aws material trace ability

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Q: Can you give a quick explanation of wha t is meant by two -wa y trace- ability?  A: Let’s define this using structural steel as an examp le. “Two-way trace abilit y” basically means that when a project is completed you should be able to do the following: 1) Go to the structure, point to a piece of steel, and be able to trace it back to its Certified Material Test Report (CMTR) supplied by the steel manufacturer; and 2) Pull out a CMTR from the project documentation and identify all areas of the structure where that steel has been installed.  There are a number of ways to accomplish this, but in every case some degree of control and documentation is req uir ed durin g the var ious pha ses of construction. One of the simplest ways is by use of the fabrication drawings and the cutting or nesting plan that is used  when the plate is first cut into pieces.  Th e fab ric ati on dra win gs sho uld, of course, indicate for each individual item the mat eria l’s type, gra de, thi ckness, dimensions, and some sort of piece mark designation. When the time comes to cut the items from raw plate, the cutting/nest- ing plan will show for each individual plate the same information (i.e., the material’s type, grade, and thickness, and the piece mar k des ign ati on and dimens ion s for each individual piece to be cut from that pla te). Prior to cut tin g, eac h ind ivi dua l piece mark should be laid out on the plate and the appropriate traceability informa- tion (piece mark as a minimum) must be ph ys ic al ly ma rk ed on th e pl at e in th e appr opri ate loca tion s. Add ition ally , the plate’s heat number or plate number must be recorded on the cutting/nesting plan.  The unique cutting/nesting plan num- ber or th e mat eri al’ s hea t num ber can then be recorded on the as-built fabrica- tion drawings, and/or the necessary infor- mation (CMTR number , heat number, cut- ting/nesting plan numbe r , fabrica tion draw ing numb er , and piece mark num- ber) can be entered into a spreadsheet.  Th is is a simpli fie d exp lan ati on of two- way trace abili ty . Of cour se, durin g fab ric ati on some deg ree of con tro l is required to ensure that each piece mark is indeed installed in its designated loca- tion in accordance with the fabrication dr awings. The re may be oth er det ail s that need to be worked out to design a fully functioning traceability system (for instance, what happens when additional cuts are made to the structure during erection). This should all be detailed in a mate rial trac eabili ty proce dure that is specific to your needs and requirements. Q: We’ve just signed on to do field insta llati on of a structur al stee l job that has bolte d conne ctio ns on gal-  van ized girde rs using high -stre ngth bolts. The spec says that before we put the joi nts toget her , we have to hand wire brush the faying surfaces. Powe r wire br ushi ng is proh ibit ed. It seems st upid to ma ke us brush th ese surfa ce s but sa y we ca n’ t  power brush them, and nobody here can figure out why this is required.  A: It took a while to find the answer to this, but it finall y was disco ver ed in a doc ume nt pub lish ed by the Res ear ch Council on Structural Connections titled “Specification for Structural Joints Using  AS TM A32 5 or A49 0 Bol ts,” June 23, 2000, edition. It seems to apply to your case. Based on what you say and what is in this documen t, the connect ions you are talking about are slip-critical joints.  When these joint s are hot- di p galva - nized, if prior to assembly the faying sur- faces are roughened by hand wire brush- ing, the mean slip coefficient and there- for e the perfo rman ce of the joint are impr oved. This docu ment spec ifica lly states in the commentary to Section 3.2.2 that power wir e brus hin g “may polish rat her than rou ghe n the surfa ce, or remove the coating.” It is likely this pub- lication is somewhere referenced in the specification for your project. It appears you may be unfamiliar with all of the requirements for this installa- tion project you’ve signed on to do. It is recommend ed you familia rize your self  with all of the project documentation and requirements. Q: We ar e do in g a structu ra l jo b to  AWS D1.1 for an international client and the drawings use the metric sys- tem. To help avoid confusion, we have used the metric system for our proce- dure s for thi s proj ect. Recent ly thi s ha s beco me a bit of an issue, fo r in st ance wi th re ga rd to we ld re in-  forc eme nt. The cod e all ows 1  ⁄ 8-i n. (3 mm). One eighth of an inch is actual- ly 3.2 mm, so our welders are being penalized by using the metric system.  What are your thoughts on this?  A: AWS D1.1:2002 in paragraph 1.8 states that “this standard makes use of both U.S. Cus tom ary Uni ts and th e Int erna tio nal System of Units (SI). The measurements may not be exact equivalents; therefore, each system shall be used independently of the other witho ut combin ing in any  way.” Basically, you need to decide which system of measurement you are going to use, and stick with it. If your point of view is that you are calculating SI equivalents from the U.S. units, then theoretically you are penal- ized on weld reinforcement, as you note. However, you gain in other areas, such as depth of undercut (refer to Table 6.1).  A better way to look at this is that you are not calculating equiv alent s, but simply using the values given in D1.1M (refer once again to paragraph 1.8). If you are having “issues” over 0.2 mm of wel d rei nfo rcemen t, th ere are oth er problems that need to be addressed inter- nally within your organization. Q: Our customer received a tubular structure that had multiple fractures at the weld heat-affected zone region after getting it back from being gal-  vanized. The customer now wants to The Society is not responsible for any statement made or opinion expressed herein. Data and information developed by the authors are for specific informational purposes only and are not intended for use without independent, substantiating investigation on the  part of potential users. ANSWERED BY KENNETH ERICKSON & KIP MANKENBERG Inspection Trends encourages question and answer submissions. Please e-mail to the editor ( [email protected]  ).  KENNETH ERICKSON is Manager of Quality at National Inspection & Consultants, Inc., Ft. Myers, Fla. He is an AWS Senior Certified Welding Inspector, an ASNT National NDT Level III Inspector in four methods, and provides expert witness review and analysis for legal considerations. CLIFFORD “KIP” MANKENBERG is a consultant for International Quality Construction Management, Inc., Slidell, La. He is an  AWS Senior Certified Welding Inspector and an ASNT National NDT Level III Inspector in five methods. He has worked abroad for the last ten years in a variety of production and quality functions.        t        h       e answer is... 8 • INSPECTION TRENDS

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Page 1: AWS Material Trace Ability

8/2/2019 AWS Material Trace Ability

http://slidepdf.com/reader/full/aws-material-trace-ability 1/2

Q: Can you give a quick explanationof what is meant by two-way trace-

ability?

 A: Let’s define this using structural steelas an example. “Two-way traceability”basically means that when a project iscompleted you should be able to do thefollowing:

1) Go to the structure, point to a pieceof steel, and be able to trace it back to itsCertified Material Test Report (CMTR)supplied by the steel manufacturer; and

2) Pull out a CMTR from the project documentation and identify all areas of the structure where that steel has been

installed.  There are a number of ways to

accomplish this, but in every case somedegree of control and documentation isrequired during the various phases of construction. One of the simplest ways isby use of the fabrication drawings andthe cutting or nesting plan that is used when the plate is first cut into pieces.

  The fabrication drawings should, of course, indicate for each individual itemthe material’s type, grade, thickness,dimensions, and some sort of piece markdesignation. When the time comes to cut 

the items from raw plate, the cutting/nest-ing plan will show for each individual platethe same information (i.e., the material’stype, grade, and thickness, and the piecemark designation and dimensions for each individual piece to be cut from that plate). Prior to cutting, each individualpiece mark should be laid out on the plateand the appropriate traceability informa-tion (piece mark as a minimum) must bephysically marked on the plate in theappropriate locations. Additionally, theplate’s heat number or plate number must be recorded on the cutting/nesting plan.

 The unique cutting/nesting plan num-ber or the material’s heat number canthen be recorded on the as-built fabrica-tion drawings, and/or the necessary infor-mation (CMTR number, heat number, cut-ting/nesting plan number, fabricationdrawing number, and piece mark num-

ber) can be entered into a spreadsheet.  This is a simplified explanation of 

two-way traceability. Of course, duringfabrication some degree of control isrequired to ensure that each piece markis indeed installed in its designated loca-tion in accordance with the fabricationdrawings. There may be other detailsthat need to be worked out to design a fully functioning traceability system (for instance, what happens when additionalcuts are made to the structure duringerection). This should all be detailed in a material traceability procedure that isspecific to your needs and requirements.

Q: We’ve just signed on to do fieldinstallation of a structural steel jobthat has bolted connections on gal-

  vanized girders using high-strengthbolts. The spec says that before weput the joints together, we have tohand wire brush the faying surfaces.Power wire br ushing is prohibited.It seems stupid to make us brushthese surfaces but say we can’t power brush them, and nobody herecan figure out why this is required.

 A: It took a while to find the answer to

this, but it finally was discovered in a document published by the ResearchCouncil on Structural Connections titled“Specification for Structural Joints Using   ASTM A325 or A490 Bolts,”  June 23,2000, edition. It seems to apply to your case. Based on what you say and what isin this document, the connections youare talking about are slip-critical joints.  When these joints are hot-dip galva-nized, if prior to assembly the faying sur-faces are roughened by hand wire brush-ing, the mean slip coefficient and there-fore the performance of the joint areimproved. This document specifically states in the commentary to Section 3.2.2that power wire brushing “may polishrather than roughen the surface, or remove the coating.” It is likely this pub-lication is somewhere referenced in thespecification for your project.

It appears you may be unfamiliar withall of the requirements for this installa-

tion project you’ve signed on to do. It isrecommended you familiarize yourself  with all of the project documentation andrequirements.

Q: We are doing a structural job to AWS D1.1 for an international client and the drawings use the metric sys-tem. To help avoid confusion, we haveused the metric system for our proce-dures for this project. Recently thishas become a bit of an issue, for instance with regard to weld rein-

  forcement. The code allows 1 ⁄ 8-in. (3

mm). One eighth of an inch is actual-ly 3.2 mm, so our welders are being penalized by using the metric system.

 What are your thoughts on this?

 A: AWS D1.1:2002 in paragraph 1.8 statesthat “this standard makes use of both U.S.Customary Units and the InternationalSystem of Units (SI). The measurementsmay not be exact equivalents; therefore,each system shall be used independently of the other without combining in any  way.” Basically, you need to decide whichsystem of measurement you are going to

use, and stick with it.If your point of view is that you arecalculating SI equivalents from the U.S.units, then theoretically you are penal-ized on weld reinforcement, as you note.However, you gain in other areas, suchas depth of undercut (refer to Table 6.1). A better way to look at this is that you arenot calculating equivalents, but simply using the values given in D1.1M (refer once again to paragraph 1.8).

If you are having “issues” over 0.2 mmof weld reinforcement, there are other problems that need to be addressed inter-nally within your organization.

Q: Our customer received a tubular structure that had multiple fracturesat the weld heat-affected zone regionafter getting it back from being gal-

 vanized. The customer now wants to

The Society is not responsible for any statement made or opinion expressed herein. Data and information developed by the authorsare for specific informational purposes only and are not intended for use without independent, substantiating investigation on the

  part of potential users.

ANSWERED BY

KENNETH ERICKSON & KIP MANKENBERG

Inspection Trends encourages question and answer submissions. Please e-mail to the editor ( [email protected] ).

 KENNETH ERICKSON is Manager of Quality at National Inspection & Consultants, Inc., Ft. Myers, Fla. He is an AWS Senior Certified Welding Inspector, an ASNT National NDT Level III Inspector in four methods, and provides expert witness review and 

analysis for legal considerations.

CLIFFORD “KIP” MANKENBERG is a consultant for International Quality Construction Management, Inc., Slidell, La. He is an AWS Senior Certified Welding Inspector and an ASNT National NDT Level III Inspector in five methods. He has worked abroad for 

the last ten years in a variety of production and quality functions.

   t   h   e

answer is...

8 • INSPECTION TRENDS

Page 2: AWS Material Trace Ability

8/2/2019 AWS Material Trace Ability

http://slidepdf.com/reader/full/aws-material-trace-ability 2/2

ultrasonically test numerous remain-ing galvanized welds on the project.

  What type of calibration block isneeded to perform UT over galva-nized surfaces?

  AWS D1.1 paragraph 6.26.3 indicatesthat surfaces need to be free from spat-ter, paint, loose scale, and such from  which a search unit will be applied and

used. Just as paint is, galvanization is a protective coating and thus can affect theUT results. The variation in test results will be directly attributable to the thick-ness, surface profile, and any potentialdisbonding of the coating applied.Should the surface from which UT shallbe performed not be first cleaned to thebase metal, another option (with prior engineering approval) that may be used would be the following:

1) Perform a standard AWS UT cali-bration for tubular structures per AWSD1.1.

2) Establish a minimum of a two-point pitch-catch distance amplitude correc-tion (DAC) from a similar thicknesstubular structure that has not been gal- vanized. If this is not available, obtain a similar material composition and thick-ness piece as that of the tubular struc-tures to be tested. The DAC constructedshould correlate to at least two material

thicknesses for the item to be examinedor the sound path required for examiningthe entire cross-section thickness of the welds in question.

3) Perform this same transfer tech-nique on several different locations that have been galvanized and note the differ-ence in gain (±) to adjust this signal tothe previously constructed DAC. Sincethe thickness of the galvanized coating

may vary from item to item and also vary upon the item itself, it is important that   you check several locations to obtain a confident comfort level for the overall dif-ference in gain to be adjusted to your pri-mary reference level before any scan-ning takes place. If you find the differ-ence varies significantly at each location,  you may need to perform a transfer check at each weld to be examined andpossibly at each potential flaw location within each weldment.

Note: Ultrasonic testing may revealthat the cracks are isolated to the surfaceonly, in which case either magnetic parti-cle (MT) and/or liquid penetrant (PT)testing can be utilized to locate the frac-tures after the galvanized coating hasbeen removed from the weld area.

Q: Our company is attempting toqualify stainless steel welding proce-dures for which we cannot locate

information on the material within AWS B2.1 or ASME Section IX. Our customer has indicated the materialis a duplex stainless 2205.

 A: The material is actually UNS S32205.UNS stands for unified numbering sys-tem, which is a method used for identify-ing and cross-referencing different met-als, alloys, and filler metals. This materi-

al offers excellent pitting and crevice cor-rosion cracking and better stress corro-sion cracking resistance than 300 seriesaustenitic stainless steels. The yieldstrengths are also two to three timeshigher than those of 304, 316, or 317stainless steels. This material is not listedunder the list of prequalified base materi-als for AWS B2.1, D1.6, or D1.3, so eachapplication for use will need to be quali-fied by testing to the applicable standard. When ordering this material, be sure toorder by the UNS number and obtain a CMTR (certified material test report)

from the material supplier. Due to thetensile strength of the material (90 ksi),  you will need to utilize filler metal that complies with AWS A5.9.  Thanks to Damian Kotecki of TheLincoln Electric Company for providinginformation concerning duplex stainlesssteel. O

 WINTER 2004 • 9

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