load case 170 of the ASME 31.3

NOTICE REGARDING CODE CASES OF THE ASME B31 CODE FOR PRESSURE PIPING

All B31 Code Cases in effect as of September 21, 2007 will remain available for use unless annulled by the B31 Standards Committee.

B31 CASE 178

B31 Case 178 continues on following page

CASES OF THE CODE FOR PRESSURE PIPING B31

B31 Case 178 Providing an Equation for Longitudinal Stress for Sustained Loads in ASME B31.3

Construction

Approval Date: May 6, 2005 This Case shall expire on May 1, 2008, unless previously annulled or reaffirmed

Inquiry:

ASME B31.3 provides a description for determining SL for sustained loads. Is there an equation that may be used? Reply:

It is the opinion of the committee that, in the absence of more applicable data and in accordance with para. 302.3.5(c), the following equation may be used to calculate SL for sustained loads.

22 )2()|(| tbaL SSSS ++= where

the definitions in para. 319.4.4 apply and,

Sa = stress due to axial loads1 = Fa/Ap

Fa = longitudinal force due to pressure2, weight, and other sustained loadings

Ap = cross-sectional area considering nominal pipe thickness less the sum of the mechanical (thread or groove depth), corrosion and erosion allowances

Sb = resultant, intensified bending stress3 due to pressure, weight, and other sustained loadings

ZMIMI

S ooiib22 )()( +=

Ii = in-plane sustained stress index4. In the absence of more applicable data, Ii is taken as the greater of (0.75ii) or 1.00

Io = out-plane sustained stress index4. In the absence of more applicable data, Io is taken as the greater of (0.75io) or 1.00

St = torsional stress3 due to pressure, weight, and other sustained loadings1 = Mt/2Z

NOTES: 1 In the absence of more applicable data, Sa and St need not be intensified.

B31 CASE 178

2 Fa includes the longitudinal force due to pressure iAP for piping systems that contain no

expansion joints, where 4/2dAi = , and d is the pipe inside diameter considering pipe wall thickness less allowances. For piping systems with expansion joints, it is the responsibility of the designer to determine the longitudinal force due to the pressure in the piping system.

3 Z shall be based on the nominal section, less the sum of the mechanical (thread or groove depth), corrosion and erosion allowances.

4 It is the responsibility of the designer to determine Ii and Io; in cases where these indices are based on stress intensification factors, it is the responsibility of the designer to determine ii and io for all components not explicitly addressed in Appendix D (e.g., elbows/bends/miters other than 90 degrees, base-ells, reducing elbows, crosses, etc.).

B31 CASE 180


B31 CASE 180 Leak Testing of Subassemblies of Jacketed Piping for use in ASME B31.3 Piping

Systems

Approval Date: January 5, 2007 Inquiry: Does ASME B31.3 permit an alternate leak test for jacketed piping in which it is impracticable to visually examine the welded joints and connections for leaks in accordance with para. 345.2.2(a)? Reply: Visually observing the joints and connections during the leak test in accordance with para. 345.2.2(a) and 345.3.1 is not required provided all of the following conditions are satisfied:

1. The welded joints and connections are on the inner pipe of jacketed piping. 2. A leak test is performed that otherwise meets the requirements of para. 345.1

except visual examination of joints and connection in accordance with para. 345.2.2(a) and 345.3.1 is not required.

3. A sensitive leak test is performed in accordance with para. 345.8 to demonstrate leak tightness of welded joints and connections that are not visually examined during the leak testing requirements in 2 above.

B31Case1812(ApprovalDate:January4,2012)UseofAlternativeUltrasonicExaminationAcceptanceCriteriainASMEB31.3

Original Inquiry: Under what conditions and limitations may alternative UT acceptance criteria apply in lieu of those described in para. 344.6.2 of ASME B31.3? When specified by the owner, the ultrasonic examination acceptance criteria included below may be applied for welds in material greater than or equal to 25mm (1.0 in.) in thickness1 in accordance with ASME B31.3 provided the following requirements are met: 1) General/Scope:

a) The examination shall be conducted using automated or semi-automated techniques utilizing computer based data acquisition.

b) The examination shall be performed in accordance with a written procedure approved by a Level III and conforming to the requirements of ASME Section V, Article 4 Mandatory Appendix VIII and: i) For Phased Array ASME Section

V, Article 4, Mandatory Appendix V

ii) For Time of Flight Diffraction (TOFD) - ASME Section V, Article 4, Mandatory Appendix III

c) Procedure qualification shall meet the requirements of ASME Section V, Article 4, Mandatory Appendix IX.

2) Equipment A mechanical guided scanner capable of maintaining a fixed and consistent search unit position relative to the weld centerline shall be used.

3) Personnel a) Set-up and scanning of welds shall be

performed by personnel certified as Level II or III (or by Level I personnel under the direct supervision of Level II personnel).

b) Interpretation and evaluation of data shall be performed by Level II or III personnel.

c) Examination personnel shall be qualified and certified following a procedure or program as described in ASME BPV Code, Section V, Article 1, T-120 (e), (f), (h) and (i).

d) Personnel demonstration requirements shall be as stated in ASME Section V, Article 4 Mandatory Appendix VII.

4) Examination a) The initial straight beam scan for

reflectors that could interfere with the angle beam examination shall be performed (a) manually, (b) as part of a previous manufacturing process, or (c) during the weld examination, provided detection of these reflectors is included in the demonstration as required in 1(c) above.

b) The examination area shall include the volume of the weld, plus the lesser of 25mm (1.0 in.) or t of adjacent base metal. Alternatively, the examination volume may be reduced to include the actual heat affected zone (HAZ) plus 6mm (0.25 in.) of base material beyond the heat affected zone on each side of the weld, provided the extent of the weld HAZ is measured and documented.

c) Scanning may be peformed at reference level provided the procedure qualification was performed at reference level.

5) Data Recording Data shall be recorded in the unprocessed form with no thresholding. The data record shall include the complete examination area as specified in (4)(b) above.

1 For wall thicknesses less than 25mm (1.0 in.), the acceptance criteria stated in paragraph 344.6.2 of B31.3 shall be used.


6) Data Analysis

a) Reflectors exceeding the limits below shall be investigated to determine whether the indication originates from a flaw or is a geometric indication in accordance with 6(b) below. i) For amplitude based techniques, the

location, amplitude, and extent of all reflectors that produce a response greater than 20% of the reference level shall be investigated.

ii) For non-amplitude based techniques, the location and extent of all images that have an indicated length greater than 4.0mm (0.16 in.) shall be investigated.

b) Ultrasonic indications of geometric and/or metallurgical origin shall be classified as specified in ASME Section V, Article 4 Paragraph T-481.

c) Alternatively, other techniques or NDE methods may be used to classify an indication as geometric (e.g., alternative beam angles, radiography). The method employed is for information only to classify the indication as geometric, and ASME B31.3 requirements for examination techniques are only required to the extent they are applicable.

7) Flaw Evaluation a) The dimension of the flaw(s) shall be

determined by the rectangle that fully contains the area of the flaw(s). (Refer to Fig. 1) i) The length, , of the flaw shall be

drawn parallel to the inside pressure retaining surface of the component.

ii) The height, h, of the flaw shall be drawn normal to the inside pressure retaining surface of the component.

iii) The flaw shall be characterized as a surface or subsurface flaw, as shown in Figure 1.

iv) A subsurface indication shall be considered as a surface flaw if the separation (S in Figure 1) of the indication from the nearest surface of the component is equal to or less than half the through wall

dimension (h in Figure 1, sketch [b]) of the subsurface indication.

b) Multiple Flaws i) Discontinuous flaws that are

oriented primarily in parallel planes shall be considered to lie in a single plane if the distance between the adjacent planes is equal to or less than 13mm (0.50 in.) or 0.5t, whichever is less.

ii) If the space between two flaws aligned along the axis of weld is less than the height of the flaw of greater height, the two flaws shall be considered a single flaw.

iii) If the space between two flaws aligned in the through-thickness dimension is less than the height of the flaw of greater height, the two flaws shall be considered a single flaw.

8) Flaw Acceptance Criteria Flaws shall be evaluated against the applicable acceptance criteria of Table 1 or 2, except that flaw length (l) shall not exceed 4t, regardless of flaw height (h) or the calculated aspect ratio.


TABLE 1

Acceptance Criteria for Surface Flaws

Aspect Ratio, h/

Weld Thickness 25mm to 64mm

(1.0 in. to 2.5 in.) 100mm to 300mm (3.9 in. to 11.8 in.)

h/t h/t0.00 < 0.031 < 0.019 0.05 < 0.033 < 0.020 0.10 < 0.036 < 0.022 0.15 < 0.041 < 0.025 0.20 < 0.047 < 0.028 0.25 < 0.055 < 0.033 0.30 < 0.064 < 0.038 0.35 < 0.074 < 0.044 0.40 < 0.083 < 0.050 0.45 < 0.085 < 0.051 0.50 < 0.087 < 0.052

General Notes: (a) t = thickness of the weld excluding any allowable reinforcement. For a

butt joint joining two members having different thickness at the joint, t is the thinner of the two thicknesses joined. If a full penetration weld includes a fillet weld, the effective throat dimension of the fillet weld shall be included in t.

(b) Aspect Ratio (h/) used may be determined by rounding the calculated h/ down to the nearest 0.05 increment value within the column, or by linear interpolation.

(c) For intermediate thickness t (weld thicknesses between 64mm and 100mm [2.5 in. and 3.9 in.]) linear interpolation is required to obtain h/t values.

TABLE 2 Acceptance Criteria for Subsurface Flaws

Aspect Ratio, h/

Weld Thickness 25mm to 64mm

(1.0 in. to 2.5 in.) 100mm to 300mm (3.9 in. to 11.8 in.)

h/t h/t0.00 < 0.068 < 0.040 0.10 < 0.076 < 0.044 0.20 < 0.086 < 0.050 0.30 < 0.098 < 0.058 0.40 < 0.114 < 0.066 0.50 < 0.132 < 0.076 0.60 < 0.156 < 0.088 0.70 < 0.180 < 0.102 0.80 < 0.210 < 0.116 0.90 < 0.246 < 0.134 1.00 < 0.286 < 0.152

General Notes: (a) t = thickness of the weld excluding any allowable reinforcement. For a

butt joint joining two members having different thickness at the joint, t is the thinner of the two thicknesses joined. If a full penetration weld


includes a fillet weld, the effective throat dimension of the fillet weld shall be included in t.

(b) Aspect Ratio (h/) used may be determined by rounding the calculated h/ down to the nearest 0.05 increment value within the column, or by linear interpolation.

(c) For intermediate thickness t (weld thicknesses between 64mm and 100mm [2.5 in. and 3.9 in.]) linear interpolation is required to obtain h/t values.

Figure 1: Surface and Subsurface Indications

h h

h

S > 0.5h

S < 0.5h

(c) Subsurface Flaw

(a) Surface Flaw (b) Surface Flaw

ASME B31.3 CASES B31 CASE 184 Use of Ultrasonic Examination of Welds as an Alternative to Radiographic Examination in ASME B31.3, Chapter IX Approval Date: 10/29/2009 This Case shall expire upon the publication of ASME B31.32010 Edition. Inquiry: Under what conditions and limitations may ultrasonic examination of welds be used as an alternative to radiographic examination for ASME B31.32008 Edition, Chapter IX piping systems? Reply: It is the opinion of the Committee that ultrasonic examination of welds may be used as an alternative to the radiographic examination specified in ASME B31.32008 Edition for Chapter IX piping systems, provided that the requirements specified in paras. K341.4.2 and K342 and Table K341.3.2 be modified as follows, and that the requirements of a new para. K344.6.3, shown below, be met: K341.4.2 Radiographic and Ultrasonic Examination

(a) All girth, longitudinal, and branch connection welds shall be 100% radiographically examined, except as permitted in (b) below.

(b) When specified in the engineering design and with the owners approval, ultrasonic examination of welds may be substituted for radiographic examination where w 13 mm ( in.).

(c) In-process examination (see para. 344.7) shall not be substituted for radiographic or ultrasonic examination of welds. NOTE: w = Twbar K342 EXAMINATION PERSONNEL

Paragraph 342 applies, except that personnel performing and evaluating results of ultrasonic examination of welds shall be qualified and certified UT Level II or III in accordance with ASNT SNT-TC-1A, ACCP (ASNT Central Certification Program), or CP-189 (Qualification and Certification of Nondestructive Testing Personnel). Qualification of these personnel shall also be by written examination.

K344.6.3 Welds. The method for ultrasonic examination of welds shall be as specified in the ASME BPV Code, Section V, Article 4 and Section VIII, Division 3, KE-301 and KE-302, except that

(a) Performance demonstration shall be required. (b) The employers written practice for UT personnel qualification shall meet ASNT SNT-TC-1A,

ACCP, or CP-189. The recommended guidelines in SNT-TC-1A, ACCP, or CP-189 shall be required. (c) Written procedure in accordance with Section V, T-421.1 shall be required. (d) Procedure qualification in accordance with Section V, T-421.1 shall be required.

REVISED TABLE K341.3.2: See Page 2.

CASES OF THE CODE FOR PRESSURE PIPING - B31

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(08)

ASME B31.3-2008

Table K341.3.2 Acceptance Criteria for WeldsCriteria (A-E) for Types of Welds, and for Required

Examination Methods [Note (I)]Type of Weld

Methods Longitudinal BranchType of Ultrasonics or Girth Groove Fillet Connection

Imperfection Visual Radiography Groove [Note (2)] [Note (3)] [Note (4)]

Crack X X A A A Alack of fusion X X A A A AIncomplete penetration X X A A A AInternal porosity X B B NA BSlag inclusion or elongated indication X C C NA CUndercutting X X A A A ASurface porosity or exposed slag inclusion X A A A AConcave root surface (suck-up) X X D D NA DSurface finish X E E E EReinforcement or internal protrusion X F F F F

GENERAL NOTE: X = required examination; NA = not applicable; ... = not required.

Criterion Value Notes for Table K341.3.2

Criterion

Symbol

A

Measure

Extent of imperfection

Acceptable Value Limits [Note (5)]

Zero (no evident imperfection)B Size and distribution of internal porosity See BPV Code, Section VIII, Division I, Appendix 4C Slag inclusion or elongated indication: Indications are unacceptable if the amplitude exceeds the reference

level, or indications have lengths that exceedIndividual length t. < 19 mm (Yo in) 19 rom (% in.) < 1;57 mm (2~ in.) t" > 57 mrn (2Y. in.)

6mrn~~ ~~~~Cumulative length ~ t .. in any 12 t.. weld length

D Depth of surface concavity Wall Thickness, Depth of Surface Concavity,Two mm (in.) mm (in.)

S 13 (%) $ 1.5 e1t6)> 13 CV2) and $ 51 (2) ~ 3 (Va)> 51 (2) $ 4 (%2)and total joint thickness including weld reinforcement

"Z TwE Su rface rough ness $ 12.5 f.Lm (500 f.Lin.) Ra (see ASME B46.1 for definition of

roughness average, Ra )

F Height of reinforcement or internal protrusion [Note (6)]in any plane through the weld shall be within thelimits of the applicable height value in the tabula-tion at the right. Weld metal shall be fused with andmerge smoothly into the component surfaces.

Wall Thickness,Tw , mm (in.)

$13 eh)> 13 (%) and $ 51 (2)> 51 (2)

External Weld Reinforcementor Internal Weld Protrusion,

mm (in.)$ 1.5 e1t6)

~ 3 (Va)$4 Wd

NOTES:(1) Criteria given are for required examination. More stringent criteria may be specified in the engineering design.(2) longitudinal welds include only those permitted in paras. K302.3.4 and K305. The radiographic criteria shall be met by all welds,

including those made in accordance with a standard listed in Table K326.1 or in Appendix K.(3) Fillet welds include only those permitted in para. K311.2.2.(4) Branch connection welds include only those permitted in para. K328.5.4.(5) Where two limiting values are given, the lesser measured value governs acceptance. Tw is the nominal wall thickness of the thinner of

two components joined by a butt weld.(6) For groove welds, height is the lesser of the measurements made from the surfaces of the adjacent components. For fillet welds,

height is measured from the theoretical throat; internal protrusion does not apply. Required thickness tm shall not include reinforce-ment or internal protrusion.

132

Copyright 2008 by the American Society of Mechanical Engineers. ~No reproduction may be made ofthis material without written consent of ASME. ~

CASES OF THE CODE FOR PRESSURE PIPING - B31

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B31 CASE 185


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ASME B31.3 CODE CASE 185

Title: Use of Standard Helium Leak Test for a Vacuum-only Piping System (Paragraph 345)

Approval Date: December 22, 2009

Inquiry:

Under what circumstances does ASME B31.3 permit the use of helium mass spectrometer leaktests performed under a vacuum as a substitute for the leak test requirements specified in ASMEB31.3, para. 345?

Reply:

In the opinion of the Committee, the qualified helium leak tests under vacuum conditions in theASME BPV Code, Section V, Article 10, Appendix V and Appendix IX are acceptablesubstitutes for the testing requirements identified in para. 345 of ASME B31.3 provided thefollowing conditions are met:

1. The piping system is expected to operate only under vacuum (i.e., sub-atmospheric pressure)conditions.

2. Any leakage into the piping system that could result in an internal reaction (e.g., combustionor explosion) that increases the pressure above atmospheric shall be prevented.

3. All system joints and connections shall be leak tested. Piping welds and joints to be testedshall be uninsulated and exposed, and shall not be primed, painted or otherwise coated.

4. Helium leak testing is performed at vacuum conditions sufficient for the mass spectrometerhelium leak tests of ASME BPV Code, Section V, Article 10, Appendices V and IX, or atpressures below 10 millibars absolute (

B31 CASE 185


Page 2 of 2

8. Test reports, including records of personnel qualifications, shall meet the requirements ofASME BPV Code, Section V, Article 10, Item T-1091 and shall be retained for at least fiveyears.

9. Options of the ASME BPV Code, Section V, Article 10 test methods, which allow theengineering design to modify specified requirements of the Appendix V and Appendix IXtest methods (such as acceptability limits for system leak tightness), may only be exercisedso as to make these requirements more sensitive or more conservative.

10. The use of the vacuum leak test instead of the pressurized leak test of ASME B31.3,para. 345 shall be specified in the engineering design and shall be accepted by the Owner.

____________________________________________________________________

B31 CASE 188

Minimum Hydrostatic Test Pressure for ASME B31.3, Chapter IX (Para. K345.4.2)

ANNULLED

Annulment Date: February 27, 2015

Reason: Requirements incorporated in ASME B31.3 Code.

B31 Code Case 191 Cu-13Zn-1.1Ni-Si-Al Alloy Seamless Pipe and Tube ASME B31.3 Approval Date: January 21, 2015

Inquiry: May precipitation-hardened (Temper Designation TF00) Cu-13Zn-1.1Ni-Si-Al alloy (UNS No. C69100) seamless pipe and tube conforming to the requirements of ASTM B706-00 (R2011) be used under the rules of ASME B31.3?

Reply: Yes, provided:

(a) The maximum allowable stress values for the material shall be those given in

Table 1;

(b) Welded and brazed construction is not permitted; (c) The maximum use temperature shall be 204C (400F);

(d) Certification to the ASTM B706-00 (R2011) specification requirements shall be

mandatory.

Table1MaximumAllowableStressValues

ForMetalTemperatureNotExceeding,F

Stress,ksi

ForMetalTemperatureNotExceeding,C

Stress,MPa

100150200250300350400

20.020.020.020.020.019.9 19.5

4065100125150175200225

138138138138138137135132

Note: The maximum use temperature for this alloy is 204C (400F). The value listed at 225C is provided for interpolation purposes only.

Case 193 Approval Date: October 9, 2014 Cu-5.5Zn-4Si Casting Alloy UNS No. C87600 ASME B31.3 Inquiry: May Cu-5.5Zn-4Si Casting Alloy UNS No. C87600 conforming to the requirements of ASTM B584 be used for construction under the rules of ASME B31.3? Reply: Yes, provided:

(a) The basic allowable stress values for the material shall be those given in Table 1. A Casting Quality Factor, Ec, needs to be applied;

(b) The maximum use temperature shall be 177C (350F); (c) Separate weld procedure and performance qualifications shall apply to this

material. The welding procedure qualifications shall be in accordance with ASME Section IX.

Table 1 Basic Allowable Stress Values

For Metal Temperature Not Exceeding, F

Stress, ksi

For Metal Temperature Not Exceeding, C

Stress, MPa

100 20.0 40 138 150 20.0 65 138200 20.0 100 138250 20.0 125 138300 20.0 150 138350 20.0 175 138

200 137

Note: The maximum use temperature for this alloy is 177C (350F): The value listed at 200C is provided for interpolation purposes only.

Case 196 Approval Date: May 15, 2015 Ductile Iron Casting UNS No. F33100 ASME B31.3 Inquiry: May Ductile Iron Castings UNS No. F33100 conforming to the requirements of ASTM A536, Grade 65-45-12 be used for construction under the rules of ASME B31.3? Reply: Yes, provided:

(a) The maximum allowable stress values for the material shall be those given in Table 1;

(b) A casting quality factor, Ec, of 0.80 shall also be applied, except as permitted in (c);

(c) The casting quality factor may be increased by performing supplementary examination(s) listed in Table 302.3.3(c). The casting shall have first been visually examined as required by MSS SP-55, Quality Standard for Steel Castings for Valves, Flanges and Fittings and other Piping Components Visual Method;

(d) The maximum use temperature shall be 260C (500F); (e) The minimum use temperature shall be -30C (-20F); (f) All other requirements of ASME B31.3 shall be followed.

Table 1 Maximum Allowable Stress Values

For Metal Temperature Not Exceeding, C

Stress, MPa

For Metal Temperature Not Exceeding, F Stress, ksi

40 149 100 21.7 65 149 150 21.7

100 149 200 21.7 125 149 250 21.7 150 149 300 21.7 175 149 350 21.7 200 148 400 21.7 225 148 450 21.7 250 148 500 21.6 275 147

Note: The maximum use temperature for this alloy is 260C (500F). The value listed at 275C is provided for interpolation purposes only.

Documents

load case 170 of the ASME 31.3