January 2003 · MIL-HDBK-5J

277 tables appear under this heading.

1. PDF page 14

Chapter(s)	Subjects
1	Nomenclature, Systems of Units, Formulas, Material Property Definitions, Failure Analysis, Column Analysis, Thin-Walled Sections
2-7	Material Properties
8	Joint Allowables
9	Data Requirements, Statistical Analysis Procedures

2. PDF page 87

Specimen Details:		Notched, K_t = 2.0
Notch Type	Gross Width	Net Width	Notch Radius
Edge	2.25	1.500	0.3175
Center	4.50	1.500	1.500
Fillet	2.25	1.500	0.1736

3. PDF page 88

Specimen Details:		Notched, K_t = 4.0
Notch	Gross	Net	Notch
Type	Width	Width	Radius
Edge	2.25	1.500	0.057
Edge	4.10	1.496	0.070
Fillet	2.25	1.500	0.0195

4. PDF page 102

TUS, ksi	TYS, ksi	Temp., °F
158	147	RT
		(unnotched)
190	—	RT
		(notched)

5. PDF page 104

TUS, ksi	TYS, ksi	Temp., °F
158	147	RT
		(unnotched)
153	121	600
		(unnotched)
190	—	RT
		(notched)
176	—	600
		(notched)

6. PDF page 106

TUS, ksi	TYS, ksi	Temp., °F
158	147	RT (unnotched)
125	101	800 (unnotched)
190	—	RT (notched)
154	—	800 (notched)

7. PDF page 107

TUS, ksi	TYS, ksi	Temp., °F
158	147	RT
		(unnotched)
81	63	1000°F
		(unnotched)
190	—	RT
		(notched)
98	—	1000°F
		(notched)

8. PDF page 111

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	266, 291	232	RT (unnotched)
	352	—	RT (notched)

9. PDF page 114

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	274-294	227-247	RT

10. PDF page 118

Specimen Thickness:	0.900-1.000 inches	Environment:	Low-humidity air
Specimen Width:	3.09-7.41 inches	Temperature:	RT
Specimen Type:	CT	Orientation:	L-T and T-L

11. PDF page 119

Specimen Thickness:	0.70-0.75 inch	Environment:	Dry air and lab air
Specimen Width:	1.5-5.0 inches	Temperature:	RT
Specimen Type:	CT	Orientation:	L-T

12. PDF page 148

a Elongation properties vary with thickness as follows:
≤0.090	2.5%
0.091-0.125	3.0%
0.126-0.250	4.0%
0.251-0.375	5.0%
≥0.376	6.0%

13. PDF page 149

a	Noncurrent specification.
b	Elongation properties vary with thickness as follows:
≤0.090	2.5%
0.091-0.125	3.0%
0.126-0.250	4.0%
0.251-0.375	5.0%
≥0.376	6.0%

14. PDF page 170

Specification	Form
AMS 5548	Sheet and strip

15. PDF page 179

Thickness, inches	e (LT), percent in 2 inches
0.0005 to 0.0015	2
Over 0.0015 to 0.0020	3
Over 0.0020 to 0.0050	5
Over 0.0050 to 0.0100	7
Over 0.0100 to 0.1875	8

16. PDF page 189

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	192	188	RT (unnotched)
	304	—	RT (notched)

17. PDF page 201

Product Form:	Bar, 1.0625 inch diameter			Test Parameters:
					Loading - Axial
Properties:	TUS, ksi	TYS, ksi	Temp., °F		Frequency - 1800 cpm
	245	242	RT (unnotched)		Temperature - RT
	361	—	RT (notched)		Environment - Air
				No. of Heats/Lots:	1
Specimen Details:	Notched, V-Groove, K₁ = 3.0			Equivalent Stress Equation:
	0.283 inch gross diameter				Log N₁ = 7.42-1.90 log (Seq-47.34)
	0.200 inch net diameter				Seq = Smax (1-R)0.515
	0.010 inch root radius, r				Std. Error of Estimate, Log (Life) = 0.246
	60( flank angle, Ȧ				Standard Deviation, Log (Life) = 0.568
					R2 = 81%
Surface Condition:	Polished with abrasive nylon cord			Sample Size =	17
Reference:	2.6.3.1.8				[Caution: The equivalent stress model may pro-vide unrealistic life predictions for stress ratios beyond those represented above.]

18. PDF page 219

Gross Diameter	Net Diameter	Notch Root Radius
0.750	0.252	0.013
0.500	0.250	0.013

19. PDF page 220

Product Form:	Forged bar, 7 x 7 inches	Test Parameters:	Loading - Axial Frequency - Not Specified Temperature - RT Environment - Air
Properties:	TUS, ksi TYS, ksi Temp., °F 210 204 RT
Specimen Details:	Unnotched 0.500 inch gross diameter 0.250 inch net diameter	No. of Heats/Lots:	2
Surface Condition:	Machined to RMS 63-270, solution treated and aged, grit blasted	Equivalent Stress Equation:	Log N_f = 18.12-6.54 log (S_eq) S_eq = S_max (1-R)^0.11 Std. Error of Estimate, Log (Life) = 0.263 Standard Deviation, Log (Life) = 0.475 R² = 69%
Reference:	2.6.6.1.8(c)

20. PDF page 233

Properties:	TUS, ksi	TYS, ksi	Temp, °F
Longitudinal	163	159	RT
Long Transverse	164	160	RT
Longitudinal	278	—	RT (notched)
Long Transverse	277	—	RT (notched)

21. PDF page 234

Product Form:	Plate, 0.808 inch, 2.024 inch, and 2.579 inch thick
Properties:
	TUS, ksi	TYS, ksi	Temp, °F
Longitudinal	169.9	165.7	RT
Long Transverse	170.2	166.1	RT
Specimen Details:	Unnotched 0.250 inch diameter
Surface Condition: Axial, ground RMS 8
Reference: 2.6.7.2.8(b)

22. PDF page 234

Test Parameters:
Loading	Axial
Frequency	30 Hz
Temperature	RT
Atmosphere	Air

23. PDF page 235

Properties:	TUS, ksi	TYS, ksi	Temp, °F
Longitudinal	170.8	165.6	RT
Long Transverse	170.2	166.1	RT

24. PDF page 235

Specimen Details: Notched, V-Groove, K_t = 3.0
Flat,	0.590-inch gross width 0.500-inch net width 0.025-inch root radius 60° flank angle, ω
Round,	0.374-inch gross diameter 0.252-inch net diameter 0.013-inch root radius 60° flank angle, ω
Surface Condition: RMS 32 notch
Reference: 2.6.7.2.8(b)

25. PDF page 244

Product Form:	Sheet, 0.025-inch
Properties:	TUS, ksi	TYS, ksi	Temp.,°F
	201	196	RT
Specimen Details:	Edge Notched, K_t = 4.0 2.25 inch gross width 1.50 inch net width 0.058 inch notch radius 0° flank angle, ω
Surface Condition:	Drilled holes near edges and slots milled from edge, corners of notch were beveled with rubber abrasive

26. PDF page 245

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	201	196	RT
	179	173	500

27. PDF page 246

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	201	196	RT
	179	173	500

28. PDF page 258

Specimen Details:	Unnotched	No. of Heats/Lots: Not specified
	1.25 inch gross diameter 0.252 inch net diameter	Equivalent Stress Equation: Log N_f = 30.6-11.2 log (S_eq)
Surface Condition:	Polished	S_eq = S_max (1-R)^0.52 Std. Error of Estimate, Log (Life) = 0.531
References:	2.6.9.1.8(a)	Standard Deviation, Log (Life) = 0.672 R² = 38%

29. PDF page 259

Gross diameter inches	Net diameter inches	Notch radius inches
0.430	0.300	0.016
0.357	0.252	0.013

30. PDF page 260

Properties:	TUS, ksi	TYS, ksi	Temp., °F
Product Form:	Bar, 0.787 inch diameter, vacuum melted			Test Parameters: Loading - Axial Frequency - 2000 cpm Temperature - RT Environment - Air
	Bar, 0.787 inch diameter, vacuum melted
	207	—	RT

31. PDF page 260

Product Form:	Bar, 0.787 inch diameter, vacuum melted
Properties:	TUS, ksi	TYS, ksi	Temp., °F
	207	—	RT
Specimen Details:	Circumferential V-Groove, Kₙ = 4.0 0.492 inch gross diameter 0.256 inch net diameter 0.008 inch notch radius, n 60° flank angle, ω
Surface Condition:	Machined and aged
Reference:	2.6.9.1.8(b)

32. PDF page 264

Product Form:	Bar, 2 x 6 inches
Properties:	TUS, ksi	TYS, ksi	Temp, °F
Longitudinal	165	161	RT
Long	164	158	RT
Transverse
Longitudinal	280	—	RT (notched)
Long	275	—	RT (notched)
Transverse

33. PDF page 265

Properties:	TUS, ksi	TYS, ksi	Temp, °F
	151	—	RT

34. PDF page 267

Treatment	Designation
1950 ± 25°F and air cool	Condition A

35. PDF page 267

Treatment	Designation
1400 ± 25°F - 90 minutes and cool to 55 ± 5°F for 30 minutes	Condition T

36. PDF page 267

Treatment	Designation
1050 ± 10°F - 90 minutes and air cool	TH1050

37. PDF page 269

Thickness, in.	Elongation (LT), percent
0.005 to 0.010	4
0.011 to 0.019	5
0.020 to 0.187	6

38. PDF page 278

Condition	Thickness, inches	Elongation (LT), percent
½ hard	0.015 and under	15
½ hard	0.016 and over	18
¾ hard	0.030 and under	10
¾ hard	0.031 and over	12
Full hard	0.015 and under	8
Full hard	0.016 and over	9

39. PDF page 323

Alloy and Temper	Test Direction	Thickness, inches	Stress, ksi	Referenced Specifications
7049-T73	ST	0.750-2.000	46^b	AMS-QQ-A-367, AMS 4111, ASTM B 247
7049-T73	ST	2.001-5.000	45^b
7050-T74	ST	0.750-6.000	35	AMS 4107
7050-T7452	ST	0.750-4.000	35	AMS 4333
7075-T73	ST	0.750-3.000	42^b	AMS-A-22771, AMS-QQ-A-367
		3.001-4.000	41^b	AMS 4241, ASTM B 247
		4.001-5.000	39^b	AMS 4141
		5.001-6.000	38^b
7075-T7352	ST	0.750-4.000	42^b	AMS-A-22771, AMS-QQ-A-367, AMS 4147, ASTM B 247
7075-T7352	ST	3.001-4.000	39^b
7075-T7354^c	ST	0.750-3.000	42	Company Specification
7075-T74^c	ST	0.750-3.000	35	AMS 4131
		3.001-4.000	31^d
		4.001-5.000	30^d
		5.001-6.000	29^d
7149-T73	ST	0.750-2.000	46^b	AMS 4320
7149-T73	ST	2.001-5.000	45^b
7175-T74	ST	0.750-3.000	35	AMS 4149, ASTM B 247
		3.001-4.000	31^d	AMS 4149
		4.001-5.000	30^d
		5.001-6.000	29^d
7175-T7452^c	ST	0.750-3.000	35	AMS 4179

40. PDF page 329

Section	Temper
3.2.1.1	T6, T62, T651, T652, T6510, and T6511

41. PDF page 330

Specification	AMS 4029
Form	Sheet						Plate
Temper	T6						T651
Thickness, in.	0.020-0.039		0.040-0.249		0.250-0.499		0.500-1.000		1.001-2.000		2.001-2.500		2.501-3.000		3.001-4.000
Basis	A	B	A	B	A	B	A	B	A	B	A	B	A	B	A	B
Mechanical Properties:
Ftu, ksi:
L	65	67	67	68	66	68	66	67	66	67	66	67	63	65	63	64
LT	64	66	66	67	67	69	67	68	67	68	65	66	63	64	62	63
ST											59	60	58	59	58	59
Fy, ksi:
L	58	60	59	60	60	62	60	61	60	62	59	61	57	59	57	58
LT	57	59	58	59	59	61	59	60	59	61	57	59	56	57	55	56
ST											54	56	53	54	53	54
Fsu, ksi:
L	58	60	59	60	58	60	58	59	58	60	57	59	56	57	56	57
LT	59	61	60	61	61	63	61	62	61	63	60	62	58	60	58	59
ST											59	61	58	59	58	59
Fbru, ksi:
(e/D = 1.5)	97	100	100	102	105	108	105	107	105	107	102	104	101	103	101	102
(e/D = 2.0)	123	127	127	129	134	138	134	136	134	136	130	132	129	131	129	130
Fbry, ksi:
(e/D = 1.5)	81	84	83	84	90	93	90	92	90	93	88	90	86	88	86	87
(e/D = 2.0)	93	96	94	96	106	110	106	109	106	110	104	106	102	104	102	103
e, percent (S-basis):
LT	6		7		7		6		4		2		2		1
E, 10³ ksi	10.5										10.5
E, 10³ ksi	10.7										10.7
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

42. PDF page 362

Gross Diameter, inches	Net Diameter, inches
1.00	0.400
0.273	0.100
---	0.200
---	0.160
1.00	0.500

43. PDF page 364

Product Form:	Rolled bar, 1.125 inch diameter			Test Parameters:
				Loading - Axial
Properties:	TUS, ksi	TYS, ksi	Temp.,°F	Frequency - 1800 cpm
	72	64	RT	Temperature - RT Environment - Air
Specimen Details:	Circumferential V-notch,			No. of Heats/Lots: Not specified
	K_t = 2.4
	0.500 inch gross diameter			Equivalent Stress Equation:
	0.400 inch net diameter			Log N_f = 10.59-4.36 log (S_eq-11.7)
	0.032 inch notch radius			S_eq = S_max (1-R)^0.52
	60° flank angle, ω			Std. Error of Estimate, Log (Life) = 0.38
Surface Condition:	Polished			Standard Deviation, Log (Life) = 1.18 R² = 90%
Reference:	3.2.1.1.8(b)
				Sample Size = 39

44. PDF page 365

Product Form:	Extruded bar, 1.125 inch diameter			Test Parameters:
					Loading - Axial
Properties:	TUS, ksi	TYS, ksi	Temp., °F		Frequency - 3600 cpm
	75	67	RT		Temperature - RT
					Environment - Air
Specimen Details:	Circumferential V-notch,			No. of Heats/Lots:	Not specified
	K_t = 3.4			Equivalent Stress Equation:
	0.450 inch gross diameter				Log N_f = 8.35-3.10 log (S_eq-10.6)
	0.400 inch net diameter				S_eq = S_max (1-R)^0.52
	0.010 inch notch radius				Std. Error of Estimate, Log (Life) = 0.34
	60° flank angle, ω				Standard Deviation, Log (Life) = 1.10
Surface Condition:	Smooth machine finish				R² = 90%
References:	3.2.1.1.8(b) and (c)			Sample Size =	45

45. PDF page 366

Product Form:	Hand forging, 3 x 6 inch	Test Parameters:	Loading - Axial
			Frequency - Not specified
			Temperature - RT
			Environment - Air
Properties:	TUS, ksi	TYS, ksi	Temp., °F
	Not specified		RT
Specimen Details:	Circumferential V-notch,	No. of Heats/Lots:	Not specified
	K_t = 2.4
	0.273 inch gross diameter	Maximum Stress Equation:	Log N_f = 12.4-5.95 log (S_max)
	0.100 inch net diameter		Std. Error of Estimate, Log (Life) = 0.53
	0.010 inch notch radius		Standard Deviation, Log (Life) = 0.91
	60° flank angle, ω		R² = 66%
Surface Condition:	Mechanically polished
Reference:	3.2.1.1.8(d)		Sample Size = 28

46. PDF page 370

Specification	Form
AMS 4037	Bare sheet and plate
AMS 4035	Bare sheet and plate
AMS-QQ-A-250/4	Bare sheet and plate
AMS-QQ-A-250/5	Clad sheet and plate
AMS 4120	Bar and rod, rolled or cold-finished
AMS-QQ-A-225/6	Rolled or drawn bar, rod, and wire
AMS 4086	Tubing, hydraulic, seamless, drawn
AMS-WW-T-700/3	Tubing
AMS 4152	Extrusion
AMS 4164	Extrusion
AMS 4165	Extrusion
AMS-QQ-A-200/3	Extruded bar, rod, and shapes

47. PDF page 372

Section	Temper
3.2.3.1	T3, T351, T3510, T3511, T4, and T42
3.2.3.2	T361 (supersedes T36)
3.2.3.3	T62 and T72
3.2.3.4	T81, T851, T8510, and T8511
3.2.3.5	T861 (supersedes T86)

48. PDF page 379

Specification	AMS-QQ-A-250/5
Form	Flat sheet and plate
Temper	T42ª										T62ª			T72ª
Thickness, in.	0.008-0.009		0.010-0.062		0.063-0.249		0.250-0.499	0.500-1.000b	1.001-2.000b	2.001-3.000bgs	0.010-0.062	0.063-0.249	0.250-0.499	0.010-0.062	0.063-0.249
Basis	A	B	A	B	A^°	B^°	Sc	Sc	Sd	S	S	Sc	Sc	S	S
Mechanical Properties:
F_tu, ksi:
L	55	57	57	59	60	62	60	59				66	62	62
LT	55	57	57	59	60	62	60	59				66	62	62
F_cy, ksi:
L	34	35	34	35	36	38	36	36				47	49	49
LT	34	35	34	35	36	38	36	36				47	49	49
F_sy, ksi:
L	38	39	38	39	40	42	39	38				49	51	51
LT	37	38	37	38	39	41	39	39				49	52	51
F_su, ksi:	33	34	34	35	36	37	36	35				35	36	36
F_bru, ksi:
(e/D = 1.5)	88	91	91	94	96	99	95	90				97	100	100
(e/D = 2.0)	109	113	113	117	119	123	119	117				126	130	130
F_bry, ksi:
(e/D = 1.5)	60	61	60	61	63	67	63	63				75	79	79
(e/D = 2.0)	72	74	72	74	76	80	76	76				89	93	93
e, percent (S-basis):
LT	10				15			12	8			5	5	5	5
E, 10³ ksi:
Primary				10.5				10.5				10.5
Secondary			9.5				10.0			10.2			10.0		10.2
E, 10³ ksi:
Primary			10.7				10.7			10.9			10.9	10.7	10.7
Secondary			9.7				10.2			10.4			10.2		10.4
G, 10³ ksi µ									0.33
Physical Properties:
w, lb/in.³									0.100
C, K, and α

49. PDF page 387

Specification	AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3
Form	Extruded bar, rod, and shapes
Temper	T3, T3510, and T3511													T81, T8510, and T8511
Thickness, in.	≤0.249		0.250-0.499		0.500-0.749		0.750-1.499		1.500-2.999			3.000-4.499		1.500- 2.999	3.000- 4.499	0.050- 0.249	0.250- 1.499	1.500- 4.500
Cross-Section Area, in.²	in.² <20								<25					>25-<32		<20		<32
Basis	A	B	A	B	A	B	A	B	A		B	A	B	S	S	S	S	S
Mechanical Properties: F, ksi:
L LT	57 54	61 58	60 56	62 57	60 54	62 56	65 56	70 60	70 55		74 58	70 54	74 57	68 53	68 52	64 64	66 62	66 61
Fy, ksi:
L	42	47	44	47	44	47	46	54	52		54	52	54	48	48	56	58	58
LT	37	41	38	40	37	39	37	43	39		41	39	41	36	36	55	57	57
Fcy, ksi:	27
L	34	38	37	39	38	40	41	48	49		50	49	51	45	45	57	59	59
LT	41	45	41	44	40	43	40	47	42		44	41	43	39	38	57	59	59
Fbry, ksi:	29	31	31	32	30	31	33	35	34		36	33	35	33	32	35	36	36
(e/D = 1.5)	84	90	78	81	78	80	84	90	88		93	86	91	86	84	94	96	92
(e/D = 2.0)	108	114	98	101	97	101	105	113	111		118	109	115	108	106	123	123	117
Fbry, ksi:
(e/D = 1.5)	61	68	55	59	55	59	57	67	63		66	62	65	59	57	82	82	82
(e/D = 2.0)	71	79	67	71	67	71	69	81	77		80	75	78	71	69	96	96	96
e, percent (S-basis):
L.	12		12		12		10		10			10		8	8	4	5	5
E, 10³ ksi										10.8
E, 10³ ksi										11.0
G, 10³ ksi										4.1
μ										0.33
Physical Properties: ρ, lb/in.³ C, K, and α									0.100
Physical Properties: ρ, lb/in.³ C, K, and α									See Figure 3.2.3.0

50. PDF page 388

Specification	AMS-QQ-A-200/3
Form	Extruded bar, rod, and shapes
Temper	T42^a
Cross-Sectional Area, in.²	≤ 25
Thickness or Diameter,^b in.	< 0.249	0.250- 0.499	0.500- 0.749	0.750- 0.999	1.000- 1.249		1.250- 1.499	1.500- 1.749	1.750- 1.999	2.000- 2.249	2.250- 2.499
Basis	S	S	S	S	S		S	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L	57	57	57	57	57	57	57	57	57	57	57
LT	55	54	52	51	49		47	45	43	41	39
F_ty, ksi:
L	38	38	38	38	38		38	38	38	38	38
LT	36	35	34	33	32		31	30	29	28	27
F_cy, ksi:
L	38	38	38	38	38		38	38	38	38	38
LT	39	38	37	36	35		34	33	32	31	30
F_su, ksi:	29	29	29	29	29		29	28	27	26	24
F_bru, ksi:
(e/D = 1.5)	81	80	79	77	75		74	71	69	67	64
(e/D = 2.0)	99	98	97	95	93		91	89	86	83	81
F_bry, ksi:
(e/D = 1.5)	56	55	53	51	49		47	44	41	39	36
(e/D = 2.0)	69	67	65	63	61		59	56	53	50	47
e, percent:
L	12	12	12	10	10		10	10	10	10	10
E_t, 10³ ksi	10.8
E_c, 10³ ksi	11.0
G, 10³ ksi	4.1
μ	0.33
Physical Properties:
ω, lb/in.³	0.100
C, K, and α	See Figure 3.2.3.0

51. PDF page 414

TUS, ksi	TYS, ksi	Temp., °F
69	45	RT (rolled)
71	44	RT (drawn)
85	65	RT (extruded)

52. PDF page 417

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	74.2	—	RT (rolled)
	84.1	—	RT (extruded)

53. PDF page 420

Notch Type	Gross Width	Net Width	Notch Radius
Center	4.50	1.50	1.50
Edge	2.25	1.50	0.3175
Fillet	2.25	1.50	0.1736

54. PDF page 421

Notch Type	Gross Width	Net Width	Notch Radius
Center	2.25	1.50	0.057
Edge	4.10	1.50	0.070
Fillet	2.25	1.50	0.0195

55. PDF page 454

Specification	Form
AMS 4338	Extruded bars, rods, and profiles

56. PDF page 459

Specification	Form
AMS 4101	Plate
AMS-QQ-A-250/29	Plate

57. PDF page 459

Section	Temper
3.2.7.1	T851

58. PDF page 463

Specimen Thickness:	0.25-0.45 and 0.15 inch	Environment:	95% R.H.
Specimen Width:	11.75 and 3.0 inches	Temperature:	RT
Specimen Type:	M(T) and C(T)	Orientation:	L-T

59. PDF page 464

Specimen Thickness:	0.25-0.45 inch	Environment:	Lab air
Specimen Width:	11.75 inches	Temperature:	300-400 °F
Specimen Type:	M(T)	Orientation:	L-T

60. PDF page 465

Specimen Thickness:	0.75 inch	Environment:	Lab air
Specimen Width:	1.75 inches	Temperature:	-100 through 400 °F
Specimen Type:	C(T)	Orientation:	L-T

61. PDF page 466

Specimen Thickness:	0.25-0.75 inch	Environment:	90-95% R.H.
Specimen Width:	4.0-11.75 inches	Temperature:	RT
Specimen Type:	M(T)	Orientation:	T-L

62. PDF page 467

Specimen Thickness:	0.25-0.45 inch	Environment:	Lab air
Width:	11.75 inches	Temperature:	300-400 °F
Type:	M(T)	Orientation:	T-L

63. PDF page 486

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	68	51	RT (unnotched)
	89	—	RT (notched)

64. PDF page 500

Properties:	TUS, ksi	TYS, ksi	Temp., °F
ST	63.5	56.0	RT
L	64.6	59.8	RT

65. PDF page 500

Stress-Strain Equations:
ST Direction
(Δε)/2 = σ/Ε + ε_p where
E = 11.3 x10³ ksi (reported),
ε_p = 6.243 x 10^-10σ^3.187 for σ < 50.86 ksi, and
ε_p = 1.606 x 10^-34σ^17.598 for σ > 50.86 ksi.

66. PDF page 504

Specification	Form
MIL-DTL-46192	Plate

67. PDF page 504

Section	Temper
3.2.11.1	T87

68. PDF page 507

Specification	Form
AMS 4296	Clad sheet and plate

69. PDF page 507

Section	Temper
3.2.12.1	T3

70. PDF page 549

Specification	Form
AMS-QQ-A-250/10	Sheet and plate
AMS-QQ-A-200/6	Extruded bar, rod, and shapes

71. PDF page 549

Section	Temper
3.5.4.1	O
3.5.4.2	H32
3.5.4.3	H34

72. PDF page 554

Specification	Form
AMS-QQ-A-250/9	Sheet and plate
AMS-QQ-A-200/7	Extruded bar, rod, and shapes

73. PDF page 554

Section	Temper
3.5.5.1	O
3.5.5.2	H111
3.5.5.3	H112
3.5.5.4	H321

74. PDF page 564

Section	Temper
3.6.2.1	T4, T42, T451, T4510, and T4511
3.6.2.2	T6, T62, T651, T652, T6510, and T6511

75. PDF page 592

Specification	Form
AMS 4125	Die forging
AMS-A-22771	Forging

76. PDF page 604

Specification	Form
AMS 4211	Plate

77. PDF page 617

Properties:	TUS, ksi	TYS, ksi	Temp., °F
(L)	78	70	RT
(LT)	74	65	RT

78. PDF page 619

Properties:	TUS, ksi	TYS, ksi	Temp., °F
(L)	77	68	RT Unnotched
(L)	95	—	RT Notched
(LT)	73	64	RT Unnotched
(LT)	77	—	RT Notched
(ST)	75	66	RT Unnotched
(ST)	87	—	RT Notched

79. PDF page 648

Product Form: Plate, 4.25 to 8.50 inches thick	References: 3.7.3.2.8(d) and (e)
Properties: TUS, ksi TYS, ksi Temp., F N/A 62-67 RT	Test Parameters: Loading – Axial, Triangular Waveform Frequency – 0.50 Hz Temperature – RT Environment – Air
Stress-Strain Equations: Cyclic Stress Strain Curve (Δσ/2) = 88.185 (Δε_p/2)^0.0578 Mean Stress Relaxation Curve Minimal relaxation for (Δε/2) < 0.00261 σ_m = 46.0 – 7500 (Δε/2) for (Δε/2) < 0.00613	Equivalent Strain Equation: log (N_f) = – 7.734 – 5.119 log (ε_eq – 0.0018) ε_eq = (Δε)^0.61 (S_max/E)^0.39 Std. Error of Estimate, Log (Life) = 0.301 Standard Deviation, Log (Life) = 1.573 R² = 96.3%
Nearly complete relaxation for (Δε/2) ≥ 0.00613	Sample Size = 53
Specimen Details: Unnotched 0.250 inch diameter	[Caution: The equivalent strain model may provide unrealistic life predictions for strain ratios beyond those represented above.]
Surface Condition: Polished, final surface finish unspecified

80. PDF page 658

Specimen Thickness:	0.999-1.000 inch	Environment:	Dry air (< 10% humidity)
Specimen Width:	3.805 inches	Temperature:	RT
Specimen Type:	C(T)	Frequency, f:	18.3 Hz
Stress Ratio, R:	0.33

81. PDF page 659

Specimen Thickness:	0.998-1.000 inch	Environment:	Humid air (>90% humidity)
Specimen Width:	3.805 inches	Temperature:	RT
Specimen Type:	C(T)	Frequency, f:	18.3 Hz
Stress Ratio, R:	0.33

82. PDF page 665

Specification	Form
AMS 4206 (T7751)	Plate
AMS 4324 (T74511)	Extrusion
AMS 4336 (T76511)	Extrusion
AMS 4337 (T77511)	Extrusion

83. PDF page 665

Section	Temper
3.7.5.1	T74511
3.7.5.2	T76511
3.7.5.3	T7751 and T77511

84. PDF page 670

Specification	Form
AMS 4044	Bare sheet and plate
AMS 4045	Bare sheet and plate
AMS 4078	Bare plate
AMS-QQ-A-250/12, 24	Bare sheet and plate
AMS-QQ-A-250/13, 25	Clad sheet and plate
AMS 4049	Clad sheet and plate
AMS 4122	Bar and rod, rolled or cold finished
AMS 4123	Bar and rod, rolled or cold finished
AMS 4124	Bar and rod, rolled or cold finished
AMS 4186	Bar and rod, rolled or cold finished
AMS 4187	Bar and rod, rolled or cold finished
AMS-QQ-A-225/9	Rolled or drawn bar and rod
AMS-QQ-A-200/11, 15	Extruded bar, rod, and shapes
AMS 4126	Forging

85. PDF page 671

Specification	Form
AMS 4141	Die forging
AMS 4147	Forging
AMS-A-22771	Forging
AMS-QQ-A-367	Forging

86. PDF page 671

Section	Temper
3.7.6.1	T6, T651, T652, T6510, T6511
3.7.6.2	T73, T7351, T7352, T73510, T73511

87. PDF page 673

Specification	AMS 4045 and AMS-QQ-A-250/12
Form	Sheet							Plate
Temper	T6 and T62^a							T651
Thickness, in.	0.008- 0.011	0.012- 0.039		0.040- 0.125		0.126- 0.249		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
Basis	S	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		76	78	78	80	78	80	77	79	77	79	76	78	75	77	71	73	70	72	66	68
LT	74	76	78	78	80	78	80	78	80	78	80	77	79	76	78	72	74	71	73	67	69
ST													70b	71b	66b		65b	67b	61b	63b
Fy, ksi:
L		69	72	70	72	71	73	69	71	70	72	69	69	66	68	63	65	60	62	56	58
LT	63	67	70	68	70	69	71	67	69	68	70	67	69	64	66	61	63	58	60	54	56
ST														59b	61b	56b	58b	54b	55b	50b	52b
Fcy, ksi:
L		68	71	69	71	70		67	69	68	70	66	68	62	64	58	60	55	57	51	52
LT		71	74	72	74	73	75	71	73	72	74	71	73	68	74	65		61	64	57	59
ST														67		64	66	61	63	57	59
Fsu, ksi		47	47	47	48	47	48	43	44	44	45	44	45	44	45	42	43	42	43	39	41
Fbru, ksi: (e/D = 1.5)		118	121	121	124	121	124	117	120	117	120	116	119	114	117	108	111	107	110	101	104
(e/D = 2.0)		152	156	156	160	156	160	145	148	145	148	143	147	141		134	137	132	135	124	128
Fbry, ksi: (e/D = 1.5)		100	105	102	105	103	106	97	100	100	103	100	103	98	101	94	97	89	93	84	87
(e/D = 2.0) (S-basis):		117	122	119	122	121	124	114	118	117	120	117	120	113	117	109	112	104	108	98	103
e, percent LT	5	7		8		8		9		7		6		5		5		5		3
E, 10³ ksi				10.3										10.3
E, 10³ ksi				10.5										10.6
G, 10³ ksi				3.9										3.9
μ				0.33										0.33
Physical Properties:
w, lb/in.³ C, K, and a												0.101	See Figure 3.7.6.0

88. PDF page 674

Specification	AMS 4044 and AMS-QQ-A-250/12
Form	Plate
Temper	T62^a
Thickness, in.	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
Basis	A	B	A	B	A	B	A	B	A	B	A	B	A	B
Mechanical Properties: ksi:
L	74	76	74	76	73	75	72	74	69	71	68	70	64	66
LT	78	80	78	80	77	79	76	78	72	74	71	73	67	69
ST							70^b	71^b	66^b	68^b	65^b	67^b	61^b	63^b
F^ry, ksi:
L	65	67	66	68	64	65	60	62	56	58	52	54	48	49
LT	67	69	68	70	67	69	64	66	61	63	58	60	54	56
ST							59^b	61^b	56^b	58^b	54^b	55^b	50^b	52^b
F^y, ksi:
L	70	72	70	72	68	70	63	65	59	61	55	57	50	52
LT	70	72	71	73	68	71	65	67	61	63	57	59	52	54
ST							63	65	60	62	57	59	53	55
F^u, ksi	43	44	44	45	44	45	44	45	42	43	42	43	39	41
F_bru, ksi:
(e/D = 1.5)	117	120	117	120	116	119	114	117	108	111	107	110	101	104
(e/D = 2.0)	145	148	145	148	143	147	141	145	134	137	132	135	124	128
F_bry, ksi:
(e/D = 1.5)	97	100	100	103	100	103	98	101	94	97	89	93	84	87
(e/D = 2.0)	114	118	117	120	117	120	113	117	109	112	104	108	98	103
e, percent (S-basis):
LT	9		7		6		5		5		5		3
E, 10³ ksi								10.3
E, 10³ ksi								10.6
G, 10³ ksi								3.9
μ								0.33
Physical Properties:
@, lb/in.³								0.101
C, K, and α
See Figure 3.7.6.0

89. PDF page 675

Specification	AMS-QQ-A-250/12	AMS 4078 and AMS-QQ-A-250/12
Form	Sheet	Plate
Temper	T73	T7351
Thickness, in.	0.040-0.249	0.250-0.499	0.500-1.000		1.001-1.500		1.501-2.000		2.001-2.500		2.501-3.000		3.001-3.500	3.501-4.000
Basis	S	S	A	B	A	B	A	B	A	B	A	B	S	S
Mechanical Properties:
Ftu, ksi:
L	67	68	68	70	67	69	66	68	65	67	63	65	62	60
LT	67	69	69	71	68		67	69		68		66	63	61
ST							63	65		64	60	62	59	57
Fcy, ksi:
L	56	57	57	59	57	59	55		52	55	49	53	49
LT	56	57	57	59	57	59	55		52	55	49	53	49
ST							52		49	52	47	50	47
Fsy, ksi:
L	55	56	56	58	56	58	53	55	50	53	47	51	47	45
LT	58	59	59	61	59		57	59	54	57	51	55	51	50
ST							59	61	55	58	51	55	50
Fsu, ksi	38	38	38	39	38	40	39	40	39	40	38	39	38	37
Fbru, ksi:
(e/D = 1.5)	105	102	103	106	103	106	102	106	102	105	100	103	99	96
(e/D = 2.0)	134	131	132	136	132	136	132	136	131	135	128	132	127	124
Fbry, ksi:
(e/D = 1.5)	84	79	81	83		86	82	85	79	83	76		76	76
(e/D = 2.0)	102	95	97	100	99	102	97	101	93	99	89	96	89	88
e, percent (S-basis):
LT	8	7	7		6		6		6				6	6
E, 103 ksi	10.3							10.3
E, 103 ksi	10.5							10.6
G, 103 ksi	3.9							3.9
μ	0.33							0.33
Physical Properties:
ρ, lb/in.³							0.101
C, K, and α	See Figure 3.7.6.0

90. PDF page 679

Thickness, in.	0.250-0.499		0.500-1.000^a		1.001-2.000^a		2.001-2.500^a		2.501-3.000^a		3.001-3.500^a		3.501-4.000^a
	AMS 4049 and AMS-QQ-A-250/13
Form	Plate
Temper	T651
Basis	A	B	A	B	A	B	A	B	A	B	A	B	A	B
Mechanical Properties:
Ftu, ksi:
L	74	76	75	77	74	76	73	75	69	71	68	70	64	66
LT	75	77	76	78	75	77	74	76	70	72	69	71	65	67
ST							70^b	71^b	66^b	68^b	65^b	67^b	61^b	63^b
Fcy, ksi:
L	67	69	68	70	67	69	64	66	61	63	58	60	54	56
LT	65	67	66	68	65	67	62	64	59	61	56	58	52	54
ST							59^b	61^b	56^b	58^b	54^b	55^b	50^b	52^b
F, ksi:
L	65	67	66	68	64	66	60	62	57	58	53	55	49	51
LT	69	71	70	72	69	71	65	68	62	64	59	61	55	57
ST							67	70	62	66	61	63	57	59
Fsu, ksi	42	43	42	44	42	44	43	44	41	42	40	42	38	39
Fbry, ksi:
(e/D = 1.5)	113	116	114	117	113	116	111	114	105	108	104	107	98	101
(e/D = 2.0)	139	143	141	145	139	143	137	141	130	134		132	121	124
FbrY, ksi:
(e/D = 1.5)	94	97	97	100	97	100	95	98	90	94	86	89	80	84
(e/D = 2.0)	111	114	113	116	113	117	110	113	105	109	100	104	93	97
e, percent (S-basis):
LT	9		7		6		5		5		5		3
E, 10³ ksi:
Primary									10.3
Secondary									10.0
G, 10³ ksi:
Primary									10.6
Secondary									10.3
μ									0.33
Physical Properties:
w, lb/in.³									0.101
C, K, and α

91. PDF page 680

Specification	AMS-QQ-A-250/13
Form	Plate
Temper	T62^a
Thickness, in.	0.250-0.499		0.500-1.000^b		1.001-2.000^b		2.001-2.500^b		2.501-3.000^b		3.001-3.500^b		3.501-4.000^b
Basis	A	B	A	B	A	B	A	B	A	B	A	B	A	B
Mechanical Properties:
F_tu, ksi:
L	72	73	72	74	72	73	71	72	67	69	66	68	62	64
LT	75	77	76	78	75	77	74	76	70	72	69	71	65	67
ST							70^c	71^c	66^c	68^c	65^c	67^c	61^c	63^c
F_cy, ksi:
L	63	65	64	66	62	64	58	60	54	56	50	52	46	48
LT	65	67	66	68	65	67	62	64	59	61	56	58	52	54
ST							59^c	61^c	56^c	58^c	54	55	50^c	52^c
F_cy, ksi:
L	68	70	68	70	66	68	62	63	57	59	54	55	48	50
LT	68	70	69	71	66	68	62	65	59	61	55	57	50	52
ST							63	65	60	62	57	59	53	55
F_su, ksi	42	43	43	44	42	44	43	44	41	42	40	42	38	39
F_bru, ksi:
(e/D= 1.5)	113	116	114	117	113	116	111	114	105	108	104	107	98	101
(e/D=2.0)	139	143	141	145	139	143	137	141	130	134	128	132	121	124
F_bry, ksi:
(e/D= 1.5)	94	97	97	100	97	100	95	98	90	94	86	89	80	84
(e/D = 2.0)	111	114	113	116	113	117	110	113	101	109	100	104	93	97
e, percent (S-basis):
LT	9		7		6		5		5		5		3
E, 10³ ksi:
Primary							10.3
Secondary							10.0
E, 10³ ksi:
Primary							10.6
Secondary							10.3
G, 10³ ksi							3.9
μ							0.33
Physical Properties:
w, lb/in.³							0.101
C, K, and α

92. PDF page 683

Specification	AMS 4126, MIL-A-22771, and QQ-A-367							MIL-A-22771 and QQ-A-367
Form								Die forging
Temper	T6ª							T652
Thickness, in.	≤ 1.000		1.001- 2.000		2.001- 3.000		3.001- 4.000	≤1.000		1.001- 2.000		2.001- 3.000		3.001- 4.000
Basis	A	B	A	B	A	B	S	A	B	A	B	A	B	S
Mechanical Properties:
Fu, ksi:	L	75	78	74	77	74		73	75	78	74	77	74	76	73
Fu, ksi:	Tcy	71d		71d		70d		70	71d		71d		70d		70
Fcy, ksi:	L	64	67	63	66	60	63	65	64	67	63	66	63	65	62
	ST	67	70	66	69	66	68	65	64	67	63	66	63	65	62
	Fs	43	45	43	44	42	43	42	43	45	43	44	42	43	42
Fbru, ksi:	(e/D = 1.5)	105	109	104	108	104	106	102	105	109	104	108	104	106	102
Fbru, ksi:	(e/D = 2.0)	135	140	133	138	133	136	131	135	140	133	138	133	136	131
Fbry, ksi:	(e/D = 1.5)	83	87	82	86	82	84	81	83	87	82	86	82	84	81
Fbry, ksi:	(e/D = 2.0)	96	100	94	99	94	97	93	96	100	94	99	94	97	93
e, percent (S-basis):	L	7		7		7		7	7		7		7		7
e, percent (S-basis):	Tcy	3		3		3		2	3		3		3		2
E, 10³ ksi								10.0
Ec, 10³ ksi								10.4
G, 10³ ksi								3.8
μ								0.33
Physical Properties:
ρ, lb/in.³								0.101
C, K, and α	See Figure 3.7.6.0(e&sub1;)

93. PDF page 685

Specification	AMS 4126, AMS-A-22771, and AMS-QQ-A-367					AMS-A-22771 and AMS-QQ-A-367
Form						Hand forging
Temper	T6a					T652
Thickness, in.	≤2.000	2.001-3.000	3.001-4.000	4.001-5.000	5.001-6.000	≤2.000	2.001-3.000	3.001-4.000	4.001-5.000	5.001-6.000
Basis	S	S	S	S	S	S	S	S	S	S
Mechanical Properties: si:
L	74	73	71	69	68	74	73	71	69	68
LT	73	71	70	68	66	73	71	70	68	66
ST		69b	68b	66b	65b		69b	68b	66b	65b
Fy, ksi:
L	63	61	60	58	56	63	61	60	58	56
LT	61	59	58	56	55	61	59	58	56	55
ST		58b	57b	56b	55b		57b	56b	55b	54b
Foy, ksi:
L	63	61				63	61
LT	61	59				61	59
Fs, ksi	44	44	43	41	41	44	44	43		41
Fbrus ksi:
(e/D = 1.5)
(e/D = 2.0)
Fbry, ksi:
(e/D = 1.5)
(e/D=2.0)
e, percent:
L	9	9	8	7	6	9	4	3	7	6
LT	4	4	3	3	2	4	3	2	3	2
ST		3	2	2	2		3	2	2	2
E, 10³ ksi		10.0
E, 10³ ksi	10.4
G, 10³ ksi	3.8
μ	0.33
Physical Properties:
w, lb/in.³		0.101 See Figure 3.7.6.0
C, K, and α		0.101 See Figure 3.7.6.0

94. PDF page 686

	AMS-A-22771 and AMS-QQ-A-367					AMS 4147, AMS-A-22771, and AMS-QQ-A-367
Form						Hand forging
Temper	T73a^a
Thickness, in.	≤2.000	2.001-3.000	3.001-4.000	4.001-5.000	5.001-6.000	≤2.000	2.001-3.000	3.001-4.000	4.001-5.000	5.001-6.000	6.001-7.000
Basis	S	S	S	S	S	S	S	A	B	S	S
Mechanical Properties:
F_tu, ksi:
L	66	66	64	62	61	66	66	64	67	62	61
LT	64	64	63	61	59	64	64	63	66	61	59
ST		61	60	58	57		61	60	63	58	57
F_cy, ksi:
L	56	56	55	53	51	54	54	53	55	51	49
LT	54	54	53	51	50	52	52	50	53	48	46
ST		52	51	50	49		50	48	51	46	44
F_su, ksi:
L	56	56				55	55	52	55	49	46
LT	52	52				55	55	52	55	49	46
ST						55	55	53	56	51	49
F_cu, ksi:
L	39	39				39	39			37	36
LT						36	36			36	35
ST						38	38			36	35
F_bru, ksi:^b
(e/D = 1.5)						86	88	89	92	86	84
(e/D = 2.0)						120	120	118	123	114	110
F_bry, ksi:^b
(e/D = 1.5)						71	73	73	77	71	68
(e/D = 2.0)						90	90	87	92	83	80
e, percent (S-basis):
L	7	7	7	7	6	7	7	7	7	7	6
LT	4	4	3	3	2	4	4	3	3	2	2
ST		3	2	2	2
E_c, 10³ ksi											10.2
E_t, 10³ ksi											10.4
G, 10³ ksi											3.8
μ											0.33
Physical Properties:
ω, lb/in.³											0.101
C, K, and α	See Figure 3.7.6.0

95. PDF page 687

Specification	AMS-QQ-A-200/11
Form	Extrusion (rod, bar, and shapes)
Temper	T6, T6510, T6511, and T62ª
Cross-Sectional Area, in.²	≤20														>20, ≤32		<32
Thickness, in.^b	<0.249		0.250-0.499		0.500-0.749		0.750-1.499				1.500-2.999		3.000-4.499			4.500-5.000
Thickness, in.^b	Basis	A	B	A	B	A	B	A	B	A	B	A	B	S	A	B
Mechanical Properties:
F, ksi:
L	78	82	81	85	81	85	81	85	81	85	81	85	81	84	78	78	81
LT ST	75	79	78	82	77	81	75	79	75	79	71 67	75 71	67 67	69 69	64 64	63 63	65 65
F_ty, ksi:
L	70	74	73	77	72	76	72	76	72	76	72	76	71	74	70	68	71
LT	66	70	69	72	67	71	65	69	61	65	61	65	56	59	55	52	55
ST											66	62	64	61	57	60
F_cy, ksi:
L	70	74	73	77	72	76	72	76	72	76	72	76	71	74	70	68	71
LT	72	76	74	78	73	77	71	75	67	71	67	71	62	64	61	57	60
ST												66	62	64	61	57	60
F_tu, ksi:	41	44	43	45	43	45	43	45	42	44	40	42	39	38	38	38	40
F_bru, ksi:
(e/D = 1.5)	111	117	115	121	115	120	113	119	110	115	106	110	102	101	102	101	105
(e/D = 2.0)	140	148	146	153	145	152	144	151	141	148	137	142	132	131	132	131	136
F_bry, ksi:
(e/D = 1.5)	92	97	96	101	94	99	93	98	89	94	84	88	83	79	83	79
(e/D = 2.0)	108	114	113	119	111	117	110	116	106	112	101	105	100	95	100	95	100
e, percent (S-basis):
L	7		7		7		7		7		7		7		6	6
E, 10³ ksi										10.4
E_t, 10³ ksi										10.7
G, 10³ ksi										4.0
μ										0.33
Physical Properties:
ρ, lb/in.³										0.101
C, K, and α										See	Figure	3.7.6.0

96. PDF page 688

Specification		AMS-QQ-A-200/11
Form		Extrusion (rod, bars, and shapes)
Temper		T73^a, T73510, T73511
Cross-Sectional Area, in.²		≤20						≤25						>20, ≤32
	Thickness, in.^b	0.062-0.249		0.250-0.499		0.500-0.749		0.750-1.499		1.500-2.999		3.000-4.499		3.000-4.499
		A	B	A	B	A	B	A	B	A	B	A	B	A	B
Mechanical Properties:
F, ksi:	L	68^c	72	70^d	74	70^d	73	70^d	73	69^d	74	68^c	71	65^c	70
F, ksi:	LT	66	70	68	72	67	70	66	69	62	67	58	61	56	60
F_y, ksi:	L	58	61	60	63	60	63	60	63	59^d	65	57^c	62	55^c	60
F_y, ksi:	LT	56	59	57	60	57	60	56	58	51	56	46	50	44	48
F_tu, ksi:	L	58	61	60	63	60	63	60	63	59	65	57	62	55	60
F_tu, ksi:	LT	59	62	60	63	60	63	58	61	54	59	49	53	47	51
F_s, ksi		37	39	38	40	38	39	38	39	37	40	37	38	35	38
F_bru, ksi:	(e/D= 1.5)	101	107	104	110	103	108	103	107		106	95	99	91	98
F_bru, ksi:	(e/D=2.0)	129	137	133	141	133	139	132	138	128	138	124	130	119	128
F_bry, ksi:	(e/D= 1.5)	82	86	84	89	84	88	83	87		87	72	79	70	76
F_bry, ksi:	(e/D = 2.0)	97	102	100	105	100	105	98	103		103	86	91	83	88
e, percent (S-basis):
	L	7		8		8		8		8		7		7




E, 10³ ksi											10.4
E, 10³ ksi										10.7
G, 10³ ksi										4.0
μ										0.33
Physical Properties:
w, lb/in.³										0.101
C, K, and α										See Figure 3.7.6.0

97. PDF page 713

Notch Type	Gross Width	Net Width	Notch Radius
Center	4.50	1.50	1.50
Edge	2.25	1.50	0.3175
Fillet	2.25	1.50	0.1736

98. PDF page 714

Notch Type	Gross Width	Net Width	Notch Radius
Edge	2.25	1.500	0.057
Edge	4.10	1.500	0.070
Fillet	2.25	1.500	0.0195

99. PDF page 716

Specimen Thickness:	0.090 inch	Environment:	Lab air
Specimen Width:	1-1/2 - 12 inches	Temperature:	RT
Specimen Type:	M(T)	Orientation:	L-T

100. PDF page 725

Specimen Thickness:	0.250-inch	Environment:	50% R.H.
Specimen Width:	8, 16, 36-inches	Temperature:	RT
Specimen Type:	M(T)	Orientation:	L-T

101. PDF page 727

Specimen Thickness:	1.00-inch	Environment:	50% R.H.
Specimen Width:	6, 8, 16, 36-inches	Temperature:	RT
Specimen Type:	M(T), C(T)	Orientation:	L-T

102. PDF page 738

Product Forms:	Extruded shape, 1.125 inch,	Test Parameters:	Loading - Axial
	1.45 inch		Frequency - 25 Hz
Properties:	TUS, ksi		Temperature - RT
	89		Environment - Air
	TYS, ksi	No. of Heats/Lots:	2
	84
	Temp.,°F	Fatigue Life Equation:	Log N_f = 21.89 - 9.32 log (S_max)
	RT		Std. Error of Estimate, Log (Life) = 0.321
Specimen Details:	Unnotched		Standard Deviation, Log (Life) = 0.753
	Round, 0.3 inch diameter,		R² = 81.8%
	removed from center of
	section
Surface Condition:	Polished to 10 micro-inch or	Sample Size:	16
	better
Reference:	3.7.7.2.8

103. PDF page 739

Product Forms:

Extruded shape, 1.125 inch, 1.45 inch

Test Parameters:

Loading - Axial Frequency - 25 Hz Temperature - RT Environment - Air

Properties:

TUS, ksi	TYS, ksi	Temp.,°F
83	78	RT

No. of Heats/Lots:

Specimen Details:

Unnotched Round, 0.3 inch diameter, removed from center of section

Fatigue Life Equation:

Log N_f = 17.98 - 7.57 log (S_max) Std. Error of Estimate, Log (Life) = 22.53(1/S_max) Standard Deviation, Log (Life) = 0.977 R² = 74.4 %

Surface Condition:

Polished to 10 micro-inch or better

Sample Size:

Reference:

3.7.7.2.8

104. PDF page 740

Properties:	TUS, ksi	TYS, ksi	Temp., °F
Longitudinal	89	84	RT
Long Transverse	83	78	RT

105. PDF page 740

Specimen Details:	Circumferentially notched,
	K_t = 3.0 round,	Fatigue Life Equation:
	0.253 inch net diameter,	Log N_f = 5.71 - 1.31 log (S_max - 16.92)
	0.013 inch root radius,	Std. Error of Estimate, Log (Life) = 4.51 (1/S_max)
	removed from center of	Standard Deviation, Log (Life) = 0.750
	section	R² = 92.4%

106. PDF page 740

Surface Condition:	Notch
Reference:	3.7.7.2.8

107. PDF page 741

Specification	Form
AMS 4148	Die forging
AMS 4149	Die and hand forging
AMS 4179	Hand forging
AMS-A-22771	Forging
AMS 4344	Extrusion

108. PDF page 741

Section	Temper
3.7.8.1	T73511
3.7.8.2	T74 and T7452 (formerly T736 and T73652)

109. PDF page 756

Specification	Form
AMS 4334	Hand forging

110. PDF page 760

Specification	Form
AMS 4084	Bare sheet
AMS 4085	Bare sheet
AMS 4090	Bare plate
AMS 4089	Bare plate
AMS 4202	Bare plate
AMS 4207	Clad sheet
AMS 4100	Clad sheet

111. PDF page 760

Section	Temper
3.7.10.1	T61 and T651
3.7.10.2	T7351
3.7.10.3	T761 and T7651

112. PDF page 762

Specification	AMS 4084	AMS 4090			AMS 4085			AMS 4089
Form	Sheet	Plate			Sheet			Plate
Temper	T61	T651			T761			T7651
Thickness, in.	0.040-0.249	0.250-0.499	0.500-1.000	1.001-1.500	0.040-0.062	0.063-0.187	0.188-0.249	0.250-0.499	0.500-1.000	1.001-1.500
Basis	S	S	S	S	S	S	S	S	S	S
Mechanical Properties:
F,,, ksi:
L	75	77	77	77	71	71	71	70	69	69
LT	75	78	78	78	71	71	71	71	70	70
Fy, ksi:
L	66	69	70	70	61	61	61	60	59	59
LT	64	67	68	68	60	60	60	60	59	59
Fay, ksi:
L	64		68	67	60	59	58	60	59	59
LT	68	70	71	71	61	63	63	63	62	59
FSU, ksi	45	44	43	41	43	42	42	41	39	37
Fbru, ksi:
(e/D = 1.5)	120	113	113	113	112	112	111	104	103	103
(e/D = 2.0)	154	144	144	144	143	143	142	136	134	134
Fbry, ksi:
(e/D = 1.5)	97	91	93	93	90	90	90	82	81	81
(e/D = 2.0)	110	106	107	107	104	104	104	97	95	95
e, percent:
L	9	10	9	9	9	9	9	9	8	6
LT	9	10	9	9	9	9	9	9	8	6
E, 10³ ksi	10.0		10.2			10.0			10.2
E, 10³ ksi	10.5		10.6			10.5			10.6
G, 10³ ksi	3.8		3.9			3.8			3.9
μ	0.33		0.33			0.33			0.33
Physical Properties:
@, lb/in.³					0.101
C, K, and a					0.23 (at 212°F)
K, Btu/[(hr)(ft²)(°F)/ft] a, 10⁶ in./in./°F		80 (at 77°F) for T61 and T651; 90 (at 77°F) for T761 and T7651 12.9 (68 to 212°F)

113. PDF page 769

Properties:	TUS, ksi	TYS, ksi	Temp., °F
T61	81	73-75	RT
T761	77	68-70	RT

114. PDF page 770

Properties:	TUS, ksi	TYS, ksi	Temp., °F
T61	80-81	73-76	RT
T761	75	66-67	RT

115. PDF page 771

Properties:	TUS, ksi	TYS, ksi	Temp., °F
T61	81-82	73-76	RT
T761	75-77	67-70	RT

116. PDF page 771

Specimen Details: Notched, edge notched	No. of Heats/Lots: 2
K_t = 3.0
1.000 inch gross width	Maximum Stress Equation:
0.700 inch net width	Log N_f = 13.4-6.29 log (S_max)
0.050 inch root radius, r	Std. Error of Estimate, Log (Life) = 0.441
60° flank angle, ω	Standard Deviation, Log (Life) = 0.931 R²=78%

117. PDF page 775

Properties:	TUS, ksi	TYS, ksi	Temp , °F
L	70	60	RT
LT	71	60	RT

118. PDF page 777

Properties:	TUS, ksi	TYS, ksi	Temp., °F
L (T7351)	70	60	RT
LT (T7351)	71	61	RT
L (T7351)	72	62	RT
(T7651)	Not specified
L (T7351)	72	63	RT
LT (T7351)	73	62	RT

119. PDF page 778

Specimen Thickness:	0.650-inch	Environment:	Lab air
Specimen Width:	1.500-inches	Temperature:	RT
Specimen Type:	C(T)	Orientation:	L-T

120. PDF page 779

Specimen Thickness:	0.528 to 0.530-inch	Environment:	95% R.H.
Specimen Width:	4.6-inches	Temperature:	RT
Specimen Type:	M(T)	Orientation:	L-T

121. PDF page 793

Product Form/Thickness:

Casting

Test Parameters:

Thermal Mechanical Processing History: T7, HIP

Strain Rate/Frequency - 20 cpm

Properties:

Wave Form - Triangular

TUS, ksi	TYS, ksi	E, ksi	Temp., °F

Temperature - 75°F

57-66

45-57

10,800

Atmosphere - Air

No. of Heats/Lots:

Stress-Strain Equations:

Equivalent Strain Equation:

Cyclic (Companion Specimen)

Log N_f = -6.54-4.60 log (ε_eq)

Proportional Limit = 42 ksi

ε_eq = (Δε)^0.37 (S_max/E)^0.63

(Δσ/2) = 72(Δε_p/2)^0.058

Std. Error of Estimate, Log (Life) = 0.242

Mean Stress Relaxation, ksi

Standard Deviation, Log (Life) = 0.587

σ_m = 33.3 - 4755(Δε/2)

Adjusted R² Statistic: 83%

Specimen Details: Uniform gage test section

0.250 inch diameter

Sample Size:

References: 3.8.1.1.8(a) and (b)

[Caution: The equivalent strain model may

provide unrealistic life predictions for strain

ratios and ranges beyond those represented

above.]

122. PDF page 795

Product Form/Thickness: Casting				Test Parameters:
				Strain Rate/Frequency - 20 cpm
Thermal Mechanical Processing History: T7, HIP				Wave Form - Triangular Temperature - 200°F Atmosphere - Air
Properties:
TUS, ksi	TYS, ksi	E, ksi	Temp., °F
53-59	47-55	10,339	200	No. of Heats/Lots: 3
Stress-Strain Equations:				Equivalent Strain Equation:
Cyclic (Companion Specimen)				Log N_f = -6.68-4.66 log (ε_eq)
Proportional Limit = 39 ksi				ε_eq = (Δε)^0.50 (S_max/E)^0.50
(Δσ/2) = 58(Δε_p/2)^0.041				Std. Error of Estimate, Log (Life) = 0.359
Mean Stress Relaxation, ksi				Standard Deviation in Log (Life) = 0.561
σ_m = 39.7 - 7049(Δε/2)				Adjusted R² Statistic: 59%
Specimen Details: Uniform gage test section				Sample Size: 18
0.250 inch diameter
Reference: 3.8.1.1.8(a)				[Caution: The equivalent strain model may provide unrealistic life predictions for strain ratios and ranges beyond those represented above.]

123. PDF page 797

Product Form/Thickness: Casting	Test Parameters: Strain Rate/Frequency - 20 cpm Wave Form - Triangular Temperature - 350°F Atmosphere - Air
Thermal Mechanical Processing History: T7, HIP	No. of Heats/Lots: 3
Properties: TUS, ksi TYS, ksi E, ksi Temp., °F 48-53 40-48 9,783 350	Equivalent Strain Equation: Log N_f = -12.44-7.07 log (ε_eq) ε_eq = (Δε)^0.52 (S_max/E)^0.48 Std. Error of Estimate, Log (Life) = 0.000817 (1/ε_eq) Standard Deviation, Log (Life) = 0.545
Stress-Strain Equations: Cyclic (Companion Specimen) Proportional Limit = 36 ksi (Δσ/2) = 50(Δε_p/2)^0.036 Mean Stress Relaxation, ksi σ_m = 30.0 - 5664(Δε/2)	Adjusted R² Statistic: 93%
Specimen Details: Uniform gage test section 0.250 inch diameter	Sample Size: 18
Reference: 3.8.1.1.8(a)	[Caution: The equivalent strain model may provide unrealistic life predictions for strain ratios and ranges beyond those represented above.]

124. PDF page 858

Product Form:	Extruded bar, 0.50 inch diameter			Test Parameters:
					Loading - Axial
					Frequency - 3600 cpm
Properties:	TUS, ksi	TYS, ksi	Temp., °F		Temperature - RT
	47.5	40.9	RT		Environment - Air
			(unnotched)	No. of Heats/Lots:	Not specified
Specimen Details:	Unnotched
	0.500 inch gross diameter			Equivalent Stress Equation:
	0.400 inch net diameter				Log N_f = 7.56-2.73 log (S_eq-23.7)
	0.750 inch root diameter				S_eq = S_max(1-R)^0.40
	7.500 inch long				Std. Error of Estimate, Log (Life) = 0.60
Surface Condition:	Polished with No. 240 grit aluminum oxide belt and then a No. 400 grit; polished with kerosene to better than 10 micro-inches				Standard Deviation, Log (Life) = 0.85
					R² = 51%
				Sample Size:	21
					[Caution: The equivalent stress model may provide unrealistic life predictions for stress ratios beyond those represented above.]

Reference:	4.2.3.2.8

125. PDF page 859

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	63.7	40.9	RT
			(notched)

126. PDF page 860

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	58.2	40.9	RT
			(notched)

127. PDF page 892

4.1.2.1.5(d)	Moore, A. A., and McDonald, J. C., “Tensile and Creep Strengths of Some Magnesium- Base Alloys at Elevated Temperatures”, American Society for Testing and Materials, Proceedings 46, pp 970-989 (1946).
4.1.2.1.5(e)	McDonald, J. C., “Tensile, Creep and Fatigue Properties of Some Magnesium-Base Alloys”, American Society for Testing and Materials, Proceedings 48, pp 737-754 (1948).
4.1.2.1.5(f)	Wyman, L. L., “High-Temperature Properties of Light Alloys (NA-137). Part II, Magnesium”, U.S. Office of Scientific Research and Development Report No. 4150, M-292, pp 101 (1944).
4.1.2.1.5(g)	Craighead, C. M., Grube, K. P., Eastwood, L. W., and Lorig, C. H., “The Effects of Temperature on the Mechanical Properties of Magnesium Alloy”, Rand Corporation Report R-146, pp 210 (October 1949).
4.1.2.1.5(h)	Wyman, L. L., “High-Temperature Properties of Light Alloys (NA-137). Part II, Magnesium”, U.S. Office of Scientific Research and Development Report No. 4150, M-292, pp 101 (1944).
4.1.2.1.6	Clapper, R. W., “Isochronous Stress-Strain Curves for Some Magnesium Alloys Showing the Effects of Varying Exposure Time on Their Creep Resistance”, American Society for Testing and Materials, Proceedings 58, pp 812-825 (1958).
4.1.2.1.7(a)	Found, G. H., “The Notch Sensitivity in Fatigue Loading of Some Magnesium-Base and Aluminum-Base Alloys”, American Society for Testing and Materials, Proceedings 46, pp 715-740 (1946).
4.1.2.1.7(b)	Schuette, E. H., “Fatigue Properties of Magnesium Alloy Forgings”, Wright-Patterson Air Force Base Technical Report No. 60-854, pp 112 (December 1960) (MCIC 43549).
4.2.3.2.8	Blatherwick, A. A., and Lazan, B. J., “Fatigue Properties of Extruded Magnesium Alloy ZK60A Under Various Combinations of Alternating and Mean Axial Stresses”, WADC Tech Report 53-181, pp 27 (August 1953) (MCIC 108173).
4.4.2(a)	Schuette, E. H., “Hyperbolic Column Formulas for Magnesium Alloy Extrusions”, Journal of the Aeronautical Sciences, 15, pp 523-529 (1948).
4.4.2(b)	Schuette, E. H., “Column Curves for Magnesium Alloy Sheet”, Journal of the Aeronautical Sciences, 16, pp 301-305 (1949).

128. PDF page 896

Orientation^b	Yield Strength Range, ksi	Product Thickness Range, inches	N	S
L-T	121-143	<3.5
T-L	124-145	<3.5

129. PDF page 900

Thickness, inches	Comp. CP-4	Comp. CP-3	Comp. CP-2	Comp. CP-1
0.188-1.000	25	20	18	15
1.001-2.000	20	18	15	12
2.001-3.000	18	15	12	10

130. PDF page 908

Specification	Form
AMS-T-9046	Sheet, strip, and plate
AMS 4926	Bar
MIL-T-9047^a	Bar
AMS-T-81556	Extruded bar and shapes
AMS 4910	Sheet, strip, and plate
AMS 4966	Forging

131. PDF page 909

		0.015-0.079	0.080-0.187	0.188-0.250
F_tu	L	123	126	130
F_tu	LT	123	126	131
F_ty	L			118
F_ty	LT		115	120

132. PDF page 916

Specimen Thickness: 0.08 inch	Environment: Lab air
Specimen Width: 2.76 inches	Temperature: RT
Specimen Type: M(T)	Orientation: L-T and T-L

133. PDF page 917

Specimen Thickness:	0.08 inch	Environment:	Distilled water
Specimen Width:	2.76 inches	Temperature:	RT
Specimen Type:	M(T)	Orientation:	L-T and T-L

134. PDF page 918

Specimen Thickness:	0.08 inch	Environment:	3.5% NaCl
Specimen Width:	2.76 inches	Temperature:	RT
Specimen Type:	M(T)	Orientation:	L-T and T-L

135. PDF page 945

a	MIL-T-9046 was canceled and superceded by AMS-T-9046
b	The rounded T99 values are higher than specification values as follows: Ftu(L) = 131 ksi, Ftu(LT) = 132 ksi, and Fty(LT) = 123 ksi.
c	The rounded T99 values are higher than specification values as follows: Ftu(L) = 133 ksi and Ftu(LT) = 133 ksi.
d	Bearing values are “dry pin” values per Section 1.4.7.1.
e	8%—0.025 to 0.062 in. and 10%—0.063 in. and above.
f	5%—0.050 in. and above; 4%—0.033 to 0.049 in. and 3%—0.032 in. and below.

136. PDF page 948

Specification	AMS 4965^a and MIL-T-9047^b
Form	Rectangular bar
	AMS 4965 and MIL-T-9047b										MIL-T-9047b
Condition		Solution treated and aged
Width, in.	0.501-	1.001-	4.001-	1.501-	4.001-	2.001-	4.001-	3.001-	4.001-		0.501-	1.001-	4.001-	1.501-	4.001-
Width, in.	8.000	4.000	8.000	4.000	8.000	4.000	8.000	8.000	8.000		8.000	4.000	8.000	4.000	8.000
Thickness, in.	≤0.500	0.501-1.000		1.001-1.500		1.501-2.000			2.001-3.000	3.001-4.000
Basis	S	S	S	S	S	S	S	S	S	S	S	S	S	S	S
Mechanical Properties:
F_tu, ksi:
L	160	155	150	150	145	145	140	135	130		165	160	155	150	140
LT	160	155	150	150	145	145	140	135	130		165	160	155	150	140
F_ty, ksi:
L	150	145	140	140	135	135	130	125	120		155	150	145	140	130
LT	150	145	140	140	135	135	130	125	120		155	150	145	140	130
F_cy, ksi:
L
LT
F_su, ksi	92
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	10	10	10	10	10	10	10	8		10	10	10	10	10
LT	10	10	10	10	10	10	10	10	8		10	10	10	10	10
RA, percent:
L	25	20	20	20	20	20	20	20	15		20	20	20	20	20
LT	25	20	20	20	20	20	20	20	15		20	20	20	20	20
E, 10³ ksi										16.9
E_c, 10³ ksi								17.2
G, 10³ ksi								6.2
μ								0.31
Physical Properties:
ω, lb/in.³											0.160
C, K, and α											See Figure 5.4.1.0

137. PDF page 949

Specification	AMS 4935				AMS 4934
Form					Extrusion
Condition	Annealed				Solution treated and aged
Thickness or diameter, in.	<2.000		2.001-3.000		<0.500		0.501-0.750			0.751-1.000		1.001-2.000	2.001-3.000
Basis..	A	B	A	B	A	B	A		B	A	B	S	S
Mechanical Properties:
F_tu, ksi:
L	130a	137	130b	135	155	163	151		157	147	153	140	130
LT^c	130a	139	130b	139	155	163	151		157	147	155	140	130
F_ty, ksi:
L	120	124	118	122	138	147	138		143	133	140	130	120
LT^c	120a	128	120	125	138	147	138		145	133	142	130	120
F_cy, ksi:
L	128	133	124	128	147	157	147		153	142	150	139	128
LT^c	129	138	…	…	147	157	147		155	139	152	139	128
F_su^d, ksi	83	89	…	…	94	99	92		96	89	93	85	79
F_bru^d, ksi:
(e/D = 1.5)	214	226	…	…	243	256	237		246	231	240	220	204
(e/D = 2.0)	264	278	…	…	311	327	303		315	295	307	281	261
F_bry, ksi:
(e/D = 1.5)	180	186	…	…	208	222	208		216	201	212	196	182
(e/D = 2.0)	210	217	…	…	242	257	242		250	233	245	228	210
e, percent (S-basis):
L	10	…	10	…	6	…	6	…	…	6	…	6	6
LT^c	8	…	…	…	…	…	…	…	…	6	…	…	6
RA, percent (S-basis):
L	20	…	20	…	12	…	12	…	…	12	…	12	12
LT^c	15	…	…	…	12	…	12	…	…	12	…	12	12
E, 10³ ksi							16.9
E_c, 10³ ksi								17.2
G, 10³ ksi									6.5
μ											0.31
Physical Properties:								0.160
w, lb/in.³								0.160
C, K, and α	See Figure 5.4.1.0

138. PDF page 963

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	112	92	400
	101	77	600

139. PDF page 966

Specimen Thickness:	0.250 inch	Environment:	50% R.H.
Specimen Width:	9.6, 16, 32 inches	Temperature:	RT
Specimen Type:	M(T)	Orientation:	L-T

140. PDF page 975

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	166-177	153-167	RT

141. PDF page 976

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	166-177	153-167	RT

142. PDF page 977

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	142-143	117-121	400°F
	125-134	102-113	600°F

143. PDF page 978

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	142-143	117-121	400°F
	129-133	103-105	600°F

144. PDF page 979

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	120-125	93-96	800°F
	110-111	84-86	900°F

145. PDF page 980

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	120-124	93-96	800°F
	110-111	84-88	900°F

146. PDF page 981

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	158	149	RT
	155	145	RT

147. PDF page 981

Gage	Hourglass
---	3.25	Reduced section radius of curvature, inch
0.195	0.250	Diameter, inch

148. PDF page 982

Properties:	TUS, ksi	TYS, ksi	Temp., °F
Product Form:	Plate, 0.50 inch thick		Test Parameters:
			Loading — Axial
	173	164	RT Frequency — Unspecified Temperature — RT Environment — Air
Specimen Details:	Unnotched, flat hourglass 10 inch reduced section radius of curvature 1 inch net section width 0.156 inch net section thickness		No. of Heats/Lots: 1 Maximum Stress Equation: Log N_f = 47.9-20.2 log (S_max) Std. Error of Estimate, Log (Life) = 0.33 Standard Deviation, Log (Life) = 0.89
Surface Conditions:	Machined to 63 RMS		R² = 87%
Reference: 5.4.1.2.8(d)			Sample Size = 14

149. PDF page 983

Ref. (c)	Ref. (e)		Std. Error of Estimate, Log (Life) = 0.24
0.195	0.430	Gross diameter, inch	Standard Deviation, Log (Life) = 0.81
0.136	0.300	Net section, inch	R² = 92%
0.005	0.016	Notch radius, r, inch
60°	60°	Flank angle, ω	Sample Size = 31

150. PDF page 999

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	154.5	148.5	RT
	159.9	151.5	RT

151. PDF page 999

Test Parameters:
Loading—Axial
Frequency—Unspecified
Temperature—RT
Atmosphere—Air

152. PDF page 1000

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	154.6	148.5	RT
Specimen Details: V-Groove, K_t = 3.0 0.195 inch gross diameter 0.136 inch net diameter 0.005 inch root radius 60° flank angle
Surface Condition: RMS 32
References: 5.4.1.2.8(c)

153. PDF page 1009

Specimen Thickness:	0.25 inch	Environment:	50% RH
Specimen Width:	2.0 inches	Temperature:	RT
Specimen Type:	C(T)	Orientation:	L-T

154. PDF page 1012

a	Inactive for new design
b	Maximum of 16 square-inch cross-sectional area.
c	Applicable, providing LT or ST dimension is ≥3.000 inches
d	Thickness 0.025 inch and above: 3 percent below 0.025 inch.

155. PDF page 1038

5.4.1.1.8(b)	Brockett, R. M., and Gottbrath, J. A., “Development of Engineering Data on Titanium Extru- sion for Use in Aerospace Design”, Lockheed-California Co., Technical Report AFML-TR- 67-189 (July 1967) (MCIC 69807, MIL-HDBK-5 Source M-543).
5.4.1.1.8(c)	Rhode, T. M., and Ertel, P. W., “Constant Amplitude Fatigue Life Data for Notched and Unnotched Annealed Ti-6Al-4V Sheet”, AFWAL-TR-88-4081, January 1988 (MIL-HDBK-5 Source M-696).
5.4.1.1.9	Fedderson, C. E., and Hyler, W. S., “Fracture and Fatigue-Crack Propagation Characteristics of ¼-Inch Mill Annealed Ti-6Al-4V Titanium Alloy Plate”, Report No. G9706, Battelle, Co- lumbus, Ohio (1971).
5.4.1.2.8(a)	“Fatigue Strength Properties for Heat Treated Ti-4Al-30Mo-1V and Ti-6Al-4V Titanium Alloys (LP-69-132 and LP-69-129)”, North American Aviation, Report No. TFD-60-521 (July 18, 1960) (MCIC 65737).
5.4.1.2.8(b)	“Determination of Design Data for Heat Treated Titanium Alloy Sheet”, Lockheed-Georgia Co., Report No. ASD-TDR-62-335, Vol. 3, Contract No. AF33(616)-6346 (May 1962) (MCIC 90172).
5.4.1.2.8(c)	Sommer, A. W., and Martin, G. R., “Design Allowables for Titanium Alloys”, North American Rockwell, AFML-TR-69-161 (June 1969) (MCIC 75727).
5.4.1.2.8(d)	Marrocco, A. G., “Fatigue Characteristics of Ti-6Al-4V and Ti-6Al-6V-2Sn Sheet and Plate”, Grumman Aircraft Engineering Corp., EMG-81 (November 18, 1968) (MCIC 76303).
5.4.1.2.8(e)	Sargent, M. R., “Fatigue Characteristics of Ti-6Al-4V Plate and Forgings (SWIP)”, General Dynamics, FGT-3218 (September 22, 1965) (MIL-HDBK-5 Source M-457).
5.4.2.1.8	Marrocco, A. G., “Evaluation of Ti-6Al-4V and Ti-6Al-6V-2Sn Forgings”, Grumman Aircraft Engineering Corporation, EMG-82, November 1968 (MIL-HDBK-5 Source M-522).
5.4.3.1	Unpublished data from NKK, January 2001, (MIL-HDBK-5 Source M-914).
5.5.1	Henning, R. G., “Mechanical Properties of Solution-Treated Titanium Sheet Alloy B120VCA”, ASD TR 61-337 (September 1961).
5.5.1.1.8	Blatherwick, A. A., “Fatigue, Creep, and Stress-Rupture Properties of Ti-13V-11Cr-3Al Titanium Alloy (B120VCA)”, AFML-TR-66-293 (September 1966).
5.5.1.2.8	Schwartzberg, F. R., Kiefer, T. F., and Keys, R. D., “Determination of Low-Temperature Fatigue Properties of Structural Metal Alloys 1 April 1962 through 30 September 1964”, Martin-Cr-64-74 (October 1964), pp 158 (MCIC 58024).
5.6(a)	“Theoretical and Experimental Determination of the Bending Modulus of Rupture for Round Titanium Tubing”, Bendix Products Division (July 31, 1958).
5.6(b)	Cozzone, F. P., “Bending Strength in Plastic Range”, Journal of the Aeronautical Sciences (May 1943).
5.6(c)	Ades, C. S., “Bending Strength of Tubing in the Plastic Range”, Journal of Aeronautical Sciences (August 1957).

156. PDF page 1050

Product Form:	Bar, air melted			Test Parameters:
Properties:	TUS, ksi	TYS, ksi	Temp.,°F	Loading - Axial Frequency - 3600 cpm
	141.4	95.3	800	Temperature - 800°F Environment - Air
Specimen Details: Unnotched
0.250 inch diameter				No. of Heats/Lots: 1
Heat Treatment:	1650°F for 2 hours, oil quenched and 1300°F for 16 hours, air cooled.			Equivalent Stress Equation:
				Log N_f = 45.1-19.5 log (S_eq)
				S_eq = S_max (1-R)^0.47 Std. Error of Estimate, Log (Life) = 0.418
Surface Condition: Not given				Standard Deviation, Log (Life) = 0.717 R² = 65.9%
Reference:	6.2.1.1.8
				Sample Size = 17

157. PDF page 1081

Product Form:	Bar, 0.75 inch diameter
Properties:	TUS, ksi	TYS, ksi	Temp., °F
	133.2	73.8	RT
Specimen Details: Unnotched 0.250 inch diameter
Surface Condition: Longitudinally polished
Reference: 6.3.3.1.8(a)
Test Parameters:
Loading -	Axial
Frequency -	Unspecified
Temperature -	RT
Environment -	Air

158. PDF page 1082

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	133.2	73.8	RT

159. PDF page 1083

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	135.4	74.6	RT
	136.7	69.8
Specimen Details:	Unnotched
	0.500 inch wide
	0.250 inch wide
Surface Condition:	As ground
References:	6.3.3.1.8(a) and (b)
Test Parameters:
	Loading - Axial
	Frequency - Unspecified
	Temperature - RT
	Environment - Air

160. PDF page 1084

Properties:	TUS, ksi	TYS, ksi	Temp., °F
	135.4	74.6	RT
	136.7	69.8

161. PDF page 1084

Specimen Details:	Edge notched, K_t = 3.0
	0.625 inch gross width
	0.030 inch root radius
	0.375 inch net width
	60° flank angle

162. PDF page 1101

Makeup of Data Collection:
Heat Treatment:	2 [See Table 6.3.5.1.7(f)]
Number of Vendors	= Unknown
Number of Lots	= 2
Number of Test Laboratories	= 1
Number of Tests	= 32
Specimen Details:
Type	- Unnotched round bar
Gage Length	- N.A.
Gage Thickness	- 0.25 inch to 0.375 inch

163. PDF page 1102

Makeup of Data Collection:

Heat Treatment: 2 [See Table 6.3.5.1.7(f)]

Number of Vendors = Unknown

Number of Lots = 2

Number of Test Laboratories = 1

Number of Tests = 31

Specimen Details:

Type - Unnotched round bar

Gage Length - N.A.

Gage Thickness - 0.25. inch - 0.375 inch

164. PDF page 1103

Makeup of Data Collection:
Heat Treatment	2 [See Table 6.3.5.1.7(f)]
Number of Vendors	Unknown
Number of Lots	2
Number of Test Laboratories	1
Number of Tests	22
Specimen Details:
Type	Unnotched round bar
Gage Length	N.A.
Gage Thickness	0.250 inch - 0.375 inch

165. PDF page 1104

Makeup of Data Collection:
Heat Treatment: 2 [See Table 6.3.5.1.7(f)]
Number of Vendors = Unknown
Number of Lots = 2
Number of Test Laboratories = 1
Number of Tests = 24
Specimen Details:
Type - Unnotched round bar
Gage Length - N.A.
Gage Thickness - 0.250 inch - 0.375 inch

166. PDF page 1114

Specimen Thickness:	0.298-0.502 inch	Environment:	Lab air
Specimen Width:	1.153-2.000 inches	Temperature:	RT
Specimen Type:	C(T)	Orientation:	L-T and T-L

167. PDF page 1115

Specimen Thickness:	0.298-0.502 inch	Environment:	Lab air
Specimen Width:	1.157-2.001 inches	Temperature:	800-1200 °F
Specimen Type:	C(T)	Orientation:	L-T and T-L

168. PDF page 1116

Specimen Thickness:	0.298-0.479 inch	Environment:	Lab air
Specimen Width:	1.151-1.993 inches	Temperature:	1000 °F
Specimen Type:	C(T)	Orientation:	L-T and T-L

169. PDF page 1138

Specification	AMS 5891
Form	Bar
Condition Thickness, in.	2250 Anneal
Basis	≤1.000		1.001 to 2.000		2.001 to 3.000		3.001 to 4.000		4.001 to 5.000		5.001 to 6.000
	A	B	A	B	A	B	A	B	A	B	A	B
Mechanical Properties:
Ftu ksi: L	110	118	110	117	110	115	110	114	109	112	107	110
Fy, ksi: L	45a	51	45a	51	45a	51	45a	51	45a	51	45a	51
Fcy, ksi
Fsu, ksi
Fbrc, ksi:
(e/D = 1.5)
(e/D = 2.0)
Fbry, ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent: L	35	46	35	46	35	46	35	46	35	46	35	46
E, 10³ ksi
E, 10³ ksi
G, 10³ ksi
μ
Physical Properties:
w, lb/in.³	0.324
C, K and α	See Figures 6.3.9.0(a), (b), and (c)

170. PDF page 1155

Makeup of Data Collection:

Stress Rupture Equation:

Makeup of Data Collection: Heat Treatment: Annealed Number of Vendors = 1 Number of Lots = Number of Test Laboratories = 1 Number of Tests = 283

Specimen Details: Type - ≤ 0.375 inch thick - Flat > 0.375 inch thick -0.25 inch rd reduced section Adjusted Gage Length -2.6 inches for flat specimens 1.35 inches for rd. specimens Gage Thickness - 0.125" for flat specimens for sheets with thickness of 0.125" or greater.
Sheet thickness for specimens from sheet with thickness < 0.125".

Stress Rupture Equation: Log t = c + b₁/T + b₂X/T + b₃X²/T + b₄X³/T T = °R X = log (stress, ksi) c = -16.671 b₁ = 49,051 b₂ = -8,375.3 b₃ = -2,403.7 b₄ = 619.59

Analysis Details: Standard Deviation = 0.598 Standard Error of Estimate = 0.155 Ratio of Between to Within Heat Treatment Variance = < 0.10 (at spec pt.) R² = 96.6%

[Caution: The stress rupture model may provide unrealistic times to rupture for stresses beyond those represented above.]

171. PDF page 1173

TUS, ksi	TYS, ksi	E, ksi	Temp., °F
Product Form/Thickness: Bar, 0.5 inch thick
diameter
Thermal Mechanical Processing History:
Solution annealed (AMS 5772)
Properties:
102*	55*		75
		29,766	800
Stress-Strain Equations:
Cyclic (Companion Specimens)
Proportional Limit = 60 ksi
(Δσ/2) = 109 (Δεp/2)^0.06
Mean Stress Relaxation
Inadequate data at low strain range values
Specimen Details: Uniform gage test section
0.250 inch diameter
Reference: 3.8.1.1.8
* Minimum values from AMS 5772.

172. PDF page 1175

TUS, ksi	TYS, ksi	E, ksi	Temp., °F
Product Form/Thickness: Bar, 1.5 inch thick
Thermal Mechanical Processing History:
Solution annealed (AMS 5772)
Properties:
120*	55*		75
		20,050	1200
Stress-Strain Equations:
Cyclic (Companion Specimens) Proportional Limit = 45 ksi
(Δσ/2) = 293 (Δε_p/2)^0.22
Specimen Details: Uniform gage test section
0.250 inch diameter
Reference: 3.8.1.1.8
* Minimum values from AMS 5772.

173. PDF page 1177

TUS, ksi	TYS, ksi	E, ksi	Temp., °F
Product Form/Thickness: Bar, 1.5 inch thick
Thermal Mechanical Processing History:
Solution treated, water quenched (AMS 5772)
Properties:
120*	55*		75
		22,406	1600
Stress-Strain Equations:
Cyclic (Companion Specimens) Proportional Limit = 36 ksi
(Δσ/2) = 81.6 (Δε_p/2)^0.094
Specimen Details: Uniform gage test section 0.250 inch diameter
Reference: 3.8.1.1.8
* Minimum values from AMS 5772.

174. PDF page 1179

TUS, ksi	TYS, ksi	E, ksi	Temp., °F
Product Form/Thickness: Bar, 1.5 inch thick
Thermal Mechanical Processing History:
Solution treated, water quenched (AMS 5772)
Properties:
120*	55*		75
		20,353	1800
Stress-Strain Equations:
Cyclic (Companion Specimens) Proportional Limit = 23 ksi
(Δσ/2) = 66.3 (Δε_p/2)^0.12
Specimen Details: Uniform gage test section 0.250 inch diameter
Reference: 3.8.1.1.8
* Minimum values from AMS 5772.

175. PDF page 1245

Undriven			Driven		Rivet Designation	Rivet Size
Rivet Material	F_su (ksi)		Rivet Material	F_su^b (ksi)		1/16	3/32	1/8	5/32	3/16	1/4	5/16	3/8
Rivet Material	Min	Max	Rivet Material	F_su^b (ksi)		Driven Single Shear Strength, lbs
5056-H32	24	n/a	5056-H321^d	28°	Bf	99	203	363	556	802	1450	2290	3275
2117-T4	26	n/a	2117-T3	30°	AD	106	217	389	596	860	1555	2455	3510
2017-T4	35	42	2017-T3	38°	D	134	275	493	755	1085	1970	3115	4445
2024-T4	37	n/a	2024-T31	41^g	DD	145	297	532	814	1175	2125	3360	4795
7050-T73	41	46	7050-T731^d	43°	Eh	152	311	558	854	1230	2230	3520	5030
Monel	49	59	Monel	52°	M	183	376	674	1030	1490	2695	4260	6085
Ti-45Cb	50	59	Ti-45Cb	53°	T	187	384	687	1050	1515	2745	4340	6200
A-286	85	95	A-286	90°		317	651	1165	1785	2575	4665	7375	10500

176. PDF page 1248

Rivet Type	NAS1198 (F_su = 90 ksi)
Sheet Material	A-286, solution treated and aged, F_ty = 140 ksi
Temperature	Room Temperature			1200°F, Stabilized 15 Minutes			1200°F, Rapid Heating in 20 Seconds, Tested in 15 Seconds
Rivet Diameter, in. (Nominal Hole Diameter, in.)	1/8 (0.1285)	5/32 (0.159)	3/16 (0.191)	1/8 (0.1285)	5/32 (0.159)	3/16 (0.191)	1/8 (0.1285)	5/32 (0.159)	3/16 (0.191)
Sheet thickness, in.:	Ultimate Strength^a
0.020	478		***	331			470b
0.025	590	740		426	626		587b	726b
0.032	745	932	1132	560	801	962	752b	930b	1117b
0.040	923	1152	1397	682	1002	1204	783	1164b	1397b
0.050	1023	1428	1677		1044	1505		1198	1729b
0.063	1131	1578	1821	***		1507
0.071	1170	1660	1909
0.080		1752	2008	***
0.090		1790	2118	***			***
0.100			2229
0.125	***		2504		***				***
0.160			2580
Rivet shear strength^c	1170	1790	2580	682	1044	1507	783	1198	1729
Sheet thickness, in.:	Yield Strength^a,d
0.020	447		***	300			300
0.025	590	695		374	464		374	464
0.032	745	932	974	479	593	713	478	593	712
0.040	867	1152	1167	598	741	890	598	740	889
0.050	938	1331	1407		925	1112		924	1110
0.063	1031	1447	1649			1400		***
0.071	1089	1518	1723	***
0.080		1597	1806
0.090		1686	1898	***
0.100			1990	***
0.125			2221	***	***				***
0.160			2543

177. PDF page 1268

Sheet thickness, in.:	(0.063)	(0.094)	(0.125)	(0.156)
Sheet thickness, in.:	Ultimate Strength, lbs.
0.032	325^c	---	---	---
0.040	396	502^c	---	---
0.050	452	612	750^c	---
0.063	498	696	923	1280^c
0.071	526	731	980	1425
0.080	531	771	1030	1585
0.090	---	814	1080	1735
0.125	---	---	1175	1985
0.160	---	---	---	2125
Rivet Shear Strength^d	531	814	1175	2125
	Yield Strength, lbs^e
Sheet thickness, in.:
0.032	268	---	---	---
0.040	326	415	---	---
0.050	399	504	619	---
0.063	493	620	759	1060
0.071	526	692	845	1175
0.080	531	771	942	1305
0.090	---	814	1050	1450
0.125	---	---	1175	1955
0.160	---	---	---	2125
Head height [ref.],^f in	0.029	0.037	0.046	0.060

178. PDF page 1288

a	Data supplied by Huck International, Inc.
b	Rivet shear strength is documented in MIL-R-7885D.
c	Permanent set at yield load: 4% of nominal hole diameter.

179. PDF page 1290

	Yield Strength, lbs^d
Sheet thickness, in.:
0.020	223	---	---
0.025	262	347	---
0.032	317	416	522
0.040	362	494	616
0.050	378	562	733
0.063	398	588	814
0.071	411	604	833
0.080	425	622	854
0.090	441	641	878
0.100	457	661	901
0.125	496	710	960
0.160	---	779	1040
0.190	---	---	1110

180. PDF page 1291

	Yield Strength, lbs^d
Sheet thickness, in.:
0.020	214	---	---
0.025	238	332	---
0.032	272	375	491
0.040	298	424	550
0.050	315	463	623
0.063	338	491	672
0.071	351	508	692
0.080	367	527	716
0.090	384	549	741
0.100	401	570	767
0.125	445	624	831

181. PDF page 1304

(Nominal Hole Diameter, in.)	(0.130)	(0.162)	(0.194)	(0.258)
	Ultimate Strength, lbs
Sheet thickness, in.:
0.040	167a
0.050	208	257a
0.063	262	324	390a
0.071	295	366	440
0.080	333	413	495
0.090	363	464	557	749a
0.100		516	620	833
0.125		556	774	1040
0.160			802	1332
0.190				1450
Rivet shear strength^b	363	556	802	1450
	Yield Strength^c, lbs
Sheet thickness, in.:
0.040	158
0.050	197	244
0.063	248	308	370
0.071	279	346	417
0.080	315	391	469
0.090	354	440	527	710
0.100		489	587	789
0.125		556	734	986
0.160		***	802	1262
0.190				1450
Head height (ref.), in.	0.042	0.055	0.070	0.095

182. PDF page 1327

Rivet shear strength^e	664	1030	1480
	Yield Strength, lbs^f
Sheet thickness, in.:
0.040	131	---	---
0.050	181	204	---
0.063	247	286	317
0.071	287	336	377
0.080	333	393	444
0.090	361	456	520
0.100	371	518	595
0.125	394	576	783
Head height [ref.], in.	0.042	0.055	0.070

183. PDF page 1328

Rivet shear strength^d	814	1245	1685
	Yield Strength, lbs^e
Sheet thickness, in.:
0.032	192	---	---
0.040	250	298	---
0.050	321	387	---
0.063	414	501	573
0.071	470	571	654
0.080	524	651	746
0.090	550	738	849
0.100	577	804	951
0.125	643	886	1120
0.160	736	1000	1250
0.190	814	---	1365
Head height (ref.), in.	0.035	0.047	0.063

184. PDF page 1329

Rivet shear strength^e	814	1245	1685
Rivet shear strength^e	Yield Strength, lbs^f
Sheet thickness, in.:
0.032	158	---	---
0.040	206	245	---
0.050	265	318	---
0.063	330	413	472
0.071	361	471	540
0.080	395	514	616
0.090	434	562	678
0.100	473	609	734
0.125	569	729	873
Head height (ref.), in	0.035	0.047	0.063

185. PDF page 1330

Rivet shear strength^e	814	1245	1685
	Yield Strength, lbs^f
Sheet thickness, in.:
0.032	138	---	---
0.040	218	217	---
0.050	317	340	---
0.063	433	500	529
0.071	475	598	643
0.080	510	675	772
0.090	527	741	889
0.100	543	781	966
0.125	585	833	1075
0.160	644	906	1160
0.190	---	968	1235
0.250	---	---	1375
Head height (ref.), in	0.035	0.047	0.063

186. PDF page 1391

		Specification.
		AMS-QQ-A-250/1	AMS-4029^b	AMS-QQ-A-250/3	AMS-QQ-A-250/4^b	AMS-QQ-A-250/5	AMS-QQ-A-250/2	AMS-QQ-A-250/8	AMS-QQ-A-250/11	AMS-QQ-A-250/12^b	AMS-QQ-A-250/13^°
Material		1100	Bare 2014	Clad 2014	Bare 2024	Clad 2024	3003	5052	6061	Bare 7075	Clad 7075
AMS-QQ-A-250/1	1100		*	*
AMS-4029	Bare 2014^b		*	*
AMS-QQ-A-250/3	Clad 2014		*	*
AMS-QQ-A-250/4	Bare 2024^b		*	*
AMS-QQ-A-250/5	Clad 2024
AMS-QQ-A-250/2	3003
AMS-QQ-A-250/8	5052
AMS-QQ-A-250/11	6061
AMS-QQ-A-250/12	Bare 7075^b		*	*
AMS-QQ-A-250/13	Clad 7075^b

187. PDF page 1392

Thickness of Thinnest Outer Sheet, in.	Spots/inch		Material Ultimate Tensile Strength, ksi
	Standard (Ns)^d	Range^e,f	56 and Above	Below 56
			Design Shear Strength, pounds per linear inch (Xm)
0.001	40	1-50	24	16
0.002	20	1-30	48	32
0.003	12	1-17	80	52
0.004	10	1-14	108	72
0.005	9	1-13	132	92
0.006	7	1-10	148	100
0.007	6	1-8	168	112
0.008	5	1-7	188	128

188. PDF page 1392

Xm	=	design shear strength in accordance with the above table
Ns	=	standard spots per inch in accordance with the above table
Nr	=	required spots per inch (production part)
Xr	=	actual design shear strength requirement
K	=	1.15 when number of spots per inch is reduced more than 15 percent of the standard spacing of the above table
K	=	0.90 when number of spots is increased more than 15 percent of the standard spacing but within range of the tabular spacing.

189. PDF page 1402

Xm	= design shear strength in accordance with the above table
Ns	= standard spots per inch in accordance with the above table
Nr	= required spots per inch (production part)
Xr	= actual design shear strength requirement
K	= 1.15 when number of spots per inch is reduced more than 15 percent of the standard spacing of the above table
K	= 0.90 when number of spots is increased more than 15 percent of the standard spacing but within range of the tabular spacing.

190. PDF page 1408

Section	Description	Page
9.3.2	Computer Software	50
9.3.3	General Data Formats	50
9.3.3.1	Data Format for the Computation of T₉₉ and T₉₀ Values	51
9.3.3.2	Data Format for Derived Properties	51
9.3.3.3	Data Format for the Construction of Typical Stress-Strain Curves	55
9.3.3.4	Data Format for Fasteners	55
9.3.3.5	Data Format for Other Properties	56
9.4	Substantiation of S-Basis Minimum Properties	59
9.5	Analysis Procedures for Statistically Computed Minimum Static Properties.	60
9.5.1	Specifying the Population	60
9.5.1.1	Deciding Between Direct and Indirect Computation	60
9.5.1.2	Testing for Regression Effects and Homogeneity	63
9.5.2	Regression Analysis.	64
9.5.2.1	Linear Regression	67
9.5.2.2	Quadratic Regression	68
9.5.2.3	Tests for Adequacy of a Regression	71
9.5.2.4	Tests for Equality of Several Regressions	74
9.5.3	Combinability of Data	77
9.5.3.1	The k-Sample Anderson-Darling Test	77
9.5.3.2	The F Test	79
9.5.3.3	The t Test	80
9.5.4	Determining the Form of Distribution	82
9.5.4.1	Anderson-Darling Test for Normality	82
9.5.4.2	Normal Probability Plot	83
9.5.4.3	Three-Parameter Weibull Acceptability Test	83
9.5.4.4	Anderson-Darling Test for Pearsonality	85
9.5.4.5	The Pearson Backoff Option	85
9.5.4.6	Pearson Probability Plot	86
9.5.4.7	Modified Anderson-Darling Test for Weibullness	89
9.5.4.8	Identifying Proper Backoff for Weibull Method.	91
9.5.4.9	Weibull Probability Plots	92
9.5.5	Direct Computation Without Regression	94
9.5.5.1	Sequential Pearson Procedure	100
9.5.5.2	Sequential Weibull Procedure	102
9.5.5.3	Nonparametric Procedures	103
9.5.6	Direct Computation by Regression Analysis	104
9.5.6.1	Performing the Regression	104
9.5.7	Indirect Computation without Regression (Reduced Ratios/ Derived Properties)	106
9.5.7.1	Treatment of Grain Direction	107
9.5.7.2	Treatment of Test Specimen Location	107
9.5.7.3	Treatment of Clad Aluminum Alloy Plate	108
9.5.7.4	Computational Procedure	108
9.5.8	Indirect Computation using Regression.	109

191. PDF page 1409

Section	Description	Page
9.6	Analysis Procedures for Dynamic and Time Dependent Properties	110
9.6.1	Load and Strain Control Fatigue Data	110
9.6.1.1	Data Collection and Interpretation	113
9.6.1.2	Analysis of Data	114
9.6.1.3	Fatigue Life Models	115
9.6.1.4	Evaluation of Mean Stress and Strain Effects	117
9.6.1.5	Estimation of Fatigue Life Model Parameters	118
9.6.1.6	Treatment of Outliers	124
9.6.1.7	Assessment of the Fatigue Life Model	125
9.6.1.8	Data Set Combination	127
9.6.1.9	Treatment of Runouts	128
9.6.1.10	Recognition of Time Dependent Effects	130
9.6.2	Fatigue Crack Growth Data	130
9.6.2.1	Data Collection and Interpretation	131
9.6.3	Fracture Toughness Data	133
9.6.3.1	Plane-Strain Fracture Toughness Data	133
9.6.3.2	Plane Stress and Transitional Fracture Toughness	133
9.6.4	Creep and Creep-Rupture Data	135
9.6.4.1	Data Collection and Interpretation	135
9.6.4.2	Analysis of Data	137
9.7	Analysis Procedures for Structural Joint Properties	142
9.7.1	Mechanically Fastened Joints	142
9.7.1.1	Definitions	143
9.7.1.2	Yield Load Determination	144
9.7.1.3	Shear Strength of Fastener	146
9.7.1.4	Sheet Critical and Transition Critical Strengths	148
9.7.1.5	Calculation of Allowable Loads	158
9.7.2	Fusion-Welded Joint Data	158
9.7.2.1	Data Collection and Interpretation	159
9.7.2.2	Data Analysis	161
9.8	Examples of Data Analysis and Data Presentation for Static Properties	162
9.8.1	Direct Analyses of Mechanical Properties	162
9.8.2	Indirect Analyses of Mechanical Properties	175
9.8.3	Tabular Data Presentation	179
9.8.3.1	Mechanical Properties	179
9.8.3.2	Modulus of Elasticity and Poisson's Ratio	183
9.8.3.3	Physical Properties	183
9.8.4	Room Temperature Graphical Mechanical Properties	184
9.8.4.1	Typical Stress-Strain	184
9.8.4.2	Compression-Tangent-Modulus Curves	191
9.8.4.3	Full-Range Tensile Stress-Strain Curves	194
9.8.4.4	Minimum Stress-Strain and Stress-Tangent-Modulus Curves	198
9.8.4.5	Biaxial Stress-Strain Behaviour	198
9.8.4.6	Mathematical Representation of Stress-Strain Curves	198

192. PDF page 1410

Section	Description	Page
9.8.5	Elevated Temperature Graphical Mechanical Properties	202
9.8.5.1	Strength Properties	202
9.8.5.2	Elongation and Reduction of Area	204
9.8.5.3	Modulus of Elasticity	206
9.8.5.4	Physical Properties	207
9.8.5.5	Effect of Thermal Exposure on Room Temperature Strength	208
9.8.5.6	Effect of Thermal Exposure on Elevated Temperature Strength	208
9.8.5.7	Simple Exposure	209
9.8.5.8	Complex Exposure	210
9.9	Examples of Data for Dynamic and Time Dependent Properties	212
9.9.1	Fatigue	212
9.9.1.1	Load Control	219
9.9.1.2	Strain Control	223
9.9.2	Fatigue Crack Growth	228
9.9.3	Fracture Toughness	230
9.9.3.1	Plane Strain	230
9.9.3.2	Plane Stress	230
9.9.4	Creep and Creep Rupture	234
9.9.4.1	Creep-Rupture Example Problem	235
9.9.5	Mechanically Fastened Joints	240
9.9.6	Fusion-Welded Joints	244
9.9.6.1	Additional Information	245
9.9.6.2	Room-Temperature Properties	245
9.9.6.3	Data on Effect of Temperature	246
9.9.6.4	Use of Design Data	246
9.10	Statistical Tables	247
9.10.1	One-Sided Tolerance Limit Factors, K, for the Normal Distribution, 0.95 Confidence, and n-1 Degrees of Freedom	248
9.10.2	0.950 Fractiles of the F Distribution Associated with n₁ and n₂ Degrees of Freedom	250
9.10.3	0.950 Fractiles of the F Distribution Associated with n₁ and n₂ Degrees of Freedom	251
9.10.4	0.95 and 0.975 Fractiles of the t Distribution Associated with df Degrees of Freedom	252
9.10.5	Area Under the Normal Curve from -∞ to the Mean + Z, Standard Deviations	253
9.10.6	One-Sided Tolerance-Limit Factors for the Three-Parameter Weibull Acceptability Test with 95 Percent Confidence	254
9.10.7	One-Sided Tolerance Factors for the Three-Parameter Weibull Distribution with 95 Percent Confidence	255
9.10.8	γ-values for Computing Threshold of Three-Parameter Weibull Distribution	261
9.10.9	Ranks, r, of Observations, n, for an Unknown Distribution Having the Probability and Confidence of T99 and T90 Values	264
Standards and References		266

193. PDF page 1474

	a = (Σy - bΣx) / n	[9.5.2.1(c)]
	b = S_xy / S_xx	[9.5.2.1(d)]
where	S_xy = Σxy - (Σx Σy) / n ,	[9.5.2.1(e)]
and
	S_xx = Σx² - (Σx)² / n .	[9.5.2.1(f)]

194. PDF page 1479

Mean Square	Linear Regression	Quadratic Regression
MSR	SSR	SSR/2
MSE	SSE/(n-2)	SSE/(n-3)
MSLF	SSLF/(k-2)	SSLF/(k-3)
MSPE	SSPE/(n-k)	SSPE/(n-k)

195. PDF page 1481

x_i	T_i
0.1	240
0.2	222
0.3	220
0.4	218
0.5	200

196. PDF page 1482

Source of Variation	Degree of Freedom, DF	Sum of Square, SS	Mean Squares, MS	F_calc
Regression	1	352.8	352.8	F₁ = 28.5
Error	8	99.2	12.4
Lack of Fit	3	51.2	17.07	F₂ = 1.78
Pure Error	5	48.0	9.6
Total	9	452.0

197. PDF page 1482

x	ŷ
0.100	118.4
0.200	114.2
0.300	110.0
0.400	105.8
0.500	101.6

198. PDF page 1486

	Product A	Product B
Sample size	20	30
Sample standard deviation, ksi	4.0	5.0
Sample mean, ksi	100.0	102.0

199. PDF page 1487

	Product A	Product B
Sample size	20	30
Sample standard deviation, ksi	4.0	5.0
Sample mean, ksi	100.0	102.0

200. PDF page 1502

Skewness	Percent Accepted	T99		T90
Skewness	Percent Accepted	Percent Coverage	Bias (Std. Dev.)	Percent Coverage	Bias (Std. Dev.)
-1.00	16	3	1.0	66	0.22
-0.75	40	11	0.7	78	0.16
-0.50	68	43	0.4	83	0.12
-0.25	91	82	0.2	88	0.08
0.00	98	98	-0.1	93	0.04
0.25	91	100	-0.4	97	-0.02
0.50	65	100	-0.6	99	-0.06
0.75	21	100	-0.7	100	-0.06
1.00	4	100	-0.7	100	-0.10

201. PDF page 1509

T₉₉ = τ₉₉ + Q₉₉ exp [ - V₉₉/(β₉₉√n)] ,	[9.5.5.2(a)]
T₉₀ = τ₉₀ + Q₉₀ exp [ - V₉₀/(β₉₀√n)] ,	[9.5.5.2(b)]

202. PDF page 1510

Rank of Test Point	Value of Test Point, ksi
1	73.3
2	74.1
3	75.2
4	75.3
5	75.6
299	85.7

203. PDF page 1524

S_eq = S_a + A₃ S_m	[9.6.1.4(d)]
or
S_eq = S_a + S_m^A₃	[9.6.1.4(e)]
and equivalent strain is defined as:
ε_eq = ε_a + A₃ S_m/E	[9.6.1.4(f)]
or
ε_eq = ε_a + (S_m/E)^A₃	[9.6.1.4(g)]

204. PDF page 1524

S_eq	= equivalent stress	ε_eq	= equivalent strain
S_a	= alternating stress	S_m	= mean stress
ε_a	= alternating strain	E	= elastic modulus (from each test result).

205. PDF page 1544

(1) log t = c + b₁/T + b₂X/T + b₃X²/T + b₄X³/T	[9.6.4.2(a)]
(2) log t = c + b₁/T + b₂X + b₃X² + b₄X³	[9.6.4.2(b)]
(3) log t = c + b₁ T + b₂X + b₃X² + b₄X³	[9.6.4.2(c)]
(4) log t = c + (T-T_a)(b₁ + b₂X + b₃X² + b₄X³).	[9.6.4.2(d)]

206. PDF page 1556

Test Specimen No.	D Diameter	D²	t Gage	t/D	Yield Load, P_y	P_y — 10⁴D²	Ultimate Load, P_u	P_u — 10⁴D²	Type of Failure

207. PDF page 1558

a, b, c	Best-fit equation coefficients
df	Degrees of freedom
F_.05(M–3,N-M)	The 5^th percentile of the F distribution with degrees of freedom M–3 and N-M
H	Estimated bound on ratio of MSE to MSPE
ln	Natural logarithm
M	Distinct levels of t/D
MSE	Mean Square Error
MSPE	Mean Square Pure Error
N	Total number of tests
q₁, q₂, …, q₆	Sums of the x_i = ln(t/D)
Q(x)	A measure of the “nearness” of x to the center of the range of independent variables
RMSE	Root Mean Square Error
(x̄)	The multiplier on s_y in the calculation of T₉₀ values for different t/D ratios
s_y	Unbiased estimate of standard deviation in average joint strengths
t/D	Sheet thickness / fastener diameter
x_i	Independent variable in quadratic regression analysis
y_ij	The j^th test value at i^th t/D ratio, used to compute dependent variable

208. PDF page 1566

BASE MATERIAL
Alloy, Composition, Form, Pre- and Post-Weld Heat Treat Condition, Material Thickness, Filler Material
WELDING PROCESS VARIABLES
Joint Preparation	Tooling	Welding Conditions	Weld Repair
Joint Type Edge Preparation Cleaning	Alignment Restraint Thermal Control	Welding Process Welding Method Welding Position Heat Input (Weld Setting) Preheat Interpress Temperature Shielding Gas	Number of Repairs Type of Repair
WELD CHARACTER
Inspection Methods		Acceptance Levels
NDT Visual Radiographic Magnetic Particle Ultrasonic DT Transverse Tensile Test		External Underfill and Undercut Cracks Pores Reinforcements Internal Pores Inclusions Cracks Tensile Properties Minimum and Minimum Average

209. PDF page 1573

Subpopulation
Subpopulation	n	X, ksi	s, ksi
Group (1& 3) TUS (LT), 0.020-0.125, Suppliers A and B	330	150.1	4.10

210. PDF page 1573

Subpopulation	n	X̄ , ksi	s, ksi
Group (2) TYS (LT), 0.020-0.125, Supplier A	300	130.0	4.00
Group (4) TYS (LT), 0.020-0.125, Supplier B	30	131.0	5.00

211. PDF page 1573

Subpopulation	n	X, ksi	s, ksi
Group (2& 4) TYS (LT), 0.020-0.125, Suppliers A and B	330	130.1	4.10

212. PDF page 1573

Subpopulation	n	X̄, ksi	s, ksi
Group (1) TUS (LT), 0.020-0.125	300	150.0	4.00
Group (5) TUS (LT), 0.126-0.249	100	145.0	4.47

213. PDF page 1575

Population	n	X̄, ksi	s, ksi
Group (1& 3) TUS (LT), 0.020-0.125	330	150.1	4.10

214. PDF page 1575

Population	n	‾X, ksi	s, ksi
Group (1 & 3) TUS (LT), 0.020 to 0.125	330	150.1	4.10

215. PDF page 1576

Population	n	X, ksi	s, ksi
Group (2 & 4) TYS(LT), 0.20 to 0.125	330	130.1	4.10

216. PDF page 1576

Rank	TYS, ksi	Rank	TYS, ksi	Rank	TYS, ksi
1	120.5	9	122.5	17	123.5
2	121.4	10	122.5	18	123.5
3	121.6	11	122.6	19	123.6
4	121.8	12	123.1	20	123.7
5	122.1	13	123.1	21	123.8
6	122.1	14	123.2	22	123.8
7	122.3	15	123.2	23	123.8
8	122.5	16	123.3	24	124.0

217. PDF page 1577

Zj	Hj	Fij	Zj	Hj	Fij	Zj	Hj	Fij
139.61	0.5	0	142.48	8.5	1	143.72	16.5	1
140.64	1.5	0	142.60	9.5	1	143.84	17.5	1
140.71	2.5	0	142.69	10.5	1	143.86	18.5	1
140.99	3.5	0	143.31	11.5	1	143.87	19.5	1
141.87	4.5	0	143.50	12.5	1	143.98	20.5	1.5
141.91	5.5	0.5	143.62	13.5	1	144.00	21.5	2
141.94	6.5	1	143.64	14.5	1	144.22	22.5	2
142.10	7.5	1	143.67	15.5	1	144.32	23.5	2

218. PDF page 1580

K = 88	W_A = 0.698
W_β = 0.678	X̅ = 150.1
S = 4.10	X₍₁₎ = 139.608
H = 139.6079	L = -259.9

219. PDF page 1580

K = 88	X̄ = 130.1
W₅₀ = 0.665	X₍₁₎ = 120.487
S = 4.10	H = 120.4869
L = -279.9

220. PDF page 1582

Σ(x)	=	2.94	(Σr)²	=	381.4209
Σ(x²)	=	0.4260	(Σx) (Σr)	=	57.4182
Σ(r)	=	19.53	Sxx	=	0.1379
Σ(r²)	=	12.7319	Sxr	=	0.0416
Σ(xr)	=	1.8723	Srr	=	0.0179
(Σx)²	=	8.6436

221. PDF page 1583

x₁	T₁	x₁	T₁
0.02	2.04	0.09	1.95
0.03	2.01	0.10	1.95
0.04	2.01	0.15	1.89
0.06	1.98	0.18	1.89
0.07	1.98	0.24	1.83

222. PDF page 1583

Source of Variation	Sum of Squares	Degrees of Freedom	Mean Squares	F calc
Regression	0.0126	1	0.0126	63.0
Error	0.0053	28	0.0002
Lack of Fit	0.0004	8	0.00005	0.208
Pure Error	0.0049	20	0.00024
Total	0.0179	29

223. PDF page 1584

t, inch	Reduced Ratio	A-basis	B-basis	S-basis
0.020	0.668	93.5	96.2
0.062	0.657	92.0	94.6
0.125	0.638	89.3	91.9
0.249	0.595			80.3

224. PDF page 1585

Basis	<0.020	0.020-0.062		0.063-0.125		0.126- 0.249
Basis	S	A	B	A	B	S
Ftu(LT), ksi	140	140	144	140	144	135
Fty(LT), ksi	115	120	124	120	124	110
Fsu, ksi		92	94	89	92	80

225. PDF page 1586

Basis	S	A	B ⑧
Specification			③
Form
Condition (or Temper)			④
Cross-Sectional Area, in.²			⑤
Location Within Casting			⑥
Thickness or Diameter, in.			⑦
Mechanical Properties:
F_tu, ksi:			124
L	120	120
LT (or T) ⑨		⑩
ST
F_ty, ksi:
L
LT (or T)
ST
F_cy, ksi:
L
LT (or T)
ST
F_su, ksi:
F_bru, ksi:⑪
(e/D = 1.5)
(e/D = 2.0)
F_bry, ksi:
(e/D = 1.5)
(e/D = 2.0)
e, percent (S-basis):
L
LT (or T)
ST
RA, percent (S-basis):
L
LT (or T)
ST
E, 10³ ksi
E_c, 10³ ksi
G, 10³ ksi
μ
Physical Properties:
ω, lb/in.³	⑫
C, Btu/(lb)/(°F)	⑫

226. PDF page 1606

Temper/Product Form	Condition	Temper- ature, °F	Grain Direction	Tension			Compression
Temper/Product Form	Condition	Temper- ature, °F	Grain Direction	n	TYS, ksi	TUS	n_e	CYS, ksi
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

227. PDF page 1607

Tension
n =	Ramberg-Osgood parameter for small plastic strains in tension from the proportional limit up to the yield stress.
TYS =	Typical yield stress in tension.
TUS =	Typical ultimate stress in tension.
Compression
n_c =	Ramberg-Osgood parameter for small plastic strains in compression up to the yield stress.
CYS =	Typical yield stress in compression.

228. PDF page 1609

	s² = Σ(r - r̄)²/(n - 1)	[9.8.5.1.1(a)]
or
	s² = [Σ(r²) - (Σr)²/n]/(n - 1)	[9.8.5.1.1(b)]
and
	R = r̄ - t s/√n	[9.8.5.1.1(c)]

229. PDF page 1624

	- Specimen Type
	- Specimen Dimensions
	- Fabrication Sequence
(7)	Surface Condition/Surface Residual Stresses/Finish
	- Finish
	- Residual Stress Data
(8)	Equivalent Strain Equation
	- Life Equation with Parameter Estimates
	- Standard Deviation of log(Life)
	- Adjusted R-Squared Statistic
	- Sample Size
(9)	Reference Numbers
(10)	No. of Heats/Lots

230. PDF page 1624

Thermal Mechanical Processing History: Annealed at 1800°F, water quench				Test Parameters: Strain Rate/Frequency - 180 cpm Wave Form - Sinusoidal Temperature - 250°F Atmosphere - Air
Product Form:	Die forging, 2 inch thick			Reference:	3.4.5.6.8(a)
Properties:				No. of Heats/Lots:	2
TUS, ksi	TYS, ksi	E, ksi	Temp., °F
155-160	135-140	29,000	250
Stress-Strain Equations:				Equivalent Strain Equation:
Monotonic Proportional Limit = 111 ksi σ = 289 (ε_p)^0.138 Cyclic (Companion Specimens) Proportional Limit = 92 ksi (Δε/2) = 156 (Δε_p/2)^0.046 Mean Stress Relaxation σ_m = 114.0-24562(Δε/2)				Log N_f = -6.56-4.20 log (ε_eq-0.0022) ε_eq = (Δε)^0.46 (S_max/E)^0.54 Standard Error of Estimate, Log (Life) = 0.123 Standard Deviation, Log (Life) = 0.465 Adjusted R² Statistic = 93%
				Sample Size	33
				[Caution: The equivalent strain model may provide unrealistic life predictions for strain ratios and ranges beyond those represented above.]
Specimen Details: Uniform gage test section 0.250 inch diameter Polished with increasingly finer grits of emery paper to surface roughness of 10 RMS with polishing marks longitudinal.

231. PDF page 1632

A₁	=	-4.62
A₂	=	-3.28
A₃	=	0.610
A₄	=	0.00198.

232. PDF page 1634

A₁ =	-5.07
A₂ =	-3.47
A₃ =	0.610
A₄ =	0.00198.

233. PDF page 1636

Product Form: Bar, 1 inch thick

Thermal Mechanical Processing History: Not available

Properties:

TUS, ksi	TYS, ksi	E, ksi	Temp., °F
175-180	150-155	27,500	70

Stress-Strain Equations:
    Monotonic
        Proportional Limit = 150 ksi
        σ = 280 (ε_p)^0.12
    Cyclic (Companion Specimens)
        Proportional Limit = 105 ksi (est.)
        (Δσ/2) = 196 (Δε_p/2)^0.076
    Mean Stress Relaxation
        σ_m = 125.4-25666(Δε/2)

Specimen Details:
    Uniform gage test section
    0.200 inch diameter

Reference: 3.4.5.6.8(a)

Test Parameters: Strain Rate/Frequency - 180 cpm Wave Form - Sinusoidal Temperature - 70°F

No. of Heats/Lots: 4

Equivalent Strain Equation: Log N = -5.07-3.47 log (ε_eq-0.00198) ε_eq = (Δε)^0.61 (S_max/E)^0.39 Standard Error of Estimate, Log(Life) = 0.111 Standard Deviation, Log (Life) = 0.555 Adjusted R² Statistic = 96%

Sample Size = 29

[Caution: The equivalent strain model may provide unrealistic life predictions for strain ratios and ranges beyond those represented above.]

234. PDF page 1643

	5	6
1	-5.748E-02	-1.606E+00
4	3.517E-05	9.843E-04
0	2.032E-01	1.634E+00
1	-1.220E-01	-4.892E-01
1	1.697E-02	3.801E-02
1	3.801E-02	1.471E+00
1	2.248E-02	1.303E+00
2	-1.245E-02	9.401E-01
3	-2.618E-02	9.124E-01

235. PDF page 1644

T E M P	3	6	10	18	32	HOURS		180	320	560	1000	3000	5600	°F
T E M P	3	6	10	18	32	56	100	180	320	560	1000	3000	5600	°F

T1			63	59	54	52	48	45	42	39	36			1600
T2			42	39	36	32	29	27	25	22	20			1750
T3			25	22	20	17	15	12	10					1900
T4
T5
T6
T7
T8

236. PDF page 1646

SPECIFICATION DATA @ 30 KSI 1800°F
Hours
41.4	33.1	70.5	36.1
16.5	27.4	37.5	34.9
35.0	33.4	48.6	74.2
33.6	51.3	29.0	47.5
32.6	42.7	26.4

237. PDF page 1647

Rivet Type ⑦	NASXXXX (F_su = AAA ksi) ⑧
Sheet Material	Clad 7075-T6 ⑨
Rivet Diameter, in. (Nominal Hole Diameter, in.)^b	3/32 ⑩	1/8 ⑩	5/32 ⑩	3/16 ⑩	1/4 ⑩
	(0.096)	(0.1285)	(0.159)	(0.191)	(0.257)
	Ultimate Strength, lbs (Estimated Lower Bound)
Sheet thickness:
0.032	⑫ 182^c
0.040	227	d⑫ 304
0.050	246	381	d⑫ 471
0.063		441	594	d⑫ 714
0.071 ⑪			670	805	d
0.080			675	907	⑯
0.090				974	⑫) 1375
0.100					1525
0.125					1765
Fastener shear strength ⑬	246 ⑭	441 ⑭	675 ⑭	974 ⑭	1765 ⑭
	Yield Strength^f, lbs (Conservatively Adjusted Average)
Sheet thickness, in.:
0.032	119 ⑮
0.040	188	224 ⑮
0.050	246	307	349 ⑮
0.063		414	481	539 ⑮
0.071 ⑪			563	637
0.080			655	748
0.090				870	1060 ⑮
0.100					1230
0.125					1640
Fastener tensile strength^g, lbs ⑱	275	495	755	1090	1975
Head height (ref.), in. ⑲	0.039	0.049	0.059	0.070	0.091

238. PDF page 1648

Rivet Diameter, in. (Nominal Hole Diameter, in.)^b	3/32 (10) (0.096)	1/8 (10) (0.1285)	5/32 (10) (0.159)	3/16 (10) (0.191)	1/4 (10) (0.257)
Ultimate Strength, lbs (B-Basis)^f					1/4 (10) (0.257)
Sheet thickness:	3/32 (10) (0.096)	1/8 (10) (0.1285)	5/32 (10) (0.159)	3/16 (10) (0.191)
0.032	(12) xxx^c
0.040	XXX	^d(12) xxx
0.050	XXX	XXX	^d(12) xxx
0.063		XXX	XXX	^d(12) XXX
0.071 (11)			XXX	XXX	^d
0.080			XXX	XXX	(16)
0.090				XXX	(12) xxxx
0.100					XXXX
0.125					XXXX
Fastener shear strength^e (13)	xxx (14)	xxx (14)	xxx (14)	xxx (14)	XXXX (14)
Yield Strength^f, lbs (B-Basis)
Sheet thickness, in.:
0.032	XXX (15)
0.040	XXX	XXX (15)
0.050	XXX	XXX	XXX (15)
0.063		XXX	XXX	XXX (15)
0.071 (11)			XXX	XXX
0.080			XXX	XXX
0.090				XXX	XXXX (15)
0.100					XXXX
0.125					XXXX
Fastener tensile strength^g, lbs (18)	XXX	XXX	XXX	XXXX	XXXX
Head height (ref.), in. (19)	X.XXX	X.XXX	X.XXX	X.XXX	X.XXX

239. PDF page 1649

0.008	0.016	0.032	0.063	0.090	0.160	0.312	0.625
0.010	0.020	0.040	0.071	0.100	0.190	0.375	0.750
0.012	0.025	0.050	0.080	0.125	0.250	0.500	0.875

240. PDF page 1666

N	V99 for T99			V90 for T90
N	Uncensored	20% Censored	50% Censored	Uncensored	20% Censored	50% Censored
1400	6.934	7.983	9.633	3.948	4.273	4.597
1500	6.924	7.969	9.612	3.943	4.266	4.589
1600	6.914	7.957	9.593	3.938	4.260	4.580
1700	6.906	7.946	9.575	3.934	4.255	4.573
1800	6.899	7.936	9.560	3.930	4.250	4.567
1900	6.892	7.926	9.545	3.927	4.246	4.560
2000	6.886	7.918	9.532	3.923	4.241	4.555
3000	6.841	7.858	9.438	3.901	4.212	4.515
4000	6.815	7.822	9.383	3.887	4.195	4.492
5000	6.797	7.798	9.346	3.878	4.183	4.477
6000	6.784	7.781	9.319	3.871	4.175	4.465
7000	6.773	7.767	9.298	3.866	4.168	4.456
8000	6.765	7.756	9.281	3.862	4.163	4.449
9000	6.758	7.747	9.267	3.859	4.159	4.443
10000	6.753	7.739	9.255	3.856	4.155	4.438
15000	6.733	7.713	9.215	3.846	4.142	4.422
20000	6.722	7.698	9.192	3.840	4.135	4.412
25000	6.714	7.688	9.176	3.836	4.130	4.405
30000	6.708	7.680	9.164	3.833	4.126	4.400

241. PDF page 1666

Constant	Uncensored	20% Censored	50% Censored
a₀₀	0.6079	0.9282	1.7162
a₀₁	-0.4740	-0.4562	-0.0428
a₁₁	0.9775	0.9841	1.2169

242. PDF page 1669

	Anderson-Darling Test		T90			T99
n	Uncensored or 20% Censored Γ50,0 or Γ50,20	50% Censored Γ50,50	Uncensored Γ90,0	20% Censored Γ90,20	50% Censored Γ90,50	Uncensored Γ99,0	20% Censored Γ99,20	50% Censored Γ99,50
975	0.66595	0.66552	0.67371	0.67360	0.67403	0.68521	0.68330	0.68369
1000	0.66597	0.66554	0.67363	0.67353	0.67393	0.68500	0.68310	0.68347
1100	0.66603	0.66565	0.67332	0.67322	0.67354	0.68414	0.68231	0.68262
1200	0.66609	0.66574	0.67305	0.67295	0.67321	0.68339	0.68162	0.68188
1300	0.66613	0.66581	0.67282	0.67271	0.67294	0.68275	0.68103	0.68126
1400	0.66617	0.66587	0.67261	0.67250	0.67269	0.68216	0.68049	0.68069
1500	0.66620	0.66592	0.67241	0.67231	0.67246	0.68162	0.68000	0.68017
1600	0.66623	0.66597	0.67225	0.67214	0.67227	0.68116	0.67958	0.67973
1700	0.66626	0.66601	0.67209	0.67198	0.67209	0.68072	0.67918	0.67931
1800	0.66628	0.66605	0.67194	0.67184	0.67193	0.68032	0.67882	0.67893
1900	0.66630	0.66608	0.67181	0.67171	0.67179	0.67997	0.67849	0.67859
2000	0.66632	0.66611	0.67168	0.67158	0.67165	0.67963	0.67819	0.67827
3000	0.66643	0.66630	0.67080	0.67071	0.67072	0.67725	0.67604	0.67604
4000	0.66649	0.66639	0.67027	0.67019	0.67017	0.67584	0.67477	0.67474
5000	0.66653	0.66644	0.66990	0.66983	0.66981	0.67487	0.67390	0.67385
6000	0.66655	0.66648	0.66963	0.66956	0.66953	0.67415	0.67326	0.67321
7000	0.66657	0.66651	0.66942	0.66935	0.66933	0.67360	0.67277	0.67271
8000	0.66658	0.66653	0.66924	0.66919	0.66916	0.67315	0.67237	0.67230
9000	0.66659	0.66654	0.66910	0.66905	0.66902	0.67278	0.67204	0.67197
10000	0.66660	0.66656	0.66898	0.66893	0.66890	0.67247	0.67176	0.67169

243. PDF page 1670

T99 Value						T90 Value
n	r99	n	r99	n	r99	n	r90	n	r90	n	r90
≤298	a	4635	36	8643	72	≤28	b	638	52	2693	340
299	1	4749	37	8753	73	29	1	660	54	3797	350
473	2	4862	38	8862	74	46	2	682	56	3901	360
628	3	4975	39	8972	75	61	3	704	58	4005	370
773	4	5088	40	9081	76	76	4	726	60	4109	380
913	5	5201	41	9190	77	89	5	781	65	4213	390
1049	6	5314	42	9300	78	103	6	836	70	4317	400
1182	7	5427	43	9409	79	116	7	890	75	4421	410
1312	8	5539	44	9518	80	129	8	945	80	4525	420
1441	9	5651	45	9627	81	142	9	999	85	4629	430
1568	10	5764	46	9736	82	154	10	1053	90	4733	440
1693	11	5876	47	9845	83	167	11	1107	95	4836	450
1818	12	5988	48	9954	84	179	12	1161	100	4940	460
1941	13	6099	49	10063	85	191	13	1269	110	5044	470
2064	14	6211	50	10172	86	203	14	1376	120	5147	480
2185	15	6323	51	10281	87	215	15	1483	130	5251	490
2305	15	6434	52	10390	88	227	16	1590	140	5354	500
2425	16	6545	53	10498	89	239	17	1696	150	5613	525
2546	18	6657	54	10607	90	251	18	1803	160	5871	550
2665	19	6768	55	10716	91	263	19	1909	170	6130	575
2784	20	6879	56	10824	92	275	20	2015	180	6388	600
2902	21	6990	57	10933	93	298	22	2120	190	6645	625
3020	22	7100	58	11041	94	321	24	2226	200	6903	650
3137	23	7211	59	11150	95	345	26	2331	210	7161	675
3254	24	7322	60	11258	96	368	28	2437	220	7418	700
3371	25	7432	61	11366	97	391	30	2542	230	7727	730
3487	26	7543	62	11475	98	413	32	2647	240	8036	760
3603	27	7653	63	11583	99	436	34	2752	250	8344	790
3719	28	7763	64	11691	100	459	36	2857	260	8652	820
3834	29	7874	65			481	38	2962	270	8960	850
3949	30	7984	66			504	40	3066	280	9268	880
4064	31	8094	67			526	42	3171	290	9576	910
4179	32	8204	68			549	44	3276	300	9884	940
4293	33	8314	69			571	46	3380	310	10191	970
4407	34	8423	70			593	48	3484	320	10499	1000
4521	35	8533	71			615	50	3589	330

244. PDF page 1672

AMS 2355	Quality Assurance Sampling and Testing of Aluminum Alloys and Magnesium Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded Rings
AMS 2370	Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel Wrought Products and Forging Stock
AMS 2371	Quality Assurance Sampling and Testing, Corrosion and Heat Resistant Steels and Alloys, Wrought Products and Forging Stock
ASTM B557	Method of Tension Testing Wrought and Cast Aluminum – and Magnesium-Alloy Products (vol. 02.02, 02.03, 03.01)
ASTM B769	Test Method for Shear Testing of Aluminum Alloys (vol. 02.02)
ASTM B831	Standard Test Method for Shear Testing of Thin Aluminum Alloy Products (vol. 02.02)
ASTM C693	Test Method for Density of Glass by Buoyancy (vol. 15.02)
ASTM C714	Test Method for Thermal Diffusivity of Carbon and Graphite by a Thermal Pulse Method (vol. 15.01)
ASTM D2766	Test Method for Specific Heat of Liquids and Solids (vol. 05.02)
ASTM E8	Test Methods of Tension Testing of Metallic Materials (vol. 01.02, 02.01, 02.03, 03.01)
ASTM E9	Compression Testing of Metallic Materials at Room Temperature (vol. 03.01)
ASTM E21	Recommended Practice for Elevated Temperature Tension Tests of Metallic Materials (vol. 03.01)
ASTM E29	Standard Practice for Using Significant Digits in Test Data to Determine Conformance with Specifications (vol. 14.02)
ASTM E83	Method of Verification and Classification of Extensometers (vol. 03.01)
ASTM E111	Test Method for Young’s Modulus, Tangent Modulus, and Chord Modulus (vol. 03.01)
ASTM E132	Test Method for Poisson’s Ratio at Room Temperature (vol. 03.01)
ASTM E139	Recommended Practice for Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic Materials (vol. 03.01)
ASTM E143	Test Method for Shear Modulus at Room Temperature (vol. 03.01)

245. PDF page 1673

ASTM E228	Test Method for Linear Thermal Expansion of Solid Materials with a Vitreous Silica Delatometer (vol. 03.01, 14.02)
ASTM E238	Method for Pin-Type Bearing Test of Metallic Materials (vol. 03.01)
ASTM E399	Test Method for Plane-Strain Fracture Toughness of Metallic Materials (vol. 02.02, 03.01)
ASTM E466	Recommended Practice for Constant Amplitude Axial Fatigue Tests of Metallic Materials (vol. 03.01)
ASTM E561	Recommended Practice for R-Curve Determination (vol. 03.01)
ASTM E606	Recommended Practice for Constant-Amplitude Low-Cycle Fatigue Testing (vol. 03.01)
ASTM E647	Test Method for Measurement of Fatigue Crack Growth Rates (vol. 03.01)
ASTM E739	Practice for Statistical Analysis of Linear or Linearized Stress-Life (S-N) and Strain-Life (ε-N) Fatigue Data (vol. 03.01)
ASTM G34	Test Method for Exfoliation Corrosion Susceptibility in 2XXX and 7XXX Series Aluminum Alloys (EXCO Test) (vol. 03.02)
ASTM G47	Test Method for Determining Susceptibility to Stress-Corrosion Cracking of High-Strength Aluminum Alloy Products (vol. 02.02, 03.02)
NASM 1312-4	Fastener Test Methods- Method 4 Lap Joint Shear
NASM 1312-8	Fastener Test Methods- Method 8 Tensile Strength
NASM 1312-13	Fastener Test Methods- Method 13 Double Shear Test
NASM 1312-20	Fastener Test Methods- Method 20 Single Shear
REFERENCES
9.1.5	Natrella, M.G., Experimental Statistics, National Bureau of Standards Handbook 91 (August 1, 1963).
9.2.3.5.3	Feddersen, C. E., “Evaluation and Prediction of the Residual Strength of Center-Cracked Tension Panels”, Damage Tolerance in Aircraft Structures, ASTM STP 486, American Society for Testing and Materials (1971).
9.2.5.1(a)	“Manual on Statistical Planning and Analysis for Fatigue Experiments”, ASTM STP 588 (1975).

246. PDF page 1674

9.2.5.1(b)	ASTM Special Technical Publication No. 91-A, “A Guide for Fatigue Testing and the Statistical Analysis of Fatigue Data”, Supplement to Manual on Fatigue Testing, STP No. 91 (1963).
9.2.5.1(c)	Landgraf, R. W., Morrow, J., and Endo, T., “Determination of the Cyclic Stress-Strain Curve”, Journal of Materials, JMLSA, Vol. 4, No. 1, March 1969, pp. 176-188.
9.2.5.2	Mandel, J., and Paule, R., “Interlaboratory Evaluation of a Material With Unequal Numbers of Replicates”, Analytical Chemistry, Vol. 42, No. 11, pp. 1194-1197 (September 1979), correction in Vol. 43, No. 10 (August 1971).
9.5.2.4	Neter, J., and Wasserman, W., “Applied Linear Statistical Models”, Richard D. Irwin (1974), pp. 160-165.
9.5.3.1	Scholz, F. W., and Stephens, M. A., “K-Sample Anderson-Darling Tests”, J. Amer. Statist. Assoc., 82, pp. 918-924 (Sept. 1987).
9.5.4.1(a)	Lawless, J. F., Statistical Models and Methods for Lifetime Data, John Wiley and Sons (1982), pp. 452-460.
9.5.4.1(b)	D’Agostina, R. B. and Stephens, M. A., “Goodness-of-Fit Techniques,” Marcel Dekker, p. 123 (1987).
9.5.4.1(c)	Pierce, D. A., and Kopecky, K. J., “Testing Goodness of Fit for the Distribution of Errors in Regression Models”, Biometrika, 66, pp. 1-5 (1979).
9.5.5.1(a)	Abramowitz, M. and Stegun, I. A. (Eds.). Handbook of Mathematical Functions with Formulas, Graphs, and Mathematical Tables, 9th printing. New York: Dover, pp. 930 (1972).
9.5.5.1(b)	Vogel, R. M., and McMartin, D. E., Probability Plot Goodness-of-Fit and Skewness Estimation Procedures for the Pearson Type 3 Distribution, Water Res., 27 (12), pp. 3149-3158 (1991).
9.5.5.2(a)	Jones, R. A., and Scholz, F. W., “A and B-Allowables for the Three Parameter Weibull Distribution”, Boeing Computer Services Company Technical Report No. 10 (October 1983).
9.5.5.2(b)	Jones, R. A., and Scholz, F. W., “Tolerance Limits for the Three Parameter Weibull Distribution”, Boeing Computer Service Company Technical Report No. 11 (1983).
9.6.1	Landgraf, R. W., “The Resistance of Metals to Cyclic Deformation”, Achievement of High Fatigue Resistance in Metals and Alloys, ASTM STP 467, 1970, pp. 3-36.
9.6.1.3	Sjodahl, L. H., “Extensions of the Multiple Heat Regression Technique Using Centered Data for Individual Heats”, Progress in Analysis of Fatigue and Stress Rupture (Data), MPC-Vol. 23, 1984, pp. 47-86.

247. PDF page 1675

9.6.1.4(a)	Walker, E. K, “The Effect of Stress Ratio During Crack Propagation and Fatigue for 2024-T3 and 7075-T6 Aluminum”, Effect of Environment and Complex Load History on Fatigue Life, ASTM STP 462 (1970) pp. 1-14.
9.6.1.4(b)	Stulen, F. L., “Fatigue Life Data Displayed by a Single Quantity Relating Alternating and Mean Stresses”, AFML-TR-65-121 (1965).
9.6.1.4(c)	Topper, T. H., and Sandor, B. I., “Effects of Mean Stress and Prestrain on Fatigue-Damage Summation”, Effects of Environment and Complex Load History on Fatigue Life, ASTM STP 462, 1970, pp. 93-104.
9.6.1.6	Snedecor, G. W., and Cochran, W. G., Statistical Methods, Seventh Edition, The Iowa State University Press, Ames, Iowa (1980), pp. 115-116.
9.6.1.7	Montgomery, D. C., and Peck, E. A., Introduction to Linear Regression Analysis, Wiley, New York (1982).
9.6.1.8	Winer, B. J., Statistic Principles in Experimental Design, 2nd Ed., McGraw-Hill, New York (1971).
9.6.1.9(a)	Kalbfleisch, J. D., and Prentice, R. L., The Statistical Analysis of Failure Time Data, Wiley, New York (1982).
9.6.1.9(b)	SAS Users Guide: Statistical Version 5 ed., Cary, N.C.: SAS Institute, Inc. (1985).
9.6.3.2.2	Skinn, D. A., Gallagher, J. P., Berens, A. P., Huber, P.D. and Smith, J., “Damage Tolerant Design Handbook”, Volumes 1-5, WL-TR-94-4052, 4053, 4054, 4055 and 4056, May 1994.
9.6.4.2	“Characterization of Materials for Service at Elevated Temperatures”, Report No. MPC-7, Presented at 1978 ASME/CSME Montreal Pressure Vessel and Piping Conference, Montreal, Quebec, Canada (June 25-29, 1978).
9.7.2	Hood, D., et al., “An Investigation of the Generation and Utilization of Engineering Data on Weldments”, AFML-TR-68-268 (October 1968).
9.8.4.1.2(a)	Ramberg, W., and Osgood, W. R., “Description of Stress Strain Curves by Three Parameters”, National Advisory Committee for Aeronautics, Technical Note 902 (July 1943).
9.8.4.1.2(b)	Hill, H. N., “Determination of Stress-Strain Relations from Offset Yield Strength Values”, National Advisory Committee for Aeronautics, Technical Note 927 (February 1944).
9.8.4.5	Burt, C. W., et al., “Mechanical Properties of Aerospace Structural Alloys Under Biaxial-Stress Conditions”, AFML-TR-66-229 (August 1966).
9.10(a)	Owen, D. B., “Factors for One-Sided Tolerance Limits and for Variables and Sampling Plans”, Sandia Corporation Monograph SCR-607 (March 1963).
9.10(b)	Johnson, N. L., and Kotz, S., Distributions in Statistics—Continuous Univariate Distributions—1, John Wiley & Sons, p. 176 (1970).

248. PDF page 1680

E_c	— Modulus of elasticity in compression; average ratio of stress to strain below proportional limit.
E_s	— Secant modulus of elasticity, Eq. 9.8.4.2(c).
E_t	— Tangent modulus of elasticity.
ELI	— Extra low interstitial (grade of titanium alloy).
ER	— Equivalent round.
ESR	— Electro-slag remelted.
f	— Internal (or calculated) tension stress; stress applied to the gross flawed section; creep stress.
f_b	— Internal (or calculated) primary bending stress.
f_c	— Internal (or calculated) compressive stress; maximum stress at fracture: gross stress limit (for screening elastic fracture data).
f_pl	— Proportional limit.
f_s	— Internal (or calculated) shear stress.
f_t	— Internal (or calculated) tensile stress.
ft	— Foot: feet.
F	— Design stress; Fahrenheit; Ratio of two sample variances.
F_A	— Design axial stress.
F_b	— Design bending stress; modulus of rupture in bending.
F_bru	— Design ultimate bearing stress.
F_bry	— Design bearing yield stress.
F_c	— Design column stress.
F_cc	— Design crushing or crippling stress (upper limit of column stress for local failure).
F_cu	— Design ultimate compressive stress.
F_cy	— Design compressive yield stress at which permanent strain equals 0.002.
F_H	— Design hoop stress.
F_s	— Design shear stress.
F_sp	— Design proportional limit in shear.
F_st	— Design modulus of rupture in torsion.
F_su	— Design ultimate stress in pure shear (this value represents the average shear stress over the cross section).
F_sy	— Design shear yield stress.
F_tp	— Design proportional limit in tension.
F_tu	— Design tensile ultimate stress.
F_ty	— Design tensile yield stress at which permanent strain equals 0.002.
g	— Gram(s).
G	— Modulus of rigidity (shear modulus).
Gpa	— Gigapascal(s).
hr	— Hour(s).
H	— Subscript “hoop”.
HIP	— Hot isostatically pressed.
i	— Slope (due to bending) of neutral plane of a beam, in radians (1 radian = 57.3 degrees).
in.	— Inch(es).
I	— Axial moment of inertia.
J	— Torsion constant (= Ip for round tubes); Joule.
k	— Tolerance limit factor for the normal distribution and the specified probability, confidence, and degrees of freedom; Strain at unit stress.
k₉₉, k₉₀	— One-sided tolerance limit factor for T₉₉ and T₉₀, respectively (see Section 9.10.1 and 9.10.7).
k_A,B	— k factor for A basis or B basis, respectively (see Section 9.10.1 and 9.10.7).
ksi	— Kips (1,000 pounds) per square inch.

249. PDF page 1681

K	— A constant, generally empirical; thermal conductivity; stress intensity; Kelvin; correction factor.
K_app	— Apparent plane stress fracture toughness or residual strength.
K_c	— Critical plane stress fracture toughness, a measure of fracture toughness at point of crack growth instability.
K_f	— Fatigue notch factor, or fatigue strength reduction factor.
K_Ic	— Plane strain fracture toughness.
K_N	— Empirically calculated fatigue notch factor.
K_t	— Theoretical stress concentration factor.
lb	— Pound.
ln	— Natural (base e) logarithm.
log	— Base 10 logarithm.
L	— Length; subscript “lateral”; longitudinal (grain direction).
LT	— Long transverse (grain direction).
m	— Subscript “mean”; metre; slope.
mm	— Millimeter(s).
M	— Applied moment or couple, usually a bending moment.
Mc	— Machine countersunk.
Mg	— Megagram(s).
MIG	— Metal-inert-gas (welding).
MPa	— Megapascal(s).
MS	— Military Standard.
M.S.	— Margin of safety.
M(T)	— Middle tension.
n	— Number of individual measurements or pairs of measurements; subscript “normal”; cycles applied to failure; shape parameter for the standard stress-strain curve (Ramberg-Osgood parameter); number of fatigue cycles endured.
N	— Fatigue life, number of cycles to failure; Newton; normalized.
N_f	— Fatigue life, cycles to failure.
N_i*	— Fatigue life, cycles to initiation.
N_t*	— Transition fatigue life where plastic and elastic strains are equal.
NAS	— National Aerospace Standard.
p	— Subscript “polar”; subscript “proportional limit”.
psi	— Pounds per square inch.
P	— Load; applied load (total, not unit, load); exposure parameter; probability.
P_a	— Load amplitude.
P_m	— Mean load.
P_max	— Maximum load.
P_min	— Minimum load.
P_u	— Test ultimate load, pounds per fastener.
P_y	— Test yield load, pounds per fastener.
q	— Fatigue notch sensitivity.
Q	— Static moment of a cross section.
Q&T	— Quenched and tempered.

250. PDF page 1682

r	— Radius; root radius; reduced ratio (regression analysis); ratio of two pair measurements; rank of test point within a sample.
r̄	— average ratio of paired measurements.
R	— Load (stress) ratio, or residual (observed minus predicted value); stress ratio, ratio of minimum stress to maximum stress in a fatigue cycle; reduced ratio.
R_b	— Stress ratio in bending.
R_c	— Stress ratio in compression; Rockwell hardness - C scale.
R_ε	— Strain ratio, ε_min/ε_max.
R_s	— Stress ratio in shear or torsion; ratio of applied load to allowable shear load.
R_t	— Ratio of applied load to allowable tension load.
RA	— Reduction of area.
R.H.	— Relative humidity.
RMS	— Root-mean-square (surface finish).
RT	— Room temperature.
s	— Estimated population standard deviation; sample standard deviation; subscript “shear”.
s²	— Sample variance.
S	— Shear force; nominal engineering stress, fatigue; S-basis for mechanical-property values (see Section 1.4.1.1).
S_a	— Stress amplitude, fatigue.
S_e	— Fatigue limit.
S_eq*	— Equivalent stress.
S_f	— Fatigue limit.
S_m	— Mean stress, fatigue.
S_max	— Highest algebraic value of stress in the stress cycle.
S_min	— Lowest algebraic value of stress in the stress cycle.
S_r	— Algebraic difference between the maximum and minimum stresses in one cycle.
S_y	— Root mean square error.
SAE	— Society of Automotive Engineers.
SCC	— Stress-corrosion cracking.
SEE	— Estimate population standard error of estimate.
SR	— Studentized residual.
ST	— Short transverse (grain direction).
STA	— Solution treated and aged.
SUS	— Individual or typical shear ultimate strength.
SYS	— Individual or typical shear yield strength.
t	— Thickness; subscript “tension”; exposure time; elapsed time; tolerance factor for the “t” distribution with the specified probability and appropriate degrees of freedom.
T	— Transverse direction; applied torsional moment; transverse (grain direction); subscript “transverse”.
T_F	— Exposure temperature.
T₉₀	— Statistically based lower tolerance bound for a mechanical property such that at least 90 percent of the population is expected to exceed T₉₀ with 95 percent confidence.
T₉₉	— Statistically based lower tolerance bound for a mechanical property such that at least 99 percent of the population is expected to exceed T₉₉ with 95 percent confidence.
TIG	— Tungsten-inert-gas (welding).
TUS	— Individual or typical tensile ultimate strength.

251. PDF page 1683

α	— (1) Coefficient of thermal expansion, mean; constant. (2) Significance level; probability (risk of erroneously rejecting the null hypothesis (see Section 9.5.3)).
α99, α90	— Shape parameter estimates for a T99 or T90 value based on an assumed three-parameter Weibull distribution.
α50	— Shape parameter estimate for the Anderson-Darling goodness-of-fit test based on an assumed three-parameter Weibull distribution.
β	— Constant.
β99, β90	— Scale parameter estimate for a T99 or T90 value based on an assumed three-parameter Weibull distribution.
β50	— Scale parameter estimate for the Anderson-Darling goodness-of-fit test based on an assumed three-parameter Weibull distribution.
Δε or εr^*	— strain range, εmax - εmin.
Δεe	— Elastic strain range.
Δεp	— Plastic strain range.
ΔS (Sr^*)	— Stress range.
Δσ	— True or local stress range.
ε	— True or local strain.
εeq^*	— Equivalent strain.
εm	— Mean strain, (εmax + εmin)/2.
εmax	— Maximum strain.
εmin	— Minimum strain.
εt	— Total (elastic plus plastic) strain at failure determined from tensile stress-strain curve.
δ	— Deflection.
Φ	— Angular deflection.
ρ	— Radius of gyration; Neuber constant (block length).
µ	— Poisson’s ratio.
σ	— True or local stress; or population standard deviation.

252. PDF page 1695

Quantity or Property	To Convert From U. S. Unit	Multiply by^a	SI Unit^b
Area	in.²	645.16^c	Millimeter² (mm²)
Force	lb	4.4482	Newton (N)
Length	in.	25.4^c	Millimeter (mm)
Stress	ksi	6.895	Megapascal (MPa)^d
Stress intensity factor	ksi √in.	1.0989	Megapascal √meter (MPa · m ½)^d
Modulus	10³ ksi	6.895	Gigapascal (GPa)^d
Temperature	°F	F + 459.67 1.8	Kelvin (K)
Density (ω)	lb/in.³	27.680	Megagram/meter³ (Mg/m³)
Specific heat (C)	Btu/lb·F (or Btu·lb^-1·F^-1)	4.1868^c	Joule/(gram·Kelvin) (J/g·K) or (J·g^-1·K^-1)
Thermal conductivity (K)	Btu/[(hr)(ft²)(F)/ft] (or Btu·hr^-1·ft^-2·F^-1·ft)	1.7307	Watt/(meter·Kelvin) W/(m·K) or (W·m^-1·K^-1)
Thermal expansion (α)	in./in./F (or in.·in.^-1·F^-1)	1.8	Meter/meter/Kelvin m/(m·K) or (m·m^-1·K^-1)

253. PDF page 1695

b Prefix	Multiple	Prefix	Multiple
giga (G)	10⁹	milli (m)	10^-3
mega (M)	10⁶	micro (µ)	10^-6
kilo (k)	10³

254. PDF page 1698

Alloy Name	Form	Specification	Section
2424	Sheet (Clad)	AMS 4270	3.2.10
2424	Sheet (Bare)	AMS 4273	3.2.10
2519	Plate	MIL-DTL-46192	3.2.11
2524	Sheet and Plate	AMS 4296	3.2.12
2618	Die and Hand Forgings	AMS 4132	3.2.13
2618	Die Forging	AMS-A-22771	3.2.13
2618	Forging	AMS-QQ-A-367	3.2.13
4130	Bar and Forging	AMS 6348	2.3.1
4130	Sheet, Strip and Plate	AMS 6350	2.3.1
4130	Sheet, Strip and Plate	AMS 6351	2.3.1
4130	Tubing	AMS 6361	2.3.1
4130	Tubing	AMS 6362	2.3.1
4130	Bar and Forging	AMS 6370	2.3.1
4130	Tubing	AMS 6371	2.3.1
4130	Tubing	AMS 6373	2.3.1
4130	Tubing	AMS 6374	2.3.1
4130	Bar and Forging	AMS 6528	2.3.1
4130	Sheet, Strip and Plate	AMS-S-18729	2.3.1
4130	Bar and Forging	AMS-S-6758	2.3.1
4130	Tubing	AMS-T-6736	2.3.1
4135	Sheet, Strip and Plate	AMS 6352	2.3.1
4135	Tubing	AMS 6365	2.3.1
4135	Tubing	AMS 6372	2.3.1
4135	Tubing	AMS-T-6735	2.3.1
4140	Bar and Forging	AMS 6349	2.3.1
4140	Tubing	AMS 6381	2.3.1
4140	Bar and Forging	AMS 6382	2.3.1
4140	Sheet, Strip and Plate	AMS 6395	2.3.1
4140	Bar and Forging	AMS 6529	2.3.1
4140	Bar and Forging	AMS-S-5626	2.3.1
4340	Sheet, Strip and Plate	AMS 6359	2.3.1
4340	Bar and Forging	AMS 6414	2.3.1
4340	Tubing	AMS 6414	2.3.1
4340	Bar and Forging	AMS 6415	2.3.1
4340	Tubing	AMS 6415	2.3.1
4340	Sheet, Strip and Plate	AMS 6454	2.3.1
4340	Bar and Forging	AMS-S-5000	2.3.1
5052	Sheet and Plate	AMS 4015	3.5.1
5052	Sheet and Plate	AMS 4016	3.5.1
5052	Sheet and Plate	AMS 4017	3.5.1
5052	Sheet and Plate	AMS-QQ-A-250/8	3.5.1
5083	Bare Sheet and Plate	AMS 4056	3.5.2
5083	Extruded Bar, Rod and Shapes	AMS-QQ-A-200/4	3.5.2
5083	Bare Sheet and Plate	AMS-QQ-A-250/6	3.5.2
5086	Extruded Bar, Rod and Shapes	AMS-QQ-A-200/5	3.5.3
5086	Sheet and Plate	AMS-QQ-A-250/7	3.5.3
5454	Extruded Bar, Rod and Shapes	AMS-QQ-A-200/6	3.5.4
5454	Sheet and Plate	AMS-QQ-A-250/10	3.5.4
5456	Extruded Bar, Rod and Shapes	AMS-QQ-A-200/7	3.5.5
5456	Sheet and Plate	AMS-QQ-A-250/9	3.5.5
6013	Sheet (T4)	AMS 4347	3.6.1
6013	Sheet (T6)	AMS 4216	3.6.1
6061	Sheet and Plate	AMS 4025	3.6.2
6061	Sheet and Plate	AMS 4026	3.6.2

255. PDF page 1699

Alloy Name	Form	Specification	Section
6061	Sheet and Plate	AMS 4027	3.6.2
6061	Tubing Seamless, Drawn	AMS 4080	3.6.2
6061	Tubing Seamless, Drawn	AMS 4082	3.6.2
6061	Bar and Rod, Rolled or Cold Finished	AMS 4115	3.6.2
6061	Bar and Rod, Cold Finished	AMS 4116	3.6.2
6061	Bar and Rod, Rolled or Cold Finished	AMS 4117	3.6.2
6061	Forging	AMS 4127	3.6.2
6061	Extrusion	AMS 4160	3.6.2
6061	Extrusion	AMS 4161	3.6.2
6061	Extrusion	AMS 4172	3.6.2
6061	Hand Forging	AMS 4248	3.6.2
6061	Forging	AMS-A-22771	3.6.2
6061	Extruded Rod, Bar Shapes and Tubing	AMS-QQ-A-200/8	3.6.2
6061	Rolled Bar, Rod and Shapes	AMS-QQ-A-225/8	3.6.2
6061	Extruded Rod, Bars and Shapes	AMS 4150	3.6.2
6061	Extruded Rod, Bars and Shapes	AMS 4173	3.6.2
6061	Sheet and Plate	AMS-QQ-A-250/11	3.6.2
6061	Forging	AMS-QQ-A-367	3.6.2
6061	Tubing Seamless, Drawn	AMS-WW-T-700/6	3.6.2
6151	Die Forging	AMS 4125	3.6.3
6151	Forging	AMS-A-22771	3.6.3
7010	Plate	AMS 4204	3.7.1
7010	Plate	AMS 4205	3.7.1
7040	Plate	AMS 4211	3.7.2
7049	Forging	AMS-QQ-A-367	3.7.3
7049	Forging	AMS 4111	3.7.3
7049	Extrusion	AMS 4157	3.7.3
7049	Forging	AMS-A-22771	3.7.3
7049	Plate	AMS 4200	3.7.3
7050	Bare Plate	AMS 4050	3.7.4
7050	Die Forging	AMS 4107	3.7.4
7050	Hand Forging	AMS 4108	3.7.4
7050	Bare Plate	AMS 4201	3.7.4
7050	Die Forging	AMS 4333	3.7.4
7050	Extruded Shape	AMS 4340	3.7.4
7050	Extruded Shape	AMS 4341	3.7.4
7050	Extruded Shape	AMS 4342	3.7.4
7050	Forging	AMS-A-22771	3.7.4
7055	Plate	AMS 4206	3.7.5
7055	Extrusion	AMS 4337	3.7.5
7055	Extrusion	AMS 4324	3.7.5
7055	Extrusion	AMS 4336	3.7.5
7075	Bare Sheet and Plate	AMS 4044	3.7.6
7075	Bare Sheet and Plate	AMS 4045	3.7.6
7075	Clad Sheet and Plate	AMS 4049	3.7.6
7075	Bare Plate	AMS 4078	3.7.6
7075	Bar and Rod, Rolled or Cold Finished	AMS 4122	3.7.6
7075	Bar and Rod, Rolled or Cold Finished	AMS 4123	3.7.6
7075	Bar and Rod, Rolled or Cold Finished	AMS 4124	3.7.6
7075	Forging	AMS 4126	3.7.6
7075	Die Forging	AMS 4141	3.7.6
7075	Forging	AMS 4147	3.7.6
7075	Bar and Rod, Rolled or Cold Finished	AMS 4186	3.7.6
7075	Bar and Rod, Rolled or Cold Finished	AMS 4187	3.7.6

256. PDF page 1700

Alloy Name		Form	Specification	Section
7075		Forging	AMS-A-22771	3.7.6
7075		Extruded Bar, Rod and Shapes	AMS-QQ-A-200/11, 15	3.7.6
7075		Rolled or Drawn Bar and Rod	AMS-QQ-A-225/9	3.7.6
7075		Bare Sheet and Plate	AMS-QQ-A-250/12, 24	3.7.6
7075		Clad Sheet and Plate	AMS-QQ-A-250/13, 25	3.7.6
7075		Forging	AMS-QQ-A-367	3.7.6
7149		Forging	AMS 4320	3.7.3
7149		Forging	AMS-A-2271	3.7.3
7149		Extrusion	ASM 4343	3.7.3
7150		Bare Plate	AMS 4252 (T7751)	3.7.7
7150		Bare Plate	AMS 4306 (T6151)	3.7.7
7150		Extrusion	AMS 4307 (T61511)	3.7.7
7150		Extrusion	AMS 4345 (T77511)	3.7.7
7175		Die Forging	AMS 4148 (T66)	3.7.8
7175		Die and Hand Forging	AMS 4149 (T74)	3.7.8
7175		Hand Forging	AMS 4179 (T7452)	3.7.8
7175		Extrusion	AMS 4344 (T73511)	3.7.8
7175		Forging	AMS-A-22771	3.7.8
7249		Hand Forging	AMS 4334	3.7.9
7475		Bare Sheet	AMS 4084 (T61)	3.7.10
7475		Bare Sheet	AMS 4085 (T761)	3.7.10
7475		Bare Plate	AMS 4089 (T7651)	3.7.10
7475		Bare Plate	AMS 4090 (T651)	3.7.10
7475		Clad Sheet	AMS 4100 (T761)	3.7.10
7475		Bare Plate	AMS 4202 (T7351)	3.7.10
7475		Clad Sheet	AMS 4207 (T61)	3.7.10
8630		Bar and Forging	AMS 6280	2.3.1
8630		Tubing	AMS 6281	2.3.1
8630		Sheet, Strip and Plate	AMS-S-18728	2.3.1
8630		Bar and Forging	AMS-S-6050	2.3.1
8630		Sheet, Strip and Plate	AMS 6350	2.3.1
8735		Tubing	AMS 6282	2.3.1
8735		Bar and Forging	AMS 6320	2.3.1
8735		Sheet, Strip and Plate	AMS 6357	2.3.1
8740		Bar and Forging	AMS 6322	2.3.1
8740		Tubing	AMS 6323	2.3.1
8740		Bar and Forging	AMS 6327	2.3.1
8740		Sheet, Strip and Plate	AMS 6358	2.3.1
8740		Bar and Forging	AMS-S-6049	2.3.1
15-5PH		Investment Casting	AMS 5400	2.6.7
15-5PH		Bar, Forging, Ring and Extrusion (CEVM)	AMS 5659	2.6.7
15-5PH		Sheet, Strip and Plate (CEVM)	AMS 5862	2.6.7
17-4PH		Investment Casting (H1100)	AMS 5342	2.6.9
17-4PH		Investment Casting (H1000)	AMS 5343	2.6.9
17-4PH		Investment Casting (H900)	AMS 5344	2.6.9
17-4PH		Sheet, Strip and Plate	AMS 5604	2.6.9
17-4PH		Bar, Forging and Ring	AMS 5643	2.6.9
17-7PH		Plate, Sheet and Strip	AMS 5528	2.6.10
2024-T3	ARAMID Fiber Reinforced	Sheet Laminate	AMS 4254	7.5.1
280 (300)		Bar	AMS 6514	2.5.1
280 (300)		Sheet and Plate	AMS 6521	2.5.1
300M (0.42C)		Bar and Forging	AMS 6257	2.3.1
300M (0.42C)		Tubing	AMS 6257	2.3.1
300M (0.42C)		Bar and Forging	AMS 6419	2.3.1

257. PDF page 1701

Alloy Name	Form	Specification	Section
300M (0.42C)	Tubing	AMS 6419	2.3.1
300M (0.4C)	Bar and Forging	AMS 6417	2.3.1
300M (0.4C)	Tubing	AMS 6417	2.3.1
4130 - N	Tubing	AMS 6360	2.3.1
4330V	Bar and Forging	AMS 6411	2.3.1
4330V	Tubing	AMS 6411	2.3.1
4330V	Bar and Forging	AMS 6427	2.3.1
4330V	Tubing	AMS 6427	2.3.1
4335V	Bar and Forging	AMS 6429	2.3.1
4335V	Tubing	AMS 6429	2.3.1
4335V	Bar and Forging	AMS 6430	2.3.1
4335V	Tubing	AMS 6430	2.3.1
4335V	Sheet, Strip and Plate	AMS 6433	2.3.1
4335V	Sheet, Strip and Plate	AMS 6435	2.3.1
5Cr-Mo-V	Sheet, Strip and Plate	AMS 6437	2.4.1
5Cr-Mo-V	Bar and Forging (CEVM)	AMS 6487	2.4.1
5Cr-Mo-V	Bar and Forging	AMS 6488	2.4.1
7475-T761 ARAMID Fiber Reinforced	Sheet Laminate	AMS 4302	7.5.2
9Ni-4Co-0.20C	Sheet, Strip and Plate	AMS 6523	2.4.2
9Ni-4Co-0.20C	Sheet, Strip and Plate	AMS 6524	2.4.3
9Ni-4Co-0.20C	Bar and Forging, Tubing	AMS 6526	2.4.3
A201.0	Casting (T7 Temper)	AMS-A-21180	3.8.1
A-286	Sheet, Strip and Plate	AMS 5525	6.2.1
A-286	Bar, Forging, Tubing and Ring	AMS 5731	6.2.1
A-286	Bar, Forging, Tubing and Ring	AMS 5732	6.2.1
A-286	Bar, Forging and Tubing	AMS 5734	6.2.1
A-286	Bar, Forging and Tubing	AMS 5737	6.2.1
A356.0	Casting	AMS 4218	3.9.5
A356.0	Casting	AMS-A-21180	3.9.5
A357.0	Casting	AMS-A-21180	3.9.6
AerMet 100	Bar and Forging	AMS 6478	2.5.3
AerMet 100	Bar and Forging	AMS 6532	2.5.3
AF1410	Bar and Forging	AMS 6527	2.5.2
AISI 1025	Sheet, Strip, and Plate	AMS 5046	2.2.1
AISI 1025	Bar	ASTM A 108	2.2.1
AISI 1025	Sheet and Strip	AMS-S-7952	2.2.1
AISI 1025	Tubing	AMS 5077	2.2.1
AISI 1025 - N	Seamless Tubing	AMS 5075	2.2.1
AISI 1025 - N	Tubing	AMS 5077	2.2.1
AISI 1025 - N	Tubing	AMS-T-5066	2.2.1
AISI 301	Sheet and Strip	AMS 5517	2.7.1
AISI 301	Sheet and Strip	AMS 5518	2.7.1
AISI 301	Sheet and Strip	AMS 5519	2.7.1
AISI 301	Sheet, Strip and Plate	AMS 5901	2.7.1
AISI 301	Sheet and Strip (175 ksi)	AMS 5902	2.7.1
AISI 302	Sheet, Strip and Plate	AMS 5516	2.7.1
AISI 302	Sheet and Strip (125 ksi)	AMS 5903	2.7.1
AISI 302	Sheet and Strip (150 ksi)	AMS 5904	2.7.1
AISI 302	Sheet and Strip (175 ksi)	AMS 5905	2.7.1
AISI 302	Sheet and Strip (185 ksi)	AMS 5906	2.7.1
AISI 304	Sheet and Strip	AMS 5913	2.7.1
AISI 304	Sheet, Strip and Plate (125 ksi)	AMS 5910	2.7.1
AISI 304	Sheet and Strip (150 ksi)	AMS 5911	2.7.1
AISI 304	Sheet and Strip (175 ksi)	AMS 5912	2.7.1

258. PDF page 1702

Alloy Name	Form	Specification	Section
AISI 304	Sheet and Strip (185 ksi)	AMS 5913	2.7.1
AISI 316	Sheet and Strip	AMS 5524	2.7.1
AISI 316	Sheet, Strip and Plate (125 ksi)	AMS 5907	2.7.1
AM100A	Investment Casting	AMS 4455	4.3.1
AM100A	Permanent Mold Casting	AMS 4483	4.3.1
AM-350	Sheet and Strip	AMS 5548	2.6.1
AM-355	Sheet and Strip	AMS 5547	2.6.2
AM-355	Plate	AMS 5549	2.6.2
AM-355	Bar, Forging and Forging Stock	AMS 5743	2.6.2
AZ31B	Sheet and Plate	AMS 4375	4.2.1
AZ31B	Plate	AMS 4376	4.2.1
AZ31B	Sheet and Plate	AMS 4377	4.2.1
AZ31B	Forging	ASTM B 91	4.2.1
AZ31B	Extrusion	ASTM B 107	4.2.1
AZ61A	Extrusion	AMS 4350	4.2.2
AZ61A	Forging	ASTM B 91	4.2.2
AZ91C/AZ91E	Sand Casting	AMS 4437	4.3.2
AZ91C/AZ91E	Sand Casting	AMS 4446	4.3.2
AZ91C/AZ91E	Investment Casting	AMS 4452	4.3.2
AZ92A	Sand Casting	AMS 4434	4.3.3
AZ92A	Permanent Mold Casting	AMS 4484	4.3.3
AZ92A	Investment Casting	AMS 4453	4.3.3
C355.0	Casting	AMS-A-21180	3.9.3
Copper Beryllium	Strip (TB00)	AMS 4530	7.3.2
Copper Beryllium	Strip (TD02)	AMS 4532	7.3.2
Copper Beryllium	Bar and Rod (TF00)	AMS 4533	7.3.2
Copper Beryllium	Bar and Rod (TH04)	AMS 4534	7.3.2
Copper Beryllium	Mechanical tubing (TF00)	AMS 4535	7.3.2
Copper Beryllium	Bar, Rod, Shapes and Forging (TB00)	AMS 4650	7.3.2
Copper Beryllium	Bar and Rod (TD04)	AMS 4651	7.3.2
Copper Beryllium	Sheet (TB00, TD01, TD02, TD04)	ASTM B 194	7.3.2
CP Titanium	Sheet, Strip and Plate	AMS 4900	5.2.1
CP Titanium	Sheet, Strip and Plate	AMS 4901	5.2.1
CP Titanium	Sheet, Strip and Plate	AMS 4902	5.2.1
CP Titanium	Bar	AMS 4921	5.2.1
CP Titanium	Extruded Bars and Shapes	AMS-T-81556	5.2.1
CP Titanium	Sheet, Strip and Plate	AMS-T-9046	5.2.1
CP Titanium	Bar	MIL-T-9047	5.2.1
Custom 450	Bar, Forging, Tubing, Wire and Ring (air melted)	AMS 5763	2.6.3
Custom 450	Bar, Forging, Tubing, Wire and Ring (CEM)	AMS 5773	2.6.3
Custom 455	Tubing (welded)	AMS 5578	2.6.4
Custom 455	Bar and Forging	AMS 5617	2.6.4
Custom 465	Bars, Wires, and Forgings	AMS 5936	2.6.5
D357.0	Sand Composite Casting	AMS 4241	3.9.7
D6AC	Bar and Forging	AMS 6431	2.3.1
D6AC	Tubing	AMS 6431	2.3.1
D6AC	Bar and Forging	AMS 6439	2.3.1
D6AC	Sheet, Strip and Plate	AMS 6439	2.3.1
EZ33A	Sand Casting	AMS 4442	4.3.4
Hastelloy X	Sheet and Plate	AMS 5536	6.3.1
Hastelloy X	Bar and Forging	AMS 5754	6.3.1
Haynes®230®	Plate, Sheet, and Strip	AMS 5878	6.3.9
Haynes®230®	Bar and Forging	AMS 5891	6.3.9
Haynes HR 120	Sheet, Strip and Plate	AMS 5916	6.3.10

259. PDF page 1703

Alloy Name	Form	Specification	Section
HS 188	Sheet and Plate	AMS 5608	6.4.2
HS 188	Bar and Forging	AMS 5772	6.4.2
Hy-Tuf	Bar and Forging	AMS 6425	2.3.1
Hy-Tuf	Tubing	AMS 6425	2.3.1
Inconel 718	Investment Casting	AMS 5383	6.3.5
Inconel 718	Tubing; Creep Rupture	AMS 5589	6.3.5
Inconel 718	Tubing; Short-Time	AMS 5590	6.3.5
Inconel 718	Sheet, Strip and Plate; Creep Rupture	AMS 5596	6.3.5
Inconel 718	Sheet, Strip and Plate; Short-Time	AMS 5597	6.3.5
Inconel 718	Bar and Forging; Creep Rupture	AMS 5662	6.3.5
Inconel 718	Bar and Forging; Creep Rupture	AMS 5663	6.3.5
Inconel 718	Bar and Forging; Short-Time	AMS 5664	6.3.5
Inconel Alloy 600	Plate, Sheet and Strip	AMS 5540	6.3.2
Inconel Alloy 600	Tubing, Seamless	AMS 5580	6.3.2
Inconel Alloy 600	Bar and Rod	ASTM B 166	6.3.2
Inconel Alloy 600	Forging	ASTM B 564	6.3.2
Inconel Alloy 625	Sheet, Strip and Plate	AMS 5599	6.3.3
Inconel Alloy 625	Bar, Forging and Ring	AMS 5666	6.3.3
Inconel Alloy 706	Sheet, Strip and Plate	AMS 5605	6.3.4
Inconel Alloy 706	Sheet, Strip and Plate	AMS 5606	6.3.4
Inconel Alloy 706	Bar, Forging and Ring	AMS 5701	6.3.4
Inconel Alloy 706	Bar, Forging and Ring	AMS 5702	6.3.4
Inconel Alloy 706	Bar, Forging and Ring	AMS 5703	6.3.4
Inconel Alloy X-750	Sheet, Strip and Plate; Annealed	AMS 5542	6.3.6
Inconel Alloy X-750	Bar and Forging; Equalized	AMS 5667	6.3.6
L-605	Sheet	AMS 5537	6.4.1
L-605	Bar and Forging	AMS 5759	6.4.1
Manganese Bronzes	Casting	AMS 4860	7.3.1
Manganese Bronzes	Casting	AMS 4862	7.3.1
MP159 Alloy	Bar (solution treated and cold drawn)	AMS 5842	7.4.2
MP159 Alloy	Bar (solution treated, cold drawn and aged)	AMS 5843	7.4.2
MP35N Alloy	Bar (solution treated and cold drawn)	AMS 5844	7.4.1
MP35N Alloy	Bar (solution treated, cold drawn and aged)	AMS 5845	7.4.1
N-155	Sheet	AMS 5532	6.2.2
N-155	Tubing (welded)	AMS 5585	6.2.2
N-155	Bar and Forging	AMS 5768	6.2.2
N-155	Bar and Forging	AMS 5769	6.2.2
PH13-8Mo	Bar, Forging Ring and Extrusion (VIM+CEVM)	AMS 5629	2.6.5
PH15-7Mo	Plate, Sheet and Strip	AMS 5520	2.6.7
QE22A Magnesium	Sand Casting	AMS 4418	4.3.5
René 41	Plate, Sheet and Strip	AMS 5545	6.3.7
René 41	Bar and Forging	AMS 5713	6.3.7
René 41 - STA	Bar and Forging	AMS 5712	6.3.7
Standard Grade Beryllium	Sheet and Plate	AMS 7902	7.2.1
Standard Grade Beryllium	Bar, Rod, Tubing and Machined Shapes	AMS 7906	7.2.1
Ti-10V-2Fe-3Al (Ti-10-2-3)	Forging	AMS 4983	5.5.3
Ti-10V-2Fe-3Al (Ti-10-2-3)	Forging	AMS 4984	5.5.3
Ti-10V-2Fe-3Al (Ti-10-2-3)	Forging	AMS 4986	5.5.3
Ti-13V-11Cr-3Al	Sheet, Strip and Plate	AMS-T-9046	5.5.1
Ti-13V-11Cr-3Al	Bar	MIL-T-9047	5.5.1
Ti-15V-3Cr-3Sn-3Al (Ti-15-3-3-3)	Sheet and Strip	AMS 4914	5.5.2
Ti-4.5Al-3V-2Fe-2Mo	Sheet	AMS 4899	5.4.3
Ti-4.5Al-3V-2Fe-2Mo	Bars, Wires, forgings and Rings	AMS 4964	5.4.3
Ti-5Al-2.5Sn	Sheet, Strip and Plate	AMS 4910	5.3.1

260. PDF page 1704

Alloy Name	Form	Specification	Section
Ti-5Al-2.5Sn	Bar	AMS 4926	5.3.1
Ti-5Al-2.5Sn	Forging	AMS 4966	5.3.1
Ti-5Al-2.5Sn	Extruded Bar and Shapes	AMS-T-81556	5.3.1
Ti-5Al-2.5Sn	Sheet, Strip and Plate	AMS-T-9046	5.3.1
Ti-5Al-2.5Sn	Bar	MIL-T-9047	5.3.1
Ti-6Al-2Sn-4Zr-2Mo	Sheet, Strip and Plate	AMS 4919	5.3.3
Ti-6Al-2Sn-4Zr-2Mo	Bar	AMS 4975	5.3.3
Ti-6Al-2Sn-4Zr-2Mo	Forging	AMS 4976	5.3.3
Ti-6Al-2Sn-4Zr-2Mo	Sheet and Strip	AMS-T-9046	5.3.3
Ti-6Al-4V	Sheet, Strip and Plate	AMS 4911	5.4.1
Ti-6Al-4V	Die Forging	AMS 4920	5.4.1
Ti-6Al-4V	Bar and Die Forging	AMS 4928	5.4.1
Ti-6Al-4V	Extrusion	AMS 4934	5.4.1
Ti-6Al-4V	Extrusion	AMS 4935	5.4.1
Ti-6Al-4V	Casting	AMS 4962	5.4.1
Ti-6Al-4V	Bar	AMS 4967	5.4.1
Ti-6Al-4V	Sheet, Strip and Plate	AMS-T-9046	5.4.1
Ti-6Al-4V	Bar	AMS 4965	5.4.1
Ti-6Al-4V	Bar	MIL-T-9047	5.4.1
Ti6Al-6V-2Sn	Sheet, Strip and Plate	AMS 4918	5.4.2
Ti6Al-6V-2Sn	Bar and Forging	AMS 4971	5.4.2
Ti6Al-6V-2Sn	Bar and Forging	AMS 4978	5.4.2
Ti6Al-6V-2Sn	Bar and Forging	AMS 4979	5.4.2
Ti6Al-6V-2Sn	Extruded Bar and Shapes	AMS-T-81556	5.4.2
Ti6Al-6V-2Sn	Sheet, Strip and Plate	AMS-T-9046	5.4.2
Ti-8Al-1Mo-1V	Sheet, Strip and Plate	AMS 4915	5.3.2
Ti-8Al-1Mo-1V	Sheet, Strip and Plate	AMS 4916	5.3.2
Ti-8Al-1Mo-1V	Forging	AMS 4973	5.3.2
Ti-8Al-1Mo-1V	Sheet, Strip and Plate	AMS-T-9046	5.3.2
Ti-8Al-1Mo-1V	Bar	MIL-T-9047	5.3.2
Waspaloy	Plate, Sheet and Strip	AMS 5544	6.3.8
Waspaloy	Forging	AMS 5704	6.3.8
Waspaloy	Bar, Forgings and Ring	AMS 5706	6.3.8
Waspaloy	Bar, Forgings and Ring	AMS 5707	6.3.8
Waspaloy	Bar, Forgings and Ring	AMS 5708	6.3.8
Waspaloy	Bar, Forgings and Ring	AMS 5709	6.3.8
ZE41A Magnesium	Sand Casting	AMS 4439	4.3.6
ZK60A-F	Extrusion	ASTM B 107	4.2.3
ZK60A-T5	Extrusion	AMS 4352	4.2.3
ZK60A-T5	Die and Hand Forging	AMS 4362	4.2.3

261. PDF page 1706

Specification	Alloy Name	Form/Application	Section
AMS 4144	2219	Hand Forging	3.2.8
AMS 4147	7075	Forging	3.7.6
AMS 4148 (T66)	7175	Die Forging	3.7.8
AMS 4149 (T74)	7175	Die and Hand Forging	3.7.8
AMS 4150	6061	Extruded Rod, Bars, and Shapes	3.6.2
AMS 4152	2024	Extrusion	3.2.3
AMS 4153	2014	Extrusion	3.2.1
AMS 4157	7049	Extrusion	3.7.3
AMS 4160	6061	Extrusion	3.6.2
AMS 4161	6061	Extrusion	3.6.2
AMS 4162	2219	Extrusion	3.2.8
AMS 4163	2219	Extrusion	3.2.8
AMS 4164	2024	Extrusion	3.2.3
AMS 4165	2024	Extrusion	3.2.3
AMS 4172	6061	Extrusion	3.6.2
AMS 4173	6061	Extruded Rod, Bars, and Shapes	3.6.2
AMS 4179 (T7452)	7175	Hand Forging	3.7.8
AMS 4186	7075	Bar and Rod, Rolled or Cold Finished	3.7.6
AMS 4187	7075	Bar and Rod, Rolled or Cold Finished	3.7.6
AMS 4200	7049	Plate	3.7.3
AMS 4201	7050	Bare Plate	3.7.4
AMS 4202 (T7351)	7475	Bare Plate	3.7.10
AMS 4204	7010	Plate	3.7.1
AMS 4205	7010	Plate	3.7.1
AMS 4206	7055	Plate	3.7.5
AMS 4207 (T61)	7475	Clad Sheet	3.7.10
AMS 4211	7040	Plate	3.7.2
AMS 4216	6013 (T4)	Sheet	3.6.1
AMS 4217	356.0	Sand Casting	3.9.4
AMS 4218	A356.0	Casting	3.9.5
AMS 4241	D357.0	Sand Composite Casting	3.9.7
AMS 4248	6061	Hand Forging	3.6.2
AMS 4251	2090	Sheet	3.2.6
AMS 4252 (T7751)	7150	Bare Plate	3.7.7
AMS 4254	2024-T3 ARAMID Fiber Reinforced	Sheet Laminate	7.5.1
AMS 4260	356.0	Investment Casting	3.9.4
AMS 4270	2424 (Clad)	Sheet	3.2.10
AMS 4273	2424 (Bare)	Sheet	3.2.10
AMS 4281	355.0	Permanent Mold Casting	3.9.2
AMS 4284	356.0	Permanent Mold Casting	3.9.4
AMS 4296	2524-T3	Sheet and Plate	3.2.12
AMS 4302	7475-T761 ARAMID Fiber Reinforced	Sheet Laminate	7.5.2
AMS 4306 (T6151)	7150	Bare Plate	3.7.7
AMS 4307 (T61511)	7150	Extrusion	3.7.7
AMS 4320	7149	Forging	3.7.3
AMS 4324	7055	Extrusion	3.7.5
AMS 4330	2297	Plate	3.2.9
AMS 4333	7050	Die Forging	3.7.4
AMS 4334	7249	Hand Forging	3.7.9
AMS 4336	7055	Extrusion	3.7.5
AMS 4337	7055	Extrusion	3.7.5
AMS 4338	2026	Bars, Rods, and Profiles	3.2.5
AMS 4340	7050	Extruded Shape	3.7.4
AMS 4341	7050	Extruded Shape	3.7.4
AMS 4342	7050	Extruded Shape	3.7.4

262. PDF page 1707

Specification	Alloy Name	Form/Application	Section
AMS 4343	7149	Extrusion	3.7.3
AMS 4344 (T73511)	7175	Extrusion	3.7.8
AMS 4345 (T77511)	7150	Extrusion	3.7.7
AMS 4347	6013 (T6)	Sheet	3.6.1
AMS 4350	AZ61A	Extrusion	4.2.2
AMS 4352	ZK60A-T5	Extrusion	4.2.3
AMS 4362	ZK60A-T5	Die and Hand Forging	4.2.3
AMS 4375	AZ31B	Sheet and Plate	4.2.1
AMS 4376	AZ31B	Plate	4.2.1
AMS 4377	AZ31B	Sheet and Plate	4.2.1
AMS 4418	QE22A Magnesium	Sand Casting	4.3.5
AMS 4434	AZ92A	Sand Casting	4.3.3
AMS 4437	AZ91C/AZ91E	Sand Casting	4.3.2
AMS 4439	ZE41A Magnesium	Sand Casting	4.3.6
AMS 4442	EZ33A	Sand Casting	4.3.4
AMS 4446	AZ91C/AZ91E	Sand Casting	4.3.2
AMS 4452	AZ91C/AZ91E	Investment Casting	4.3.2
AMS 4453	AZ92A	Investment Casting	4.3.3
AMS 4455	AM100A	Investment Casting	4.3.1
AMS 4483	AM100A	Permanent Mold Casting	4.3.1
AMS 4484	AZ92A	Permanent Mold Casting	4.3.3
AMS 4530	Copper Beryllium	Strip (TB00)	7.3.2
AMS 4532	Copper Beryllium	Strip (TD02)	7.3.2
AMS 4533	Copper Beryllium	Bar and Rod (TF00)	7.3.2
AMS 4534	Copper Beryllium	Bar and Rod (TH04)	7.3.2
AMS 4535	Copper Beryllium	Mechanical tubing (TF00)	7.3.2
AMS 4650	Copper Beryllium	Bar, Rod, Shapes and Forging (TB00)	7.3.2
AMS 4651	Copper Beryllium	Bar and Rod (TD04)	7.3.2
AMS 4860	Manganese Bronzes	Casting	7.3.1
AMS 4862	Manganese Bronzes	Casting	7.3.1
AMS 4899	Ti-4.5Al-3V-2Fe-2Mo	Sheet	5.4.3
AMS 4900	CP Titanium	Sheet, Strip and Plate	5.2.1
AMS 4901	CP Titanium	Sheet, Strip and Plate	5.2.1
AMS 4902	CP Titanium	Sheet, Strip and Plate	5.2.1
AMS 4910	Ti-5Al-2.5Sn	Sheet, Strip and Plate	5.3.1
AMS 4911	Ti-6Al-4V	Sheet, Strip and Plate	5.4.1
AMS 4914	Ti-15V-3Cr-3Sn-3Al (Ti-15-3)-3-3	Sheet and Strip	5.5.2
AMS 4915	Ti-8Al-1Mo-1V	Sheet, Strip and Plate	5.3.2
AMS 4916	Ti-8Al-1Mo-1V	Sheet, Strip and Plate	5.3.2
AMS 4918	Ti6Al-6V-2Sn	Sheet, Strip and Plate	5.4.2
AMS 4919	Ti-6Al-2Sn-4Zr-2Mo	Sheet, Strip and Plate	5.3.3
AMS 4920	Ti-6Al-4V	Die Forging	5.4.1
AMS 4921	CP Titanium	Bar	5.2.1
AMS 4926	Ti-5Al-2.5Sn	Bar	5.3.1
AMS 4928	Ti-6Al-4V	Bar and Die Forging	5.4.1
AMS 4934	Ti-6Al-4V	Extrusion	5.4.1
AMS 4935	Ti-6Al-4V	Extrusion	5.4.1
AMS 4962	Ti-6Al-4V	Casting	5.4.1
AMS 4964	Ti-4.5Al-3V-2Fe-2Mo	Bars, Wires, Forgings and Rings	5.4.3
AMS 4965	Tii-6Al-4V	Bar	5.4.1
AMS 4966	Ti-5Al-2.5Sn	Forging	5.3.1
AMS 4967	Ti-6Al-4V	Bar	5.4.1
AMS 4971	Ti6Al-6V-2Sn	Bar and Forging	5.4.2
AMS 4973	Ti-8Al-1Mo-1V	Forging	5.3.2
AMS 4975	Ti-6Al-2Sn-4Zr-2Mo	Bar	5.3.3
AMS 4976	Ti-6Al-2Sn-4Zr-2Mo	Forging	5.3.3

263. PDF page 1708

Specification	Alloy Name	Form/Application	Section
AMS 4978	Ti6Al-6V-2Sn	Bar and Forging	5.4.2
AMS 4979	Ti6Al-6V-2Sn	Bar and Forging	5.4.2
AMS 4983	Ti-10V-2Fe-3Al (Ti-10-2-3)	Forging	5.5.3
AMS 4984	Ti-10V-2Fe-3Al (Ti-10-2-3)	Forging	5.5.3
AMS 4986	Ti-10V-2Fe-3Al (Ti-10-2-3)	Forging	5.5.3
AMS 5046	AISI 1025	Sheet, Strip, and Plate	2.2.1
AMS 5075	AISI 1025 - N	Seamless Tubing	2.2.1
AMS 5077	AISI 1025 - N	Tubing	2.2.1
AMS 5342	17-4PH	Investment Casting (H1100)	2.6.9
AMS 5343	17-4PH	Investment Casting (H1000)	2.6.9
AMS 5344	17-4PH	Investment Casting (H900)	2.6.9
AMS 5383	Inconel 718	Investment Casting	6.3.5
AMS 5400	15-5PH	Investment Casting	2.6.7
AMS 5513	AISI 301	Sheet, Strip and Plate	2.7.1
AMS 5516	AISI 302	Sheet, Strip and Plate	2.7.1
AMS 5517	AISI 301	Sheet and Strip (125 ksi)	2.7.1
AMS 5518	AISI 301	Sheet and Strip (150 ksi)	2.7.1
AMS 5519	AISI 301	Sheet and Strip (185 ksi)	2.7.1
AMS 5520	PH15-7Mo	Plate, Sheet and Strip	2.6.8
AMS 5524	AISI 316	Sheet, Strip and Plate	2.7.1
AMS 5525	A-286	Sheet, Strip and Plate	6.2.1
AMS 5528	17-7PH	Plate, Sheet and Strip	2.6.10
AMS 5532	N-155	Sheet	6.2.2
AMS 5536	Hastelloy X	Sheet and Plate	6.3.1
AMS 5537	L-605	Sheet	6.4.1
AMS 5540	Inconel Alloy 600	Plate, Sheet and Strip	6.3.2
AMS 5542	Inconel Alloy X-750	Sheet, Strip and Plate; Annealed	6.3.6
AMS 5544	Waspaloy	Plate, Sheet and Strip	6.3.8
AMS 5545	René 41	Plate, Sheet and Strip	6.3.7
AMS 5547	AM-355	Sheet and Strip	2.6.2
AMS 5548	AM-350	Sheet and Strip	2.6.1
AMS 5549	AM-355	Plate	2.6.2
AMS 5578	Custom 455	Tubing (welded)	2.6.4
AMS 5580	Inconel Alloy 600	Tubing, Seamless	6.3.2
AMS 5585	N-155	Tubing (welded)	6.2.2
AMS 5589	Inconel 718	Tubing; Creep Rupture	6.3.5
AMS 5590	Inconel 718	Tubing; Short-Time	6.3.5
AMS 5596	Inconel 718	Sheet, Strip and Plate; Creep Rupture	6.3.5
AMS 5597	Inconel 718	Sheet, Strip and Plate; Short-Time	6.3.5
AMS 5599	Inconel Alloy 625	Sheet, Strip and Plate	6.3.3
AMS 5604	17-4PH	Sheet, Strip and Plate	2.6.9
AMS 5605	Inconel Alloy 706	Sheet, Strip and Plate	6.3.4
AMS 5606	Inconel Alloy 706	Sheet, Strip and Plate	6.3.4
AMS 5608	HS 188	Sheet and Plate	6.4.2
AMS 5617	Custom 455	Bar and Forging	2.6.4
AMS 5629	PH13-8Mo	Bar, Forging Ring and Extrusion (VIM+CEVM)	2.6.6
AMS 5643	17-4PH	Bar, Forging and Ring	2.6.9
AMS 5659	15-5PH	Bar, Forging, Ring and Extrusion (CEVM)	2.6.7
AMS 5662	Inconel 718	Bar and Forging; Creep Rupture	6.3.5
AMS 5663	Inconel 718	Bar and Forging; Creep Rupture	6.3.5
AMS 5664	Inconel 718	Bar and Forging; Short-Time	6.3.5
AMS 5666	Inconel Alloy 625	Bar, Forging and Ring	6.3.3
AMS 5667	Inconel Alloy X-750	Bar and Forging; Equalized	6.3.6
AMS 5701	Inconel Alloy 706	Bar, Forging and Ring	6.3.4
AMS 5702	Inconel Alloy 706	Bar, Forging and Ring	6.3.4
AMS 5703	Inconel Alloy 706	Bar, Forging and Ring	6.3.4

264. PDF page 1709

Specification	Alloy Name	Form/Application	Section
AMS 5704	Waspaloy	Forging	6.3.8
AMS 5706	Waspaloy	Bar, Forgings and Ring	6.3.8
AMS 5707	Waspaloy	Bar, Forgings and Ring	6.3.8
AMS 5708	Waspaloy	Bar, Forgings and Ring	6.3.8
AMS 5709	Waspaloy	Bar, Forgings and Ring	6.3.8
AMS 5712	René 41 - STA	Bar and Forging	6.3.7
AMS 5713	René 41	Bar and Forging	6.3.7
AMS 5731	A-286	Bar, Forging, Tubing and Ring	6.2.1
AMS 5732	A-286	Bar, Forging, Tubing and Ring	6.2.1
AMS 5734	A-286	Bar, Forging and Tubing	6.2.1
AMS 5737	A-286	Bar, Forging and Tubing	6.2.1
AMS 5743	AM-355	Bar, Forging and Forging Stock	2.6.2
AMS 5754	Hastelloy X	Bar and Forging	6.3.1
AMS 5759	L-605	Bar and Forging	6.4.1
AMS 5763	Custom 450	Bar, Forging, Tubing, Wire and Ring (air melted)	2.6.3
AMS 5768	N-155	Bar and Forging	6.2.2
AMS 5769	N-155	Bar and Forging	6.2.2
AMS 5772	HS 188	Bar and Forging	6.4.2
AMS 5773	Custom 450	Bar, Forging, Tubing, Wire and Ring (CEM)	2.6.3
AMS 5842	MP159 Alloy	Bar (solution treated and cold drawn)	7.4.2
AMS 5843	MP159 Alloy	Bar (solution treated, cold drawn and aged)	7.4.2
AMS 5844	MP35N Alloy	Bar (solution treated and cold drawn)	7.4.1
AMS 5845	MP35N Alloy	Bar (solution treated, cold drawn and aged)	7.4.1
AMS 5862	15-5PH	Sheet, Strip and Plate (CEVM)	2.6.7
AMS 5878	Haynes®230®	Plate, Sheet and Strip	6.3.9
AMS 5891	Haynes®230®	Bar and Forging	6.3.9
AMS 5901	AISI 301	Plate, Sheet and Strip	2.7.1
AMS 5902	AISI 301	Sheet and Strip (175 ksi)	2.7.1
AMS 5903	AISI 302	Sheet and Strip (125 ksi)	2.7.1
AMS 5904	AISI 302	Sheet and Strip (150 ksi)	2.7.1
AMS 5905	AISI 302	Sheet and Strip (175 ksi)	2.7.1
AMS 5906	AISI 302	Sheet and Strip (185 ksi)	2.7.1
AMS 5907	AISI 316	Sheet, Strip and Plate (125 ksi)	2.7.1
AMS 5910	AISI 304	Sheet, Strip and Plate (125 ksi)	2.7.1
AMS 5911	AISI 304	Sheet and Strip (150 ksi)	2.7.1
AMS 5912	AISI 304	Sheet and Strip (175 ksi)	2.7.1
AMS 5913	AISI 304	Sheet and Strip (185 ksi)	2.7.1
AMS 5916	Haynes HR-120	Sheet, Strip and Plate	6.3.10
AMS 5936	Custom 465	Bar, Wires and Forgings	2.6.5
AMS 6257	300M (0.42C)	Bar and Forging	2.3.1
AMS 6257	300M (0.42C)	Tubing	2.3.1
AMS 6280	8630	Bar and Forging	2.3.1
AMS 6281	8630	Tubing	2.3.1
AMS 6282	8735	Tubing	2.3.1
AMS 6320	8735	Bar and Forging	2.3.1
AMS 6322	8740	Bar and Forging	2.3.1
AMS 6323	8740	Tubing	2.3.1
AMS 6327	8740	Bar and Forging	2.3.1
AMS 6348	4130	Bar and Forging	2.3.1
AMS 6349	4140	Bar and Forging	2.3.1
AMS 6350	4130	Sheet, Strip and Plate	2.3.1
AMS 6350	8630	Sheet, Strip and Plate	2.3.1
AMS 6351	4130	Sheet, Strip and Plate	2.3.1
AMS 6352	4135	Sheet, Strip and Plate	2.3.1
AMS 6355	8630	Tubing	2.3.1
AMS 6357	8735	Sheet, Strip and Plate	2.3.1

265. PDF page 1710

Specification	Alloy Name	Form/Application	Section
AMS 6358	8740	Sheet, Strip and Plate	2.3.1
AMS 6359	4340	Sheet, Strip and Plate	2.3.1
AMS 6360	4130	Tubing (normalized)	2.3.1
AMS 6361	4130	Tubing	2.3.1
AMS 6362	4130	Tubing	2.3.1
AMS 6365	4135	Tubing	2.3.1
AMS 6370	4130	Bar and Forging	2.3.1
AMS 6371	4130	Tubing	2.3.1
AMS 6372	4135	Tubing	2.3.1
AMS 6373	4130	Tubing	2.3.1
AMS 6374	4130	Tubing	2.3.1
AMS 6381	4140	Tubing	2.3.1
AMS 6382	4140	Bar and Forging	2.3.1
AMS 6395	4140	Sheet, Strip and Plate	2.3.1
AMS 6411	4330V	Bar and Forging	2.3.1
AMS 6411	4330V	Tubing	2.3.1
AMS 6414	4340	Bar and Forging	2.3.1
AMS 6414	4340	Tubing	2.3.1
AMS 6415	4340	Bar and Forging	2.3.1
AMS 6415	4340	Tubing	2.3.1
AMS 6417	300M (0.4C)	Bar and Forging	2.3.1
AMS 6417	300M (0.4C)	Tubing	2.3.1
AMS 6419	300M (0.42C)	Bar and Forging	2.3.1
AMS 6419	300M (0.42C)	Tubing	2.3.1
AMS 6425	Hy-Tuf	Bar and Forging	2.3.1
AMS 6425	Hy-Tuf	Tubing	2.3.1
AMS 6427	4330V	Bar and Forging	2.3.1
AMS 6427	4330V	Tubing	2.3.1
AMS 6429	4335V	Bar and Forging	2.3.1
AMS 6429	4335V	Tubing	2.3.1
AMS 6430	4335V	Bar and Forging	2.3.1
AMS 6430	4335V	Tubing	2.3.1
AMS 6431	D6AC	Bar and Forging	2.3.1
AMS 6431	D6AC	Tubing	2.3.1
AMS 6433	4335V	Sheet, Strip and Plate	2.3.1
AMS 6435	4335V	Sheet, Strip and Plate	2.3.1
AMS 6437	5Cr-Mo-V	Sheet, Strip and Plate	2.4.1
AMS 6439	D6AC	Sheet, Strip and Plate	2.3.1
AMS 6439	D6AC	Bar and Forging	2.3.1
AMS 6454	4340	Sheet, Strip and Plate	2.3.1
AMS 6478	AerMet 100	Bar and Forging	2.5.3
AMS 6487	5Cr-Mo-V	Bar and Forging (CEVM)	2.4.1
AMS 6488	5Cr-Mo-V	Bar and Forging	2.4.1
AMS 6512	250	Bar	2.5.1
AMS 6514	280 (300)	Bar	2.5.1
AMS 6520	250	Sheet and Plate	2.5.1
AMS 6521	280 (300)	Sheet and Plate	2.5.1
AMS 6523	9Ni-4Co-0.20C	Sheet, Strip and Plate	2.4.2
AMS 6524	9Ni-4Co-0.20C	Sheet, Strip and Plate	2.4.3
AMS 6526	9Ni-4Co-0.20C	Bar and Forging, Tubing	2.4.3
AMS 6527	AF1410	Bar and Forging	2.5.2
AMS 6528	4130	Bar and Forging	2.3.1
AMS 6529	4140	Bar and Forging	2.3.1
AMS 6532	AerMet 100	Bar and Forging	2.5.3
AMS 7902	Standard Grade Beryllium	Sheet and Plate	7.2.1
AMS 7906	Standard Grade Beryllium	Bar, Rod, Tubing and Machined Shapes	7.2.1

266. PDF page 1711

Specification	Alloy Name	Form/Application	Section
AMS-A-21180	A201.0	Casting (T7 Temper)	3.8.1
AMS-A-21180	354.0	Casting	3.9.1
AMS-A-21180	C355.0	Casting	3.9.3
AMS-A-21180	A356.0	Casting	3.9.5
AMS-A-21180	A357.0	Casting	3.9.6
AMS-A-21180	359.0	Casting	3.9.8
AMS-A-22771	2014	Forging	3.2.1
AMS-A-22771	2618	Die Forging	3.2.13
AMS-A-22771	6061	Forging	3.6.2
AMS-A-22771	6151	Forging	3.6.3
AMS-A-22771	7049/7149	Forging	3.7.3
AMS-A-22771	7050	Forging	3.7.4
AMS-A-22771	7075	Forging	3.7.6
AMS-A-22771	7175	Forging	3.7.8
AMS-QQ-A-367	2014	Forging	3.2.1
AMS-QQ-A-367	2618	Forging	3.2.13
AMS-QQ-A-367	6061	Forging	3.6.2
AMS-QQ-A-367	7049/7149	Forging	3.7.3
AMS-QQ-A-367	7075	Forging	3.7.6
AMS-QQ-A-200/2	2014	Extruded Bar, Rod and Shapes	3.2.1
AMS-QQ-A-200/3	2024	Extruded Bar, Rod and Shapes	3.2.3
AMS-QQ-A-200/4	5083	Extruded Bar, Rod and Shapes	3.5.2
AMS-QQ-A-200/5	5086	Extruded Bar, Rod and Shapes	3.5.3
AMS-QQ-A-200/6	5454	Extruded Bar, Rod and Shapes	3.5.4
AMS-QQ-A-200/7	5456	Extruded Bar, Rod and Shapes	3.5.5
AMS-QQ-A-200/8	6061	Extruded Rod, Bar Shapes and Tubing	3.6.2
AMS-QQ-A-200/11, 15	7075	Extruded Bar, Rod and Shapes	3.7.6
AMS-QQ-A-225/4	2014	Rolled or Drawn Bar, Rod and Shapes	3.2.1
AMS-QQ-A-225/5	2017	Rolled Bar and Rod	3.2.2
AMS-QQ-A-225/6	2024	Rolled or Drawn Bar, Rod and Wire	3.2.3
AMS-QQ-A-225/8	6061	Rolled Bar, Rod and Shapes	3.6.2
AMS-QQ-A-225/9	7075	Rolled or Drawn Bar and Rod	3.7.6
AMS-QQ-A-250/3	2014	Clad Sheet and Plate	3.2.1
AMS-QQ-A-250/4	2024	Bare Sheet and Plate	3.2.3
AMS-QQ-A-250/5	2024	Clad Sheet and Plate	3.2.3
AMS-QQ-A-250/6	5083	Bare Sheet and Plate	3.5.2
AMS-QQ-A-250/7	5086	Sheet and Plate	3.5.3
AMS-QQ-A-250/8	5052	Sheet and Plate	3.5.1
AMS-QQ-A-250/9	5456	Sheet and Plate	3.5.5
AMS-QQ-A-250/10	5454	Sheet and Plate	3.5.4
AMS-QQ-A-250/11	6061	Sheet and Plate	3.6.2
AMS-QQ-A-250/12, 24	7075	Bare Sheet and Plate	3.7.6
AMS-QQ-A-250/13, 25	7075	Clad Sheet and Plate	3.7.6
AMS-QQ-A-250/29	2124	Plate	3.2.7
AMS-QQ-A-250/30	2219	Sheet and Plate	3.2.8
AMS-QQ-A-367	7049	Forging	3.7.3
AMS-S-5000	4340	Bar and Forging	2.3.1
AMS-S-5626	4140	Bar and Forging	2.3.1
AMS-S-6049	8740	Bar and Forging	2.3.1
AMS-S-6050	8630	Bar and Forging	2.3.1
AMS-S-6758	4130	Bar and Forging	2.3.1
AMS-S-7952	AISI 1025	Sheet and Strip	2.2.1
AMS-S-18728	8630	Sheet, Strip and Plate	2.3.1
AMS-S-18729	4130	Sheet, Strip and Plate	2.3.1
AMS-T-5066	AISI 1025 - N	Tubing	2.2.1
AMS-T-6735	4135	Tubing	2.3.1

267. PDF page 1712

Specification	Alloy Name	Form/Application	Section
AMS-T-6736	4130	Tubing	2.3.1
AMS-T-81556	CP Titanium	Extruded Bars and Shapes	5.2.1
AMS-T-81556	Ti-5Al-2.5Sn	Extruded Bar and Shapes	5.3.1
AMS-T-81556	Ti6Al-6V-2Sn	Extruded Bar and Shapes	5.4.2
AMS-T-9046	CP Titanium	Sheet, Strip and Plate	5.2.1
AMS-T-9046	Ti-5Al-2.5Sn	Sheet, Strip and Plate	5.3.1
AMS-T-9046	Ti-8Al-1Mo-1V	Sheet, Strip and Plate	5.3.2
AMS-T-9046	Ti-6Al-2Sn-4Zr-2Mo	Sheet and Strip	5.3.3
AMS-T-9046	Ti-6Al-4V	Sheet, Strip and Plate	5.4.1
AMS-T-9046	Ti6Al-6V-2Sn	Sheet, Strip and Plate	5.4.2
AMS-T-9046	Ti-13V-11Cr-3Al	Sheet, Strip and Plate	5.5.1
AMS-WW-T-700/3	2024	Tubing	3.2.3
AMS-WW-T-700/6	6061	Tubing Seamless, Drawn	3.6.2
ASTM A 108	AISI 1025	Bar	2.2.1
ASTM B 91	AZ31B	Forging	4.2.1
ASTM B 91	AZ61A	Forging	4.2.2
ASTM B 107	ZK60A-F	Extrusion	4.2.3
ASTM B 107	AZ31B	Extrusion	4.2.1
ASTM B 166	Inconel Alloy 600	Bar and Rod	6.3.2
ASTM B 194	Copper Beryllium	Sheet (TB00, TD01, TD02, TD04)	7.3.2
ASTM B 564	Inconel Alloy 600	Forging	6.3.2
MIL-DTL-46192	2519	Plate	3.2.11
MIL-T-9047	CP Titanium	Bar	5.2.1
MIL-T-9047	Ti-5Al-2.5Sn	Bar	5.3.1
MIL-T-9047	Ti-8Al-1Mo-1V	Bar	5.3.2
MIL-T-9047	Ti-6Al-4V	Bar	5.4.1
MIL-T-9047	Ti-13V-11Cr-3Al	Bar	5.5.1

268. PDF page 1714

Data Format, 9-50	Derived Properties, 9-30
A- and B-basis, 9-52	Design Mechanical Properties, 9-60
Derived Properties, 9-51	By Regression, 9-63, 9-64
Fasteners, 9-55	Determining Form of Distribution, 9-82
Stress-Strain Curves, 9-55	Determining Population, 9-60
Other Property, 9-56	Direct Computation,
Data Generation, 9-24	Non Parametric, 9-103
Creep/Stress Rupture, 9-46	Pearson, 9-100
Fatigue, 9-40	Weibull, 9-102
Fatigue Crack Growth, 9-130	Example Problems, 9-162, 9-175
Fracture Toughness, 9-133	Presentation, 9-179
Fusion-Welded Joints, 9-48	Dimensionally Discrepant Castings, 9-11
Mechanically Fastened Joints, 9-142	Direct Computation of Allowables, 9-60, 9-94, 9-104, 9-162
Mechanical Properties, 9-24, 9-30	Nonparametric Distribution, 9-103
Stress-Strain, 9-184	Pearson Distribution, 9-100
Data Presentation	Weibull Distribution, 9-102
Creep-Rupture, 9-234	Distribution, Form of, 9-82
Elevated Temperature Curves, 9-202	Documentation Requirements, 9-5
Fatigue, 9-212	Elastic Properties, 9-183
Fatigue Crack Growth, 1-26, 9-228	Element Properties
Fracture Toughness, 9-230	Aluminum, 3-518
Fusion-Welded Joints, 9-244	Magnesium, 4-53
Mechanically Fastened Joints, 9-240	Steel, 2-237 Titanium, 5-144
Room-Temperature Design Values, 9-179, 9-184	Elevated Temperature Curves, 1-13, 9-68, 9-202
Typical (Full-Range) Stress-Strain, 9-194	Data Requirements, 9-32
Typical Stress-Strain, 9-184	Presentation, 9-203
Data Requirements, 9-24, 9-26, 9-29	Working Curves, 9-202
Creep/Stress Rupture, 9-26, 9-35	Environmental Effects, 1-21
Derived Properties, 9-26, 9-30	Elongation, 1-8, 9-204
Directly Calculated, 9-9, 9-26	Examples of Computation Procedures
Elevated Temperature Properties, 9-26, 9-32	Complex Exposure, 9-210
Experimental Design, 9-40	Creep/Stress Rupture, 9-235
Fatigue, 9-27, 9-32, 9-40	Design Allowables, 9-162
Fatigue Crack Growth, 9-27, 9-35	Fatigue, 9-212, 9-219, 9-223
Fracture Toughness, 9-35	F-Test, 9-79
Fusion-Welded Joints, 9-40	Linear Regression, 9-104
Mechanically Fastened Joints, 9-36	Strain-Departure Method, 9-185
Mechanical Properties, 9-24, 9-25, 9-27	t-Test, 9-80
Modulus, 9-26, 9-31	F-Distribution Fractiles, 9-253, 9-254
New Materials, 9-7, 9-24	F-Test, 9-79
Physical Properties, 9-26, 9-27	Failure
Stress-Strain, 9-28, 9-31	General, 1-28
Data Submission, 9-50	Identification code, 9-57, 9-58
Definition of Terms, 9-30	Instability, 1-29
Creep/Stress Rupture, 9-135	Local, 1-30
Fatigue, 9-110	Material, 1-28
Fracture Toughness, 9-133	Types, 1-28
Mechanically Fastened Joints, 9-142	Fasteners, 9-142
Mechanical Properties, 9-14	Data Format, 9-55
Statistics, A-6	H-Type, 9-144
Degrees of Freedom, 9-81, A-8	S-Type, 9- 144
Density, 9-16

269. PDF page 1715

Fatigue, 9-8, 9-17, 9-110

Data Analysis, 9-114, 9-127

Data Generation, 9-40, 9-113, 9-223

Data Requirements, 9-17, 9-110, 9-223, 9-34

Example Problems, 9-212, 9-223

Life Models, 9-115, 9-125, 9-221, 9-226, 9-227

Load Control, 9-219

Outliers, 9-124, 9-221, 9-227

Presentation of Data, 1-15, 9-223

Properties, 1-14

Run-outs, 9-128, 9-222, 9-228

Strain Control, 9-223

Terminology, 9-40

Test Planning, 9-40

Time Dependent Effects, 9-130

Fatigue Crack Growth, 1-24, 9-17, 9-130, 9-228

Crack-Growth Analysis, 1-24

Data Analysis, 9-134

Data Generation, 9-133

Data Requirements, 9-35, 9-131

Presentation of Data, 1-26, 9-228

Forgings, Definition of Grain Directions in, 9-15

Fracture Toughness, 1-19, 9-18, 9-230

Analysis, 1-20, 9-133

Apparent Fracture Toughness, 1-23

Brittle Fracture, 1-20

Critical Plane-Strain, 1-21

Data Analysis, 9-133

Data Generation, 9-35

Data Requirements, 9-35

Definitions, 9-133

Environmental, 1-21

Middle Tension Panels, 1-23, 9-19, 9-35, 9-134

Plane Stress, 1-22, 9-18, 9-133

Plane Strain, 1-21, 9-18, 9-133

Presentation of Data, 9-230

Transitional Stress States, 1-22, 9-133

Full-Range Stress-Strain Curves, 9-194

Fusion-Welded Joints, 9-23, 9-40, 9-158

Data Analysis, 9-161

Data Generation, 9-48, 9-159, 9-160

Data Requirements, 9-40, 9-160

Presentation of Data, 9-244

Goodness-of-Fit Tests, 9-82

Anderson-Darling, 9-82

Normality, 9-82

Pearsonality, 9-85

Weibullness, 9-83

Grain Direction, Treatment of, 9-106

Grouped Data Analysis, 9-77

Heat Requirements, 9-7

270. PDF page 1715

Indirect Design Allowables	9-7, 9-60, 9-106
Without Regression	9-108
With Regression	9-109
Instability	1-29
Bending	1-29
Combined Loadings	1-29
Compression	1-29
Local	1-30
Torsion	1-29
International System of Units	1-3
k-Sample Anderson-Darling Test	9-77
Larson-Miller Analysis	9-138
Location of Test Specimens	9-14
Lot Requirements	9-7
Material Failures	1-28
Bearing	1-28
Bending	1-28
Combined Stress	1-28
Compression	1-28
Shear	1-28
Stress Concentrations	1-28
Tension	1-28
Material Specifications	9-11
Maximum Likelihood Estimation	9-129
Mean Stress/Strain Effects, Evaluation of	9-117
Mechanical Properties	9-60
Computation of Design Allowables	9-60
Derived Properties	9-30, 9-106, 9-109
Example Problems	9-162, 9-175
Presentation	9-179
Terminology for	9-14
Test Matrix	9-29
Mechanically Fastened Joints	9-22, 9-142
Data Analysis	9-144, 9-146, 9-148, 9-158
Data Requirements	9-36
Definitions	9-143
Presentation of Data	9-240
Melt, Definition of	9-30
Metallurgical Instability	1-17
Modulus of Elasticity	1-9, 9-16, 9-31, 9-183, 9-206
Modulus of Rigidity	1-12
NASM-1312	9-11, 9-12, 9-22, 9-23, 9-38, 9-144
Nomenclature	1-3
Nonparametric Data Analysis	9-103
Normal Curve Statistics	9-256
Normality, Assessment of	9-82
Outliers, Treatment of	9-124, 9-221, 9-227
Pearson Method	9-100
Anderson-Darling	9-85
Backoff	9-85
Probability Plot	9-86

271. PDF page 1716

Physical Properties, 9-16, 9-207	Specific Heat, 9-16
Poisson’s Ratio, 1-8, 9-16, 9-183	Specifying the Population, 9-60
Presentation of Data, 9-162, 9-212	Statistics Symbols, A-5 Terms/Definitions, A-6
Creep/Stress Rupture, 9-234	Strain, 1-8 Rate, 1-8 Shear, 1-8
Design Allowables, 9-179	Strain Departure Method, 9-194
Effect of Temperature Curves, 9-246	Stress, 1-8, 1-28
Fatigue, 9-212	Stress-Strain Curves, 9-184 Biaxial, 9-198 Compression Tangent Modulus, 9-202 Data Requirements, 9-31, 9-55 Example Computation, 9-198 Full-Range, 9-194 Presentation, 9-184 Typical, 9-184
Fatigue Crack Growth, 9-228	Stress Rupture, 1-13
Fracture Toughness, 9-230	Symbols and Definitions, 1-3 Creep/Stress Rupture, 9-136, A-7 Fatigue, 9-110, A-8 Fracture Toughness, 9-133 General, 1-3, A-5, A-6 Mechanically Fastened Joints, 9-143 Mechanical Properties, 9-14 Physical Properties, 9-16, 9-183, 9-184 Statistics, A-5, A-6
Fusion-Welded Joints, 9-244, 9-245	t-Distribution Fractiles, 9-255
Mechanically Fastened Joints, 9-240	t-Test, 9-80
Physical Properties, 9-183	Tangent Modulus Curves, 9-202
Stress-Strain, 9-184	Temperature Effects, 1-13, 9-202
Primary Test Direction, 9-15	Tensile Properties, 1-9 Tensile Proportional Limit, 1-9 Tensile Ultimate Stress, 1-11 Tensile Yield Stress, 1-9
Probability, A-12	Terminology Creep Rupture, 9-135 Fatigue, 1-15, 9-110 Mechanical Property, 9-14
Probability Plots Normal, 9-83 Pearson, 9-86 Weibull, 9-92	Test Specimens, 9-14 Duplication, 9-29 Location, 9-14, 9-107 Orientation, 9-14 Primary Test Direction, 9-15
Proportional Limit Shear, 1-12 Stress, 9-201 Tension and Compression 9-201	Testing Procedures, 9-11 Bearing, 9-12 Creep/Stress Rupture, 9-12, 9-22 Elastic Properties, 9-12 Fatigue, 9-12, 9-17 Fatigue Crack Growth, 9-12, 9-17 Fusion-Welded Joints, 9-23 Fracture Toughness, 9-18
Pulleys, 8-172
Ramberg-Osgood Method, 9-8, 9-188, 9-191
Ratioed Values, 1-7
Rank Values for A- and B-Basis, 9-267
Ratioing of Mechanical Properties, 9-106
Reduced Ratios By Regression, 9-109 Direct Computation, 9-106
Reduction in Area, 1-8, 1-11, 9-204
Reduction of Column Test Results, 1-31
Regression, 9-63, 9-64 Direct Computation, 9-104 Determining Design Allowables, 9-65 Determining Reduced Ratios, 9-106 Example Computations, 9-175 Least Squares, 9-67 Linear, 9-67 Tests for Adequacy of, 9-71 Tests for Equality, 9-74 Quadratic, 9-68
Rounding, 9-10
Runouts, Treatment of, 9-128
S-Basis, 1-7, 9-24, 9-59
Separately Cast Test Bars, 9-11
Shear Failure, 1-28
Shear Properties, 1-11, 9-7
Shear Test Procedures, 9-106, 9-109
Shear Yield Stress, 9-202
Significance, A-14
Skewness, 9-101

272. PDF page 1717

Mechanically Fastened Joints, 9-22

Mechanical Properties, 9-15

Modulus, 9-16

Physical Properties, 9-16

Shear, 9-13

Stress-Strain, 9-28, 9-184

Testing Standards, 9-12, 9-15

Tests of Significance, 9-77

Definitions, A-6

F-Test, 9-79

t-Test, 9-80

Thermal Conductivity, 9-16

Thermal Exposure, 9-8, 9-208

Complex, 9-210

Simple, 9-209

Thin Walled Sections, 1-40

Tolerance Bounds, A-15

T90, 9-10

T99, 9-10

Tolerance Interval, A-15

Tolerance Level, A-15

Tolerance Limit Factors

Normal, One-Sided, 9-248

Weibull, One-Sided, 9-257, 9-258

Torsion, Properties

Aluminum, 3-521

Magnesium, 4-56

Steel, 2-240

Typical Basis, 9-8

Ultimate Bearing Stress, 1-12

Ultimate Compression Stress, 1-1

Ultimate Shear Stress, 1-12

Ultimate Tensile Stress, 1-11

Units, 9-16

Weibull Procedure, 9-102

Weibull Acceptability Test, 9-83, 9-89

Weibull Back-Off, 9-91

Weibull Distribution Estimating, 9-89

Weibullness, Assessment of, 9-215

Weibull Probability Plot, 9-92

Wire Rope, 8-172

Working Curves, Determination of, 9-202

273. PDF page 1727

Figure No.	Current Form	Figure No.	Current Form
5.3.2.0	Scanned	5.4.1.2.6(g)	Vector Graphic
5.3.2.1.1	Scanned	5.4.1.2.6(h)	Scanned
5.3.2.1.4	Scanned	5.4.1.2.7	Scanned
5.3.2.1.6(a)	Vector Graphic	5.4.1.2.8(a)	Scanned
5.3.2.1.6(b)	Vector Graphic	5.4.1.2.8(b)	Scanned
5.3.2.2.1	Scanned	5.4.1.2.8(c)	Scanned
5.3.2.2.6(a)	Vector Graphic	5.4.1.2.8(d)	Scanned
5.3.2.2.6(b)	Vector Graphic	5.4.1.2.8(e)	Scanned
5.3.2.2.8(a)	Scanned	5.4.1.2.8(f)	Scanned
5.3.2.2.8(b)	Scanned	5.4.1.2.8(g)	Scanned
5.3.2.2.8(c)	Scanned	5.4.1.2.8(h)	Scanned
5.3.2.2.8(d)	Scanned	5.4.1.2.8(i)	Scanned
5.3.2.2.8(e)	Scanned	5.4.2.0	Scanned
5.3.2.2.8(f)	Scanned	5.4.2.1.1(a)	Scanned
5.3.3.0	Scanned	5.4.2.1.1(b)	Scanned
5.3.3.1.1	Scanned	5.4.2.1.2(a)	Scanned
5.3.3.1.2	Scanned	5.4.2.1.2(b)	Scanned
5.3.3.1.4	Scanned	5.4.2.1.3(a)	Scanned
5.3.3.1.6(a)	Vector Graphic	5.4.2.1.3(b)	Scanned
5.3.3.1.6(b)	Vector Graphic	5.4.2.1.6(a)	Vector Graphic
5.3.3.1.6(c)	Scanned	5.4.2.1.6(b)	Vector Graphic
5.4.1.0	Vector Graphic	5.4.2.1.6(c)	Scanned
5.4.1.1.1	Vector Graphic	5.4.2.1.8(a)	Scanned
5.4.1.1.2	Scanned	5.4.2.1.8(b)	Scanned
5.4.1.1.3	Scanned	5.4.2.2.1	Scanned
5.4.1.1.4	Scanned	5.4.2.2.2	Scanned
5.4.1.1.5	Scanned	5.4.3.1(a)	Vector Graphic
5.4.1.1.6(a)	Vector Graphic	5.4.3.1(b)	Vector Graphic
5.4.1.1.6(b)	Vector Graphic	5.4.3.1(c)	Vector Graphic
5.4.1.1.6(c)	Vector Graphic	5.4.3.2(a)	Scanned
5.4.1.1.6(d)	Scanned	5.4.3.2(b)	Scanned
5.4.1.1.8(a)	Scanned	5.4.3.3	Scanned
5.4.1.1.8(b)	Scanned	5.5.1.0	Scanned
5.4.1.1.8(c)	Scanned	5.5.1.1.1	Scanned
5.4.1.1.8(d)	Scanned	5.5.1.1.2	Scanned
5.4.1.1.8(e)	Scanned	5.5.1.1.3(a)	Scanned
5.4.1.1.8(f)	Scanned	5.5.1.1.3(b)	Scanned
5.4.1.1.8(g)	Scanned	5.5.1.1.4	Scanned
5.4.1.1.9	Scanned	5.5.1.1.6	Vector Graphic
5.4.1.2.1	Scanned	5.5.1.1.8(a)	Scanned
5.4.1.2.2	Scanned	5.5.1.1.8(b)	Scanned
5.4.1.2.3	Scanned	5.5.1.1.8(c)	Scanned
5.4.1.2.4	Scanned	5.5.1.1.8(d)	Scanned
5.4.1.2.6(a)	Vector Graphic	5.5.1.2.1	Scanned
5.4.1.2.6(b)	Vector Graphic	5.5.1.2.2	Scanned
5.4.1.2.6(c)	Vector Graphic	5.5.1.2.3	Scanned
5.4.1.2.6(d)	Vector Graphic	5.5.1.2.4	Scanned
5.4.1.2.6(e)	Vector Graphic	5.5.1.2.6	Vector Graphic
5.4.1.2.6(f)	Vector Graphic	5.5.1.2.8(a)	Scanned

274. PDF page 1728

Figure No.	Current Form	Figure No.	Current Form
5.5.1.2.8(b)	Scanned	6.3.4.1.4	Vector Graphic
5.5.1.2.8(c)	Scanned	6.3.4.1.5	Vector Graphic
5.5.2.0	Scanned	6.3.4.1.6(a)	Vector Graphic
5.5.2.1.6(a)	Vector Graphic	6.3.4.1.6(b)	Vector Graphic
5.5.2.1.6(b)	Vector Graphic	6.3.4.1.6(c)	Scanned
5.5.3.1.6	Vector Graphic	6.3.5.0	Vector Graphic
5.5.3.2.6	Vector Graphic	6.3.5.1.1	Scanned
5.6.1.1.1	Scanned	6.3.5.1.4(a)	Scanned
6.2.1.0	Scanned	6.3.5.1.4(b)	Scanned
6.2.1.1.1	Scanned	6.3.5.1.4(c)	Scanned
6.2.1.1.3	Scanned	6.3.5.1.6(a)	Vector Graphic
6.2.1.1.4(a)	Scanned	6.3.5.1.6(b)	Vector Graphic
6.2.1.1.4(b)	Scanned	6.3.5.1.6(c)	Vector Graphic
6.2.1.1.4(c)	Scanned	6.3.5.1.6(d)	Scanned
6.2.1.1.8(a)	Scanned	6.3.5.1.7(a)	Scanned
6.2.1.1.8(b)	Scanned	6.3.5.1.7(b)	Scanned
6.2.1.1.8(c)	Scanned	6.3.5.1.7(c)	Scanned
6.2.1.1.8(d)	Scanned	6.3.5.1.7(d)	Vector Graphic
6.2.1.1.8(e)	Scanned	6.3.5.1.7(e)	Vector Graphic
6.2.2.0	Scanned	6.3.5.1.8(a)	Vector Graphic
6.2.2.1.1(a)	Scanned	6.3.5.1.8(b)	Vector Graphic
6.2.2.1.1(b)	Scanned	6.3.5.1.8(c)	Vector Graphic
6.2.2.1.4(a)	Scanned	6.3.5.1.8(d)	Vector Graphic
6.2.2.1.4(b)	Scanned	6.3.5.1.8(e)	Vector Graphic
6.3.1.0	Scanned	6.3.5.1.8(f)	Vector Graphic
6.3.1.1.1	Scanned	6.3.5.1.8(g)	Vector Graphic
6.3.1.1.4	Scanned	6.3.5.1.9(a)	Vector Graphic
6.3.1.1.6(a)	Vector Graphic	6.3.5.1.9(b)	Scanned
6.3.1.1.6(b)	Vector Graphic	6.3.5.1.9(c)	Scanned
6.3.2.0	Scanned	6.3.6.0	Scanned
6.3.2.1.1	Scanned	6.3.6.1.1	Scanned
6.3.2.1.2	Scanned	6.3.6.1.2	Scanned
6.3.2.1.3	Scanned	6.3.6.1.3	Scanned
6.3.2.1.4	Scanned	6.3.6.2.1(a)	Scanned
6.3.3.0	Scanned	6.3.6.2.1(b)	Scanned
6.3.3.1.1(a)	Scanned	6.3.6.2.4(a)	Scanned
6.3.3.1.1(b)	Scanned	6.3.6.2.4(b)	Scanned
6.3.3.1.4(a)	Scanned	6.3.7.0	Scanned
6.3.3.1.4(b)	Scanned	6.3.7.1.1	Vector Graphic
6.3.3.1.6(a)	Vector Graphic	6.3.7.1.2	Vector Graphic
6.3.3.1.6(b)	Vector Graphic	6.3.7.1.3(a)	Scanned
6.3.3.1.6(c)	Vector Graphic	6.3.7.1.3(b)	Scanned
6.3.3.1.6(d)	Vector Graphic	6.3.7.1.4	Scanned
6.3.3.1.8(a)	Scanned	6.3.7.1.5	Scanned
6.3.3.1.8(b)	Scanned	6.3.7.1.7	Scanned
6.3.3.1.8(c)	Scanned	6.3.8.0	Scanned
6.3.3.1.8(d)	Scanned	6.3.8.1.1	Scanned
6.3.4.0	Vector Graphic	6.3.8.1.4	Scanned
6.3.4.1.1	Vector Graphic	6.3.8.1.5(a)	Scanned

275. PDF page 1729

Figure No.	Current Form	Figure No.	Current Form
6.3.8.1.5(b)	Scanned	7.2.1.1.1	Vector Graphic
6.3.8.1.6(a)	Scanned	7.2.1.1.4	Vector Graphic
6.3.8.1.6(b)	Scanned	7.3.2.0	Vector Graphic
6.3.9.0(a)	Vector Graphic	7.3.2.1.6(a)	Vector Graphic
6.3.9.0(b)	Vector Graphic	7.3.2.1.6(b)	Vector Graphic
6.3.9.0(c)	Vector Graphic	7.3.2.2.6	Vector Graphic
6.3.9.1.1(a)	Vector Graphic	7.4.1.0	Scanned
6.3.9.1.1(b)	Vector Graphic	7.4.1.1.1	Scanned
6.3.9.1.4	Vector Graphic	7.4.1.1.4(a)	Scanned
6.3.9.1.5	Vector Graphic	7.4.1.1.4(b)	Scanned
6.3.9.1.6(a)	Vector Graphic	7.4.1.1.5	Scanned
6.3.9.1.6(b)	Vector Graphic	7.4.1.1.6	Vector Graphic
6.3.9.1.6(c)	Vector Graphic	7.4.2.0	Scanned
6.3.9.1.6(d)	Vector Graphic	7.4.2.1.4	Scanned
6.3.9.1.6(e)	Vector Graphic	7.4.2.1.6	Vector Graphic
6.3.9.1.6(f)	Vector Graphic	7.5.1.1.6(a)	Vector Graphic
6.3.9.1.6(g)	Vector Graphic	7.5.1.1.6(b)	Vector Graphic
6.3.9.1.6(h)	Vector Graphic	7.5.1.1.6(c)	Vector Graphic
6.3.9.1.6(i)	Vector Graphic	7.5.1.1.6(d)	Vector Graphic
6.3.10.0(a)	Vector Graphic	7.5.1.1.6(e)	Vector Graphic
6.3.10.0(b)	Vector Graphic	7.5.1.1.6(f)	Vector Graphic
6.3.10.0(c)	Vector Graphic	7.5.1.1.6(g)	Vector Graphic
6.3.10.0(d)	Vector Graphic	7.5.1.1.6(h)	Vector Graphic
6.3.10.1.1(a)	Vector Graphic	7.5.1.1.6(i)	Vector Graphic
6.3.10.1.7(a)	Vector Graphic	7.5.1.1.6(j)	Vector Graphic
6.3.10.1.7(b)	Vector Graphic	7.5.1.1.6(k)	Vector Graphic
6.4.1.0	Scanned	7.5.1.1.6(l)	Vector Graphic
6.4.1.1.1	Vector Graphic	7.5.2.1.6(a)	Vector Graphic
6.4.1.1.2	Vector Graphic	7.5.2.1.6(b)	Vector Graphic
6.4.1.1.3	Vector Graphic	7.5.2.1.6(c)	Vector Graphic
6.4.1.1.4(a)	Vector Graphic	7.5.2.1.6(d)	Vector Graphic
6.4.1.1.4(b)	Scanned	7.5.2.1.6(e)	Vector Graphic
6.4.1.1.5	Scanned	7.5.2.1.6(f)	Vector Graphic
6.4.1.1.7	Scanned	7.5.2.1.6(g)	Vector Graphic
6.4.2.0	Scanned	7.5.2.1.6(h)	Vector Graphic
6.4.2.1.1(a)	Scanned	7.5.2.1.6(i)	Vector Graphic
6.4.2.1.1(b)	Scanned	7.5.2.1.6(j)	Vector Graphic
6.4.2.1.2	Scanned	8.2.1	Scanned
6.4.2.1.4(a)	Scanned	8.2.2.3.1.1(a)	Scanned
6.4.2.1.4(b)	Scanned	8.2.2.3.1.1(b)	Scanned
6.4.2.1.4(c)	Scanned	8.2.2.3.1.1(c)	Scanned
6.4.2.1.5	Scanned	8.2.2.3.2.1	Scanned
6.4.2.1.6(a)	Vector Graphic	8.2.2.3.2.2(a)	Scanned
6.4.2.1.6(b)	Vector Graphic	8.2.2.3.2.2(b)	Scanned
6.4.2.1.8(a)	Scanned	8.2.2.3.2.2(c)	Scanned
6.4.2.1.8(b)	Scanned	8.2.2.3.2.2(d)	Scanned
6.4.2.1.8(c)	Scanned	8.2.2.3.2.2(e)	Scanned
6.4.2.1.8(d)	Scanned	9.2.3	Scanned
7.2.1.0	Vector Graphic	9.2.4	Scanned

276. PDF page 1730

Figure No.	Current Form	Figure No.	Current Form
9.2.6	Scanned	9.3.5.1(a)	Scanned
9.2.11	Scanned	9.3.5.1(b)	Scanned
9.2.12	Scanned	9.3.5.2	Scanned
9.2.15(a)	Scanned	9.3.5.6	Scanned
9.2.15(b)	Scanned	9.3.6.2	Scanned
9.3.1.1.2	Scanned	9.3.6.7	Scanned
9.3.1.1.3(a)	Scanned	9.3.6.8(a)	Scanned
9.3.1.1.3(b)	Scanned	9.3.6.8(b)	Scanned
9.3.1.2	Scanned	9.3.6.8(c)	Scanned
9.3.1.3	Scanned	9.3.6.8(d)	Scanned
9.3.1.4(a)	Scanned	9.4.1.3	Scanned
9.3.1.4(b)	Scanned	9.4.1.3.4(a)	Scanned
9.3.1.5	Scanned	9.4.1.3.4(b)	Scanned
9.3.1.6.1	Scanned	9.4.1.3.4(c)	Scanned
9.3.1.6.2	Vector Graphic	9.4.1.3.4(d)	Scanned
9.3.2.3(a)	Scanned	9.4.1.3.4(e)	Scanned
9.3.2.3(b)	Scanned	9.4.1.5.2(a)	Scanned
9.3.2.3(c)	Vector Graphic	9.4.1.5.2(b)	Scanned
9.3.2.4	Scanned	9.4.1.5.2(c)	Scanned
9.3.2.5(a)	Scanned	9.4.1.5.2(d)	Scanned
9.3.2.5(b)	Vector Graphic	9.4.1.5.2(e)	Scanned
9.3.2.5(c)	Vector Graphic	9.4.1.5.2(f)	Scanned
9.3.2.5(d)	Vector Graphic	9.4.1.5.2(g)	Scanned
9.3.2.7(a)	Scanned	9.4.1.5.2(h)	Scanned
9.3.2.7(b)	Scanned	9.4.1.5.3	Scanned
9.3.2.7(c)	Scanned	9.4.1.6	Scanned
9.3.4.1(a)	Scanned	9.4.1.7.2	Scanned
9.3.4.1(b)	Scanned	9.4.1.7.2, cont.	Scanned
9.3.4.1(c)	Scanned	9.4.2.2	Scanned
9.3.4.1(d)	Scanned	9.4.2.3.2	Scanned
9.3.4.3	Scanned	9.4.2.3.5(a)	Scanned
9.3.4.4	Scanned	9.4.2.3.5(b)	Scanned
9.3.4.5	Scanned	9.4.2.5.2	Scanned
9.3.4.7	Scanned	9.4.2.5.3	Scanned
9.3.4.10(a)	Scanned	9.5.1.3	Scanned
9.3.4.10(b)	Scanned	9.5.1.5.1(a)	Scanned
9.3.4.10(c)	Scanned	9.5.1.5.1(b)	Scanned
9.3.4.12(a)	Scanned	9.5.1.5.1(c)	Scanned
9.3.4.12(b)	Scanned	9.5.1.5.3	Scanned
9.3.4.13	Scanned	9.6.3	Scanned
9.3.4.16(a)	Scanned	A.1	Scanned
9.3.4.17(a)	Scanned
9.3.4.17(b)	Scanned
9.3.4.17(c)	Scanned
9.3.4.17(d)	Scanned
9.3.4.17(e)	Scanned
9.3.4.17(f)	Scanned
9.3.4.17(g)	Scanned
9.3.4.17(h)	Scanned

277. PDF page 1731

Custodians:	Preparing activity:
Army – AV	Air Force – 11
Navy – AS	(Project 1560-0027)
Air Force – 11

Found in

January