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									MIL-HDBK-5H 1 December 1998

APPENDIX A
 

 	
 (also see Sections 1.2.1, 9.2.2, 9.3.4.3, 9.3.6.2, 9.4.1.2, 9.5.1.2, and 9.6).
a ac ao A — — — — Amplitude; crack or flaw dimension; measure of flaw size, inches. Critical half crack length. Initial half crack length. Area of cross section, square inches; ratio of alternating stress to mean stress; subscript “axial”; A basis for mechanical-property values (see Section 1.4.1.1 or Section 9.2.2.1); “A” ratio, loading amplitude/mean load; or area. Strain “A” ratio, strain amplitude/mean strain. Model parameter. Anderson-Darling test statistic, computed in goodness-of-fit tests for normality or Weibullness. American Iron and Steel Institute. Aerospace Materials Specification (published by Society of Automotive Engineers, Inc.). Annealed. Air Force-Navy Aeronautical Standard. American Society for Testing and Materials. Width of sections; subscript “bending”. Subscript “bearing”. Biaxial ratio (see Equation 1.3.2.8); B-basis for mechanical-property values (see Section 1.4.1.1 or Section 9.2.2.1). British thermal unit(s). Individual or typical bearing ultimate strength. Individual or typical bearing yield strength. Fixity coefficient for columns; subscript “compression”. Cycles per minute. Specific heat; Celsius; Constant. Consumable electrode melted. Corrosion resistant steel (stainless steel). Compact tension. Individual or typical compressive yield strength. Mathematical operator denoting differential. Diameter, or Durbin Watson statistic; hole or fastener diameter; dimpled hole. Degrees of freedom. Elongation in percent, a measure of the ductility of a material based on a tension test; unit deformation or strain; subscript “fatigue or endurance”; the minimum distance from a hole, center to the edge of the sheet; Engineering strain. Elastic strain. Plastic strain. Ratio of edge distance (center of the hole to edge of the sheet) to hole diameter (bearing strength). Modulus of elasticity in tension or compression; average ratio of stress to strain for stress below proportional limit. Modulus of elasticity in compression; average ratio of stress to strain below proportional limit. A-1

A Ai AD AISI AMS Ann AN ASTM b br B Btu BUS BYS c cpm C CEM CRES C(T) CYS d D or d df e

— — — — — — — — — — — — — — — — — — — — — — — — —

ee ep e/D E Ec

— — — — —

MIL-HDBK-5H 1 December 1998 Es Et ELI ER ESR f fb fc fpl fs ft ft F FA Fb Fbru Fbry Fc Fcc Fcu Fcy FH Fs Fsp Fst Fsu Fsy Ftp Ftu Fty g G Gpa hr H HIP i in. I J k k99, k90 kA,B ksi K Kapp — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — Secant modulus of elasticity, Eq. 9.3.2.5b. Tangent modulus of elasticity. Extra low interstitial (grade of titanium alloy). Equivalent round. Electro-slag remelted. Internal (or calculated) tension stress; stress applied to the gross flawed section; creep stress. Internal (or calculated) primary bending stress. Internal (or calculated) compressive stress; maximum stress at fracture: gross stress limit (for screening elastic fracture data). Proportional limit. Internal (or calculated) shear stress. Internal (or calculated) tensile stress. Foot: feet. Design stress; Fahrenheit; Ratio of two sample variances. Design axial stress. Design bending stress; modulus of rupture in bending. Design ultimate bearing stress. Design bearing yield stress. Design column stress. Design crushing or crippling stress (upper limit of column stress for local failure). Design ultimate compressive stress. Design compressive yield stress at which permanent strain equals 0.002. Design hoop stress. Design shear stress. Design proportional limit in shear. Design modulus of rupture in torsion. Design ultimate stress in pure shear (this value represents the average shear stress over the cross section). Design shear yield stress. Design proportional limit in tension. Design tensile ultimate stress. Design tensile yield stress at which permanent strain equals 0.002. Gram(s). Modulus of rigidity (shear modulus). Gigapascal(s). Hour(s). Subscript “hoop”. Hot isostatically pressed. Slope (due to bending) of neutral plane of a beam, in radians (1 radian = 57.3 degrees). Inch(es). Axial moment of inertia. Torsion constant (= Ip for round tubes); Joule. Tolerance limit factor for the normal distribution and the specified probability, confidence, and degrees of freedom; Strain at unit stress. One-sided tolerance limit factor for T99 and T90, respectively (see Section 9.2.7.2). K to A basis or B basis, respectively (see Section 9.2.7.2). Kips (1,000 pounds) per square inch. A constant, generally empirical; thermal conductivity; stress intensity; Kelvin; correction factor. Apparent plane stress fracture toughness or residual strength. A-2

MIL-HDBK-5H 1 December 1998 Kc Kf KIc KN Kt lb ln log L LT m mm M Mc Mg MIG MPa MS M.S. M(T) n — Critical plane stress fracture toughness, a measure of fracture toughness at point of crack growth instability. — Fatigue notch factor, or fatigue strength reduction factor. — Plane strain fracture toughness. — Empirically calculated fatigue notch factor. — Theoretical stress concentration factor. — Pound. — Natural (base e) logarithm. — Base 10 logarithm. — Length; subscript “lateral”; longitudinal (grain direction). — Long transverse (grain direction). — Subscript “mean”; metre; slope. — Millimeter(s). — Applied moment or couple, usually a bending moment. — Machine countersunk. — Megagram(s). — Metal-inert-gas (welding). — Megapascal(s). — Military Standard. — Margin of safety. — Middle tension. — 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. — Fatigue life, number of cycles to failure; Newton; normalized. — Fatigue life, cycles to failure. — Fatigue life, cycles to initiation. — Transition fatigue life where plastic and elastic strains are equal. — National Aerospace Standard. — Subscript “polar”; subscript “proportional limit”. — Pounds per square inch. — Load; applied load (total, not unit, load); exposure parameter; probability. — Load amplitude. — Mean load. — Maximum load. — Minimum load. — Test ultimate load, pounds per fastener. — Test yield load, pounds per fastener. — Fatigue notch sensitivity. — Static moment of a cross section. — Quenched and tempered. — Radius; root radius; reduced ratio (regression analysis); ratio of two pair measurements; rank of test point within a sample. — average ratio of paired measurements. — Load (stress) ratio, or residual (observed minus predicted value); stress ratio, ratio of minimum stress to maximum stress in a fatigue cycle; reduced ratio. — Stress ratio in bending. — Stress ratio in compression; Rockwell hardness - C scale.

N Nf Ni* Nt* NAS p psi P Pa Pm Pmax Pmin Pu Py q Q Q&T r r R Rb Rc

* Different from ASTM. A-3

MIL-HDBK-5H 1 December 1998 R Rs Rt RA R.H. RMS RT s s2 S Sa Se Seq* Sf sm Smax Smin Sr Sy SAE SCC SEE SR ST STA SUS SYS t T TF T90 T99 TIG TUS TUS (Su)* TYS u U V99,V90 W — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — — Strain ratio, min/max. Stress ratio in shear or torsion; ratio of applied load to allowable shear load. Ratio of applied load to allowable tension load. Reduction of area. Relative humidity. Root-mean-square (surface finish). Room temperature. Estimated population standard deviation; sample standard deviation; subscript “shear”. Sample variance. Shear force; nominal engineering stress, fatigue; S-basis for mechanical-property values (see Section 1.4.1.1). Stress amplitude, fatigue. Fatigue limit. Equivalent stress. Fatigue limit. Mean stress, fatigue. Highest algebraic value of stress in the stress cycle. Lowest algebraic value of stress in the stress cycle. Algebraic difference between the maximum and minimum stresses in one cycle. Root mean square error. Society of Automotive Engineers. Stress-corrosion cracking. Estimate population standard error of estimate. Studentized residual. Short transverse (grain direction). Solution treated and aged. Individual or typical shear ultimate strength. Individual or typical shear yield strength. Thickness; subscript “tension”; exposure time; elapsed time; tolerance factor for the “t” distribution with the specified probability and appropriate degrees of freedom. Transverse direction; applied torsional moment; transverse (grain direction); subscript “transverse”. Exposure temperature. 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. 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. Tungsten-inert-gas (welding). Individual or typical tensile ultimate strength. Tensile ultimate strength. Individual or typical tensile yield strength. Subscript “ultimate”. Factor of utilization. The tolerance limit factor corresponding to T99, T90 for the three-parameter Weibull distribution, based on a 95 percent confidence level and a sample of size n. Width of center-through-cracked tension panel; Watt. Distance along a coordinate axis. Sample mean based upon n observations.

x
x

* Different from ASTM. A-4

MIL-HDBK-5H 1 December 1998 X y Y z Z — Value of an individual measurement; average value of individual measurements. — Deflection (due to bending) of elastic curve of a beam; distance from neutral axis to given fiber; subscript “yield”; distance along a coordinate axis. — Nondimensional factor relating component geometry and flaw size. See Reference 1.4.12.2.1(a) for values. — Distance along a coordinate axis. — Section modulus, I/y.

  (also see Sections 1.2.1, 9.2.2, 9.3.4.3, 9.3.6.2, 9.4.1.2, 9.5.1.2, and 9.6).
 99, 90 50  99, 90 50  or r* e p S (Sr)*   eq* m max min t   
µ — (1) Coefficient of thermal expansion, mean; constant. (2) Significance level; probability (risk of erroneously rejecting the null hypothesis (see Section 9.6.2)). — Shape parameter estimates for a T99 or T90 value based on an assumed three-parameter Weibull distribution. — Shape parameter estimate for the Anderson-Darling goodness-of-fit test based on an assumed three-parameter Weibull distribution. — Constant. — Scale parameter estimate for a T99 or T90 value based on an assumed three-parameter Weibull distribution. — Scale parameter estimate for the Anderson-Darling goodness-of-fit test based on an assumed three-parameter Weibull distribution. — strain range, max - min. — Elastic strain range. — Plastic strain range. — Stress range. — True or local stress range. — True or local strain. — Equivalent strain. — Mean strain, (max + min)/2. — Maximum strain. — Minimum strain. — Total (elastic plus plastic) strain at failure determined from tensile stress-strain curve. — Deflection. — Angular deflection. — Radius of gyration; Neuber constant (block length). — Poisson’s ratio. — True or local stress; or population standard deviation. — Population standard deviation of x. — Population variance of x. — Threshold estimates for a T99 or T90 value based on an assumed three-parameter Weibull distribution. — Threshold estimate for the Anderson-Darling goodness-of-fit test based on an assumed three-parameter Weibull distribution. — Density; flank angle. — Infinity. — The sum of. — Superscript that denotes value determined by regression analysis.

 x  x2  99,  90  50

	  
 

* Different from ASTM. A-5

MIL-HDBK-5H 1 December 1998

 	




(also see Sections 1.2.1, 9.2.2, 9.3.6.2, 9.4.1.2, 9.5.1.2 and 9.6).

A-Basis.—The lower of either a statistically calculated number, or the specification minimum (S-basis). The statistically calculated number indicates that at least 99 percent of the population of values is expected to equal or exceed the A-basis mechanical design property, with a confidence of 95 percent. Alternating Load.—See Loading Amplitude. B-Basis.—At least 90 percent of the population of values is expected to equal or exceed the B-basis mechanical property allowable, with a confidence of 95 percent. Cast.—Cast consists of the sequential ingots which are melted from a single furnace change and poured in one or more drops without changes in the processing parameters. (The cast number is for internal identification and is not reported.) (See Table 9.1.6.1). Casting.—One or more parts which are melted from a single furnace change and poured in one or more molds without changes in the processing parameters. (The cast number is for internal identification and is not reported.) (See Table 9.1.6.1). Confidence.—A specified degree of certainty that at least a given proportion of all future measurements can be expected to equal or exceed the lower tolerance limit. Degree of certainty is referred to as the confidence coefficient. For MIL-HDBK-5, the confidence coefficient is 95 percent which, as related to design properties, means that, in the long run over many future samples, 95 percent of conclusions regarding exceedance of A and B-values would be true. Confidence Interval.—An interval estimate of a population parameter computed so that the statement “the population parameter lies in this interval” will be true, on the average, in a stated proportion of the times such statements are made. Confidence Interval Estimate.—Range of values, computed with the sample that is expected to include the population variance or mean. Confidence Level (or Coefficient).—The stated portion of the time the confidence interval is expected to include the population parameter. Confidence Limits*.—The two numeric values that define a confidence interval. Constant-Amplitude Loading.—A loading in which all of the peak loads are equal and all of the valley loads are equal. Constant-Life Fatigue Diagram.—A plot (usually on Cartesian coordinates) of a family of curves, each of which is for a single fatigue life, N—relating S, S max, and/or Smin to the mean stress, Sm. Generally, the constant life fatigue diagram is derived from a family of S/N curves, each of which represents a different stress ratio (A or R) for a 50 percent probability of survival. NOTE—MIL-HDBK-5 no longer presents fatigue data in the form of constant-life diagrams. Creep.—The time-dependent deformation of a solid resulting from force.

* Different from ASTM. A-6

MIL-HDBK-5H 1 December 1998 Note 1—Creep tests are usually made at constant load and temperature. For tests on metals, initial loading strain, however defined, is not included. Note 2—This change in strain is sometimes referred to as creep strain. Creep-Rupture Curve.—Results of material tests under constant load and temperature; usually plotted as strain versus time to rupture. A typical plot of creep-rupture data is shown in Figure 9.3.6.2. The strain indicated in this curve includes both initial deformation due to loading and plastic strain due to creep.

 	
	 
 

 	
Creep-Rupture Strength.—Stress that will cause fracture in a creep test at a given time, in a specified constant environment. Note: This is sometimes referred to as the stress-rupture strength. Creep-Rupture Test.—A creep-rupture test is one in which progressive specimen deformation and time for rupture are measured. In general, deformation is much larger than that developed during a creep test. Creep-Strain.—The time-dependent part of the strain resulting from stress, excluding initial loading strain and thermal expansion. Creep Strength.—Stress that causes a given creep in a creep test at a given time in a specified constant environment. Creep Stress.—The constant load divided by the original cross-sectional area of the specimen. Creep Test.—A creep test has the objective of measuring deformation and deformation rates at stresses usually well below those which would result in fracture during the time of testing. Critical Stress Intensity Factor.—A limiting value of the stress intensity factor beyond which continued flaw propagation and/or fracture may be expected. This value is dependent on material and may vary with type of loading and conditions of use. Cycle.—Under constant-amplitude loading, the load varies from the minimum to the maximum and then to the minimum load (see Figure 9.3.4.3). The symbol n or N (see definition of fatigue life) is used to indicate the number of cycles.

A-7

MIL-HDBK-5H 1 December 1998 Deformable Shank Fasteners.—A fastener whose shank is deformed in the grip area during normal installation processes. Degree of Freedom.—Number of degrees of freedom for n variables may be defined as number of variables minus number of constraints between them. Since the standard deviation calculation contains one fixed value (the mean) it has n - 1 degrees of freedom. Degrees of Freedom.—Number of independent comparisons afforded by a sample. Discontinued Test.—See Runout. Elapsed Time.—The time interval from application of the creep stress to a specified observation. Fatigue.—The process of progressive localized permanent structural change occurring in a material subjected to conditions that produce fluctuating stresses and strains at some point or points, and which may culminate in cracks or complete fracture after a sufficient number of fluctuations. NOTE—fluctuations in stress and in time (frequency), as in the case of “random vibration”. Fatigue Life.—N—the number of cycles of stress or strain of a specified character that a given specimen sustains before failure of a specified nature occurs. Fatigue Limit.—Sf—the limiting value of the median fatigue strength as N becomes very large. NOTE—Certain materials and environments preclude the attainment of a fatigue limit. Values tabulated as “fatigue limits” in the literature are frequently (but not always) values of SN for 50 percent survival at N cycles of stress in which Sm = 0. Fatigue Loading.—Periodic or non-periodic fluctuating loading applied to a test specimen or experienced by a structure in service (also known as cyclic loading). Fatigue Notch Factor*.—The fatigue notch factor, Kf (also called fatigue strength reduction factor), is the ratio of the fatigue strength of a specimen with no stress concentration to the fatigue strength of a specimen with a stress concentration at the same number of cycles for the same conditions. NOTE—In specifying Kf, it is necessary to specify the geometry, mode of loading, and the values of Smax, Sm, and N for which it is computed. Fatigue Notch Sensitivity.—The fatigue notch sensitivity, q, is a measure of the degree of agreement between Kf and Kt. NOTE—the definition of fatigue notch sensitivity is q = (Kf - 1)/(Kt - 1).

Heat.—All material identifiable to a single molten metal source. (All material from a heat is considered to have the same composition. A heat may yield one or more ingots. A heat may be divided into several lots by subsequent processing.) Heat.—Heat is material which, in the case of batch melting, is cast at the same time from the same furnace and is identified with the same heat number; or, in the case of continuous melting, is poured without interruption. (See Table 9.1.6.2) Heat.—Heat is a consolidated (vacuum hot pressed) billet having a distinct chemical composition. (See Table 9.1.6.2)

* Different from ASTM. A-8

MIL-HDBK-5H 1 December 1998 Hysteresis Diagram.—The stress-strain path during a fatigue cycle. Isostrain Lines.—Lines representing constant levels of creep. Isothermal Lines.—Lines of uniform temperature on a creep or stress-rupture curve. Interrupted Test*.—Tests which have been stopped before failure because of some mechanical problem, e.g., power failure, load or temperature spikes. Loading Amplitude.—The loading amplitude, Pa, Sa, or a represents one-half of the range of a cycle (see Figure 9.3.4.3). (Also known as alternating load, alternating stress, or alternating strain.) Loading Strain.—Loading strain is the change in strain during the time interval from the start of loading to the instant of full-load application, sometimes called initial strain. Loading (Unloading) Rate.—The time rate of change in the monotonically increasing (decreasing) portion of the load-time function. Load Ratio.—The load ratio, R, A, or R, A, or R, A, is the algebraic ratio of the two loading parameters of a cycle; the two most widely used ratios are
R  P minimum load  min Pmax maximum load

or
R  Smin Smax

or
R  min/max

and
A  P S loading amplitude  a or a Pm SM mean load

A 

 strain amplitude  a or max  min / max  min mean strain M

.

NOTE—load ratios R or R are generally used in MIL-HDBK-5.

* Different from ASTM. A-9

MIL-HDBK-5H 1 December 1998 Longitudinal Direction.—Parallel to the principal direction of flow in a worked metal. For die forgings this direction is within ±15 of the predominate grain flow. Long-Transverse Direction.—The transverse direction having the largest dimension, often called the “width” direction. For die forgings this direction is within ±15 of the longitudinal (predominate) grain direction and parallel, within ±15, to the parting plane. (Both conditions must be met.) Lot.—All material from a heat or single molten metal source of the same product type having the same thickness or configuration, and fabricated as a unit under the same conditions. If the material is heat treated, a lot is the above material processed through the required heat-treating operations as a unit. Master Creep Equation.—An equation expressing combinations of stress, temperature, time and creep, or a set of equations expressing combinations of stress, temperature and time for given levels of creep. Master Rupture Equation.—An equation expressing combinations of stress, temperature, and time that cause complete separation (fracture or rupture) of the specimen. Maximum Load.—The maximum load, Pmax, Smax, max is the load having the greatest algebraic value. Mean Load.—The mean load, Pm, is the algebraic average of the maximum and minimum loads in constantamplitude loading:
Pm  Pmax  Pmin 2

, or

Sm 

Smax  Smin 2

, or

m 

max  min
2

,

or the integral average of the instantaneous load values. Median Fatigue Life.—The middlemost of the observed fatigue life values (arranged in order of magnitude) of the individual specimens in a group tested under identical conditions. In the case where an even number of specimens are tested, it is the average of the two middlemost values (based on log lives in MIL-HDBK-5). NOTE 1—The use of the sample median instead of the arithmetic mean (that is, the average) is usually preferred. NOTE 2—In the literature, the abbreviated term “fatigue life” usually has meant the median fatigue life of the group. However, when applied to a collection of data without further qualification, the term “fatigue life” is ambiguous. Median Fatigue Strength at N Cycles.—An estimate of the stress level at which 50 percent of the population would survive N cycles. NOTE—The estimate of the median fatigue strength is derived from a particular point of the fatigue-life distribution, since there is no test procedure by which a frequency distribution of fatigue strengths at N cycles can be directly observed. That is, one can not perform constant-life tests. A-10

MIL-HDBK-5H 1 December 1998 Melt.—Melt is a single homogeneous batch of molten metal for which all processing has been completed and the temperature has been adjusted and made ready to pour castings. (For metal-matrix composites, the molten metal includes unmelted reinforcements such as particles, fibers, or whiskers.) (See Table 9.1.6.2) Minimum Load.—The minimum load, Pmin, Smin, or min, is the load having the least algebraic value. Nominal Hole Diameters.—Nominal hole diameters for deformable shank fasteners shall be according to Table 9.4.1.2(a). When tests are made with hole diameters other than those tabulated, hole sizes used shall be noted in the report and on the proposed joint allowables table. Nominal Shank Diameter.—Nominal shank diameter of fasteners with shank diameters equal to those used for standard size bolts and screws (NAS 618 sizes) shall be the decimal equivalents of stated fractional or numbered sizes. These diameters are those listed in the fourth column of Table 9.4.1.2. Nominal shank diameters for nondeformable shank blind fasteners are listed in the fifth column of Table 9.4.1.2. Nominal shank diameters for other fasteners shall be the average of required maximum and minimum shank diameters. Nondeformable Shank Fasteners.—A fastener whose shank does not deform in the grip area during normal installation processes. Outlier*—An experimental observation which deviates markedly from other observations in the sample. An outlier is often either an extreme value of the variability in the data, or the result of gross deviation in the material or experimental procedure. Peak.—The point at which the first derivative of the load-time history changes from a positive to a negative sign; the point of maximum load in constant-amplitude loading (see Figure 9.3.4.3). Plane Strain.—The stress state in which all strains occur only in the principal loading plane. No strains occur out of the plane, i.e., z = 0, and z  0. Plane Stress.—The stress state in which all stresses occur only in the principal loading plane. No stresses occur out of the plane, i.e., z = 0, and z  0. Plastic Strain During Loading.—Plastic strain during loading is the portion of the strain during loading determined as the offset from the linear portion to the end of a stress-strain curve made during load application. Plane-Strain Fracture Toughness.—A generic term now generally adopted for the critical plane-strain stress intensity factor characteristic of plane-strain fracture, symbolically denoted KIc. This is because in current fracture testing practices, specification of the slowly increasing load test of specimen materials in the plane-strain stress state and in opening mode (I) has been dominant. Plane-Stress and Transitional Fracture Toughness.—A generic term denoting the critical stress intensity factor associated with fracture behavior under nonplane-strain conditions. Because of plasticity effects and stable crack growth which can be encountered prior to fracture under these conditions, designation of a specific value is dependent on the stage of crack growth detected during testing. Residual strength or apparent fracture toughness is a special case of plane-stress and transitional fracture toughness wherein the reference crack length is the initial pre-existing crack length and subsequent crack growth during the test is neglected.

* Different from ASTM. A-11

MIL-HDBK-5H 1 December 1998 Population.—All potential measurements having certain independent characteristics in common; i.e., “all possible TUS(L) measurements for 17-7PH stainless steel sheet in TH1050 condition”. Precision.*—The degree of mutual agreement among individual measurements. Relative to a method of test, precision is the degree of mutual agreement among individual measurements made under prescribed like conditions. The lack of precision in a measurement may be characterized as the standard deviation of the errors in measurement. Primary Creep.—Creep occurring at a diminishing rate, sometimes called initial stage of creep. Probability.—Ratio of possible number of favorable events to total possible number of equally likely events. For example, if a coin is tossed, the probability of heads is one-half (or 50 percent) because heads can occur one way and the total possible events are two, either heads or tails. Similarly, the probability of throwing a three or greater on a die is 4/6 or 66.7 percent. Probability, as related to design allowables, means that chances of a material-property measurement equaling or exceeding a certain value (the onesided lower tolerance limit) is 99 percent in the case of a A-basis value and 90 percent in the case of a Bbasis value. Range.—Range, P, Sr, , r,  is the algebraic difference between successive valley and peak loads (positive range or increasing load range) or between successive peak and valley loads (negative range or decreasing load range), see Figure 9.3.4.3. In constant-amplitude loading, for example, the range is given by P = Pmax - Pmin. Rate of Creep.—The slope of the creep-time curve at a given time determined from a Cartesian plot. Residual.*—The difference between the observed fatigue (log) life and the fatigue (log) life estimated from the fatigue model at a particular stress/strain level. Runout.*—A test that has been terminated prior to failure. Runout tests are usually stopped at an arbitrary life value because of time and economic considerations. NOTE—Runout tests are useful for estimating a pseudo-fatigue-limit for a fatigue data sample. Sample.—A finite number of observations drawn from the population. Sample.—The number of specimens selected from a population for test purposes. NOTE—The method of selecting the sample determines the population about which statistical inferences or generalization can be made. Sample Average (Arithmetic Mean).—The sum of all the observed values in a sample divided by the sample size (number). It is a point estimate of the population mean. Sample Mean.—Average of all observed values in the sample. It is an estimate of population mean. A mean is indicated by a bar over the symbol for the value observed. Thus, the mean of n observations of TUS would be expressed as:
TUS  TUS1  TUS2  ...  TUSn n



1 (TUS ) i
n i

n

* Different from ASTM. A-12

MIL-HDBK-5H 1 December 1998 Sample Median.—Value of the middle-most observation. If the sample is nearly normally distributed, the sample median is also an estimate of the population mean. Sample Median.—The middle value when all observed values in a sample are arranged in order of magnitude if an odd number of samples are tested. If the sample size is even, it is the average of the two middlemost values. It is a point estimate of the population median, or 50 percentile point. Sample Point Deviation.—The difference between an observed value and the sample mean. Sample Standard Deviation.*—The standard deviation of the sample, s, is the square root of the sample variance. It is a point estimate of the standard deviation of a population, a measure of the "spread" of the frequency distribution of a population. NOTE—This value of s provides a statistic that is used in computing interval estimates and several test statistics. Sample Variance.*—Sample variance, s2, is the sum of the squares of the differences between each observed value and the sample average divided by the sample size minus one. It is a point estimate of the population variance. NOTE—This value of s2 provides both an unbiased point estimate of the population variance and a statistic that is used on computing the interval estimates and several test statistics. Some texts define s2 as “the sum of the squared differences between each observed value and the sample average divided by the sample size”, however, this statistic underestimates the population variance, particularly for small sample sizes. Sample Variance.—The sum of the squared deviations, divided by n - 1, and, based on n observations of TUS, expressed as

2 STUS



 TUS  TUS
n i1 i

2

n

n  1



 (TUS )
n i1 i

2



 TUS
n i1

2 i

n(n  1)

S-Basis.—The S-value is the minimum property value specified by the governing industry specification (as issued by standardization groups such as SAE Aerospace Materials Division, ASTM, etc.) or federal or military standards for the material. (See MIL-STD-970 for order of preference for specifications.) For certain products heat treated by the user (for example, steels hardened and tempered to a designated Ftu), the S-value may reflect a specified quality-control requirement. Statistical assurance associated with this value is not known. Secondary Creep.—Creep occurring at a constant rate, sometimes called second stage creep. Short-Transverse Direction.—The transverse direction having the smallest dimension, often called the “thickness” direction. For die forgings this direction is within ±15 of the longitudinal (predominate) grain direction and perpendicular, within ±15, to the parting plane. (Both conditions must be met.) When possible, short transverse specimens shall be taken across the parting plane.

* Different from ASTM. A-13

MIL-HDBK-5H 1 December 1998 Significance Level (As Used Here).—Risk of concluding that two samples were drawn from different populations when, in fact, they were drawn from the same population. A significance level of  = 0.05 is employed through these Guidelines.* Significance Level.—The stated probability (risk) that a given test of significance will reject the hypothesis that a specified effect is absent when the hypothesis is true. Significant (Statistically Significant).—An effect or difference between populations is said to be present if the value of a test statistic is significant, that is, lies outside of predetermined limits. NOTE—An effect that is statistically significant may not have engineering importance. S/N Curve for 50 Percent Survival.**—A curve fitted to the median values of fatigue life at each of several stress levels. It is an estimate of the relationship between applied stress and the number of cycles-to-failure that 50 percent of the population would survive. NOTE 1—This is a special case of the more general definition of S/N curve for P percent survival. NOTE 2—In the literature, the abbreviated term “S/N Curve” usually has meant either the S/N curve drawn through the mean (averages) or through the medians (50 percent values) for the fatigue life values. Since the term “S/N Curve” is ambiguous, it should be used only when described appropriately. NOTE 3—Mean S/N curves (based on log lives) are shown in MIL-HDBK-5. S/N Diagram.—A plot of stress against the number of cycles to failure. The stress can be Smax, Smin, or Sa. The diagram indicates the S/N relationship for a specified value of Sm, A, or R and a specified probability of survival. Typically, for N, a log scale (base 10) is used. Generally, for S, a linear scale is used, but a log scale is used occasionally. NOTE—Smax-versus-log N diagrams are used commonly in MIL-HDBK-5. Standard Deviation.—An estimate of the population standard deviation; the square root of the variance, or

STUS


n i1

TUSi  TUS 2 n  1

n




n i1

TUSi 2 

 TUS
n i1

2 i

n(n  1)

Stress Intensity Factor.—A physical quantity describing the severity of a flaw in the stress field of a loaded structural element. The gross stress in the material and flaw size are characterized parametrically by the stress intensity factor,
K  f a Y, ksi  in.1/2

[9.5.1.2]

Stress-Rupture Test—A stress-rupture test is one in which time for rupture is measured, no deformation measurement being made during the test. Tertiary Creep.—Creep occurring at an accelerating rate, sometimes called third stage creep. Theoretical Stress Concentration Factor (or Stress Concentration Factor).—This factor, Kt, is the ratio of the nominal stress to the greatest stress in the region of a notch (or other stress concentrator) as determined * This is appropriate, since a confidence level of 1 -  = 0.95 is used in establishing A and B-values. ** Different from ASTM. A-14

MIL-HDBK-5H 1 December 1998 by the theory of elasticity (or by experimental procedures that give equivalent values). NOTE—The theory of plasticity should not be used to determine Kt. Tolerance Interval.—An interval computed so that it will include at least a stated percentage of the population with a stated probability. Tolerance Level.—The stated probability that the tolerance interval includes at least the stated percentage of the population. It is not the same as a confidence level, but the term confidence level is frequently associated with tolerance intervals. Tolerance Limits.—The two statistics that define a tolerance interval. (One value may be “minus infinity” or “plus infinity”.) Total Plastic Strain.—Total plastic strain at a specified time is equal to the sum of plastic strain during loading plus creep. Total Strain.—Total strain at any given time, including initial loading strain (which may include plastic strain in addition to elastic strain) and creep strain, but not including thermal expansion. Transition Fatigue Life.*—The point on a strain-life diagram where the elastic and plastic strains are equal. Transverse Direction.—Perpendicular to the principal direction of flow in a worked metal; may be defined as T, LT or ST. Typical Basis.—A typical property value is an average value and has no statistical assurance associated with it. Waveform.—The shape of the peak-to-peak variation of a controlled mechanical test variable (for example, load, strain, displacement) as a function of time.

* Different from ASTM. A-15

MIL-HDBK-5H 1 December 1998

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A-16

MIL-HDBK-5H 1 December 1998

APPENDIX B

	


Alloy Name 250 250 354.0 355.0 356.0 356.0 356.0 359.0 2014 2014 2014 2014 2014 2014 2014 2014 2014 2014 2017 2017 2024 2024 2024 2024 2024 2024 2024 2024 2024 2024 2024 2024 2025 2090 2124 2124 2219 2219 2219 2219 2219 2519 2524 2618 2618 2618 Form Bar Sheet and Plate Casting Permanent Mold Casting Sand Casting Investment Casting Permanent Mold Casting Casting Bare Sheet and Plate Bare Sheet and Plate Bar and Rod, Rolled or Cold Finished Forging Extrusion Forging Extruded Bar, Rod and Shapes Rolled or Drawn Bar, Rod and Shapes Clad Sheet and Plate Forging Bar and Rod, Rolled or Cold-Finished Rolled Bar and Rod Bare Sheet and Plate Bare Sheet and Plate Tubing, Hydraulic, Seamless, Drawn Bar and Rod, Rolled or Cold-Finished Extrusion Extrusion Extrusion Extruded Bar, Rod and Shapes Rolled or Drawn Bar, Rod and Wire Bare Sheet and Plate Clad Sheet and Plate Tubing Die Forging Sheet Plate Plate Sheet and Plate Hand Forging Extrusion Extrusion Sheet and Plate Plate Sheet and Plate Die and Hand Forgings Die Forging Forging Specification AMS 6512 AMS 6520 MIL-A-21180 AMS 4281 AMS 4217 AMS 4260 AMS 4284 MIL-A-21180 AMS 4028 AMS 4029 AMS 4121 AMS 4133 AMS 4153 MIL-A-22771 AMS-QQ-A-200/2 AMS-QQ-A-225/4 AMS-QQ-A-250/3 QQ-A-367 AMS 4118 AMS-QQ-A-225/5 AMS 4035 AMS 4037 AMS 4086 AMS 4120 AMS 4152 AMS 4164 AMS 4165 AMS-QQ-A-200/3 AMS-QQ-A-225/6 AMS-QQ-A-250/4 AMS-QQ-A-250/5 WW-T-700/3 AMS 4130 AMS 4251 AMS 4101 AMS-QQ-A-250/29 AMS 4031 AMS 4144 AMS 4162 AMS 4163 AMS-QQ-A-250/30 MIL-A-46192 AMS 4296 AMS 4132 MIL-A-22771 QQ-A-367 Section 2.5.1 2.5.1 3.9.1 3.9.2 3.9.4 3.9.4 3.9.4 3.9.8 3.2.1 3.2.1 3.2.1 3.2.1 3.2.1 3.2.1 3.2.1 3.2.1 3.2.1 3.2.1 3.2.2 3.2.2 3.2.3 3.2.3 3.2.3 3.2.3 3.2.3 3.2.3 3.2.3 3.2.3 3.2.3 3.2.3 3.2.3 3.2.3 3.2.4 3.2.5 3.2.6 3.2.6 3.2.7 3.2.7 3.2.7 3.2.7 3.2.7 3.2.8 3.2.9 3.2.10 3.2.10 3.2.10

Key: Underline indicates inactive for new design.

B-1

MIL-HDBK-5H 1 December 1998
Alloy Name 4130 4130 4130 4130 4130 4130 4130 4130 4130 4130 4130 4130 4130 4135 4135 4135 4135 4140 4140 4140 4140 4140 4140 4140 4340 4340 4340 4340 4340 4340 4340 4340 4340 5052 5052 5052 5052 5083 5083 5083 5086 5086 5454 5454 5456 5456 6061 6061 6061 6061 6061 6061 6061 6061 6061 Form Bar and Forging Sheet, Strip and Plate Sheet, Strip and Plate Tubing Tubing Bar and Forging Tubing Tubing Tubing Bar and Forging Sheet, Strip and Plate Bar and Forging Tubing Sheet, Strip and Plate Tubing Tubing Tubing Bar and Forging Tubing Bar and Forging Tubing Sheet, Strip and Plate Bar and Forging Bar and Forging Sheet, Strip and Plate Bar and Forging Tubing Bar and Forging Tubing Sheet, Strip and Plate Bar and Forging Tubing Bar and Forging Sheet and Plate Sheet and Plate Sheet and Plate Sheet and Plate Bare Sheet and Plate Extruded Bar, Rod and Shapes Bare Sheet and Plate Extruded Bar, Rod and Shapes Sheet and Plate Extruded Bar, Rod and Shapes Sheet and Plate Extruded Bar, Rod and Shapes Sheet and Plate Sheet and Plate Sheet and Plate Sheet and Plate Tubing Seamless, Drawn Tubing Seamless, Drawn Bar and Rod, Rolled or Cold Finished Bar and Rod, Cold Finished Bar and Rod, Rolled or Cold Finished Forging Specification AMS 6348 AMS 6350 AMS 6351 AMS 6361 AMS 6362 AMS 6370 AMS 6371 AMS 6373 AMS 6374 AMS 6528 MIL-S-18729 MIL-S-6758 MIL-T-6736 AMS 6352 AMS 6365 AMS 6372 MIL-T-6735 AMS 6349 AMS 6381 AMS 6382 AMS 6390 AMS 6395 AMS 6529 MIL-S-5626 AMS 6359 AMS 6414 AMS 6414 AMS 6415 AMS 6415 AMS 6454 MIL-S-5000 MIL-S-8844 MIL-S-8844 AMS 4015 AMS 4016 AMS 4017 AMS-QQ-A-250/8 AMS 4056 AMS-QQ-A-200/4 AMS-QQ-A-250/6 AMS-QQ-A-200/5 AMS-QQ-A-250/7 AMS-QQ-A-200/6 AMS-QQ-A-250/10 AMS-QQ-A-200/7 AMS-QQ-A-250/9 AMS 4025 AMS 4026 AMS 4027 AMS 4080 AMS 4082 AMS 4115 AMS 4116 AMS 4117 AMS 4127 Section 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 3.5.1 3.5.1 3.5.1 3.5.1 3.5.2 3.5.2 3.5.2 3.5.3 3.5.3 3.5.4 3.5.4 3.5.5 3.5.5 3.6.2 3.6.2 3.6.2 3.6.2 3.6.2 3.6.2 3.6.2 3.6.2 3.6.2

Key: Underline indicates inactive for new design.

B-2

MIL-HDBK-5H 1 December 1998
Alloy Name 6061 6061 6061 6061 6061 6061 6061 6061 6061 6061 6061 6151 6151 7010 7010 7050 7050 7050 7050 7050 7050 7050 7050 7050 7075 7075 7075 7075 7075 7075 7075 7075 7075 7075 7075 7075 7075 7075 7075 7075 7075 7075 7150 7150 7150 7150 7175 7175 7175 7175 7175 7249 7475 7475 7475 Form Extrusion Extrusion Extrusion Hand Forging Forging Pipe Extruded Rod, Bar Shapes and Tubing Rolled Bar, Rod and Shapes Sheet and Plate Forging Tubing Seamless, Drawn Die Forging Forging Plate Plate Bare Plate Die Forging Hand Forging Bare Plate Die Forging Extruded Shape Extruded Shape Extruded Shape Forging Bare Sheet and Plate Bare Sheet and Plate Clad Sheet and Plate Bare Plate Bar and Rod, Rolled or Cold Finished Bar and Rod, Rolled or Cold Finished Bar and Rod, Rolled or Cold Finished Forging Die Forging Forging Bar and Rod, Rolled or Cold Finished Bar and Rod, Rolled or Cold Finished Forging Extruded Bar, Rod and Shapes Rolled or Drawn Bar and Rod Bare Sheet and Plate Clad Sheet and Plate Forging Bare Plate Bare Plate Extrusion Extrusion Die Forging Die and Hand Forging Hand Forging Extrusion Forging Hand Forging Bare Sheet Bare Sheet Bare Plate Specification AMS 4160 AMS 4161 AMS 4172 AMS 4248 MIL-A-22771 MIL-P-25995 AMS-QQ-A-200/8 AMS-QQ-A-225/8 AMS-QQ-A-250/11 QQ-A-367 WW-T-700/6 AMS 4125 MIL-A-22771 AMS 4204 AMS 4205 AMS 4050 AMS 4107 AMS 4108 AMS 4201 AMS 4333 AMS 4340 AMS 4341 AMS 4342 MIL-A-22771 AMS 4044 AMS 4045 AMS 4049 AMS 4078 AMS 4122 AMS 4123 AMS 4124 AMS 4126 AMS 4141 AMS 4147 AMS 4186 AMS 4187 MIL-A-22771 AMS-QQ-A-200/11, 15 AMS-QQ-A-225/9 AMS-QQ-A-250/12, 24 AMS-QQ-A-250/13, 25 QQ-A-367 AMS 4252 (T7751) AMS 4306 (T6151) AMS 4307 (T61511) AMS 4345 (T77511) AMS 4148 (T66) AMS 4149 (T74) AMS 4179 (T7452) AMS 4344 (T73511) MIL-A-22771 AMS 4334 AMS 4084 (T61) AMS 4085 (T761) AMS 4089 (T7651) Section 3.6.2 3.6.2 3.6.2 3.6.2 3.6.2 3.6.2 3.6.2 3.6.2 3.6.2 3.6.2 3.6.2 3.6.3 3.6.3 3.7.1 3.7.1 3.7.3 3.7.3 3.7.3 3.7.3 3.7.3 3.7.3 3.7.3 3.7.3 3.7.3 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.4 3.7.5 3.7.5 3.7.5 3.7.5 3.7.6 3.7.6 3.7.6 3.7.6 3.7.6 3.7.7 3.7.8 3.7.8 3.7.8

Key: Underline indicates inactive for new design.

B-3

MIL-HDBK-5H 1 December 1998
Alloy Name 7475 7475 7475 7475 8630 8630 8630 8630 8630 8735 8735 8735 8740 8740 8740 8740 8740 15-5PH 15-5PH 15-5PH 17-4PH 17-4PH 17-4PH 17-4PH 17-4PH 17-7PH 17-7PH 2024-T3 ARAMID Fiber Reinforced 280 (300) 280 (300) 300M (0.42C) 300M (0.42C) 300M (0.42C) 300M (0.42C) 300M (0.4C) 300M (0.4C) 4130 - N 4330V 4330V 4330V 4330V 4335V 4335V 4335V 4335V 4335V 4335V 5Cr-Mo-V 5Cr-Mo-V 5Cr-Mo-V 6013-T4 6013-T6 7049/7149 7049/7149 7049/7149 Form Bare Plate Clad Sheet Bare Plate Clad Sheet Bar and Forging Tubing Sheet, Strip and Plate Sheet, Strip and Plate Bar and Forging Tubing Bar and Forging Sheet, Strip and Plate Bar and Forging Tubing Bar and Forging Sheet, Strip and Plate Bar and Forging Investment Casting Bar, Forging, Ring and Extrusion (CEVM) Sheet, Strip and Plate (CEVM) Investment Casting (H1100) Investment Casting (H1000) Investment Casting (H900) Sheet, Strip and Plate Bar, Forging and Ring Plate, Sheet and Strip Plate, Sheet and Strip Sheet Laminate Bar Sheet and Plate Bar and Forging Tubing Bar and Forging Tubing Bar and Forging Tubing Tubing Bar and Forging Tubing Bar and Forging Tubing Bar and Forging Tubing Bar and Forging Tubing Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Bar and Forging (CEVM) Bar and Forging Sheet Sheet Forging Extrusion Plate Specification AMS 4090 (T651) AMS 4100 (T761) AMS 4202 (T7351) AMS 4207 (T61) AMS 6280 AMS 6281 AMS 6355 MIL-S-18728 MIL-S-6050 AMS 6282 AMS 6320 AMS 6357 AMS 6322 AMS 6323 AMS 6327 AMS 6358 MIL-S-6049 AMS 5400 AMS 5659 AMS 5862 AMS 5342 AMS 5343 AMS 5344 AMS 5604 AMS 5643 AMS 5528 MIL-S-25043 AMS 4254 AMS 6514 AMS 6521 AMS 6257 AMS 6257 AMS 6419 AMS 6419 AMS 6417 AMS 6417 AMS 6360 AMS 6411 AMS 6411 AMS 6427 AMS 6427 AMS 6429 AMS 6429 AMS 6430 AMS 6430 AMS 6433 AMS 6435 AMS 6437 AMS 6487 AMS 6488 AMS 4216 AMS 4347 AMS 4111 AMS 4157 AMS 4200 Section 3.7.8 3.7.8 3.7.8 3.7.8 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.6.6 2.6.6 2.6.6 2.6.8 2.6.8 2.6.8 2.6.8 2.6.8 2.6.9 2.6.9 7.5.1 2.5.1 2.5.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.4.1 2.4.1 2.4.1 3.6.1 3.6.1 3.7.2 3.7.2 3.7.2

Key: Underline indicates inactive for new design.

B-4

MIL-HDBK-5H 1 December 1998
Alloy Name 7049/7149 7049/7149 7049/7149 7049/7149 7475-T761 ARAMID Fiber Reinforced 9Ni-4Co-0.20C 9Ni-4Co-0.20C 9Ni-4Co-0.20C A201.0 A-286 A-286 A-286 A-286 A-286 A356.0 A356.0 A357.0 AerMet 100 AerMet 100 AF1410 AISI 1025 AISI 1025 AISI 1025 AISI 1025 AISI 1025 - N AISI 1025 - N AISI 301 AISI 301 AISI 301 AISI 301 Alloy 188 Alloy 188 AM100A AM100A AM100A AM-350 AM-355 AM-355 AM-355 AZ31B AZ31B AZ31B AZ31B AZ31B AZ61A AZ61A AZ91C/AZ91E AZ91C/AZ91E AZ91C/AZ91E AZ91C/AZ91E AZ92A AZ92A AZ92A C355.0 Copper Beryllium Form Forging Extrusion Forging Forging Sheet Laminate Sheet, Strip and Plate Sheet, Strip and Plate Bar and Forging, Tubing Casting (T7 Temper) Sheet, Strip and Plate Bar, Forging, Tubing and Ring Bar, Forging, Tubing and Ring Bar, Forging and Tubing Bar, Forging and Tubing Casting Casting Casting Bar and Forging Bar and Forging Bar and Forging Sheet, Strip, and Plate Bar Sheet and Strip Tubing Seamless Tubing Tubing Sheet and Strip Sheet and Strip Sheet and Strip Plate, Sheet and Strip Sheet and Plate Bar and Forging Investment Casting Permanent Mold Casting Casting Sheet and Strip Sheet and Strip Plate Bar, Forging and Forging Stock Sheet and Plate Plate Sheet and Plate Forging Extrusion Extrusion Forging Sand Casting Sand Casting Investment Casting Casting Sand Casting Permanent Mold Casting Casting Casting Strip (TB00) Specification AMS 4320 AMS 4343 MIL-A-22771 QQ-A-367 AMS 4302 AMS 6523 AMS 6524 AMS 6526 MIL-A-21180 AMS 5525 AMS 5731 AMS 5732 AMS 5734 AMS 5737 AMS 4218 MIL-A-21180 MIL-A-21180 AMS 6478 AMS 6532 AMS 6527 AMS 5046 MIL-S-7079, Comp. 3 MIL-S-7952 MIL-T-5066 AMS 5075 AMS 5077 AMS 5517 AMS 5518 AMS 5519 MIL-S-5059 AMS 5608 AMS 5772 AMS 4455 AMS 4483 MIL-M-46062 AMS 5548 AMS 5547 AMS 5549 AMS 5743 AMS 4375 AMS 4376 AMS 4377 ASTM B 91 ASTM B 107 AMS 4350 ASTM B 91 AMS 4437 AMS 4446 AMS 4452 MIL-M-46062 AMS 4434 AMS 4484 MIL-M-46062 MIL-A-21180 AMS 4530 Section 3.7.2 3.7.2 3.7.2 3.7.2 7.5.2 2.4.2 2.4.3 2.4.3 3.8.1 6.2.1 6.2.1 6.2.1 6.2.1 6.2.1 3.9.5 3.9.5 3.9.6 2.5.3 2.5.3 2.5.2 2.2.1 2.2.1 2.2.1 2.2.1 2.2.1 2.2.1 2.7.1 2.7.1 2.7.1 2.7.1 6.4.2 6.4.2 4.3.1 4.3.1 4.3.1 2.6.1 2.6.2 2.6.2 2.6.2 4.2.1 4.2.1 4.2.1 4.2.1 4.2.1 4.2.2 4.2.2 4.3.2 4.3.2 4.3.2 4.3.2 4.3.3 4.3.3 4.3.3 3.9.3 7.3.2

Key: Underline indicates inactive for new design.

B-5

MIL-HDBK-5H 1 December 1998
Alloy Name Copper Beryllium Copper Beryllium Copper Beryllium Copper Beryllium Copper Beryllium Copper Beryllium Copper Beryllium CP Titanium CP Titanium CP Titanium CP Titanium CP Titanium CP Titanium CP Titanium Custom 450 Custom 450 Custom 455 Custom 455 D357.0 D6AC D6AC D6AC D6AC EZ33A Hastelloy X Hastelloy X Hy-Tuf Hy-Tuf Hy-Tuf Hy-Tuf Inconel 718 Inconel 718 Inconel 718 Inconel 718 Inconel 718 Inconel 718 Inconel 718 Inconel 718 Inconel Alloy 600 Inconel Alloy 600 Inconel Alloy 600 Inconel Alloy 600 Inconel Alloy 625 Inconel Alloy 625 Inconel Alloy 706 Inconel Alloy 706 Inconel Alloy 706 Inconel Alloy 706 Inconel Alloy 706 Inconel Alloy X-750 Inconel Alloy X-750 L-605 L-605 Manganese Bronzes Manganese Bronzes Form Strip (TD02) Bar and Rod (TF00) Bar and Rod (TH04) Mechanical tubing (TF00) Bar, Rod, Shapes and Forging (TB00) Bar and Rod (TD04) Sheet (TB00, TD01, TD02, TD04) Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Bar Extruded Bars and Shapes Sheet, Strip and Plate Bar Bar, Forging, Tubing, Wire and Ring (air melted) Bar, Forging, Tubing, Wire and Ring (CEM) Tubing (welded) Bar and Forging Sand Composite Casting Bar and Forging Tubing Bar and Forging Sheet, Strip and Plate Sand Casting Sheet and Plate Bar and Forging Bar and Forging Tubing Bar and Forging Tubing Investment Casting Tubing; Creep Rupture Tubing; Short-Time Sheet, Strip and Plate; Creep Rupture Sheet, Strip and Plate; Short-Time Bar and Forging; Creep Rupture Bar and Forging; Creep Rupture Bar and Forging; Short-Time Plate, Sheet and Strip Tubing, Seamless Bar and Rod Forging Sheet, Strip and Plate Bar, Forging and Ring Sheet, Strip and Plate Sheet, Strip and Plate Bar, Forging and Ring Bar, Forging and Ring Bar, Forging and Ring Sheet, Strip and Plate; Annealed Bar and Forging; Equalized Sheet Bar and Forging Casting Casting Specification AMS 4532 AMS 4533 AMS 4534 AMS 4535 AMS 4650 AMS 4651 ASTM B 194 AMS 4900 AMS 4901 AMS 4902 AMS 4921 MIL-T-81556 MIL-T-9046 MIL-T-9047 AMS 5763 AMS 5773 AMS 5578 AMS 5617 AMS 4241 AMS 6431 AMS 6431 MIL-S-8949 MIL-S-8949 AMS 4442 AMS 5536 AMS 5754 AMS 6418 AMS 6418 AMS 6425 AMS 6425 AMS 5383 AMS 5589 AMS 5590 AMS 5596 AMS 5597 AMS 5662 AMS 5663 AMS 5664 AMS 5540 AMS 5580 ASTM B 166 ASTM B 564 AMS 5599 AMS 5666 AMS 5605 AMS 5606 AMS 5701 AMS 5702 AMS 5703 AMS 5542 AMS 5667 AMS 5537 AMS 5759 AMS 4860 AMS 4862 Section 7.3.2 7.3.2 7.3.2 7.3.2 7.3.2 7.3.2 7.3.2 5.2.1 5.2.1 5.2.1 5.2.1 5.2.1 5.2.1 5.2.1 2.6.3 2.6.3 2.6.4 2.6.4 3.9.7 2.3.1 2.3.1 2.3.1 2.3.1 4.3.4 6.3.1 6.3.1 2.3.1 2.3.1 2.3.1 2.3.1 6.3.5 6.3.5 6.3.5 6.3.5 6.3.5 6.3.5 6.3.5 6.3.5 6.3.2 6.3.2 6.3.2 6.3.2 6.3.3 6.3.3 6.3.4 6.3.4 6.3.4 6.3.4 6.3.4 6.3.6 6.3.6 6.4.1 6.4.1 7.3.1 7.3.1

Key: Underline indicates inactive for new design.

B-6

MIL-HDBK-5H 1 December 1998
Alloy Name MP159 Alloy MP159 Alloy MP35N Alloy MP35N Alloy N-155 N-155 N-155 N-155 PH13-8Mo PH15-7Mo QE22A Magnesium QE22A Magnesium René 41 René 41 René 41 - STA Standard Grade Beryllium Standard Grade Beryllium Ti-10V-2Fe-3Al (Ti-10-2-3) Ti-10V-2Fe-3Al (Ti-10-2-3) Ti-10V-2Fe-3Al (Ti-10-2-3) Ti-13V-11Cr-3Al Ti-13V-11Cr-3Al Ti-15V-3Cr-3Sn-3Al (Ti-15-3-3-3) Ti-5Al-2.5Sn Ti-5Al-2.5Sn Ti-5Al-2.5Sn Ti-5Al-2.5Sn Ti-5Al-2.5Sn Ti-5Al-2.5Sn Ti-6Al-2Sn-4Zr-2Mo Ti-6Al-2Sn-4Zr-2Mo Ti-6Al-2Sn-4Zr-2Mo Ti-6Al-2Sn-4Zr-2Mo Ti-6Al-4V Ti-6Al-4V Ti-6Al-4V Ti-6Al-4V Ti-6Al-4V Ti-6Al-4V Ti-6Al-4V Ti-6Al-4V Ti-6Al-4V Ti6Al-6V-2Sn Ti6Al-6V-2Sn Ti6Al-6V-2Sn Ti6Al-6V-2Sn Ti6Al-6V-2Sn Ti6Al-6V-2Sn Ti-8Al-1Mo-1V Ti-8Al-1Mo-1V Ti-8Al-1Mo-1V Ti-8Al-1Mo-1V Ti-8Al-1Mo-1V Waspaloy Waspaloy Form Bar (solution treated and cold drawn) Bar (solution treated, cold drawn and aged) Bar (solution treated and cold drawn) Bar (solution treated, cold drawn and aged) Sheet Tubing (welded) Bar and Forging Bar and Forging Bar, Forging Ring and Extrusion (VIM+CEVM) Plate, Sheet and Strip Sand Casting Sand Casting Plate, Sheet and Strip Bar and Forging Bar and Forging Sheet and Plate Bar, Rod, Tubing and Machined Shapes Forging Forging Forging Sheet, Strip and Plate Bar Sheet and Strip Sheet, Strip and Plate Bar Forging Extruded Bar and Shapes Sheet, Strip and Plate Bar Sheet, Strip and Plate Bar Forging Sheet and Strip Sheet, Strip and Plate Die Forging Bar and Die Forging Extrusion Extrusion Casting Bar Sheet, Strip and Plate Bar Sheet, Strip and Plate Bar and Forging Bar and Forging Bar and Forging Extruded Bar and Shapes Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Forging Sheet, Strip and Plate Bar Plate, Sheet and Strip Forging Specification AMS 5842 AMS 5843 AMS 5844 AMS 5845 AMS 5532 AMS 5585 AMS 5768 AMS 5769 AMS 5629 AMS 5520 AMS 4418 MIL-M-46062 AMS 5545 AMS 5713 AMS 5712 AMS 7902 AMS 7906 AMS 4983 AMS 4984 AMS 4986 MIL-T-9046 MIL-T-9047 AMS 4914 AMS 4910 AMS 4926 AMS 4966 MIL-T-81556 MIL-T-9046 MIL-T-9047 AMS 4919 AMS 4975 AMS 4976 MIL-T-9046 AMS 4911 AMS 4920 AMS 4928 AMS 4934 AMS 4935 AMS 4962 AMS 4967 MIL-T-9046 MIL-T-9047 AMS 4918 AMS 4971 AMS 4978 AMS 4979 MIL-T-81556 MIL-T-9046 AMS 4915 AMS 4916 AMS 4973 MIL-T-9046 MIL-T-9047 AMS 5544 AMS 5704 Section 7.4.2 7.4.2 7.4.1 7.4.1 6.2.2 6.2.2 6.2.2 6.2.2 2.6.5 2.6.7 4.3.5 4.3.5 6.3.7 6.3.7 6.3.7 7.2.1 7.2.1 5.5.3 5.5.3 5.5.3 5.5.1 5.5.1 5.5.2 5.3.1 5.3.1 5.3.1 5.3.1 5.3.1 5.3.1 5.3.3 5.3.3 5.3.3 5.3.3 5.4.1 5.4.1 5.4.1 5.4.1 5.4.1 5.4.1 5.4.1 5.4.1 5.4.1 5.4.2 5.4.2 5.4.2 5.4.2 5.4.2 5.4.2 5.3.2 5.3.2 5.3.2 5.3.2 5.3.2 6.3.8 6.3.8

Key: Underline indicates inactive for new design.

B-7

MIL-HDBK-5H 1 December 1998
Alloy Name Waspaloy Waspaloy Waspaloy Waspaloy ZE41A Magnesium ZK60A-F ZK60A-T5 ZK60A-T5 Form Bar, Forgings and Ring Bar, Forgings and Ring Bar, Forgings and Ring Bar, Forgings and Ring Sand Casting Extrusion Extrusion Die and Hand Forging Specification AMS 5706 AMS 5707 AMS 5708 AMS 5709 AMS 4439 ASTM B 107 AMS 4352 AMS 4362 Section 6.3.8 6.3.8 6.3.8 6.3.8 4.3.6 4.2.3 4.2.3 4.2.3

Key: Underline indicates inactive for new design.

B-8

MIL-HDBK-5H 1 December 1998

APPENDIX C

	
		

Specification AMS 4015 AMS 4016 AMS 4017 AMS 4025 AMS 4026 AMS 4027 AMS 4028 AMS 4029 AMS 4031 AMS 4035 AMS 4037 AMS 4044 AMS 4045 AMS 4049 AMS 4050 AMS 4056 AMS 4078 AMS 4080 AMS 4082 AMS 4084 (T61) AMS 4085 (T761) AMS 4086 AMS 4089 (T7651) AMS 4090 (T651) AMS 4100 (T761) AMS 4101 AMS 4107 AMS 4108 AMS 4111 AMS 4115 AMS 4116 AMS 4117 AMS 4118 AMS 4120 AMS 4121 AMS 4122 AMS 4123 AMS 4124 AMS 4125 AMS 4126 AMS 4127 AMS 4130 AMS 4132 AMS 4133 Alloy Name 5052 5052 5052 6061 6061 6061 2014 2014 2219 2024 2024 7075 7075 7075 7050 5083 7075 6061 6061 7475 7475 2024 7475 7475 7475 2124 7050 7050 7049/7149 6061 6061 6061 2017 2024 2014 7075 7075 7075 6151 7075 6061 2025 2618 2014 Form/Application Sheet and Plate Sheet and Plate Sheet and Plate Sheet and Plate Sheet and Plate Sheet and Plate Bare Sheet and Plate Bare Sheet and Plate Sheet and Plate Bare Sheet and Plate Bare Sheet and Plate Bare Sheet and Plate Bare Sheet and Plate Clad Sheet and Plate Bare Plate Bare Sheet and Plate Bare Plate Tubing Seamless, Drawn Tubing Seamless, Drawn Bare Sheet Bare Sheet Tubing, Hydraulic, Seamless, Drawn Bare Plate Bare Plate Clad Sheet Plate Die Forging Hand Forging Forging Bar and Rod, Rolled or Cold Finished Bar and Rod, Cold Finished Bar and Rod, Rolled or Cold Finished Bar and Rod, Rolled or Cold-Finished Bar and Rod, Rolled or Cold-Finished Bar and Rod, Rolled or Cold Finished Bar and Rod, Rolled or Cold Finished Bar and Rod, Rolled or Cold Finished Bar and Rod, Rolled or Cold Finished Die Forging Forging Forging Die Forging Die and Hand Forgings Forging Section 3.5.1 3.5.1 3.5.1 3.6.2 3.6.2 3.6.2 3.2.1 3.2.1 3.2.7 3.2.3 3.2.3 3.7.4 3.7.4 3.7.4 3.7.3 3.5.2 3.7.4 3.6.2 3.6.2 3.7.8 3.7.8 3.2.3 3.7.8 3.7.8 3.7.8 3.2.6 3.7.3 3.7.3 3.7.2 3.6.2 3.6.2 3.6.2 3.2.2 3.2.3 3.2.1 3.7.4 3.7.4 3.7.4 3.6.3 3.7.4 3.6.2 3.2.4 3.2.10 3.2.1

Key: Underline indicates inactive for new design.

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MIL-HDBK-5H 1 December 1998
Specification AMS 4141 AMS 4144 AMS 4147 AMS 4148 (T66) AMS 4149 (T74) AMS 4152 AMS 4153 AMS 4157 AMS 4160 AMS 4161 AMS 4162 AMS 4163 AMS 4164 AMS 4165 AMS 4172 AMS 4179 (T7452) AMS 4186 AMS 4187 AMS 4200 AMS 4201 AMS 4202 (T7351) AMS 4204 AMS 4205 AMS 4207 (T61) AMS 4216 AMS 4217 AMS 4218 AMS 4241 AMS 4248 AMS 4251 AMS 4252 (T7751) AMS 4254 AMS 4260 AMS 4281 AMS 4284 AMS 4296 AMS 4302 AMS 4306 (T6151) AMS 4307 (T61511) AMS 4320 AMS 4333 AMS 4334 AMS 4340 AMS 4341 AMS 4342 AMS 4343 AMS 4344 (T73511) AMS 4345 (T77511) AMS 4347 AMS 4350 AMS 4352 AMS 4362 AMS 4375 AMS 4376 Alloy Name 7075 2219 7075 7175 7175 2024 2014 7049/7149 6061 6061 2219 2219 2024 2024 6061 7175 7075 7075 7049/7149 7050 7475 7010 7010 7475 6013 (T4) 356.0 A356.0 D357.0 6061 2090 7150 2024-T3 ARAMID Fiber Reinforced 356.0 355.0 356.0 2524-T3 7475-T761 ARAMID Fiber Reinforced 7150 7150 7049/7149 7050 7249 7050 7050 7050 7049/7149 7175 7150 6013 (T6) AZ61A ZK60A-T5 ZK60A-T5 AZ31B AZ31B Form/Application Die Forging Hand Forging Forging Die Forging Die and Hand Forging Extrusion Extrusion Extrusion Extrusion Extrusion Extrusion Extrusion Extrusion Extrusion Extrusion Hand Forging Bar and Rod, Rolled or Cold Finished Bar and Rod, Rolled or Cold Finished Plate Bare Plate Bare Plate Plate Plate Clad Sheet Sheet Sand Casting Casting Sand Composite Casting Hand Forging Sheet Bare Plate Sheet Laminate Investment Casting Permanent Mold Casting Permanent Mold Casting Sheet and Plate Sheet Laminate Bare Plate Extrusion Forging Die Forging Hand Forging Extruded Shape Extruded Shape Extruded Shape Extrusion Extrusion Extrusion Sheet Extrusion Extrusion Die and Hand Forging Sheet and Plate Plate Section 3.7.4 3.2.7 3.7.4 3.7.6 3.7.6 3.2.3 3.2.1 3.7.2 3.6.2 3.6.2 3.2.7 3.2.7 3.2.3 3.2.3 3.6.2 3.7.6 3.7.4 3.7.4 3.7.2 3.7.3 3.7.8 3.7.1 3.7.1 3.7.8 3.6.1 3.9.4 3.9.5 3.9.7 3.6.2 3.2.5 3.7.5 7.5.1 3.9.4 3.9.2 3.9.4 3.2.9 7.5.2 3.7.5 3.7.5 3.7.2 3.7.3 3.7.7 3.7.3 3.7.3 3.7.3 3.7.2 3.7.6 3.7.5 3.6.1 4.2.2 4.2.3 4.2.3 4.2.1 4.2.1

Key: Underline indicates inactive for new design.

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MIL-HDBK-5H 1 December 1998
Specification AMS 4377 AMS 4418 AMS 4434 AMS 4437 AMS 4439 AMS 4442 AMS 4446 AMS 4452 AMS 4455 AMS 4483 AMS 4484 AMS 4530 AMS 4532 AMS 4533 AMS 4534 AMS 4535 AMS 4650 AMS 4651 AMS 4860 AMS 4862 AMS 4900 AMS 4901 AMS 4902 AMS 4910 AMS 4911 AMS 4914 AMS 4915 AMS 4916 AMS 4918 AMS 4919 AMS 4920 AMS 4921 AMS 4926 AMS 4928 AMS 4934 AMS 4935 AMS 4962 AMS 4966 AMS 4967 AMS 4971 AMS 4973 AMS 4975 AMS 4976 AMS 4978 AMS 4979 AMS 4983 AMS 4984 AMS 4986 AMS 5046 AMS 5075 AMS 5077 AMS 5342 AMS 5343 AMS 5344 AMS 5383 Alloy Name AZ31B QE22A Magnesium AZ92A AZ91C/AZ91E ZE41A Magnesium EZ33A AZ91C/AZ91E AZ91C/AZ91E AM100A AM100A AZ92A Copper Beryllium Copper Beryllium Copper Beryllium Copper Beryllium Copper Beryllium Copper Beryllium Copper Beryllium Manganese Bronzes Manganese Bronzes CP Titanium CP Titanium CP Titanium Ti-5Al-2.5Sn Ti-6Al-4V Ti-15V-3Cr-3Sn-3Al (Ti-15-3)-3-3 Ti-8Al-1Mo-1V Ti-8Al-1Mo-1V Ti6Al-6V-2Sn Ti-6Al-2Sn-4Zr-2Mo Ti-6Al-4V CP Titanium Ti-5Al-2.5Sn Ti-6Al-4V Ti-6Al-4V Ti-6Al-4V Ti-6Al-4V Ti-5Al-2.5Sn Ti-6Al-4V Ti6Al-6V-2Sn Ti-8Al-1Mo-1V Ti-6Al-2Sn-4Zr-2Mo Ti-6Al-2Sn-4Zr-2Mo Ti6Al-6V-2Sn Ti6Al-6V-2Sn Ti-10V-2Fe-3Al (Ti-10-2-3) Ti-10V-2Fe-3Al (Ti-10-2-3) Ti-10V-2Fe-3Al (Ti-10-2-3) AISI 1025 AISI 1025 - N AISI 1025 - N 17-4PH 17-4PH 17-4PH Inconel 718 Form/Application Sheet and Plate Sand Casting Sand Casting Sand Casting Sand Casting Sand Casting Sand Casting Investment Casting Investment Casting Permanent Mold Casting Permanent Mold Casting Strip (TB00) Strip (TD02) Bar and Rod (TF00) Bar and Rod (TH04) Mechanical tubing (TF00) Bar, Rod, Shapes and Forging (TB00) Bar and Rod (TD04) Casting Casting Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Sheet and Strip Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Die Forging Bar Bar Bar and Die Forging Extrusion Extrusion Casting Forging Bar Bar and Forging Forging Bar Forging Bar and Forging Bar and Forging Forging Forging Forging Sheet, Strip, and Plate Seamless Tubing Tubing Investment Casting (H1100) Investment Casting (H1000) Investment Casting (H900) Investment Casting Section 4.2.1 4.3.5 4.3.3 4.3.2 4.3.6 4.3.4 4.3.2 4.3.2 4.3.1 4.3.1 4.3.3 7.3.2 7.3.2 7.3.2 7.3.2 7.3.2 7.3.2 7.3.2 7.3.1 7.3.1 5.2.1 5.2.1 5.2.1 5.3.1 5.4.1 5.5.2 5.3.2 5.3.2 5.4.2 5.3.3 5.4.1 5.2.1 5.3.1 5.4.1 5.4.1 5.4.1 5.4.1 5.3.1 5.4.1 5.4.2 5.3.2 5.3.3 5.3.3 5.4.2 5.4.2 5.5.3 5.5.3 5.5.3 2.2.1 2.2.1 2.2.1 2.6.8 2.6.8 2.6.8 6.3.5

Key: Underline indicates inactive for new design.

C-3

MIL-HDBK-5H 1 December 1998
Specification AMS 5400 AMS 5517 AMS 5518 AMS 5519 AMS 5520 AMS 5525 AMS 5528 AMS 5532 AMS 5536 AMS 5537 AMS 5540 AMS 5542 AMS 5544 AMS 5545 AMS 5547 AMS 5548 AMS 5549 AMS 5578 AMS 5580 AMS 5585 AMS 5589 AMS 5590 AMS 5596 AMS 5597 AMS 5599 AMS 5604 AMS 5605 AMS 5606 AMS 5608 AMS 5617 AMS 5629 AMS 5643 AMS 5659 AMS 5662 AMS 5663 AMS 5664 AMS 5666 AMS 5667 AMS 5701 AMS 5702 AMS 5703 AMS 5704 AMS 5706 AMS 5707 AMS 5708 AMS 5709 AMS 5712 AMS 5713 AMS 5731 AMS 5732 AMS 5734 AMS 5737 AMS 5743 AMS 5754 AMS 5759 Alloy Name 15-5PH AISI 301 AISI 301 AISI 301 PH15-7Mo A-286 17-7PH N-155 Hastelloy X L-605 Inconel Alloy 600 Inconel Alloy X-750 Waspaloy René 41 AM-355 AM-350 AM-355 Custom 455 Inconel Alloy 600 N-155 Inconel 718 Inconel 718 Inconel 718 Inconel 718 Inconel Alloy 625 17-4PH Inconel Alloy 706 Inconel Alloy 706 Alloy 188 Custom 455 PH13-8Mo 17-4PH 15-5PH Inconel 718 Inconel 718 Inconel 718 Inconel Alloy 625 Inconel Alloy X-750 Inconel Alloy 706 Inconel Alloy 706 Inconel Alloy 706 Waspaloy Waspaloy Waspaloy Waspaloy Waspaloy René 41 - STA René 41 A-286 A-286 A-286 A-286 AM-355 Hastelloy X L-605 Form/Application Investment Casting Sheet and Strip Sheet and Strip Sheet and Strip Plate, Sheet and Strip Sheet, Strip and Plate Plate, Sheet and Strip Sheet Sheet and Plate Sheet Plate, Sheet and Strip Sheet, Strip and Plate; Annealed Plate, Sheet and Strip Plate, Sheet and Strip Sheet and Strip Sheet and Strip Plate Tubing (welded) Tubing, Seamless Tubing (welded) Tubing; Creep Rupture Tubing; Short-Time Sheet, Strip and Plate; Creep Rupture Sheet, Strip and Plate; Short-Time Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Sheet and Plate Bar and Forging Bar, Forging Ring and Extrusion (VIM+CEVM) Bar, Forging and Ring Bar, Forging, Ring and Extrusion (CEVM) Bar and Forging; Creep Rupture Bar and Forging; Creep Rupture Bar and Forging; Short-Time Bar, Forging and Ring Bar and Forging; Equalized Bar, Forging and Ring Bar, Forging and Ring Bar, Forging and Ring Forging Bar, Forgings and Ring Bar, Forgings and Ring Bar, Forgings and Ring Bar, Forgings and Ring Bar and Forging Bar and Forging Bar, Forging, Tubing and Ring Bar, Forging, Tubing and Ring Bar, Forging and Tubing Bar, Forging and Tubing Bar, Forging and Forging Stock Bar and Forging Bar and Forging Section 2.6.6 2.7.1 2.7.1 2.7.1 2.6.7 6.2.1 2.6.9 6.2.2 6.3.1 6.4.1 6.3.2 6.3.6 6.3.8 6.3.7 2.6.2 2.6.1 2.6.2 2.6.4 6.3.2 6.2.2 6.3.5 6.3.5 6.3.5 6.3.5 6.3.3 2.6.8 6.3.4 6.3.4 6.4.2 2.6.4 2.6.5 2.6.8 2.6.6 6.3.5 6.3.5 6.3.5 6.3.3 6.3.6 6.3.4 6.3.4 6.3.4 6.3.8 6.3.8 6.3.8 6.3.8 6.3.8 6.3.7 6.3.7 6.2.1 6.2.1 6.2.1 6.2.1 2.6.2 6.3.1 6.4.1

Key: Underline indicates inactive for new design.

C-4

MIL-HDBK-5H 1 December 1998
Specification AMS 5763 AMS 5768 AMS 5769 AMS 5772 AMS 5773 AMS 5842 AMS 5843 AMS 5844 AMS 5845 AMS 5862 AMS 6257 AMS 6257 AMS 6280 AMS 6281 AMS 6282 AMS 6320 AMS 6322 AMS 6323 AMS 6327 AMS 6348 AMS 6349 AMS 6350 AMS 6351 AMS 6352 AMS 6355 AMS 6357 AMS 6358 AMS 6359 AMS 6360 AMS 6361 AMS 6362 AMS 6365 AMS 6370 AMS 6371 AMS 6372 AMS 6373 AMS 6374 AMS 6381 AMS 6382 AMS 6390 AMS 6395 AMS 6411 AMS 6411 AMS 6414 AMS 6414 AMS 6415 AMS 6415 AMS 6417 AMS 6417 AMS 6418 AMS 6418 AMS 6419 AMS 6419 AMS 6425 AMS 6425 Alloy Name Custom 450 N-155 N-155 Alloy 188 Custom 450 MP159 Alloy MP159 Alloy MP35N Alloy MP35N Alloy 15-5PH 300M (0.42C) 300M (0.42C) 8630 8630 8735 8735 8740 8740 8740 4130 4140 4130 4130 4135 8630 8735 8740 4340 4130 - N 4130 4130 4135 4130 4130 4135 4130 4130 4140 4140 4140 4140 4330V 4330V 4340 4340 4340 4340 300M (0.4C) 300M (0.4C) Hy-Tuf Hy-Tuf 300M (0.42C) 300M (0.42C) Hy-Tuf Hy-Tuf Form/Application Bar, Forging, Tubing, Wire and Ring (air melted) Bar and Forging Bar and Forging Bar and Forging Bar, Forging, Tubing, Wire and Ring (CEM) Bar (solution treated and cold drawn) Bar (solution treated, cold drawn and aged) Bar (solution treated and cold drawn) Bar (solution treated, cold drawn and aged) Sheet, Strip and Plate (CEVM) Bar and Forging Tubing Bar and Forging Tubing Tubing Bar and Forging Bar and Forging Tubing Bar and Forging Bar and Forging Bar and Forging Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Tubing (normalized) Tubing Tubing Tubing Bar and Forging Tubing Tubing Tubing Tubing Tubing Bar and Forging Tubing Sheet, Strip and Plate Bar and Forging Tubing Bar and Forging Tubing Bar and Forging Tubing Bar and Forging Tubing Bar and Forging Tubing Bar and Forging Tubing Bar and Forging Tubing Section 2.6.3 6.2.2 6.2.2 6.4.2 2.6.3 7.4.2 7.4.2 7.4.1 7.4.1 2.6.6 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1

Key: Underline indicates inactive for new design.

C-5

MIL-HDBK-5H 1 December 1998
Specification AMS 6427 AMS 6427 AMS 6429 AMS 6429 AMS 6430 AMS 6430 AMS 6431 AMS 6431 AMS 6433 AMS 6435 AMS 6437 AMS 6454 AMS 6478 AMS 6487 AMS 6488 AMS 6512 AMS 6514 AMS 6520 AMS 6521 AMS 6523 AMS 6524 AMS 6526 AMS 6527 AMS 6528 AMS 6529 AMS 6532 AMS 7902 AMS 7906 AMS-QQ-A-200/2 AMS-QQ-A-200/3 AMS-QQ-A-200/4 AMS-QQ-A-200/5 AMS-QQ-A-200/6 AMS-QQ-A-200/7 AMS-QQ-A-200/8 AMS-QQ-A-200/11, 15 AMS-QQ-A-225/4 AMS-QQ-A-225/5 AMS-QQ-A-225/6 AMS-QQ-A-225/8 AMS-QQ-A-225/9 AMS-QQ-A-250/3 AMS-QQ-A-250/4 AMS-QQ-A-250/5 AMS-QQ-A-250/6 AMS-QQ-A-250/7 AMS-QQ-A-250/8 AMS-QQ-A-250/9 AMS-QQ-A-250/10 AMS-QQ-A-250/11 AMS-QQ-A-250/12, 24 AMS-QQ-A-250/13, 25 AMS-QQ-A-250/29 AMS-QQ-A-250/30 ASTM B 91 Alloy Name 4330V 4330V 4335V 4335V 4335V 4335V D6AC D6AC 4335V 4335V 5Cr-Mo-V 4340 AerMet 100 5Cr-Mo-V 5Cr-Mo-V 250 280 (300) 250 280 (300) 9Ni-4Co-0.20C 9Ni-4Co-0.20C 9Ni-4Co-0.20C AF1410 4130 4140 AerMet 100 Standard Grade Beryllium Standard Grade Beryllium 2014 2024 5083 5086 5454 5456 6061 7075 2014 2017 2024 6061 7075 2014 2024 2024 5083 5086 5052 5456 5454 6061 7075 7075 2124 2219 AZ31B Form/Application Bar and Forging Tubing Bar and Forging Tubing Bar and Forging Tubing Bar and Forging Tubing Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Bar and Forging Bar and Forging (CEVM) Bar and Forging Bar Bar Sheet and Plate Sheet and Plate Sheet, Strip and Plate Sheet, Strip and Plate Bar and Forging, Tubing Bar and Forging Bar and Forging Bar and Forging Bar and Forging Sheet and Plate Bar, Rod, Tubing and Machined Shapes Extruded Bar, Rod and Shapes Extruded Bar, Rod and Shapes Extruded Bar, Rod and Shapes Extruded Bar, Rod and Shapes Extruded Bar, Rod and Shapes Extruded Bar, Rod and Shapes Extruded Rod, Bar Shapes and Tubing Extruded Bar, Rod and Shapes Rolled or Drawn Bar, Rod and Shapes Rolled Bar and Rod Rolled or Drawn Bar, Rod and Wire Rolled Bar, Rod and Shapes Rolled or Drawn Bar and Rod Clad Sheet and Plate Bare Sheet and Plate Clad Sheet and Plate Bare Sheet and Plate Sheet and Plate Sheet and Plate Sheet and Plate Sheet and Plate Sheet and Plate Bare Sheet and Plate Clad Sheet and Plate Plate Sheet and Plate Forging Section 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.3.1 2.4.1 2.3.1 2.5.3 2.4.1 2.4.1 2.5.1 2.5.1 2.5.1 2.5.1 2.4.2 2.4.3 2.4.3 2.5.2 2.3.1 2.3.1 2.5.3 7.2.1 7.2.1 3.2.1 3.2.3 3.5.2 3.5.3 3.5.4 3.5.5 3.6.2 3.7.4 3.2.1 3.2.2 3.2.3 3.6.2 3.7.4 3.2.1 3.2.3 3.2.3 3.5.2 3.5.3 3.5.1 3.5.5 3.5.4 3.6.2 3.7.4 3.7.4 3.2.6 3.2.7 4.2.1

Key: Underline indicates inactive for new design.

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MIL-HDBK-5H 1 December 1998
Specification ASTM B 91 ASTM B 107 ASTM B 107 ASTM B 166 ASTM B 194 ASTM B 564 MIL-A-21180 MIL-A-21180 MIL-A-21180 MIL-A-21180 MIL-A-21180 MIL-A-21180 MIL-A-22771 MIL-A-22771 MIL-A-22771 MIL-A-22771 MIL-A-22771 MIL-A-22771 MIL-A-22771 MIL-A-22771 MIL-A-46192 MIL-M-46062 MIL-M-46062 MIL-M-46062 MIL-M-46062 MIL-P-25995 MIL-S-18728 MIL-S-18729 MIL-S-25043 MIL-S-5000 MIL-S-5059 MIL-S-5626 MIL-S-6049 MIL-S-6050 MIL-S-6758 MIL-S-7079, Comp. 3 MIL-S-7952 MIL-S-8844 MIL-S-8844 MIL-S-8949 MIL-S-8949 MIL-T-5066 MIL-T-6735 MIL-T-6736 MIL-T-81556 MIL-T-81556 MIL-T-81556 MIL-T-9046 MIL-T-9046 MIL-T-9046 MIL-T-9046 MIL-T-9046 MIL-T-9046 MIL-T-9046 MIL-T-9047 Alloy Name AZ61A ZK60A-F AZ31B Inconel Alloy 600 Copper Beryllium Inconel Alloy 600 A201.0 354.0 C355.0 A356.0 A357.0 359.0 2014 2618 6061 6151 7049/7149 7050 7075 7175 2519 AM100A AZ91C/AZ91E AZ92A QE22A Magnesium 6061 8630 4130 17-7PH 4340 AISI 301 4140 8740 8630 4130 AISI 1025 AISI 1025 4340 4340 D6AC D6AC AISI 1025 4135 4130 CP Titanium Ti-5Al-2.5Sn Ti6Al-6V-2Sn CP Titanium Ti-5Al-2.5Sn Ti-8Al-1Mo-1V Ti-6Al-2Sn-4Zr-2Mo Ti-6Al-4V Ti6Al-6V-2Sn Ti-13V-11Cr-3Al CP Titanium Form/Application Forging Extrusion Extrusion Bar and Rod Sheet (TB00, TD01, TD02, TD04) Forging Casting (T7 Temper) Casting Casting Casting Casting Casting Forging Die Forging Forging Forging Forging Forging Forging Forging Plate Casting Casting Casting Sand Casting Pipe Sheet, Strip and Plate Sheet, Strip and Plate Plate, Sheet and Strip Bar and Forging Plate, Sheet and Strip Bar and Forging Bar and Forging Bar and Forging Bar and Forging Bar Sheet and Strip Tubing Bar and Forging Bar and Forging Sheet, Strip and Plate Tubing Tubing Tubing Extruded Bars and Shapes Extruded Bar and Shapes Extruded Bar and Shapes Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Sheet and Strip Sheet, Strip and Plate Sheet, Strip and Plate Sheet, Strip and Plate Bar Section 4.2.2 4.2.3 4.2.1 6.3.2 7.3.2 6.3.2 3.8.1 3.9.1 3.9.3 3.9.5 3.9.6 3.9.8 3.2.1 3.2.10 3.6.2 3.6.3 3.7.2 3.7.3 3.7.4 3.7.6 3.2.8 4.3.1 4.3.2 4.3.3 4.3.5 3.6.2 2.3.1 2.3.1 2.6.9 2.3.1 2.7.1 2.3.1 2.3.1 2.3.1 2.3.1 2.2.1 2.2.1 2.3.1 2.3.1 2.3.1 2.3.1 2.2.1 2.3.1 2.3.1 5.2.1 5.3.1 5.4.2 5.2.1 5.3.1 5.3.2 5.3.3 5.4.1 5.4.2 5.5.1 5.2.1

Key: Underline indicates inactive for new design.

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MIL-HDBK-5H 1 December 1998
Specification MIL-T-9047 MIL-T-9047 MIL-T-9047 MIL-T-9047 QQ-A-367 QQ-A-367 QQ-A-367 QQ-A-367 QQ-A-367 WW-T-700/3 WW-T-700/6 Alloy Name Ti-5Al-2.5Sn Ti-8Al-1Mo-1V Ti-6Al-4V Ti-13V-11Cr-3Al 2014 2618 6061 7049/7149 7075 2024 6061 Form/Application Bar Bar Bar Bar Forging Forging Forging Forging Forging Tubing Tubing Seamless, Drawn Section 5.3.1 5.3.2 5.4.1 5.5.1 3.2.1 3.2.10 3.6.2 3.7.2 3.7.4 3.2.3 3.6.2

Key: Underline indicates inactive for new design.

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MIL-HDBK-5H 1 December 1998

APPENDIX D
 	


A-Basis, 1-9, 9-18, 9-65 AMS, 9-7 Anderson-Darling Test k-Sample Test, 9-23, 9-217 Normality, 9-26, 9-28, 9-210 Weibullness, 9-26, 9-28, 9-212 Applicability of Procedures, 9-5 Approval Procedures, 9-5 ASTM, 1-9, 9-7, 9-10, 9-59, 9-73, 9-89, 9-92, 9-151, 9-198 ASTM B 769, 9-10 ASTM C 693, 9-60 ASTM C 714, 9-60 ASTM D 2766, 9-60 ASTM E 8, 1-10, 1-11 ASTM E 83, 9-73 ASTM E 111, 9-59 ASTM E 132, 9-59 ASTM E 139, 9-151 ASTM E 143, 9-59 ASTM E 228, 9-60 ASTM E 238, 1-14, 9-10 ASTM E 399, 9-203 ASTM E 606, 9-89, 9-100, 9-103, 9-106 ASTM E 647, 9-144 B-Basis, 1-9, 9-18 Bearing Properties, 1-14 Bearing Test Procedures, 9-10 Biaxial Properties, 1-19 Modulus of Elasticity, 1-20 Ultimate Stress, 1-21 Yield Stress, 1-20 Biaxial Stress-Strain Curves, 9-87 Brittle Fracture, 1-21 Analysis, 1-22 Cast, Definition of, 9-9 Chi-Squared Distribution Values, 9-236 Clad Aluminum Alloy Plate, 9-37 Coefficient of Thermal Expansion, 9-59 Columns, 1-31 Primary Instability, 1-31 Stable Sections, 1-31 Yield Stress, 1-32 Combinability of Populations, 9-210 Anderson-Darling k-Sample Test, 9-214, 9-217 D-1 F-Test, 9-214, 9-215 t-Test, 9-214, 9-216 Compressive Properties, 1-13 Computational Procedures Derived Properties, 9-33, 9-35, 9-39, 9-40 Normal Distribution 9-29 Unknown Distribution, 9-32 Weibull Distribution, 9-31 Confidence, 9-21 Confidence Interval, 9-92, 9-215 Confidence Level, 9-92 Confidence Limit, 9-94 Creep/Stress Rupture, 1-15, 9-147 Data Analysis, 9-154, 9-156 Data Generation, 9-149, 9-151 Data Requirements, 9-151, 9-153 Definitions, 9-154 Example Problems, 9-163 Presentation of Data, 9-160 Terminology, 9-150 Test Planning, 9-152 Data Basis, 9-18, 9-63 Data Generation Creep/Stress Rupture, 9-151 Fatigue, 9-108 Fatigue Crack Growth, 9-144 Fracture Toughness, 9-205 Fusion-Welded Joints, 9-196 Mechanically Fastened Joints, 9-168 Mechanical Properties, 9-10 Stress-Strain, 9-73 Data Presentation Creep-Rupture, 9-160 Elevated Temperature Curves, 9-66 Fatigue, 9-125 Fatigue Crack Propagation, 1-27, 9-147 Fracture Toughness, 9-208 Fusion-Welded Joints, 9-200 Mechanically Fastened Joints, 9-187 Room-Temperature Design Values, 9-60 Typical (Full-Range) Stress-Strain, 9-83 Typical Stress-Strain, 9-76 Data Requirements Creep/Stress Rupture, 9-151 Derived Properties, 9-34 Directly Calculated, 9-7

MIL-HDBK-5H 1 December 1998 Elevated Temperature Properties, 9-65 Fatigue, 9-100 Fatigue Crack Growth, 9-146 Fusion-Welded Joints, 9-196 Mechanically Fastened Joints, 9-171 Mechanical Properties, 9-12, 9-29, 9-34 New Materials, 9-7 Normal Distribution, 9-29 Physical Properties, 9-11 Stress-Strain, 9-73 Unknown Distribution, 9-32 Weibull Distribution, 9-31 Definition of Terms Creep/Stress Rupture, 9-154 Fatigue, 9-98 Fracture Toughness, 9-203 Mechanically Fastened Joints, 9-166 Mechanical Properties, 9-19 Statistics, 9-20, 9-92, 9-214 Degrees of Freedom, 9-21, 9-215 Density, 9-11, 9-59 Derived Properties, 1-9, 9-33 Design Mechanical Properties By Regression, 9-37 Determining Form of Distribution, 9-25 Determining Population, 9-23 Direct Computation, Non Parametric, 9-33 Normal, 9-29 Weibull, 9-31 Example Problems, 9-41 General Procedures, 9-21 Presentation, 9-60 Dimensionally Discrepant Castings, 9-10 Direct Computation of Allowables Normal Distribution, 9-29 Unknown Distribution, 9-33 Weibull Distribution, 9-31 Distribution, Form of, 9-26 Documentation Requirements, 9-5 Elastic Properties, 9-59 Elevated Temperature Curves, 1-9, 9-65 Data Requirements, 9-65 Presentation, 9-66 Working Curves, 9-66 Environmental Effects, 1-23 Elongation, 1-12, 9-63, 9-67 Examples of Computation Procedures Complex Exposure, 9-71 Creep/Stress Rupture, 9-163 Design Allowables, 9-41 Fatigue, 9-132 D-2 F-Test, 9-215 Linear Regression, 9-227 Strain-Departure Method, 9-74, 9-84 t-Test, 9-216 F-Distribution Fractiles, 9-237, 9-247 F-Test, 9-215 Fasteners H-Type, 9-189 S-Type, 9-189 Fatigue, 9-87 Data Analysis, 9-109 Data Generation, 9-108 Data Requirements, 9-100 Definitions, 9-98 Example Problems, 9-132 Life Models, 9-111 Presentation of Data, 9-125 Properties, 1-17 Terminology, 9-92 Test Planning, 9-101 Time Dependent Effects, 9-124 Fatigue Crack Growth, 1-25, 9-144 Crack-Propogation Analysis, 1-26 Data Analysis, 9-144 Data Generation, 9-144 Data Requirements, 9-146 Presentation of Data, 1-26, 9-147 Forgings, Definition of Grain Directions in, 9-10 Fracture Strength, 1-21 Analysis, 1-22, 1-24 Apparent Fracture Toughness, 1-25 Brittle Fracture, 1-21 Center-Cracked Tension Panels, 1-25 Critical Plane-Strain, 1-22 Environmental, 1-23 Plane Stress, 1-23 Transitional Stress States, 1-23 Fracture Toughness, 9-203 Critical Plain-Strain, 1-22 Data Analysis, 9-205 Data Generation, 9-205 Definitions, 9-203 Presentation of Data, 9-208 Full-Range Stress-Strain Curves, 9-83 Fusion-Welded Joints, 9-192 Data Analysis, 9-200 Data Generation, 9-196 Data Requirements, 9-196 Presentation of Data, 9-200 Goodness-of-Fit Tests, 9-210 Normality, 9-210 Weibullness, 9-212

MIL-HDBK-5H 1 December 1998 Grain Direction, Treatment of, 9-10, 9-34, 9-36 Grouped Data Analysis, 9-29 Heat Requirements, 9-7, 9-9 Indirect Design Allowables, 9-35 Instability, 1-30 Bending, 1-31 Combined Loadings, 1-31 Compression, 1-31 International System of Units, 1-5 k-Sample Anderson-Darling Test, 9-23, 9-217 Larson-Miller Analysis, 9-163 Location of Test Specimens, 9-10 Lot Requirements, 9-7, 9-10, 9-11, 9-73, 9-83 Material Failures, 1-29 Bearing, 1-29 Bending, 1-29 Combined Stress, 1-30 Compression, 1-29 Fatigue, 1-30 Shear, 1-29 Stress Concentrations, 1-30 Tension, 1-29 Material Specifications, 9-7, 9-18 Maximum Likelihood Estimation, 9-123 Mean Stress/Strain Effects, Evaluation of, 9-111 Mechanical Properties Computation of Design Allowables, 9-18 Derived Properties, 9-33 Example Problems, 9-41 Presentation, 9-60 Terminology for, 9-19 Test Matrix, 9-8 Mechanically Fastened Joints, 9-166 Data Analysis, 9-176 Data Generation, 9-168 Data Requirements, 9-171 Definitions, 9-166 Presentation of Data, 9-187 Melt, Definition of, 9-9 Metallurgical Instability, 1-19 MIL-STD-1312, 9-168, 9-171, 9-191 Modulus of Elasticity, 1-11, 9-59, 9-68 Modulus of Rigidity, 1-13 Nonparametric Data Analysis, 9-33 Normal Curve Statistics, 9-230 Normality, Assessment of, 9-210 Outliers, Treatment of, 9-119 Physical Properties, 9-59, 9-69 Poisson’s Ratio, 1-10, 9-59 Precision Modulus Data, 9-10 Presentation of Data Creep/Stress Rupture, 9-160 D-3 Design Allowables, 9-60 Effect of Temperature Curves, 9-66 Fatigue, 9-125 Fatigue Crack Growth, 9-147 Fracture Toughness, 9-208 Fusion-Welded Joints, 9-200 Mechanically Fastened Joints, 9-187 Physical Properties, 9-59 Primary Test Direction, 9-34 Probability, 9-21 Probability Plots Normal, 9-211 Weibull, 9-213 Proportional Limit Shear, 1-13 Tensile, 1-12 Ramberg-Osgood Method, 9-76 Rank Values for A- and B-Basis, 9-34, 9-235 Ratioing of Mechanical Properties, 9-34 Reduced Ratios By Regression, 9-37 Direct Computation, 9-34 Reduction in Area, 1-10, 1-12, 9-63, 9-67 References, 9-253 Regression, 9-219 Determining Design Allowables, 9-37 Determining Reduced Ratios, 9-40 Example Computations, 9-227 Least Squares, 9-219 Tests for Adequacy of, 9-224 Runouts, Treatment of, 9-123 S-Basis, 1-8, 9-18, 9-60 Separately Cast Test Bars, 9-9 Shear Properties, 1-13 Shear Test Procedures, 9-10 Significance, 9-215 Specific Heat, 9-59 Specifying the Population, 9-23, 9-197 Statistics Symbols, 9-6, 9-98 Terms/Definitions, 9-20, 9-92, 9-214 Strain Normal, 1-10 Poisson's Ratio, 1-10 Principal, 1-10 Rate, 1-10 Shear, 1-10 Strain Departure Method, 9-74 Stress Normal, 1-9 Principal, 1-9 Shear, 1-9

MIL-HDBK-5H 1 December 1998 State of, 1-9 Stress-Strain Curves, 9-73 Biaxial, 9-87 Data Requirements, 9-73 Example Computation, 9-75, 9-84 Full-Range, 9-83 Presentation, 9-76, 9-83 Typical, 9-76 Stress-Tangent Modulus Curves, 9-83 Symbols and Definitions Creep/Stress Rupture, 9-150 Fatigue, 9-98 Fatigue Crack Growth, 9-144 Fracture Toughness, 9-203 General, 1-2, 9-6 Mechanically Fastened Joints, 9-166 Mechanical Properties, 9-19 Statistics, 9-6, 9-20, 9-92, 9-98, 9-214 t-Distribution Fractiles, 9-238 t-Test, 9-216 Tangent Modulus Curves, 9-79 Temperature Effects, 1-15 Tensile Proportional Limit, 1-12 Tensile Yield Stress, 1-12 Terminology Creep Rupture, 9-150 Fatigue, 1-17, 9-92 Mechanical Property, 9-19 Test Specimens Duplication, 9-10 Location, 9-7, 9-37 Orientation, 9-10, 9-34 Primary Test Direction, 9-34 Testing Procedures Bearing, 9-10 Creep/Stress Rupture, 9-152 Elastic Properties, 9-59 Fatigue, 9-101 Fatigue Crack Growth, 9-144 Fusion-Welded Joints, 9-200 Mechanically Fastened Joints, 9-168 Physical Properties, 9-59 Shear, 9-10 Stress-Strain, 9-73 Tests of Significance, 9-214 Definitions, 9-214 F-Test, 9-215 t-Test, 9-216 Thermal Conductivity, 9-59 Thermal Exposure, 9-70 Complex, 9-71 Simple, 9-70 D-4 Tolerance Bounds T90, 9-6, 9-21 T99, 9-6, 9-21 Tolerance Interval, 9-98 Tolerance Level, 9-98 Tolerance Limit Factors Normal, One-Sided, 9-230 Weibull, One-Sided, 9-240, 9-241 Typical Basis, 9-18, 9-65, 9-73 Ultimate Bearing Stress, 1-15 Ultimate Compression Stress, 1-13 Ultimate Tensile Stress, 1-12 Weibull Acceptability Test, 9-25 Weibull Distribution Allowables, 9-29 Weibullness, Assessment of, 9-212 Working Curves, Determination of, 9-66 Yield Bearing Stress, 1-14 Yield Stress Column, 1-32 Bearing, 1-14 Tensile, 1-12

MIL-HDBK-5H 1 December 1998

APPENDIX E
	


Figure No. 1.4.4.1 1.4.8.2.1(a) 1.4.8.2.1(b) 1.4.9.3(a) 1.4.11.1 1.4.11.3 1.4.12.2 1.4.12.3 1.4.12.4 1.4.12.4.1 1.4.13.2(a) 1.4.13.2(b) 1.4.13.4 1.6.2.2 1.6.4.4(a) 1.6.4.4(b) 1.6.4.4(c) 1.6.4.4(d) 1.6.4.4(e) 1.6.4.4(f) 1.6.4.4(g) 1.6.4.4(h) 1.6.4.4(i) 2.2.1.0 2.3.0.2 2.3.1.0 2.3.1.1.1 2.3.1.1.2 2.3.1.1.3 2.3.1.1.4 2.3.1.2.6(a) 2.3.1.2.6(b) 2.3.1.2.6(c) 2.3.1.2.8(a) 2.3.1.2.8(b) 2.3.1.2.8(c) 2.3.1.2.8(d) 2.3.1.2.8(e) 2.3.1.2.8(f) 2.3.1.2.8(g) 2.3.1.2.8(h) 2.3.1.3.6(a) Current Form Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics

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MIL-HDBK-5H 1 December 1998
Figure No. 2.3.1.3.6(b) 2.3.1.3.6(c) 2.3.1.3.6(d) 2.3.1.3.6(e) 2.3.1.3.6(f) 2.3.1.3.6(g) 2.3.1.3.8(a) 2.3.1.3.8(b) 2.3.1.3.8(c) 2.3.1.3.8(d) 2.3.1.3.8(e) 2.3.1.3.8(f) 2.3.1.3.8(g) 2.3.1.3.8(h) 2.3.1.3.8(i) 2.3.1.3.8(j) 2.3.1.3.8(k) 2.3.1.3.8(l) 2.3.1.3.8(m) 2.3.1.3.8(n) 2.3.1.3.8(o) 2.3.1.4.8(a) 2.3.1.4.8(b) 2.3.1.4.8(c) 2.3.1.4.8(d) 2.3.1.4.9 2.3.1.5.9 2.4.1.0 2.4.1.1.1(a) 2.4.1.1.1(b) 2.4.1.1.2(a) 2.4.1.1.2(b) 2.4.1.1.3(a) 2.4.1.1.3(b) 2.4.1.1.4 2.4.2.0 2.4.2.1.1 2.4.2.1.2 2.4.2.1.4 2.4.2.1.6(a) 2.4.2.1.6(b) 2.4.3.0 2.4.3.1.1 2.4.3.1.2 2.4.3.1.3 2.4.3.1.4 2.4.3.1.6(a) 2.4.3.1.6(b) 2.4.3.1.6(c) Current Form Vector Graphics Vector Graphics Scanned Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics

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Figure No. 2.4.3.1.6(d) 2.4.3.1.8 2.5.0.2(a) 2.5.1.0 2.5.1.1.1 2.5.1.1.2 2.5.1.1.3 2.5.1.1.4 2.5.1.1.6(a) 2.5.1.1.6(b) 2.5.1.1.6(c) 2.5.1.1.6(d) 2.5.1.1.6(e) 2.5.2.1.6(a) 2.5.2.1.6(b) 2.5.3.1.6(a) 2.5.3.1.6(b) 2.5.3.1.6(c) 2.5.3.2.6(a) 2.5.3.2.6(b) 2.5.3.2.6(c) 2.6.1.0 2.6.1.1.1 2.6.1.1.2 2.6.1.1.3 2.6.1.1.4 2.6.1.1.6(a) 2.6.1.1.6(b) 2.6.2.0 2.6.2.1.1 2.6.2.1.2 2.6.2.1.3 2.6.2.1.4 2.6.3.0 2.6.3.1.1 2.6.3.1.2 2.6.3.1.5 2.6.3.1.6 2.6.3.1.8 2.6.3.2.1 2.6.3.2.2 2.6.3.2.5 2.6.3.2.6 2.6.3.2.8 2.6.4.0 2.6.4.1.1 2.6.4.1.2 2.6.4.1.5 2.6.4.1.6 Current Form Vector Graphics Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Scanned Scanned Vector Graphics Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics

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MIL-HDBK-5H 1 December 1998
Figure No. 2.6.4.1.8(a) 2.6.4.1.8(b) 2.6.4.2.1 2.6.4.2.2 2.6.4.2.5 2.6.4.2.6 2.6.4.2.8 2.6.5.0 2.6.5.1.1 2.6.5.1.6(a) 2.6.5.1.6(b) 2.6.5.1.6(c) 2.6.5.1.8(a) 2.6.5.1.8(b) 2.6.5.1.8(c) 2.6.6.0 2.6.6.1.1 2.6.6.1.4 2.6.6.1.6(a) 2.6.6.1.6(b) 2.6.6.1.6(c) 2.6.6.2.2 2.6.6.2.6(a) 2.6.6.2.6(b) 2.6.6.2.8(a) 2.6.6.2.8(b) 2.6.6.2.8(c) 2.6.6.3.2 2.6.6.3.6 2.6.7.0 2.6.7.1.1 2.6.7.1.4 2.6.7.1.6(a) 2.6.7.1.6(b) 2.6.7.1.6(c) 2.6.7.1.8(a) 2.6.7.1.8(b) 2.6.7.1.8(c) 2.6.7.1.8(d) 2.6.7.1.8(e) 2.6.7.1.8(f) 2.6.8.0 2.6.8.1.2 2.6.8.1.3 2.6.8.1.4 2.6.8.1.8(a) 2.6.8.1.8(b) 2.6.8.1.8(c) 2.6.8.2.1 Current Form Scanned Scanned Vector Graphics Vector Graphics Scanned Vector Graphics Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Vector Graphics Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Vector Graphics

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MIL-HDBK-5H 1 December 1998
Figure No. 2.6.8.2.6(a) 2.6.8.2.6(b) 2.6.8.3.6(a) 2.6.8.3.6(b) 2.6.8.4.8 2.6.8.5.8 2.6.8.6.1 2.6.9.0 2.6.9.1.1 2.6.9.1.2 2.6.9.1.4(a) 2.6.9.1.4(b) 2.6.9.1.6(a) 2.6.9.1.6(b) 2.6.9.1.6(c) 2.7.1.0 2.7.1.1.1(a) 2.7.1.1.1(b) 2.7.1.2.6(a) 2.7.1.2.6(b) 2.7.1.3.1 2.7.1.3.2 2.7.1.3.3 2.7.1.3.4 2.7.1.3.6(a) 2.7.1.3.6(b) 2.7.1.4.6(a) 2.7.1.4.6(b) 2.7.1.5.1 2.7.1.5.2(a) 2.7.1.5.2(b) 2.7.1.5.3 2.7.1.5.4 2.7.1.5.6(a) 2.7.1.5.6(b) 2.7.1.5.6(c) 2.7.1.5.6(d) 2.8.1.1(a) 2.8.1.1(b) 2.8.3.2(a) 2.8.3.2(b) 2.8.3.2(c) 2.8.3.2(d) 2.8.3.2(e) 2.8.3.2(f) 2.8.3.2(g) 2.8.3.2(h) 2.8.3.2(i) 2.8.3.2(j) Current Form Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Vector Graphics Scanned Scanned Vector Graphics Scanned

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MIL-HDBK-5H 1 December 1998
Figure No. 3.1.2.1.1(a) 3.1.2.1.1(b) 3.1.2.1.1(c) 3.2.1.0 3.2.1.1.1(a) 3.2.1.1.1(b) 3.2.1.1.1(c) 3.2.1.1.1(d) 3.2.1.1.1(e) 3.2.1.1.1(f) 3.2.1.1.2(a) 3.2.1.1.2(b) 3.2.1.1.3(a) 3.2.1.1.3(b) 3.2.1.1.4 3.2.1.1.5(a) 3.2.1.1.5(b) 3.2.1.1.6(a) 3.2.1.1.6(b) 3.2.1.1.6(c) 3.2.1.1.6(d) 3.2.1.1.6(e) 3.2.1.1.6(f) 3.2.1.1.6(g) 3.2.1.1.6(h) 3.2.1.1.6(i) 3.2.1.1.6(j) 3.2.1.1.6(k) 3.2.1.1.6(l) 3.2.1.1.6(m) 3.2.1.1.6(n) 3.2.1.1.6(o) 3.2.1.1.6(p) 3.2.1.1.6(q) 3.2.1.1.6(r) 3.2.1.1.6(s) 3.2.1.1.6(t) 3.2.1.1.6(u) 3.2.1.1.6(v) 3.2.1.1.8(a) 3.2.1.1.8(b) 3.2.1.1.8(c) 3.2.1.1.8(d) 3.2.1.1.8(e) 3.2.2.0 3.2.2.1.4 3.2.3.0 3.2.3.1.1(a) 3.2.3.1.1(b) Current Form Scanned Scanned Scanned Vector Graphics Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics

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Figure No. 3.2.3.1.1(c) 3.2.3.1.1(d) 3.2.3.1.1(e) 3.2.3.1.1(f) 3.2.3.1.2(a) 3.2.3.1.2(b) 3.2.3.1.3(a) 3.2.3.1.3(b) 3.2.3.1.4 3.2.3.1.5(a) 3.2.3.1.5(b) 3.2.3.1.6(a) 3.2.3.1.6(b) 3.2.3.1.6(c) 3.2.3.1.6(d) 3.2.3.1.6(e) 3.2.3.1.6(f) 3.2.3.1.6(g) 3.2.3.1.6(h) 3.2.3.1.6(i) 3.2.3.1.6(j) 3.2.3.1.6(k) 3.2.3.1.6(l) 3.2.3.1.6(m) 3.2.3.1.6(n) 3.2.3.1.6(o) 3.2.3.1.6(p) 3.2.3.1.6(q) 3.2.3.1.6(r) 3.2.3.1.6(s) 3.2.3.1.6(t) 3.2.3.1.6(u) 3.2.3.1.6(v) 3.2.3.1.6(w) 3.2.3.1.6(x) 3.2.3.1.6(y) 3.2.3.1.6(z) 3.2.3.1.6(aa) 3.2.3.1.8(a) 3.2.3.1.8(b) 3.2.3.1.8(c) 3.2.3.1.8(d) 3.2.3.1.8(e) 3.2.3.1.8(f) 3.2.3.1.8(g) 3.2.3.1.8(h) 3.2.3.1.8(i) 3.2.3.3.1(a) 3.2.3.3.1(b) Current Form Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics

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MIL-HDBK-5H 1 December 1998
Figure No. 3.2.3.3.1(c) 3.2.3.3.1(d) 3.2.3.3.5(a) 3.2.3.3.5(b) 3.2.3.3.6(a) 3.2.3.3.6(b) 3.2.3.3.6(c) 3.2.3.3.6(d) 3.2.3.3.6(e) 3.2.3.4.1(a) 3.2.3.4.1(b) 3.2.3.4.1(c) 3.2.3.4.1(d) 3.2.3.4.1(e) 3.2.3.4.1(f) 3.2.3.4.2(a) 3.2.3.4.2(b) 3.2.3.4.3(a) 3.2.3.4.3(b) 3.2.3.4.5(a) 3.2.3.4.5(b) 3.2.3.4.6(a) 3.2.3.4.6(b) 3.2.3.4.6(c) 3.2.3.4.6(d) 3.2.3.4.6(e) 3.2.3.4.6(f) 3.2.3.4.6(g) 3.2.3.4.6(h) 3.2.3.4.6(i) 3.2.3.4.6(j) 3.2.3.5.1(a) 3.2.3.5.1(b) 3.2.3.5.1(c) 3.2.3.5.1(d) 3.2.3.5.2(a) 3.2.3.5.2(b) 3.2.3.5.3(a) 3.2.3.5.3(b) 3.2.3.5.3(c) 3.2.3.5.5(a) 3.2.3.5.5(b) 3.2.3.5.6(a) 3.2.3.5.6(b) 3.2.3.5.6(c) 3.2.3.5.6(d) 3.2.3.5.10(a) 3.2.3.5.10(b) 3.2.4.0 Current Form Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Vector Graphics

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MIL-HDBK-5H 1 December 1998
Figure No. 3.2.5.1.6(a) 3.2.5.1.6(b) 3.2.6.1.1(a) 3.2.6.1.1(b) 3.2.6.1.6(a) 3.2.6.1.6(b) 3.2.6.1.9(a) 3.2.6.1.9(b) 3.2.6.1.9(c) 3.2.6.1.9(d) 3.2.6.1.9(e) 3.2.7.0 3.2.7.1.1(a) 3.2.7.1.1(b) 3.2.7.1.6(a) 3.2.7.1.6(b) 3.2.7.2.1(a) 3.2.7.2.1(b) 3.2.7.2.6(a) 3.2.7.2.6(b) 3.2.7.2.8(a) 3.2.7.2.8(b) 3.2.7.2.8(c) 3.2.7.2.8(d) 3.2.7.3.6(a) 3.2.7.3.6(b) 3.2.7.3.6(c) 3.2.7.3.6(d) 3.2.7.3.6(e) 3.2.7.4.1(a) 3.2.7.4.1(b) 3.2.7.4.6(a) 3.2.7.4.6(b) 3.2.7.4.6(c) 3.2.7.4.6(d) 3.2.7.4.6(e) 3.2.8.1.6(a) 3.2.8.1.6(b) 3.2.10.0 3.2.10.1.1(a) 3.2.10.1.1(b) 3.2.10.1.1(c) 3.2.10.1.1(d) 3.2.10.1.2 3.2.10.1.3 3.2.10.1.4 3.2.10.1.5 3.2.10.1.6(a) 3.2.10.1.6(b) Current Form Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics

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MIL-HDBK-5H 1 December 1998
Figure No. 3.5.1.0 3.5.1.1.1 3.5.1.1.4 3.5.1.1.5 3.5.1.3.1(a) 3.5.1.3.1(b) 3.5.1.3.1(c) 3.5.1.3.1(d) 3.5.1.3.5(a) 3.5.1.3.5(b) 3.5.1.5.1(a) 3.5.1.5.1(b) 3.5.1.5.1(c) 3.5.1.5.1(d) 3.5.1.5.5(a) 3.5.1.5.5(b) 3.5.2.0 3.5.2.1.6(a) 3.5.2.1.6(b) 3.5.2.1.6(c) 3.5.3.1.6(a) 3.5.3.1.6(b) 3.5.3.1.6(c) 3.5.3.2.6(a) 3.5.3.2.6(b) 3.5.3.2.6(c) 3.5.3.3.6(a) 3.5.3.3.6(b) 3.5.3.3.6(c) 3.5.3.4.6 3.5.3.7.6 3.5.4.1.6 3.5.4.2.6 3.5.4.3.6(a) 3.5.4.3.6(b) 3.5.5.0 3.5.5.1.6(a) 3.5.5.1.6(b) 3.5.5.2.6 3.5.5.4.6 3.6.1.1.6(a) 3.6.1.1.6(b) 3.6.2.0 3.6.2.2.1(a) 3.6.2.2.1(b) 3.6.2.2.1(c) 3.6.2.2.1(d) 3.6.2.2.4 3.6.2.2.5(a) Current Form Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics

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MIL-HDBK-5H 1 December 1998
Figure No. 3.6.2.2.5(b) 3.6.2.2.6(a) 3.6.2.2.6(b) 3.6.2.2.6(c) 3.6.2.2.6(d) 3.6.2.2.6(e) 3.6.2.2.6(f) 3.6.2.2.6(g) 3.6.2.2.6(h) 3.6.2.2.6(i) 3.6.2.2.6(j) 3.6.2.2.6(k) 3.6.2.2.6(l) 3.6.2.2.6(m) 3.6.2.2.6(n) 3.6.2.2.6(o) 3.6.2.2.8 3.6.3.0 3.7.1.1.1 3.7.1.1.6(a) 3.7.1.1.6(b) 3.7.1.1.6(c) 3.7.1.1.6(d) 3.7.1.2.6(a) 3.7.1.2.6(b) 3.7.1.2.6(c) 3.7.1.2.6(d) 3.7.2.1.1 3.7.2.1.6(a) 3.7.2.1.6(b) 3.7.2.1.6(c) 3.7.2.1.6(d) 3.7.2.1.6(e) 3.7.2.1.6(f) 3.7.2.1.6(g) 3.7.2.1.8(a) 3.7.2.1.8(b) 3.7.2.1.8(c) 3.7.2.1.8(d) 3.7.2.1.8(e) 3.7.2.1.8(f) 3.7.2.1.8(g) 3.7.3.1.6(a) 3.7.3.1.6(b) 3.7.3.1.6(c) 3.7.3.1.6(d) 3.7.3.1.8(a) 3.7.3.1.8(b) 3.7.3.2.1 Current Form Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Vector Graphics

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MIL-HDBK-5H 1 December 1998
Figure No. 3.7.3.2.6(a) 3.7.3.2.6(b) 3.7.3.2.6(c) 3.7.3.2.6(d) 3.7.3.2.6(e) 3.7.3.2.6(f) 3.7.3.2.6(g) 3.7.3.2.6(h) 3.7.3.2.6(i) 3.7.3.2.6(j) 3.7.3.2.8(a) 3.7.3.2.8(b) 3.7.3.2.8(c) 3.7.3.2.8(d) 3.7.3.2.8(e) 3.7.3.2.8(f) 3.7.3.2.8(g) 3.7.3.2.8(h) 3.7.3.2.8(i) 3.7.3.2.9(a) 3.7.3.2.9(b) 3.7.3.2.9(c) 3.7.3.3.6(a) 3.7.3.3.6(b) 3.7.3.3.6(c) 3.7.3.3.6(d) 3.7.3.3.6(e) 3.7.3.3.6(f) 3.7.3.3.8(a) 3.7.3.3.8(b) 3.7.4.0 3.7.4.1.1(a) 3.7.4.1.1(b) 3.7.4.1.1(c) 3.7.4.1.1(d) 3.7.4.1.2(a) 3.7.4.1.2(b) 3.7.4.1.3(a) 3.7.4.1.3(b) 3.7.4.1.4 3.7.4.1.5(a) 3.7.4.1.5(b) 3.7.4.1.6(a) 3.7.4.1.6(b) 3.7.4.1.6(c) 3.7.4.1.6(d) 3.7.4.1.6(e) 3.7.4.1.6(f) 3.7.4.1.6(g) Current Form Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Vector Graphics Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics

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MIL-HDBK-5H 1 December 1998
Figure No. 3.7.4.1.6(h) 3.7.4.1.6(i) 3.7.4.1.6(j) 3.7.4.1.6(k) 3.7.4.1.6(l) 3.7.4.1.6(m) 3.7.4.1.6(n) 3.7.4.1.6(o) 3.7.4.1.6(p) 3.7.4.1.6(q) 3.7.4.1.8(a) 3.7.4.1.8(b) 3.7.4.1.8(c) 3.7.4.1.8(d) 3.7.4.1.8(e) 3.7.4.1.8(f) 3.7.4.1.8(g) 3.7.4.1.8(h) 3.7.4.1.9 3.7.4.1.10(a) 3.7.4.1.10(b) 3.7.4.1.10(c) 3.7.4.1.10(d) 3.7.4.1.10(e) 3.7.4.1.10(f) 3.7.4.1.10(g) 3.7.4.1.10(h) 3.7.4.2.6(a) 3.7.4.2.6(b) 3.7.4.2.6(c) 3.7.4.2.6(d) 3.7.4.2.6(e) 3.7.4.2.6(f) 3.7.4.2.9(a) 3.7.4.2.9(b) 3.7.4.2.9(c) 3.7.4.2.10(a) 3.7.4.2.10(b) 3.7.5.1.6(a) 3.7.5.1.6(b) 3.7.5.1.6(c) 3.7.5.1.6(d) 3.7.5.2.6(a) 3.7.5.2.6(b) 3.7.5.2.6(c) 3.7.5.2.6(d) 3.7.5.2.8(a) 3.7.5.2.8(b) 3.7.5.2.8(c) Current Form Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned

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MIL-HDBK-5H 1 December 1998
Figure No. 3.7.6.1.6(a) 3.7.6.1.6(b) 3.7.6.1.8(a) 3.7.6.1.8(b) 3.7.6.1.8(c) 3.7.6.1.8(d) 3.7.6.2.6(a) 3.7.6.2.6(b) 3.7.6.2.6(c) 3.7.6.2.6(d) 3.7.6.2.6(e) 3.7.6.2.6(f) 3.7.6.2.8(a) 3.7.6.2.8(b) 3.7.7.1.6(a) 3.7.7.1.6(b) 3.7.7.1.6(c) 3.7.8.1.6(a) 3.7.8.1.6(b) 3.7.8.1.6(c) 3.7.8.1.6(d) 3.7.8.1.6(e) 3.7.8.1.6(f) 3.7.8.1.6(g) 3.7.8.1.8(a) 3.7.8.1.8(b) 3.7.8.1.8(c) 3.7.8.1.10(a) 3.7.8.1.10(b) 3.7.8.1.10(c) 3.7.8.1.10(d) 3.7.8.2.6(a) 3.7.8.2.6(b) 3.7.8.2.8(a) 3.7.8.2.8(b) 3.7.8.2.9(a) 3.7.8.2.9(b) 3.7.8.3.6(a) 3.7.8.3.6(b) 3.7.8.3.6(c) 3.7.8.3.6(d) 3.7.8.3.6(e) 3.7.8.3.6(f) 3.7.8.3.6(g) 3.7.8.3.6(h) 3.7.8.3.6(i) 3.7.8.3.6(j) 3.7.8.3.6(k) 3.7.8.3.6(l) Current Form Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics

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MIL-HDBK-5H 1 December 1998
Figure No. 3.7.8.3.10(a) 3.7.8.3.10(b) 3.8.1.0 3.8.1.1.6 3.8.1.1.8(a) 3.8.1.1.8(b) 3.8.1.1.8(c) 3.9.2.0 3.9.4.0 3.9.5.1.6(a) 3.9.5.1.6(b) 3.9.6.1.6 3.9.7.1.6 3.11.1.1.1 3.11.2.3(a) 3.11.2.3(b) 3.11.3.2(a) 3.11.3.2(b) 3.11.3.2(c) 3.11.3.2(d) 3.11.3.2(e) 3.11.3.2(f) 3.11.3.2(g) 4.2.1.0 4.2.1.1.4 4.2.1.1.6 4.2.1.2.1 4.2.1.2.2 4.2.1.2.3 4.2.1.2.4 4.2.1.2.6 4.2.1.4.8(a) 4.2.1.4.8(b) 4.2.3.0 4.2.3.2.6(a) 4.2.3.2.6(b) 4.2.3.2.8(a) 4.2.3.2.8(b) 4.2.3.2.8(C) 4.3.2.1.4 4.3.2.1.6 4.3.3.0 4.3.3.1.1(a) 4.3.3.1.1(b) 4.3.3.1.1(C) 4.3.3.1.4 4.3.3.1.6(a) 4.3.3.1.6(b) 4.3.4.0 Current Form Scanned Scanned Vector Graphics Vector Graphics Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Vector Graphics Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Vector Graphics Scanned Scanned Scanned Scanned Vector Graphics Scanned Scanned Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics

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MIL-HDBK-5H 1 December 1998
Figure No. 4.3.4.1.1(a) 4.3.4.1.1(b) 4.3.4.1.1(C) 4.3.4.1.6 4.3.5.1.1 4.3.5.1.4 4.3.5.1.6 4.3.6.0 4.3.6.1.1 4.3.6.1.4 4.3.6.1.6(a) 4.3.6.1.6(b) 4.4.2.3(a) 4.4.2.3(b) 4.4.3.2 5.2.1.0 5.2.1.1.1(a) 5.2.1.1.1(b) 5.2.1.1.2(a) 5.2.1.1.2(b) 5.2.1.1.3(a) 5.2.1.1.3(b) 5.2.1.1.6(a) 5.2.1.1.6(b) 5.3.1.0 5.3.1.1.1 5.3.1.1.2 5.3.1.1.3 5.3.1.1.4 5.3.1.1.5 5.3.1.1.9(a) 5.3.1.1.9(b) 5.3.1.1.9(c) 5.3.2.0 5.3.2.1.1 5.3.2.1.4 5.3.2.1.6(a) 5.3.2.1.6(b) 5.3.2.2.1 5.3.2.2.6(a) 5.3.2.2.6(b) 5.3.2.2.8(a) 5.3.2.2.8(b) 5.3.2.2.8(c) 5.3.2.2.8(d) 5.3.2.2.8(e) 5.3.2.2.8(f) 5.3.3.0 5.3.3.1.1 Current Form Scanned Scanned Scanned Vector Graphics Scanned Scanned Vector Graphics Scanned Scanned Scanned Scanned Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Scanned Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned

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MIL-HDBK-5H 1 December 1998
Figure No. 5.3.3.1.2 5.3.3.1.4 5.3.3.1.6(a) 5.3.3.1.6(b) 5.3.3.1.6(c) 5.4.1.0 5.4.1.1.1 5.4.1.1.2 5.4.1.1.3 5.4.1.1.4 5.4.1.1.5 5.4.1.1.6(a) 5.4.1.1.6(b) 5.4.1.1.6(c) 5.4.1.1.6(d) 5.4.1.1.8(a) 5.4.1.1.8(b) 5.4.1.1.8(c) 5.4.1.1.8(d) 5.4.1.1.8(e) 5.4.1.1.8(f) 5.4.1.1.8(g) 5.4.1.1.9 5.4.1.2.1 5.4.1.2.2 5.4.1.2.3 5.4.1.2.4 5.4.1.2.6(a) 5.4.1.2.6(b) 5.4.1.2.6(c) 5.4.1.2.6(d) 5.4.1.2.6(e) 5.4.1.2.6(f) 5.4.1.2.6(g) 5.4.1.2.6(h) 5.4.1.2.7 5.4.1.2.8(a) 5.4.1.2.8(b) 5.4.1.2.8(c) 5.4.1.2.8(d) 5.4.1.2.8(e) 5.4.1.2.8(f) 5.4.1.2.8(g) 5.4.1.2.8(h) 5.4.1.2.8(i) 5.4.2.0 5.4.2.1.1(a) 5.4.2.1.1(b) 5.4.2.1.2(a) Current Form Scanned Scanned Vector Graphics Vector Graphics Scanned Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned

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MIL-HDBK-5H 1 December 1998
Figure No. 5.4.2.1.2(b) 5.4.2.1.3(a) 5.4.2.1.3(b) 5.4.2.1.6(a) 5.4.2.1.6(b) 5.4.2.1.6(c) 5.4.2.1.8(a) 5.4.2.1.8(b) 5.4.2.2.1 5.4.2.2.2 5.5.1.0 5.5.1.1.1 5.5.1.1.2 5.5.1.1.3(a) 5.5.1.1.3(b) 5.5.1.1.4 5.5.1.1.6 5.5.1.1.8(a) 5.5.1.1.8(b) 5.5.1.1.8(c) 5.5.1.1.8(d) 5.5.1.2.1 5.5.1.2.2 5.5.1.2.3 5.5.1.2.4 5.5.1.2.6 5.5.1.2.8(a) 5.5.1.2.8(b) 5.5.1.2.8(c) 5.5.2.0 5.5.2.1.6(a) 5.5.2.1.6(b) 5.5.3.1.6 5.5.3.2.6 5.6.1.1.1 6.2.1.0 6.2.1.1.1 6.2.1.1.3 6.2.1.1.4(a) 6.2.1.1.4(b) 6.2.1.1.4(c) 6.2.1.1.8(a) 6.2.1.1.8(b) 6.2.1.1.8(c) 6.2.1.1.8(d) 6.2.1.1.8(e) 6.2.2.0 6.2.2.1.1(a) 6.2.2.1.1(b) Current Form Scanned Scanned Scanned Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned

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MIL-HDBK-5H 1 December 1998
Figure No. 6.2.2.1.4(a) 6.2.2.1.4(b) 6.3.1.0 6.3.1.1.1 6.3.1.1.4 6.3.1.1.6(a) 6.3.1.1.6(b) 6.3.2.0 6.3.2.1.1 6.3.2.1.2 6.3.2.1.3 6.3.2.1.4 6.3.3.0 6.3.3.1.1(a) 6.3.3.1.1(b) 6.3.3.1.4(a) 6.3.3.1.4(b) 6.3.3.1.6(a) 6.3.3.1.6(b) 6.3.3.1.6(c) 6.3.3.1.6(d) 6.3.3.1.8(a) 6.3.3.1.8(b) 6.3.3.1.8(c) 6.3.3.1.8(d) 6.3.4.0 6.3.4.1.1 6.3.4.1.4 6.3.4.1.5 6.3.4.1.6(a) 6.3.4.1.6(b) 6.3.4.1.6(c) 6.3.5.0 6.3.5.1.1 6.3.5.1.4(a) 6.3.5.1.4(b) 6.3.5.1.4(c) 6.3.5.1.6(a) 6.3.5.1.6(b) 6.3.5.1.6(c) 6.3.5.1.6(d) 6.3.5.1.7(a) 6.3.5.1.7(b) 6.3.5.1.7(c) 6.3.5.1.7(d) 6.3.5.1.7(e) 6.3.5.1.8(a) 6.3.5.1.8(b) 6.3.5.1.8(c) Current Form Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Vector Graphics Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics

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MIL-HDBK-5H 1 December 1998
Figure No. 6.3.5.1.8(d) 6.3.5.1.8(e) 6.3.5.1.8(f) 6.3.5.1.8(g) 6.3.5.1.9(a) 6.3.5.1.9(b) 6.3.5.1.9(c) 6.3.6.0 6.3.6.1.1 6.3.6.1.2 6.3.6.1.3 6.3.6.2.1(a) 6.3.6.2.1(b) 6.3.6.2.4(a) 6.3.6.2.4(b) 6.3.7.0 6.3.7.1.1 6.3.7.1.2 6.3.7.1.3(a) 6.3.7.1.3(b) 6.3.7.1.4 6.3.7.1.5 6.3.7.1.7 6.3.8.0 6.3.8.1.1 6.3.8.1.4 6.3.8.1.5(a) 6.3.8.1.5(b) 6.3.8.1.6(a) 6.3.8.1.6(b) 6.4.1.0 6.4.1.1.1 6.4.1.1.2 6.4.1.1.3 6.4.1.1.4(a) 6.4.1.1.4(b) 6.4.1.1.5 6.4.1.1.7 6.4.2.0 6.4.2.1.1(a) 6.4.2.1.1(b) 6.4.2.1.2 6.4.2.1.4(a) 6.4.2.1.4(b) 6.4.2.1.4(c) 6.4.2.1.5 6.4.2.1.6(a) 6.4.2.1.6(b) 6.4.2.1.8(a) Current Form Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Vector Graphics Scanned

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MIL-HDBK-5H 1 December 1998
Figure No. 6.4.2.1.8(b) 6.4.2.1.8(c) 6.4.2.1.8(d) 7.2.1.0 7.2.1.1.1 7.2.1.1.4 7.3.2.0 7.3.2.1.6(a) 7.3.2.1.6(b) 7.3.2.2.6 7.4.1.0 7.4.1.1.1 7.4.1.1.4(a) 7.4.1.1.4(b) 7.4.1.1.5 7.4.1.1.6 7.4.2.0 7.4.2.1.4 7.4.2.1.6 7.5.1.1.6(a) 7.5.1.1.6(b) 7.5.1.1.6(c) 7.5.1.1.6(d) 7.5.1.1.6(e) 7.5.1.1.6(f) 7.5.1.1.6(g) 7.5.1.1.6(h) 7.5.1.1.6(i) 7.5.1.1.6(j) 7.5.1.1.6(k) 7.5.1.1.6(l) 7.5.2.1.6(a) 7.5.2.1.6(b) 7.5.2.1.6(c) 7.5.2.1.6(d) 7.5.2.1.6(e) 7.5.2.1.6(f) 7.5.2.1.6(g) 7.5.2.1.6(h) 7.5.2.1.6(i) 7.5.2.1.6(j) 8.2.1 8.2.2.3.1.1(a) 8.2.2.3.1.1(b) 8.2.2.3.1.1(c) 8.2.2.3.2.1 8.2.2.3.2.2(a) 8.2.2.3.2.2(b) 8.2.2.3.2.2(c) Current Form Scanned Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Vector Graphics Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned

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MIL-HDBK-5H 1 December 1998
Figure No. 8.2.2.3.2.2(d) 8.2.2.3.2.2(e) 9.2.3 9.2.4 9.2.6 9.2.11 9.2.12 9.2.15(a) 9.2.15(b) 9.3.1.1.2 9.3.1.1.3(a) 9.3.1.1.3(b) 9.3.1.2 9.3.1.3 9.3.1.4(a) 9.3.1.4(b) 9.3.1.5 9.3.1.6.1 9.3.1.6.2 9.3.2.3(a) 9.3.2.3(b) 9.3.2.3(c) 9.3.2.4 9.3.2.5(a) 9.3.2.5(b) 9.3.2.5(c) 9.3.2.5(d) 9.3.2.7(a) 9.3.2.7(b) 9.3.2.7(c) 9.3.4.1(a) 9.3.4.1(b) 9.3.4.1(c) 9.3.4.1(d) 9.3.4.3 9.3.4.4 9.3.4.5 9.3.4.7 9.3.4.10(a) 9.3.4.10(b) 9.3.4.10(c) 9.3.4.12(a) 9.3.4.12(b) 9.3.4.13 9.3.4.16(a) 9.3.4.17(a) 9.3.4.17(b) 9.3.4.17(c) 9.3.4.17(d) Current Form Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Vector Graphics Scanned Scanned Vector Graphics Scanned Scanned Vector Graphics Vector Graphics Vector Graphics Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned

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MIL-HDBK-5H 1 December 1998
Figure No. 9.3.4.17(e) 9.3.4.17(f) 9.3.4.17(g) 9.3.4.17(h) 9.3.5.1(a) 9.3.5.1(b) 9.3.5.2 9.3.5.6 9.3.6.2 9.3.6.7 9.3.6.8(a) 9.3.6.8(b) 9.3.6.8(c) 9.3.6.8(d) 9.4.1.3 9.4.1.3.4(a) 9.4.1.3.4(b) 9.4.1.3.4(c) 9.4.1.3.4(d) 9.4.1.3.4(e) 9.4.1.5.2(a) 9.4.1.5.2(b) 9.4.1.5.2(c) 9.4.1.5.2(d) 9.4.1.5.2(e) 9.4.1.5.2(f) 9.4.1.5.2(g) 9.4.1.5.2(h) 9.4.1.5.3 9.4.1.6 9.4.1.7.2 9.4.1.7.2, cont. 9.4.2.2 9.4.2.3.2 9.4.2.3.5(a) 9.4.2.3.5(b) 9.4.2.5.2 9.4.2.5.3 9.5.1.3 9.5.1.5.1(a) 9.5.1.5.1(b) 9.5.1.5.1(c) 9.5.1.5.3 9.6.3 A.1 Current Form Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned Scanned

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STANDARDIZATION DOCUMENT IMPROVEMENT PROPOSAL
INSTRUCTIONS

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The preparing activity must complete blocks 1, 2, 3, and 8. In block 1, both the document number and revision letter should b given. The submitter of this form must complete blocks 4, 5, 6, and 7, and send to preparing activity. The preparing activity must provide a reply within 30 days from receipt of the form.

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NOTE: This form may not be used to request copies of documents, nor to request waivers, or clarification of requirements on curr ontracts. Comments submitted on this form do not constitute or imply authorization to waive any portion of the referenced ocument(s) or to amend contractual requirements.
1. DOCUMENT NUMBER 2. DOCUMENT DATE (YYYYMMDD)

I RECOMMEND A CHANGE:

MIL-HDBK-5H

1998-12-01

DOCUMENT TITLE METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLES STRUCTURES

NATURE OF CHANGE (Identify paragraph number and include proposed rewrite, if possible. Attach extra sheets as needed.)

REASON FOR RECOMMENDATION

SUBMITTER b. ORGANIZATION d. TELEPHONE (Include Area Code) (1) Commercial (2) AUTOVON (if applicable) NAME ASC/ENSI b. TELEPHONE Include Area Code) (1) Commercial 7.DATE SUBMITTED (YYYYMMDD)

NAME (Last, First, Middle Initial)

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PREPARING ACTIVITY (2) AUTOVON

ADDRESS (Include Zip Code) 2530 LOOP ROAD W B560

WRIGHT-PATTERSON AFB, OH 45433-7101

IF YOU DO NOT RECEIVE A REPLY WITHIN 45 DAYS, CONTACT: Defense Standardization Program Office (DLSC-LM) 8725 John J. Kingman road, Suite 2533 Ft. Belvoir, VA 22060-2533 Telephone (703) 767-6888 AUTOVON 427-6888

orm 1426, FEB 1999 (EG)

PREVIOUS EDITION IS OBSOLETE

WHS/DIOR, Feb 99


								
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