87	90	85	87	85	88	84	87	82	84	82	84	82	84	82	84
(e/D = 2.0)	86	89	91	94	102	106	100	102	100	104	98	102	96	100	96	100	96	100	96	100
e, percent (S-basis):
LT	7		8		8		6		4		2		2		1		1		1
E, 10³ ksi			10.5										10.7
E, 10³ ksi			10.7										10.9
G, 10³ ksi					4.0								4.0
					0.33								0.33
Physical Properties:
w, lb/in.³																			0.101
C, K, and α

32. PDF page 334

Specification	AMS 4121 and AMS-QQ-A-225/4							AMS-QQ- A-225/4
Form	Bar, rod, and shapes, rolled, drawn, or cold-finished
Temper	T6 and T651							T62^a
Thickness, in.	Up to 1.000	1.001- 2.000	2.001- 3.000	3.001- 4.000	4.001- 5.000^b	5.001- 6.000^b	6.001- 8.000^b	≤8.000^b
Basis	S	S	S	S	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L	65	65	65	65	65	65	65	65
LT	64^c	63^c	62^c	61^c	60^c	59^c	…	…
F_ty, ksi:
L	55	55	55	55	55	55	55	55
LT	53^c	52^c	51^c	50^c	49^c	48^c	…	…
F_cy, ksi:
L	53	53	53	53	53	53	53	…
LT	…	…	…	…	…	…	…	…
F_su, ksi	38	38	38	38	38	38	38	…
F_bru, ksi:	…	…	…	…	…	…	…	…
(e/D = 1.5)	98	…	…	…	…	…	…	…
(e/D = 2.0)	124	…	…	…	…	…	…	…
F_bry, ksi:	…	…	…	…	…	…	…	…
(e/D = 1.5)	77	…	…	…	…	…	…	…
(e/D = 2.0)	88	…	…	…	…	…	…	…
e, percent:
L	8	8	8	8	8	8	8	8
E, 10³ ksi					10.5
E_c, 10³ ksi					10.7
G, 10³ ksi						4.0
μ						0.33
Physical Properties:
ω, lb/in.³							0.101
C, K, and α								See Figure 3.2.1.0

33. PDF page 336

Specification	AMS 4133, AMS-A-22771, and AMS-QQ-A-367
Form	Hand forging
Temper	T6^a
Cross-Sectional Area, in.²	< 256
Thickness, in.	≤2.000	2.001-3.000	3.001-4.000	4.001-5.000	5.001-6.000	6.001-7.000	7.001-8.000	≤2.000	2.001-3.000	3.001-4.000	4.001-5.000	5.001-6.000	6.001-7.000	7.001-8.000
Basis	S	S	S	S	S	S	S	S	S	S	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L	65	64	63	62	61	60	59	65	64	63	62	61	60	59
LT	65	64	63	62	61	60	59	65	64	63	62	61	60	59
ST	…	62°	61°	60°	59°	58°	57°	…	62°	61°	60°	59°	58°	57°
F_ty, ksi:
L	56	56	55	54	53	52	51	56	55	55	54	53	52	51
LT	56	55	55	54	53	52	51	56	55	55	54	53	52	51
ST	…	55°	54°	53°	53°	52°	51°	…	52°	51°	50°	50°	49°	48°
F_cy, ksi:
L	56	56	55	54	53	…	…	56	55	55	54	53	…	…
LT	56	55	55	54	53	…	…	57	56	56	55	54	…	…
ST	…	…	…	…	…	…	…	…	57	56	55	55	…	…
F_su, ksi:	40	39	39	38	38	…	…	38	37	37	36	36	…	…
F_bru, ksi:
(e/D = 1.5)	91	90	88	87	85	…	…	88	87	85	84	83	…	…
(e/D = 2.0)	117	115	113	112	110	…	…	115	113	111	110	108	…	…
F_bry, ksi:
(e/D = 1.5)	78	78	77	76	74	…	…	77	76	76	74	73	…	…
(e/D = 2.0)	90	90	88	87	85	…	…	91	89	89	87	86	…	…
e, percent:
L	8	8	8	7	7	6	6	8	8	8	7	7	6	6
LT	…	3	3	2	2	1	1	…	3	3	2	2	1	1
ST	…	2	2	1	1	1	1	…	2	2	1	1	1	1
E, 10³ ksi								10.5
E_c, 10³ ksi								10.8
G, 10³ ksi								4.0
μ								0.33
Physical Properties:
w, lb/in.³								0.101
C, K, and α								See Figure 3.2.1.0

34. PDF page 337

Specification	AMS 4153 and AMS-QQ-A-200/2										AMS-QQ-A-200/2
Form	Extruded bar, ro
Temper	T6, T6510, and T6511
Cross-Sectional Area, in.²	<25										All	<25	>25-<32
Thickness or Dia., in.^b	0.125-0.499		0.500-0.749		0.750-1.499		1.500-1.750		1.751-2.999	3.000-4.499	≥0.750	≤0.749	≥0.750	≥0.750
Basis	A	B	A	B	A	B	A	B	S	S	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L	60	62	64	68	68	70	68	71	68	68	68	60	60	60
LT (S-basis)	60°		64°		63°		61°		61
F_ty, ksi:
L	53	57	58	62	60	63	60	63	60	60	58	53	53	53
LT (S-basis)	53°		55°		54°		52°		52	49	47
F_cy, ksi:
L	52	56	57	61	59	62	59	62
LT
F_su, ksi	35	36	37	39	39	41	39	41
F_bru, ksi:
(e/D = 1.5)	90	93	96	102	102	105	102	106
(e/D = 2.0)	116	120	124	132	132	136	132	138
F_bry, ksi:
(e/D = 1.5)	73	78	80	85	82	86	82	86
(e/D = 2.0)	85	91	93	99	96	101	96	101
e, percent (S-basis):
L	7		7		7		7		7	7		7	7	6
LT	5°		5		2				2
E, 10³ ksi									10.8
E, 10³ ksi									11.0
G, 10³ ksi									4.1
μ									0.33
Physical Properties:
ω, lb/in.³									0.101
C, K, and α								See Figure

35. PDF page 338

Temper/Product Form	Condition	Temper- ature, °F	Grain Direction	Tension, ksi			Compression, ksi
Temper/Product Form	Condition	Temper- ature, °F	Grain Direction	n	TYS	TUS	n_c	CYS
T6 Clad Sheet	0.02-0.039 in. thickness	RT	L	32	57		17	57
	0.02-0.039 in. thickness		LT	17	57		13	60
	0.04-0.249 in. thickness		L	27	62		15	62
	0.04-0.249 in. thickness		LT	20	60		17	65
	½ hr. exposure	200°F	LT				9.5	60
	100 hr. exposure	200°F					8.0	62
	½ and 2 hr. exposure	300°F					4.0	54
	1000 hr. exposure	300°F					6.4	46
	½ hr. exposure	400°F					8.2	47
	100 hr. exposure						10	20
	1000 hr. exposure						6.0	16
	½ hr. exposure	500°F					7.0	22
	½ hr. exposure	600°F					4.3	9
	10 hr. exposure						6.0	8
	100 hr. exposure						13	7
T62 Clad Plate	0.250 - 2.000 in. thickness	RT	L	29	64		27	69
T62 Clad Plate	0.250 - 2.000 in. thickness	RT	LT	29	64		27	70
T651 Plate	0.250 - 2.000 in. thickness	RT	L	30	66		15	68
T651 Plate	0.250 - 2.000 in. thickness	RT	LT	19	65		18	66
T6 Bar, Rod and Shapes	> 3 in. thickness	RT	L	31	62		25	60
T6 Forging		RT	L			70
T6 Forging		RT	LT			68
T652 Hand Forging	2.001 - 3.000 in. thickness	RT	L	18	62	67	17	63
			LT	18	62	66	18	65
			ST	13	60		22	67
T6 Extrusion	0.125 - 0.499 in. thickness	RT	L	23	62		15	64
T6 Extrusion	> 0.500 in. thickness	RT	L	26	68		14	72
T62 Extrusion	< 0.499 in. thickness	RT	L	29	64	71	17	68
T62 Extrusion	< 0.499 in. thickness	RT	LT	29	64		32	68
T651X Extrusion	0.500 - 0.749 in. thickness	RT	L	32	64	74	16	68
T651X Extrusion	0.500 - 0.749 in. thickness	RT	LT	18	64	70	18	68

36. PDF page 376

	Elongation (LT), percent
Condition	T3, T4, and T42
Thickness, in.:
0.010-0.020	12
0.021-0.249	15
0.250-0.499	12
0.500-1.000	8
1.001-1.500	7
1.501-2.000	6

37. PDF page 381

	Elongation (LT), percent
Temper	T3, T4, T42
Thickness, in.:
0.010-0.020	12
0.021-0.062	15
1.001-1.500	7
1.501-2.000	6

38. PDF page 383

	Elongation (L), percentª
Temper	T3, T42
Wall Thickness, in.:
0.018-0.024	10
0.025-0.049	12
0.050-0.259	14
0.260-0.500	16
Temper	T81
0.010-0.024
0.025-0.049	5
0.050-0.249	6

39. PDF page 385

Specification	AMS 4120 and AMS-QQ-A-225/6
Form	Bar and rod; rolled, drawn, or cold-finished
Temper	T4a											T42b
Thickness, in.	0.125-0.499	0.500-1.000	1.001-2.000	2.001-3.000	3.001-4.000	4.001-4.500^c		4.501-5.000^d	5.001-6.000^e	6.001-6.500^d	6.501-8.000^d	≤6.500^d
Basis	S	S	S	S	S	S		S	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L	62	62	62	62	62	62		62	62	62	58	62
LT	61°	61°	59°	57°	55°	54°		54°	52°
F_ty, ksi:
L	45	42	42	42	42	42		40	40	40	38	40
LT	45°	42°	41°	40°	39°	39°		37°	36°
F_cy, ksi:
L	36	33	33	33	33	33		32	32
LT			32
F_su, ksi	37	37	37	37	37	37		37	37	37
F_bru, ksi:
(e/D = 1.5)	93	93	93	93	93	93		93	93
(e/D = 2.0)	118	118	118	118	118	118		118	118
F_bry, ksi:
(e/D = 1.5)	63	59			59			56	56
(e/D = 2.0)	72	67	67	67	67	67		64	64
e, percent:
L	10	10	10	10	10	10		10	10	10	10	10
E, 10³ ksi												10
E_c, 10³ ksi												10.5
G, 10³ ksi							4.0
μ												0.33
Physical Properties:
w, lb/in.³							0.100
C and α	See Figure 3.2.3.0
K, Btu/[(hr)(ft²)(°F)/ft]	71 (at 77°F) for T4X (See Figure 3.2.3.0)

40. PDF page 455

Specification	AMS 4338
Form	Extrusions
Temper	T3511
Thickness, in.	≤0.249		0.250-0.499		0.500-1.499		1.500-2.249		2.250-3.250
Basis	A	B	A	B	A	B	A	B	S
Mechanical Properties:
F_tu, ksi:
L	66	69	70	72	72	75	73	76	73
LT	58	61	62	64	66	67	64	67	61
F_ty, ksi:
L	48	51	52	53	53	56	54	57	54
LT	41	44	45	46	46	48	44	49	42
F_cy, ksi:
L	43	45	46	47	47	47	49	52	50
LT	42	45	44	46	46	49	45	47	43
F_su, ksi	37	39	37	38	32	33	32	33	32
F_bru^a, ksi:
(e/D = 1.5)	90	94	92	95	87	90	85	89	85
(e/D = 2.0)	112	117	113	117	109	114	108	112	105
F_bry^a, ksi:
(e/D = 1.5)	62	66	66	67	61	64	61	64	61
(e/D = 2.0)	76	81	81	83	76	81	76	80	76
e, percent (S-basis):
L	11	…	12	…	11	…	11	…	10
LT	…	…	…	…	8	…	8	…	8
E, 10³ ksi	10.7
E, 10³ ksi	10.9
G, 10³ ksi	4.0
μ	0.33
Physical Properties:
ω, lb/in.³	0.100
C, Btu/(lb)(°F)	…
K, Btu/[(hr)(ft²)(°F)/ft] α, 10^-6 in./in./°F	…

41. PDF page 456

Specification	Form
AMS 4251	Sheet

42. PDF page 456

Section	Temper
3.2.6.1	T83

43. PDF page 474

Specification	AMS 4162 and AMS 4163^a
Form	Extruded shapes
Temper	T8511
Cross-Sectional Area, in.²	<25
Thickness or Diameter, in.^b	≤0.499	0.500-2.999
Basis	S	S
Mechanical Properties:
F_tu, ksi:
L	58	58
LT^c	56	56
F_ty, ksi:
L	42	42
LT^c	39	39
F_cy, ksi:
L	43	42
LT	43	41
F_su, ksi	33	33
F_bru, ksi:
(e/D = 1.5)	87	81
(e/D = 2.0)	113	107
F_bry, ksi:
(e/D = 1.5)	69	67
(e/D = 2.0)	84	82
e, percent:
L	6	6
LT^c	4	4
E, 10³ ksi	10.5
E_c, 10³ ksi	10.8
G, 10³ ksi	4.0
μ	0.33
Physical Properties:
ω, lb/in.³	0.103
C, K, and α	See Figure 3.2.8.0

44. PDF page 505

Specification	MIL-DTL-46192
Form	Plate
Temper	T87
Thickness or Diameter, in	0.250- 1.000	1.001- 2.000	2.001- 3.000	3.001- 4.000
Basis	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L	66	66	67	68
LT	68	68	68	68
ST			63	62
F_ty, ksi:
L	59	59	60	61
LT	58	58	59	59
ST			55	55
F_cy, ksi:
L	57	57	58	58
LT	60	60	61	61
ST			58	58
F_su, ksi	42	41	41	40
F_bru^a, ksi:
(e/D = 1.5)	105	105	104	103
(e/D = 2.0)	135	134	133	131
F_bry^a, ksi:
(e/D = 1.5)	85	85	87	87
(e/D = 2.0)	99	99	100	100
e, percent:
L	10	9	8	7
LT	7	7	6	5
E_t, 10³ ksi	10.5
E_c, 10³ ksi	10.8
G, 10³ ksi	4.0
μ	0.33
Physical Properties:
ω, lb/in.³	0.102
C, K, and α

45. PDF page 523

Temper	Thickness Range, inch	Elongation (L), percent
O	0.006-0.007
	0.008-0.012	14
	0.013-0.019	15
	0.020-0.031	16
	0.032-0.050	18
	0.051-0.113	19
	0.114-0.249	20
	0.250-3.000	18
H32	0.017-0.019	4
	0.020-0.050	5
	0.051-0.113	7
	0.114-0.249	9
	0.250-0.499	11
	0.500-2.000	12
H34	0.009-0.019	3
	0.020-0.050	4
	0.051-0.113	6
	0.114-0.249	7
	0.250-1.000	10
H36	0.006-0.007	2
	0.008-0.031	3
	0.032-0.162	4
H38	0.006-0.007	2
	0.008-0.031	3
	0.032-0.128	4

46. PDF page 535

Specification	AMS-QQ-A-200/4
Form	Extrusion
Temper	O	H111		H112
Thickness, in.	<5.000ª	<0.500ª	0.501- 5.000ª	<5.000ª
Basis	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L	39	40	40 22	39
LT		40	32
F_ty, ksi:
L	16	24	24 19	16
LT		24	19
F_cy, ksi:
L
LT
F_su ksi
F_bru, ksi:
(e/D = 1.5)
(e/D = 2.0)
F_bry, ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent:
L	14	12	12	12
E, 10³ ksi	10.2
E_c, 10³ ksi		10.4
G, 10³ ksi	3.35
μ	0.33
Physical Properties:
ω, lb/in.³	0.096
C, Btu/(lb)(°F)	0.23 (at 212°F)
K, Btu/[(hr)(ft²)(°F)/ft]	68 (at 77°F)
α, 10^-6 in./in./°F	See Figure 3.5.2.0

47. PDF page 541

Temper	Thickness Range, inch	Elongation (L), percent
O	0.020-0.050	15
	0.051-0.249	18
	0.250-2.000	16
H32	0.020-0.050	6
	0.051-0.249	8
	0.250-2.000	12
H34	0.009-0.019	4
	0.020-0.050	5
	0.051-0.249	6
	0.250-1.000	10
H36	0.006-0.019	3
	0.020-0.050	4
	0.051-0.162	6

48. PDF page 551

Temper	Thickness Range, inch	Elongation (L), percent
O	0.020-0.031	12
	0.030-0.050	14
	0.051-0.113	16
	0.114-3.000	18
H32	0.020-0.050	5
	0.051-0.249	8
	0.250-2.000	12
H34	0.020-0.050	4
	0.051-0.161	6
	0.162-0.249	7
	0.250-1.000	10
H112	0.500-2.000	11
H112	2.001-3.000	15

49. PDF page 556

Specification	AMS-QQ-A-200/7
Form	Extruded bar, rod, and shapes
Temper	O	H111	H112
Cross-Sectional Area, in.²	≤32
Thickness or Diameter, in.	≤5.000	≤5.000	≤5.000
Basis	S	S	S
Mechanical Properties:
F_u, ksi:
L	41	42	41
LT			41
F_ty, ksi:
L	19	26	19
LT			19
F_cy, ksi:
L	19		19
LT			19
F_su, ksi:			23
F_bru, ksi:
(e/D = 1.5)			57
(e/D = 2.0)			74
F_bry, ksi:
(e/D = 1.5)			34
(e/D = 2.0)			38
e, percent:
L	14	12	12
E, 10³ ksi	10.2
E_c, 10³ ksi	10.4
G, 10³ ksi	3.85
μ	0.33
Physical Properties:
ω, lb/in.³	0.096
C, Btu/(lb)(°F)	0.23 (at 212°F)
K, Btu/[(hr)(ft²)(°F)/ft]
α, 10^-6 in./in./°F	See Figure 3.5.5.0

50. PDF page 565

Specification	Form
AMS 4025	Sheet and plate
AMS 4026	Sheet and plate
AMS 4027	Sheet and plate
AMS-QQ-A-250/11	Sheet and plate
AMS 4115	Bar and rod, rolled or cold-finished
AMS 4116	Bar and rod, cold-finished
AMS 4117	Bar and rod, rolled or cold-finished
AMS-QQ-A-225/8	Rolled bar, rod, and shapes
AMS 4150	Extruded rod, bar, and shapes
AMS 4160	Extrusion
AMS 4161	Extrusion
AMS 4172	Extrusion
AMS 4173	Extruded rod, bar, and shapes
AMS-QQ-A-200/8	Extruded rod, bar, shapes, and tubing
AMS-A-22771	Forging
AMS 4080	Tubing, seamless, drawn
AMS 4082	Tubing, seamless, drawn
AMS-WW-T-700/6	Seamless drawn tubing
AMS 4127	Forging
AMS 4248	Hand forging
AMS-QQ-A-367	Forging

51. PDF page 567

Specification	AMS 4026 and AMS-QQ-A-250/11				AMS-QQ-A-250/11		AMS 4025, AMS 4027 and AMS-QQ-A-250/11
Form	Plate
Temper	T451				T42^a		T651 and T62^b
Thickness, in.	0.250-2.000		2.001-3.000		0.250-1.000	1.001-3.000	0.250-2.000		2.001-3.000		3.001-4.000	4.001-6.000°
Basis	A	B	A	B	S	S	A	B	A	B	S	S
Mechanical Properties:
F_tu, ksi:
L
LT	30	32	30	32	30	30	42	43
F_y, ksi:
L							36	38
LT	16	18	16	18	14	14	36	38	35	37	35	35
F_cy, ksi:
L
LT	16	18					36	38
F_su, ksi	20	21					27	28
F_bru, ksi:
(e/D= 1.5)	48	52					67	69
(e/D=2.0)	63	67					88	90
F_bry, ksi:
(e/D= 1.5)		22					50	53
(e/D=2.0)	22	29					58	61
e, percent:
L	d		16		18	16
E, 10³ ksi												9.9
E, 10³ ksi												10.1
G, 10³ ksi												3.8
μ												0.33
Physical Properties:
ω, lb/in.³												0.098
C, K, and α,												See Figure 3.6.2.0

52. PDF page 568

Temper and Product	Thickness, inch	Elongation (LT), percent
T4 or T42 sheet	0.010-0.020	14
T4 or T42 sheet	0.021-0.249	16
T451 plate	0.250-1.000	18
T451 plate	1.001-2.000	16
T6 or T62 sheet	0.010-0.020	8
T6 or T62 sheet	0.021-0.249	10
T651 or T62 plate	0.250-0.499	10
	0.500-1.000	9
	1.001-2.000	8

53. PDF page 570

Temper	Wall Thickness, inch	Elongation (L), percent
Temper	Wall Thickness, inch	Full-Section Specimen	Cut-Out Specimen
T4 or T42	0.025-0.049	16	14
	0.050-0.259	18	16
	0.260-0.500	20	18
T6 or T62	0.025-0.049	10	8
	0.050-0.259	12	10
	0.260-0.500	14	12

54. PDF page 571

Specification	AMS 4116 & AMS-QQ-A- 225/8	AMS 4128 & AMS-QQ-A- 225/8	AMS-QQ-A- 225/8	AMS 4117 & AMS-QQ-A-225/8	AMS 4128 & AMS-QQ-A-225/8	AMS 4115, AMS 4116, & AMS-QQ-A- 225/8
Form
Temper	Rolled, drawn, or cold-finished rod and special shapes
Cross-Sectional Area, in²	T4	T451	T42¹	T6	T651	T62¹
Thickness, in.	<50
Basis	≤8.000	0.500-8.000	≤8.000	≤8.000	0.500-8.000	≤8.000
Basis	S	S	S	S	S	S
Mechanical Properties:
Ftu, ksi:
L	30	30	30	42	42	42
Fty, ksi:
L	16	16	14	35	35	35
Fcy, ksi:
L	14	14		34	34
Fsu, ksi:
L	20	20		27	27
Fbru, ksi:
(e/D = 1.5)	48	48		67	67
(e/D = 2.0)	63	63		88	88
Fbry, ksi:
(e/D = 1.5)	22	22		49	49
(e/D = 2.0)	26	26		56	56
e, percent:
L	18	18	18	10	10	10
E, 10³ ksi				9.9
Ec, 10³ ksi				10.1
G, 10³ ksi				3.8
μ				0.33
Physical Properties:
ω, lb/in.³				0.098
C, K, and α,				See Figure 3.6.2.0

55. PDF page 593

Specification	AMS 4125 and AMS-A-22771
Form	Die forging
Temper	T6
Thickness^a, in.	<4.000
Basis	S
Mechanical Properties:
F_tu, ksi:
L	44
T^b	44
F_ty, ksi:
L	37
T^b	37
F_cy, ksi:
L	39
T^b	35
F_su, ksi	28
F_bru, ksi:
(e/D = 1.5)
(e/D = 2.0)
F_bry, ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent:
L	10
T^b	6
E, 10³ ksi	10.1
E_c, 10³ ksi	10.3
G, 10³ ksi	3.85
μ	0.33
Physical Properties:
ω, lb/in.³	0.098
C, Btu/(lb)(°F)	0.23 (at 212°F)
K, Btu/[(hr)(ft²)(°F)/ft]	100 (at 77°F)
α, 10^-6 in./in./°F	See Figure 3.6.3.0

56. PDF page 668

Specification	AMS 4206
Form	Plate
Temper	T7751
Thickness, in.	0.500 - 1.500
Basis	A	B
Mechanical Properties:
F_tu, ksi:
L	89	91
LT	89	91
F_ty, ksi:
L	86	88
LT	85	87
F_cy, ksi:
L	86	88
LT	89	91
F_su^a ksi	48	49
F_bru^b ksi:
(e/D = 1.5)	128	131
(e/D = 2.0)	167	170
F_bry^b ksi:
(e/D = 1.5)	112	115
(e/D = 2.0)	130	133
e, percent (S-basis):
L	7
LT	8
E, 10³ ksi		10.4
E_c, 10³ ksi		10.7
G, 10³ ksi		3.9
μ		0.32
Physical Properties:
ω, lb/in.³		0.103
C, Btu/(lb)(°F)
K, Btu/[(hr)(ft²)(°F)/ft]
α, 10^-6 in./in./°F

57. PDF page 676

Specification	AMS-QQ-A-250/24
Form	Sheet and plate
Temper	T76	T7651
Thickness, in.	0.063-0.249	0.250-0.499	0.500-1.000	1.001-1.500	1.501-2.000
Basis	S	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L	72	71	70	70	70
LT	73	72	71	71	71
ST					65
F_ty, ksi:
L	62	60	59	59	59
LT	62	61	60	60	60
ST					56
F_cy, ksi:
L	61	60	59	59	59
LT	65	64	63	63	63
ST					63
F_su, ksi	42	40	41	42	43
F_bru^a, ksi:
(e/D = 1.5)	112	109	108	108	108
(e/D = 2.0)	145	141	140	140	140
F_bry^a, ksi:
(e/D = 1.5)	88	86	86	86	87
(e/D = 2.0)	102	99	99	99	100
e, percent:
LT	8	8	6	5	5
E, 10³ ksi	10.3	10.3
E_c, 10³ ksi	10.5	10.6
G, 10³ ksi	3.9	3.9
μ	0.33	0.33
Physical Properties:
ω, lb/in.³	0.101
C, K, and α	See Figure 3.7.6.0

58. PDF page 689

Specification	AMS-QQ-A-200/15
Form	Extrusion (rod, bar, and shapes)
Temper	T76, T76510, T76511
Cross-Sectional Area, in.²	<20
Thickness, in.^a	0.062-0.249		0.250-0.499	0.500-0.749		0.750-1.000
Basis	A	B	S	A	B	A	B
Mechanical Properties:
F_tu, ksi:
L	71	74	75	75	76	75	76
LT	68	71	72	71	73	70	71
F_ty, ksi:
L	61	65	65	65	67	65	67
LT	57	61	61	60	62	59	61
F_cy, ksi:
L	61	65	65	65	67	65	67
LT	62	66	66	65	67	64	66
F_su, ksi	38	40	41	41	42	40	41
F_bru^b, ksi:
(e/D = 1.5)	103	107	109	109	110	109	110
(e/D = 2.0)	131	137	139	139	141	139	141
F_bry^b, ksi:
(e/D = 1.5)	82	88	88	88	90	88	90
(e/D = 2.0)	98	104	104	104	107	104	107
e, percent (S-basis):
L	7		7	7		7
E, 10³ ksi	10.4
E_c, 10³ ksi	10.7
G, 10³ ksi	4.0
μ	0.33
Physical Properties:
ω, lb/in.³	0.101
C, K, and α	See Figure 3.7.6.0

59. PDF page 816

Specification	AMS 4241
Form	Casting
Temper	T6
Thickness, in.	≤2.500
Location Within Casting	Designated area		Nondesignated area
Basis	A	B	S
Mechanical Properties^a:
F_tu, ksi	46	49	45
F_ty, ksi	39	41	36
F_cy, ksi	39	41	36
F_su, ksi	29	31	28
F_bru^b, ksi:
(e/D = 1.5)	79	84	77
(e/D = 2.0)	99	105	96
F_bry^b, ksi:
(e/D = 1.5)	62	65	57
(e/D = 2.0)	73	77	67
e, percent (S-basis)	3		2
E, 10³ ksi		10.4
E_c, 10³ ksi		10.5
G, 10³ ksi		3.9
μ		0.33
Physical Properties:
ω, lb/in.³		0.097
C, Btu/(lb)(°F)		0.23 (at 212°F)
K, Btu/[(hr)(ft²)(°F)/ft]		88 (at 77°F)
α, 10^-6 in./in./°F		12.0 (68 to 212°F)

60. PDF page 854

Specification	ASTM B 107
Form	Extruded rod, bar, and solid shapes				Extruded hollow shapes	Extruded tube
Temper	F
Cross-sectional area, in.²	<2.000	2.000-2.999	3.000-4.999	5.000-39.999	All	≤3.000 in. O.D.
Thickness, in.	All	All	All	All	All	0.028-0.750 wall
Basis	S	S	S	S	S	S
Mechanical Properties:
F_u, ksi:
L	43	43	43	43	40	40
LT
F_ty, ksi:
L	31	31	31	31	28	28
LT
F_cy, ksi:
L	27	26	25	20	20	20
LT	22	22				21
F_su, ksi:	22	22	22
F_bru^a, ksi:
(e/D = 1.5)
(e/D = 2.0)	70	70	70
F_bry^a, ksi:
(e/D = 1.5)
(e/D = 2.0)	45	45	45
e, percent:
L	5	5	5	4	5	5
E, 10³ ksi	6.5
E_c, 10³ ksi	6.5
G, 10³ ksi	2.4
μ	0.35
Physical Properties:
ω, lb/in.³	0.0659
C, K, and α	See Figure 4.2.3.0

61. PDF page 855

Specification	AMS 4352									AMS 4362
Form	Extruded rod, bar, and solid shapes						Extruded hollow shapes	Extruded tube		Die forging	Hand forging
Temper	T5
Cross-sectional area, in.²	<2.000	2.000- 2.999	3.000- 4.999	5.000- 9.999	10.000- 24.999	25.000- 39.999	All	≤3.000 in. O.D.	3.000- 8.500 in. O.D.
Thickness, in.	All	All	All	All	All	All	All	0.028- 0.250 wall	0.094- 1.188 wall	≤3.000	≤6.000
Basis	S	S	S	S	S	S	S	S	S	S	S
Mechanical Properties:
Ftu, ksi:
L	45	45	45	45	45	43	46	46	44	42	38
LT									1
Fy, ksi:
L	36	36	36	34	34	31	38	38	33	26	20
LT											20
Fcy, ksi:
L	30	28	25	23	22	20	26	26	21
LT
Fsu, ksi	22	22	22
Fbru, ksi:
(e/D = 1.5)
(e/D = 2.0)	71	71	71
Fbry, ksi:
(e/D = 1.5)
(e/D = 2.0)	47	47	47
e, percent:
L	4	4	4	6	6	6	4	4	4	7	7
E, 10³ ksi										6.5
E_c, 10³ ksi										6.5
G, 10³ ksi										2.4
μ										0.35
Physical Properties:
w, lb/in.³										0.0659
C, K, and α										See Figure 4.2.3.0

62. PDF page 864

Specification	AMS 4437	AMS 4452
Form	Sand casting	Investment casting
Temper	T6	T6
Location within casting	Any area
Basis	S	S
Mechanical Properties^a:
F_tu, ksi	17^b	17^b
F_ty, ksi	12^b	12^b
F_cy, ksi	12	12
F_su, ksi
F_bru, ksi:
(e/D = 1.5)
(e/D = 2.0)
F_bry, ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent	0.75^b	1^b
E, 10³ ksi	6.5
E_a, 10³ ksi		6.5
G, 10³ ksi	2.4
μ		0.35
Physical Properties:
ω, lb./in.³	0.0652
C, Btu/(lb)(°F)	0.25^c
K, Btu/[(hr)(ft²)(°F)/ft]	41 (212°F to 572°F)
a, 10^-6 in./in./°F	14 (65°F to 212°F)

63. PDF page 868

Specification	AMS 4484^a	AMS 4434	AMS 4453
Form	Permanent mold casting	Sand casting	Investment Casting
Temper	T6	T6	T6
Location within casting	Any area
Basis	S	S	S
Mechanical Properties^b:
F_tu, ksi	17^c	17^c	19
F_ty, ksi	13.5^c	13.5^c	15
F_cy, ksi	13.5	13.5	…
F_su, ksi	…	…	…
F_bru, ksi:
(e/D = 1.5)	…	…	…
(e/D = 2.0)	…	…	…
F_bry, ksi:
(e/D = 1.5)	…	…	…
(e/D = 2.0)	…	…	…
e, percent	…	…	0.7
E, 10³ ksi		6.5
E_c, 10³ ksi		6.5
G, 10³ ksi		2.4
μ		0.35
Physical Properties:
ω, lb./in.³		0.0659
C, Btu/(lb)(°F)		0.25^d
K and α		See Figure 4.3.3.0

64. PDF page 874

Specification	AMS 4442
Form	Sand casting
Temper	T5
Location within casting	Any area
Basis	S
Mechanical Properties^a:
F_tu, ksi	13^b
F_ty, ksi	11^b
F_cy, ksi	11
F_su, ksi
F_bru, ksi:
(e/D = 1.5)
(e/D = 2.0)
F_bry, ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent	1.5
E, 10³ ksi	6.5
E_c, 10³ ksi	6.5
G, 10³ ksi	2.4
μ	0.35
Physical Properties:
ω, lb/in.³	0.0659
C, Btu/(lb)(°F)	0.25
K and α	See Figure 4.3.4.0

65. PDF page 898

Specification	Form
AMS 4900	Sheet, strip, and plate
AMS 4901	Sheet, strip, and plate
AMS 4902	Sheet, strip, and plate
AMS-T-9046	Sheet, strip, and plate
MIL-T-9047^a	Bar
AMS 4921	Bar
AMS-T-81556	Extruded bars and shapes

66. PDF page 922

Specification	AMS 4916, AMS-T-9046, and Comp. A-4
Form	Sheet			Plate
Condition	Duplex Annealed
Thickness, in.	0.015-0.024	0.025-0.1875	0.1875-0.500	0.501-1.000	1.001-2.000	2.001-4.000
Basis	S	S	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L	135	135	130	130	125	120
LT	135	135	130	130	125	120
F_ty, ksi:
L	120	120	120	120	115	110
LT	120	120	120	120	115	110
F_cy, ksi:
L	126	126
LT	126	126
F_sy, ksi	84	84
F_bru, ksi:
(e/D = 1.5)	223	223
(e/D = 2.0)	269	269
F_bry, ksi:
(e/D = 1.5)	174	174
(e/D = 2.0)	191	191
e, percent:
L	8	10	10	10	10	8
LT	8	10	10	10	10	8
E, 10³ ksi				17.5^a
E, 10³ ksi				18.0^a
G, 10³ ksi				6.7
μ				0.32
Physical Properties:
ω, lb/in.³					0.158
C, Btu/(lb)(°F)					0.12
K and a					See Figure 5.3.2.0

67. PDF page 951

Specification	AMS 4962
Form	HIP Casting
Temper	Annealed
Thickness, in.	≤1.000
Location within casting	Designated area
Basis	A	B
Mechanical Properties:
F_u, ksi	125^a	128
F_y, ksi	119	122
F_cv, ksi
F_su, ksi
F_bru, ksi:
(e/D = 1.5)
(e/D = 2.0)
F_bry, ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent (S-basis)	5
E, 10³ ksi	16.9
E_c, 10³ ksi	16.9
G, 10³ ksi
μ
Physical Properties:
ω, lb/in.³
C, Btu/(lb)(°F)
K, Btu/[(hr)(ft²)(°F)/ft]
α, 10^-6 in./in./°F

68. PDF page 989

Specification	MIL-T-81556 & AMS-T-81556, Comp. AB-3
Form	Extruded bar and shapes
Condition	Annealed				Solution treated and aged
Thickness or diameter, in.	≤2.000		2.001- 3.000	3.001- 4.000	0.188- 0.500	0.501- 1.500	1.501- 2.500	2.501- 4.000
Basis	A	B	S	S	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L	142	148	145	140	170	165	160	150
LT	141	148	145	140	170	165	160	150
F_ty, ksi:
L	129	135	135	130	160	155	150	140
LT	128	135	135	130	160	155	150	140
F_cy, ksi:
L	137	144	140	135	165	160	155	145
LT	136	142	140	135	165	160	155	145
F_su, ksi	93	97
F_bru^a, ksi:
(e/D=1.5)	218	229
(e/D=2.0)	268	281
F_bry^a, ksi:
(e/D=1.5)	196	203
(e/D=2.0)	227	235
e, percent (S-basis):
L	10		10	10	8	8	8	8
LT	8		8			6	6	6
RA, percent (S-basis):
L	20		20	20	15	15	15	15
LT	15			15	12	12	12	12
E, 10³ ksi					16.0
E_c, 10³ ksi					16.4
G, 10³ ksi					6.2
μ					0.31
Physical Properties:
ω, lb/in.³					0.164
C, K, and α					See Figure 5.4.2.0

69. PDF page 1032

Specification	Form
AMS 4983	Forging
AMS 4984	Forging
AMS 4986	Forging

70. PDF page 1037

5.1.2(a)	Jaffe, R. I., “The Physical Metallurgy of Titanium Alloys”, Progress in Metal Physics, Vol. 7, Pergammon Press, Oxford, England, pp 65-167 (1958).
5.1.2(b)	“Aircraft Designer's Handbook for Titanium and Titanium Alloys”, AFML-TR-67-142 (March 1967).
5.1.2(c)	Larson, F. R., “Anisotropy in Titanium Sheet in Uniaxial Tension”, ASM Transactions, 57, pp 620-631 (1964).
5.1.2(d)	Larson, F. R., “Textures in Titanium Sheet and Its Effects on Plastic Flow Properties”, Army Materials Research Agency, AMRA-TR-65-24 (October 1965).
5.1.4(a)	VanEcho, J. A., “Low Temperature Creep Characteristics of Ti-5A1-2.4Sn and Ti-6A1-4V Alloys”, DMIC Technical Note, Defense Metals Information Center, Battelle Memorial Institute, Columbus, Ohio (June 8, 1964).
5.1.4(b)	Broadwell, R. G., Hatch, A. J., Partridge, J. M., “The Room Temperature Creep and Fatigue Properties of Titanium Alloys”, Journal of Materials, 2, (1), pp 111-119 (March 1967).
5.1.4(c)	Reimann, W. H., “Room Temperature Creep in Ti-6A1-4V”, AFML-TR-68-171 (June 1968).
5.1.4(d)	White, E. L., and Ward, J. J., “Ignition of Metals in Oxygen”, DMIC Report 224, Defense Metals Information Center, Battelle Memorial Institute, Columbus, Ohio (February 1, 1966).
5.1.4(e)	Jackson, J. D., and Boyd, W. K., “Corrosion of Titanium”, DMIC Memorandum 218, Defense Metals Information Center, Battelle Memorial Institute, Columbus, Ohio (September 1, 1966).
5.1.4(f)	“Accelerated Crack Propagation of Titanium by Methanol, Halogenated Hydrocarbons, and Other Solutions”, DMIC Memorandum 228, Defense Metals Information Center, Battelle Memorial Institute, Columbus, Ohio (March 6, 1967).
5.1.4(g)	Lectures from AICE Materials Conference, “Titanium for the Chemical Engineer”, DMIC Memorandum 234, Defense Metals Information Center, Battelle Memorial Institute, Colum-bus, Ohio (April 1, 1968).
5.3.1.1.9	Wanhill, R. J. et al, “Fatigue Crack Propagation Data for Titanium Sheet Alloys”, Interim Report NLR-TR-72093U, National Aerospace Laboratory, The Netherlands (July 1972) (MCIC 88911).
5.3.2.2.8(a)	McCulloch, A. J., Melcon, M. A., and Young, L., “Fatigue Behavior of Sheet Materials for the Supersonic Transport, Volume 1—Summary and Analysis of Fatigue and Static Test Data”, Lockheed-California Company, AFML-TR-64-399, Volume 1, January 1965 (MCIC 62421).
5.3.2.2.8(b)	McCulloch, A. J., Melcon, M. A., and Young, L., “Fatigue Behavior of Sheet Materials for the Supersonic Transport: Volume 11—Static Test Data, S/N Test Data and S/N Diagrams”, Lockheed-California Company, AFML-TR-64-399, Volume II, January 1965 (MCIC 62422).
5.4.1.1.8(a)	“Fatigue Evaluation of Ti-6Al-4V Bar Stock”, Sikorsky Aircraft, Report No. SER-50631 (MIL-HDBK-5 Source M-459) (March 1970).

71. PDF page 1180

6.1.1.1	“Cryogenic Materials Data Handbook,” Air Force Materials Laboratory, Wright-Patterson Air Force Base, Ohio, AFML-TDR-64-280, 1970.
6.2.1.1.8	Blatherwick, A. A. and Cers, A., “Fatigue, Creep and Stress-Rupture Properties of Nicro-tung, Super A-286, and Inconel 718”, AFML-TR-65-4447 (June 1966) (MCIC 65927).
6.3.3.1.8(a)	Ruff, P. E., “Effect of Manufacturing Processes on Structural Allowables—Phase II”, AFWAL-TR-86-4120, Battelle (November 1986) (MIL-HDBK-5 Source M-656).
6.3.3.1.8(b)	Deel, O. L., and Mindlin, H., “Engineering Data on New Aerospace Structural Materials”, AFML-TR-71-249, Battelle (December 1971) (MIL-HDBK-5 Source M-465).
6.3.5.1.8(a)	Ruff, P. E., “Effect of Manufacturing Processes on Structural Allowables—Phase I,” AFWAL-TR-85-4128, Battelle (January 1986) (MIL-HDBK-5 Source M-654).
6.3.5.1.8(b)	Korth, G. E. and Smokik, G. R., “Status Report of Physical and Mechanical Test Data of Alloy 718”, EG&G Idaho Inc., TREE-1254 (March 1978) (MIL-HDBK-5 Source M-603).
6.3.5.1.9(a)	James, L. A., “Heat-to-Heat and/or Melt Practice Variations in Crack Growth Behavior of Inconel 718”, Mechanical Properties Test Data for Structural Materials, Quarterly Report for Period Ending October 31, 1977, Report ORNL-5349, pp. 196-199, Oak Ridge National Laboratory (December 1977).
6.3.5.1.9(b)	Mills, W. J. and James, L. A., “Effect of Heat-Treatment on Elevated Temperature Fatigue-Crack Growth Behavior of Two Heats of Alloy 718”, ASME Paper 78-WA-PVP-3 (December 1978).
6.3.5.1.9(c)	James, L. A., “Investigation of Potential Product Form Effects Upon the Fatigue-Crack Growth Behavior of Alloy 718”, Mechanical Properties Test Data for Structural Materials, Semiannual Progress Report for Period Ending July 31, 1979, Report ORNL/BRP-79/5, pp. 5.1-5.4, Oak Ridge National Laboratory (October 1979).
6.3.5.1.9(d)	James, L. A., “The Effect of Product Form Upon Fatigue-Crack Growth Behavior in Alloy 718”, Report HEDL-TME-80-11, Hanford Engineering Development Laboratory (March 1980).
6.3.5.1.9(e)	James, L. A. and Mills, W. J., “Effect of Heat-Treatment and Heat-to-Heat Variations in the Fatigue-Crack Growth Response of Alloy 718—Phase I: Macroscopic Variation”, Report HEDL-TME-80-9, Hanford Engineering Development Laboratory (March 1980).
6.3.5.1.9(f)	James, L. A., “Fatigue-Crack Propagation Behavior of Inconel 718”, Report HEDL-TME-75-80, Hanford Engineering Development Laboratory (September 1975).
6.3.5.1.9(g)	James, L. A., “Heat-to-Heat and/or Melt Practice Variations in Crack Growth Behavior of Alloy 718”, Mechanical Properties Test Data for Structural Materials, Quarterly Progress Report for Period Ending January 31, 1978, Report ORNL-5380, pp. 153-160, Oak Ridge National Laboratory (March 1978).

72. PDF page 1190

Specification	AMS 4860
Form	Sand and centrifugal casting
Condition	As cast
Location within casting	Any area
Basis	S
Mechanical Properties:
F_tu, ksi	65^a
F_ty, ksi	25^a
F_cy, ksi
F_su, ksi
F_bru, ksi:
(e/D = 1.5)
(e/D = 2.0)
F_bry, ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent	20^a
E, 10³ ksi	15.0
E_c, 10³ ksi
G, 10³ ksi
μ
Physical Properties:
ω, lb/in.³	0.301
C, Btu/(lb)(°F)	0.09 (at 68°F)
K, Btu/[(hr)(ft²)(°F)/ft]	50 (at 68°F)
α, 10^-6 in./in/°F	11.3 (68 to 212°F)
Electrical conductivity, % IACS	22.0

73. PDF page 1191

Specification	AMS 4862
Form	Sand and centrifugal casting
Condition	As cast
Location within casting	Any area
Basis	S
Mechanical Properties:
F_tu, ksi	110^a
F_ty, ksi	60^a
F_cy, ksi
F_su, ksi
F_bru, ksi:
(e/D = 1.5)
(e/D = 2.0)
F_bry, ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent	12^a
E, 10³ ksi	14.2
E_c, 10³ ksi
G, 10³ ksi
μ
Physical Properties:
ω, lb/in.³	0.283
C, Btu/(lb)(°F)	0.09 (at 68°F)
K, Btu/[(hr)(ft²)(°F)/ft]	20.5 (at 68°F)
α, 10^-6 in./in/°F	12.0 (68 to 500°F)
Electrical conductivity, % IACS	8.0

74. PDF page 1193

Specification	Form
ASTM B194	Strip (TB00, TD01, TD02, TD04)
AMS 4530^a	Strip (TB00)
AMS 4532^a	Strip (TD02)
AMS 4650	Bar, rod, shapes, and forgings (TB00)
AMS 4533	Bar and rod (TF00)
AMS 4535	Mechanical tubing (TF00)
AMS 4651	Bar and rod (TD04)
AMS 4534	Bar and rod (TH04)

75. PDF page 1193

Section	Temper
7.3.2.1	TF00
7.3.2.2	TH04

76. PDF page 1196

Specification…	AMS 4651
Form…	Rod and bar
Condition…	TH04
Thickness, in.…	<0.375	0.376-1.000	1.001-1.500	1.501-2.000
Basis…	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L…	185	180	175	175
ST…	…	…	…	169
F_ty, ksi:
L…	145	145	145	145
ST…	…	…	…	140
F_cy, ksi:
L…	…	148	148	148
ST…	…	…	…	154
F_su, ksi…	…	89	90	93
F_bru^a, ksi:
(e/D = 1.5)	…	242	235	235
(e/D = 2.0)	…	306	298	298
F_bry^a, ksi:
(e/D = 1.5)	…	207	207	207
(e/D = 2.0)	…	225	225	225
e, percent:
L…	…	1	2	2
E, 10³ ksi…	18.5
E, 10³ ksi…	18.7
G, 10³ ksi…	7.3
μ…	0.27
Physical Properties:
ω, lb/in.³…	0.298
C, K, and α…	…

77. PDF page 1213

Specification	Form
AMS 4254	Sheet laminate

78. PDF page 1246

	Unit Bearing Strength for Indicated Rivet Diameter, lbs
Sheet thickness, in.	1/16	3/32	1/8	5/32	3/16	1/4	5/16	3/8
0.012	80	…	…	…	…	…	…	…
0.016	107	…	…	…	…	…	…	…
0.018	121	173	…	…	…	…	…	…
0.020	134	192	…	…	…	…	…	…
0.025	168	240	321	…	…	…	…	…
0.032	214	307	411	509	…	…	…	…
0.036	241	346	462	572	688	…	…	…
0.040	268	384	514	636	764	…	…	…
0.045	302	432	578	716	860	…	…	…
0.050	335	480	642	795	955	1285	…	…
0.063	422	605	810	1002	1203	1619	2035	…
0.071	476	682	912	1129	1356	1825	2293	2741
0.080	536	768	1028	1272	1528	2056	2584	3088
0.090	603	864	1156	1431	1719	2313	2907	3474
0.100	670	960	1285	1590	1910	2570	3230	3860
0.125	838	1200	1606	1988	2388	3212	4038	4825
0.160	1072	1536	2056	2544	3056	4112	5168	6176
0.190	1273	1824	2442	3021	3629	4883	6137	7334
0.250	1670	2400	3210	3975	4775	6425	8075	9650

79. PDF page 1253

Rivet Type	MS20426DD (F_su = 41 ksi)
Sheet Material	2024-T3 2024-T42		2024-T62 2024-T81		2024-T86 7075-T6
Rivet Diameter, in.	3/16	1/4	3/16	1/4	3/16	1/4
(Nominal Hole Diameter, in.)	(0.191)	(0.257)	(0.191)	(0.257)	(0.191)	(0.257)
	Ultimate Strength, lbs.
Sheet thickness, in.:
0.032	744		786		786
0.040	941	879	982	1300	982	1300
0.050	1110	1359	1152	1705	1152	1705
0.063	1175	1727	1175	2010	1175	2010
0.071		1883		2125		2125
0.080		2025
0.090		2125
Rivet shear strength^c	1175	2125	1175	2125	1175	2125
	Yield Strength^d, lbs.
Sheet thickness, in.:
0.032	582		649		786
0.040	666	879	816	962	982	978
0.050	738	1308	961	1308	1152	1543
0.063	925	1564	1068	1564	1175	1958
0.071		1711		1711		2125
0.080		1928
0.090		2121
Head height (max.), in.	0.070	0.095	0.070	0.095	0.070	0.095

80. PDF page 1275

Rivet Type	NAS1398C^a and NAS1398C, Code A^b (F_su = 75 ksi)			CR 2643^a (F_su = 95 ksi)
Sheet Material	Alloy Steel F_tu = 180 ksi
Rivet Diameter, in (Nominal Hole Diameter, in.)	1/8 (0.130)	5/32 (0.162)	3/16 (0.194)	1/8 (0.130)	5/32 (0.162)	3/16 (0.194)
	Ultimate Strength^c, lbs
Sheet thickness, in.:
0.025	697			697
0.032	785	1112		807	1112
0.040	860	1211	1628	911	1246	1639
0.050	956	1325	1772	1043	1406	1833
0.063	970	1480	1958	1215	1615	2090
0.071		1490	2070	1230	1748	2240
0.080			2150		1885	2420
0.090						2610
0.100						2720
Rivet shear strength	970^d	1490^d	2150^d	1230^e	1885^e	2720^e

81. PDF page 1278

Rivet Type	NAS1398B^a (F_su = 30 ksi)				NAS1398D^a (F_su = 38 ksi)
Sheet Material	Clad 2024-T3
Rivet Diameter, in. (Nominal Hole Diameter, in.)	1/8 (0.130)	5/32 (0.162)	3/16 (0.194)	1/4 (0.258)	1/8 (0.130)	5/32 (0.162)	3/16 (0.194)	1/4 (0.258)
	Ultimate Strength, lbs.
Sheet thickness, in.:
0.025	228				228
0.032	289		364	412	304	364
0.040	337	448	553	670	355	470	553
0.050	388	521	662	914	418	548	696	914
0.063		596	781	1145	494	647	816	1205
0.071			854	1240		710	894	1303
0.080			862	1350		755	975	1420
0.090				1475			1069	1545
0.100				1550			1090	1670
0.125								1970
Rivet shear strength^b	388	596	862	1550	494	755	1090	1970

82. PDF page 1298

Rivet Type	MS20601M (F_su = 55 ksi)
Sheet Material	AISI 301-Annealed				AISI 301-1/4 Hard
Rivet Diameter, in.	1/8	5/32	3/16	1/4	1/8	5/32	3/16	1/4
(Nominal Hole Diameter, in.)	(0.130)	(0.162)	(0.194)	(0.258)	(0.130)	(0.162)	(0.194)	(0.258)
	Ultimate Strength, lbs.
Sheet thickness, in.:
0.010	224				277	377
0.012	254	338			302	428	560
0.016	313	412	519		358	485	632
0.020	375	486	610		415	542	705	1135
0.025	447	576	722	1045	482	642	808	1230
0.032	516	705	876	1255	543	750	963	1400
0.040	536	793	1055	1490	585	833	1110	1660
0.050	565	825	1150^a	1790	628	910	1240	1930
0.063		868	1200^a	2065		964	1330	2175
0.071				2100		973	1375	2275
0.080				2150			1405	2340
0.090				2200				2440
0.100								2510
Rivet shear strength^a	635	973	1405	2540	635	973	1405	2540
	Yield Strength^b, lbs.
Sheet thickness, in.:
0.010	188				244	291
0.012	214	281			259	335	423
0.016	270	352	438		333	428	535
0.020	328	422	518		398	528	639	896
0.025	397	506	627	873	443	612	774	1080
0.032	498	627	770	1070	505	689	912	1330
0.040	536	772	939	1310	576	779	1015	1590
0.050	565	825	1150	1590	619	883	1145	1770
0.063		868	1200	1970		954	1305	2000
0.071				2100		973	1350	2140
0.080				2150			1400	2305
0.090				2200				2395
0.100								2475
Head height (ref.), in.	0.042	0.055	0.070	0.095	0.042	0.055	0.070	0.095

83. PDF page 1326

	Ultimate Strength, lbs.
Sheet thickness, in.:
0.040	143°	---	---
0.050	247	224°	---
0.063	383	393	370°
0.071	414	497	494
0.080	435	614	634
0.090	457	647	790
0.100	480	676	902
0.125	537	746	987
0.160	616	846	1105
0.190	---	931	1205
0.250	---	---	1410

84. PDF page 1326

Rivet shear strength^d	664	1030	1480
	Yield Strength, lbs^e
Sheet thickness, in.:
0.040	143	---	---
0.050	235	224	---
0.063	310	371	370
0.071	330	431	491
0.080	353	486	572
0.090	379	518	662
0.100	404	549	713
0.125	468	629	808
0.160	557	740	914
0.190	---	835	1055
0.250	---	---	1280
Head height [ref.], in	0.042	0.055	0.070

85. PDF page 1336

Fastener Type	FF-200^a		FF-260^a		FF-312^a
Sheet and Plate Material	Clad 2024-T42	Clad 7075-T6	Clad 2024-T42	Clad 7075-T6	Clad 2024-T42	Clad 7075-T6
Fastener Diameter, in.	3/16	3/16	1/4	1/4	5/16	5/16
(Nominal Shank Diameter, in.)	(0.198)	(0.198)	(0.259)	(0.259)	(0.311)	(0.311)
	Ultimate Strength, lbs
Sheet or plate thickness, in.:
0.071	1220^b,c	1360^b,c
0.080	1380^b	1500^b
0.090	1520^b	1620^b
0.100	1650^b	1740^b	2250^b,c	2700^b,c
0.125	1890^b	1960	2940^b	3220^b	2720^c	3080^b,c
0.160	2160	2200	3390^b	3570^b	3600^b	3940^b
0.190	2400	2420	3730^b	2860^b	4490^b	4810^b
0.250	2620	2620	4260^b	4320	5550^b	6000^b
0.312			4500	4500	6000^b
Fastener shear strength^d			4500	4500	6000	6000
	Yield Strength^e, lbs
Sheet or plate thickness, in.:
0.071	685	850
0.080	770	930
0.090	870	1025
0.100	980	1130	1120	1280
0.125	1200	1350	1380	1600	1440	1540
0.160	1500	1640	1700	2050	1820	1980
0.190	1800	1960	2010	2470	2200	2520
0.250	2400	2550	2600	3190	2950	3710
0.312			3200	3880	3690
Head height (ref.), in.	0.077		0.102		0.134

86. PDF page 1377

Fastener Type	HL 18 Pin (F_su = 95 ksi), HL 70 Collar^a
Sheet Material	Clad 7075-T6
Fastener Diameter, in. (Nominal Shank Diameter, in.)^b	5/32	3/16	1/4	5/16
Fastener Diameter, in. (Nominal Shank Diameter, in.)^b	(0.164)	(0.190)	(0.250)	(0.312)
Sheet thickness, in.:	Ultimate Strength, lbs.
0.050	1078
0.063	1353	1559
0.071	1520	1776
0.080	1718	1957	2593
0.090	1890	2224	2937
0.100	1930	2473	3250	4050
0.125	2007	2580	4063	5075
0.160		2694	4450	6509
0.190			4620	6880
0.250			4660	7290
Rivet shear strength^c	2007	2694	4660	7290
Sheet thickness, in.:	Yield Strength^d, lbs.
0.050	976
0.063	1251	1426
0.071	1430	1624
0.080	1589	1848	2344
0.090	1746	2065	2687
0.100	1875	2242	3031	3660
0.125		2563	3750	4734
0.160			4406	6051
0.190				6686

87. PDF page 1378

Fastener Type	HL 19 Pin (F_su = 95 ksi), HL 70 Collar^a
Sheet Material	Clad 7075-T6
Fastener Diameter, in.	5/32	3/16	1/4	5/16
(Nominal Shank Diameter, in.)^b	(0.164)	(0.190)	(0.250)	(0.312)
Sheet thickness, in.:	Ultimate Strength, lbs.
0.050	968	…	…	…
0.063	1251	1408	…	…
0.071	1400	1606	…	…
0.080	1595	1823	2344	…
0.090	1815	2050	2675	…
0.100	1903	2300	3000	3660
0.125	2005	2570	3781	4685
0.160	…	2694	4420	6051
0.190	…	…	4625	6832
0.250	…	…	4660	7290
Rivet shear strength^c	2007	2694	4660	7290
Sheet thickness, in.:	Yield Strength^d, lbs.
0.050	839	…	…	…
0.063	1031	1191	…	…
0.071	1141	1336	…	…
0.080	1279	1480	2013	…
0.090	1416	1632	2219	…
0.100	1540	1805	2420	3143
0.125	1807	2173	3000	3777
0.160	…	2545	3670	4800
0.190	…	…	4144	5514
0.250	…	…	…	6686
Head height (nom.), in.	0.040	0.046	0.060	0.067

88. PDF page 1380

Fastener Type	MIL-B-8831/4^a (F_su = 108 ksi)
Sheet Material	Clad 7075-T6
Fastener Diameter, in. (Nominal Hole Diameter, in.)^b,c	3/16 (0.2390)	1/4 (0.3032)	5/16 (0.3695)	3/8 (0.4350)	7/16 (0.5022)	1/2 (0.5735)
Sheet thickness, in.:	Ultimate Strength, lbs.
0.100	2585
0.125	3205	4100	5035
0.160	3290	5205	6385	7560	8790
0.190		5670	7535	8925	10360	11900
0.250			8760	11640	13495	15480
0.312				12395	16195	19180
0.375				12640	16625	21265
0.500					17100	22250
Rivet shear strength^d	3290	5670	8760	12640	17100	22250
Sheet thickness, in.:	Yield Strength, lbs.^e
0.100	2080
0.125	2570	3300	4075
0.160	3255	4170	5135	6105	7125
0.190		4915	6040	7175	8360	9635
0.250			7855	9310	10825	12450
0.312				11520	13375	15360
0.375				12355	15620	18320
0.500						21570
Sleeve head height (ref.), in.	0.062	0.075	0.082	0.093	0.115	0.120

89. PDF page 1388

Material Ultimate Tensile Strength, ksi	Design Shear Strength, pounds per spot
Material Ultimate Tensile Strength, ksi	Above 185	150 to 185	90 to 149	Below 90
Nominal thickness of thinner sheet, in.:
0.009..	160	140	104	80
0.010..	196	164	128	92
0.012.	280	220	160	120
0.016..	384	320	236	172
0.018.	472	392	272	200
0.020.	508	424	312	224
0.022.	584	488	360	264
0.025	696	580	424	320
0.028.	820	684	508	372
0.032.	1000	836	620	452
0.036.	1200	1004	736	552
0.040.	1400	1168	852	652
0.045.	1680	1436	1028	804
0.050.	1960	1700	1204	956
0.056..	2304	2040	1416	1168
0.063.	2840	2472	1688	1408
0.071.	3360	2984	2028	1664
0.080..	3880	3528	2404	1964
0.090..	4480	4072	2812	2308
0.100.	5040	4576	3200	2640
0.112.	5600	5092	3636	3036
0.125.	6228	5664	4052	3440

90. PDF page 1393

Material Ultimate Tensile Strength, ksi	Design Shear Strength, pounds per spot
Material Ultimate Tensile Strength, ksi	56 and Above	35 to 56	19.5 to 34.9	Below 19.5
Nominal thickness of thinner sheet, in.:
0.010	48	40	…	…
0.012	60	52	24	16
0.016	88	80	56	40
0.018	100	92	68	52
0.020	112	108	80	64
0.022	128	124	96	76
0.025	148	140	116	88
0.028	172	164	140	108
0.032	208	188	168	132
0.036	244	220	204	156
0.040	276	248	240	180
0.045	324	296	280	208
0.050	372	344	320	236
0.056	444	412	380	272
0.063	536	488	456	316
0.071	660	576	516	360
0.080	820	684	612	420
0.090	1004	800	696	476
0.100	1192	936	752	540
0.112	1424	1072	800	588
0.125	1696	1300	840	628
0.140	2020	1538	…	…
0.160	2496	1952	…	…
0.180	2980	2400	…	…
0.190	3228	2592	…	…
0.250	5880	5120	…	…

91. PDF page 1394

	Single Row Joints						Multiple Row Joints
	7075-T6 clad		2024-T3 clad		6061-T6		7075-T6 clad		2024-T3 clad		6061-T6
Thickness of Thinnest Sheet, in.	Strength, lbs/in.	Pitch, in.	Strength, lbs/in.	Pitch, in.	Strength, lbs/in.	Pitch, in.	Strength, lbs/in.	Pitch+No. of Rows, in.	Strength, lbs/in.	Pitch+No. of Rows, in.	Strength, lbs/in.	Pitch+No. of Rows, in.
0.010	288	0.167	250	0.192	210	0.190	438	0.110	384	0.125	329	0.122
0.012	346	0.173	300	0.200	252	0.206	526	0.114	461	0.130	395	0.132
0.016	461	0.191	400	0.220	336	0.238	701	0.126	614	0.143	526	0.152
0.020	577	0.194	500	0.224	420	0.257	876	0.128	768	0.146	658	0.164
0.025	721	0.205	625	0.237	525	0.267	1095	0.135	960	0.154	822	0.170
0.032	923	0.225	800	0.260	672	0.280	1402	0.148	1229	0.169	1053	0.179
0.040	1059	0.261	918	0.301	778	0.319	1752	0.158	1536	0.180	1316	0.188
0.050	1230	0.302	1067	0.349	910	0.378	2190	0.170	1920	0.194	1645	0.209
0.063	1452	0.369	1259	0.426	1082	0.451	2759	0.194	2419	0.222	2073	0.235
0.071	1589	0.415	1378	0.479	1187	0.485	3110	0.212	2726	0.242	2336	0.247
0.080	1742	0.471	1511	0.543	1306	0.524	3504	0.234	3072	0.267	2632	0.260
0.090	1913	0.525	1660	0.605	1438	0.556	3942	0.255	3456	0.290	2961	0.270
0.100	2084	0.572	1808	0.659	1580	0.596	4380	0.272	3840	0.310	3290	0.284
0.112	2289	0.622	1986	0.717	1728	0.620	4906	0.290	4301	0.331	3685	0.291
0.125	2511	0.675	2179	0.788	1900	0.684	5475	0.310	4800	0.353	4112	0.316

92. PDF page 1403

Material Ultimate Tensile Strength, ksi	Design Shear Strength, pounds per spot
Material Ultimate Tensile Strength, ksi	Above 100	100 and Below
Nominal thickness of thinner sheet, in.:
0.010	164	128
0.012	220	160
0.016	320	236
0.018	392	272
0.020	424	312
0.022	488	360
0.025	580	424
0.028	684	508
0.032	836	620
0.036	1004	736
0.040	1168	852
0.045	1438	1028
0.050	1702	1204
0.056	2040	1416
0.063	2400	1688
0.071	2702	1914
0.080	3048	2160
0.090	3430	2435
0.100	3810	2702
0.112	4260	3030
0.125	4760	3380

93. PDF page 1572

Subpopulation	n	X̅, ksi	s, ksi
Group (1) TUS (LT), 0.020 to 0.125	300	150.0	4.00
Group (3) TUS (LT), 0.020 to 0.125	30	151.0	5.00

Found in

January