ML20107C501
| ML20107C501 | |
| Person / Time | |
|---|---|
| Site: | Diablo Canyon  |
| Issue date: | 10/29/1984 |
| From: | Lockert S AFFILIATION NOT ASSIGNED |
| To: | |
| Shared Package | |
| ML20107C466 | List: |
| References | |
| OL, NUDOCS 8411020550 | |
| Download: ML20107C501 (38) | |
Text
{{#Wiki_filter:_-- - - - _ _ - _ - - _ - _ - - - - - - - - - - - - _ - - - - - - ( o $ UNIT ED STATES OF- AMERICA # 3' - N UCLEAR. REGULATORY COMMISSION
, -cqm8775Hl1&lT y BEFORE THE NUCLEAR REGULATORY C O M MI'S SIO N
'84 wy -1 PS:13 In the Matter of ) y n.
i
) D6cketi'Nos PACIFIC GAS AND ELECTRIC ) *
- rE50-275 50-323 COMPANY )
) Construction Quality (Diablo Canyon Nuclear Power ') Assurance, Licensee Plant, Units 1 and 2) ) Character and Compe-
-) tence .
AF FID AVIT OF STEVEN LOCKERT STATE OF CALIFORNIA '
)
) ss.
COUNTY OF SAN LUIS OBISPO ) My name is Steven Lockert and I am writing this affida- { vit in my own words without threat or inducement from anyone. The purpose of this statement is to inform the USNRC, court authorities, and public that officials of Pullman Power 1roducts Corporation (Pullman) and Pacific Gas & Electric Company (PG6E) t have made false statements. False statements before the Atomic t I Safety and Licensing Appeals Board (ASLB) and false statements before the Region V staff of the US NRC . The subjects of this discussion will be welded studs, quality control inspector training, and quality control inspector harassment and retaliation. The documents that contain false i i statements are: Diablo Canyon Letter (DCL) 84-067 dated 2/17/84, i DCL-84-078 dated 2/29/84, DCL-84-195 dated 5/29/84, DCL-84-239 dated 6/26/84,DCL-84-243 dated 6/29/84, Affidavit of ; 1 1 8411020550 841101 i PDR ADOCK 05000275 0 PDR I
et
'7. '
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- s. C. M. Neary, Pullman's Quality. Engineering Group Welding En- l
'. . gineer, F. I{lLyautey, Pullman's Assistant QA/QC Manager, J. P. Watson, Pullman's QC Welding Supervisor dated 3/18/84 and submitted to the ASLB for consideration of Construction Quality Assurance matters at Diablo Canyon, Affi-davit of-F. C. Breismeister, Bechtel' Manager of Research and '
Engineering, C . M . Neary , 'H. W. Karner, Pullman's QA/QC Manager, R. D. Kerr, PG&E Welding Engineer dated 3/19/84 and submit-ted to the ASLB. l.0 WELDED STUDS
-l 1.1 On January 13, 1984 a Pullman QC Inspector documented i
the use of ASTM A-307 and ASME SA-307 Grade B bolts for , I welded installations on hangers and supports for Class 1 safe-l
- ty related systems
- 07 (Reactor Coolant), 08 (Chemical and l
t Volume Control), 09 (Safety Injection), 10 (Residual Heat Re-moval), 12 (Containment Spray), and 14 (Component Cooling Water) . The bolts were not specifically ordered to be made from j a P-1 dlassified base n'aterial. The purchase orders for the bolts did not specify that the supplementary requirements for I
*I welded applications would be in effect. As stated in ASTM
- . y l A-307-82a (Exhibit 1) the supplementary requirements shall apply .
i 2 cl
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-:._. . . + . . . . . . ,.. .
only when specified in the purchase order or contract. Exhibit I was first presented by myself in a 3/21/84 affidavit to which PG&$ has yet.to show purchase orders showing supplementary requirements applicable. . 1.2 PG&E has stated in DCL-84-195 at para.. 226,241, DCL-84-239 at JIR-28 (pages 1-6) that the bolts installed without supplementary requirements in the purchase order for the bolts are acceptable because ASME Sec. III tells them so. Note that ; PG&E has convertently left out where in Sec. III this is stated. What has PG6E got to lose from a full and open disclosure of I the facts? Regardless, it is well known and universally prac-ticed that the master P-Number list for materials and their weld-l ability is found in Sec. IX of the ASME code. - t 1.3 For example Article IV, para. QW 421 of ASME-83, Sec. , i IX states ". . . base metals have beed assigned P-Numbers and ' t for ferrous base metals which have specified impact test require- l ments, Group Numbers within P-Numbers. These assignments are based essentially on comparable base metal characteristics such as composition, weldability, and mechanical properties, where this can be logically done. These assignments do not im-ply that base metals may be indiscriminate 1y substittited for a base metal which was used in a qualification test without con-sideration of compatibility from the standpoint of metallurgical I 3 1 L Il
( C properties, postweld heat treatment, design, mechanical proper-ties, and service requirements." < l.4 Gro'ut>1ng of Base Meta is for Qualification is the title for the master list of P-Numbers for procedure qualification pur-poses. QW-422 does not list A-307, grade B bolts as a P-1 base metal. Any claim to the contrary would be patently false. QW 422 in the place in the code where P-Numbers shall be de-termined and QW .422 is contained in Sec. IX; as it should be, 1: behind the definition in QW 421 for a quick and final reference. , 1.5 DCL-84-195 at 226 and 241, DCL-84-239 at JIR-28 (pages 2,5, and 6) allude to the Code Case N71-7 es; qualifying ' A-307, grade B bolts installed at Diablo Canyon Project. Breis- I meister at 12 and 13 also presents this case stating that this proof qualifies A-301, grade B bolts as P-1 base metal. The i j USNRC Re g ton V staff has also accepted the above citations as a final, " straw grabbing" qualification basis. Have any of-the above individuals even read the text of the Case before cit-ing its number? Conspicuously, the text was deleted from all references and no details were used to support the position. 1.6 ASME Section III Code Case N71-7 was approved 11/12/76
- 1 and annulled 11/21/80 The Case is no longer in effect because of a three year time restraint. This is an oversight PG&E forgot mention. Additional oversights noted are:
i
+ Clearly citing the the full Code reference N-71 -7 (1644-7), l I
l 4 i
+ Stating the time period of PG&E's contract specification verses the time N-71-7 was in effect,
+ Clearly stating where in PG&E's contract specifications the Code Chse had been implemented into design and quality assurance specifications for the project.
- 1. 7 The title of Code Case N-71'-l Additional Materials for Component Supports Sec. III, Division 1 Subsection NF Class 1, 2,3 and MC Component Supports clearly defines its boundaries.
The case was available only to nuclear power plants whose de-sign and quality assurance programs were dedicated to ASME Sec. i III. By PG&E's own admission in DCL-84-195, paragraph 250, "ASME Sections III and VIII only apply in a very limited degree to Pullman's scope of work at this site and are, therefore, not a part of the training program." 1.8 Had PG&E and the NRC Region V staff even read the Code i i Case text there were 7 conditions to be met. Three ccnditions i are worthy of note:
+ Adherence to Sec. III
+ 0.35 % limit on carbon for base metals to be welded
+ All supports built under the provisions of the Case be ident- s l'
i ified with the Case number. l Pullman had welded A-307 bolts with no limit on the percent of i i carbon, did not adhere to Sec. III, and did not identify the sup- I, 5 i i
1 ports where the special conditions of the code case applied. Pullm,an's quality assurance program was still struggling to 1. meet'its B 31.1 and B 31.7 commitments after 10 ' to 12 years ' of Diablo construction. To even imply that ASME Sec. III is applicable at Diablo in defense of welding A-307 grade B bolt-ing material as structural members holding base plates on Clas's i l systems is simply false and unsupported by the fact:,. ASME I-Sec. III Subsection NF, para. 4311.1 restricts stud welding to non-structural applications such as insulation, name plates, and locating lugs, Welded A-307 grade B bolts as reported per the i January 13, 1984 Discrepency Report temain a Codt non-confor-i mance. PG&E's positioit has been one false statement after a-nother in an inept coverup that just show a sloppy Code distor-tions to untenable positions. Note that PG&E and the NRC have 8 not offered to consult the ASME Code writing body for conforma-l tion of their position; an act they should of done instead of wast- 1 l t ing effort on useless Code citations that remain unsupported. ASME Code Case N-71-7 is openly presented as Exhibit 2. 2 .0 INSFECTOR TRAIN"' . 2.1 PG&E has attempted to support Pullman's position on QC I inspector training in DCL-84-195 at 248-258, DCL-84-243 at ' III-51 Federal law and the capstone of Nuclear Quality Assur- ! ( ance programs for plant construction, Appendix B of 10 C F R 50, _ , _ . i 6 1
J. wa s conspicuously absent from not only Pullman's training pro-l gram but also Pullman's reading list. See PG&E's response at
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249 'and attachnient 9 to DCL-84-195. If 'PG&E's trump card for Pullman's inspector training program is the supplemental reading list shown as attachment 9, it's quite obvious, there was' no I training. The original allegation stated training was inadequate. Let's not prop up reading and pretend it's training. 2.2 Directly beneath the capstone is ANSI N45.2, Quality As-surance Procram Requirements for Nuclear Facilities universally ' recognized to be in complete support with 10 CFR 50, Appendix i B. Again, conspicuously absent from Pullman's training or read- ' ing assignments. PG&E proudly proclaims in the Final Safety I Analysis Report, Chapter 17, bottom of page 17.0-1, "PG &E has actively contributed to the development of ANSI N45.2-1971, I and the PG&E quality assurance program is in substantial agree-ment with it." PG&E's QA program is directly responsible for its I i contractors QA programs and why QC inspectors did not recieve i i direct training or even a referral to ANSI N45.2 is incomprehens- ' ible. Pullman QC inspectors were the very people responsible for the implementation of procedures, codes, and standards in the ' I field working with the hardware that by law must be installed to the above requirements. The lack of training in ANSI N45.2 and ' the failure to even reference it to Pullman QC inspectors must be 7 d
1 f 4 seen in the proper context; a . complete'and criminal failure to meet the quality assurance commitments stated in .the FSAR.
- v. .
12.3 8. . DCL-84-195 at 251'shows the response PG&E's lawers
. provide to the lack of training accusations ". . . there is only an infrequent need for inspectors to interpret the code; they just-need to understand what the code covers and .the requirements ,
of the specific inspection activity." Pullman's Procedures ESD
^
223 for piping. supports and 243 for rupture restraints were pat-ently lacking in code and construction standards adherence. Pullman's procedures were attempts to interpret the code, right - or wrong, the QC inspector was then faced with interpreting the procedure. Hence ,' to say there was an infrequent need to inter-pret the codes is false and a patheticly weak response from lawers who know very little about inspection. 2.4 DCL-84-243 at 111-51 states "It was not until 1983 that t Pullman Power Products was first required by PG6E Specification 8711 to develop a Quality Assurance Program in accordance with ANSI N45.2. " There you have it ladies and gentleman, straight i from the horses mouth. Impossible as it may seem PG&E allowed '! \ l the construction of Diablo Canyon to procede for twelve years l t without requiring its major piping and piping supports contractor . j to adhere to the industry standard ANSI N45.2. Yet PG&E has I I claimed thats its Quality Assurance Program is in substantial l l- 8 i [, l
- .. .. . . . . ~ . . - . . . ..-.._~.v n - -- .- -=
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- agreement with ANSI N45.2 (FSAR, page 17.0-1.) Perhaps PG&E would like to ellaborate on just how Pullman's Quality Assurance 7
Program met the' licensee's FSAR commitments before the change to the 8711 contract in 1983 I don't quite see how the hardware constructed to something less than the FSAR commitments to both ANSI N45.2 and 10 C FR 50, Appendix B is magically qualified., 2.5 PG&E's attitude is aptly explained in their response to my [ allegation that the Diablo Canyon Project (DCP) purposely failed I to state to the Pullman QC inspector "you are certified to and re-sponsible for ANSI N45.2.6 Level II capabilities." DCL-84-243 i g at III-51 (page 2) responds "There is no requirement anywhere I that an inspector be specifically told that he is qualified to ANSI N45.2.6, and it should not m .ko any practical difference wether or not the individual knows that he is qualified to N45.1.6." ; 1 This is a falso statement. ANSI N45.2.6-1973 states at 2.2.4 l that the certificate of qualification shall include the basis used ! for certification. Pullman's certificate of qualification makes no mention of ANSI N45.2.6 as the basis of certification. As to wether it makes any difference the inspector know what he is certified to and responsible for, the samo could be said for the l t contractor knowing what the utility is committed to in the Final .! Safety Analysis Report. Of course it makes a difference! Any Ii words to the contrary are completely asinino. , 9 I f
t o' 3.0 OC INSPECTOR HARASSMENT AND RETAMATION 3.1~ In December of 1983, I had noted the failure' of Pullman s 7 to cotiduct ' welder qualification testing under the' full supervision and control of its ASME Sec. IX requirements. In attempting to document.the extent of the problem, I was denied access to in-spection records on the subject by the production foreman and QC
'l,-
Welding Supervisor involved in the testing. Three days after ' attempting to visually examine the test's inspection records I ' was fired. 3.2 In an affidavit presented before the ASLB, the QC Weld-ing Supervisor, J. P. Watson, states on page 3, para. 4 "Re-cords of each of the 13 Welder Performance Tests show QC in-spection occured for fitup, rootpass, filler pass, final visual,
, and bend test." However, at the Department of Labor hearing a 1
conducted on my behalf July lith and 12th Pullman QC Welding Supervisor, }. P. Watson, had a different response. The follow-ing is taken from court transcripts page 458 at 12 and ending on . o page 459 at 1
'l Q What records did you maintain of the tests that were undertaken during that time? {
?
}
, s A I just told you, I maintained my log, a record of each and eve.y test that is performed, and the actual perm- '
anent certification that is made from the record. I Q And the certification just states that so-and-so is certified as a welder under certain procedures? 10 g i
.a.... ..
A There are regular forms for it, yes.
,, Q Did you-- Does your log reflect all the various hold I, . points that you--
A No sir. Q Did you--are there records of what hold points you examined ? A There are no permanent records, no required records ' i for that purpose, No sir. Mr. J. P. Watson has impeached himself under oath in attempt- 1 ing to have it both ways. Wether permanent, auditable, QC in-spection records exist for welder qualification testing is still un-i known. ,
,i 3.3 With respect to welder qualification testing, I refer the I reader to 10 C FR 50, Appendix B.
Criteria IX CiONTROL OF SPECIAL PROCESSES " Measures shall l i be established to assure that special processes, including weld-l ing. . . are controlled and accomplished by qualified personnel using qualified procedures in accordance with applicable codes, standards, specifications, criteria, and other special requirements." Criteria X _ INSPECTION A program for inspection of activities !: affecting quality shall be established and executed. . . to verify a conformance with documented instructions, procedures, and drawings. Examinations, measurements, or tests of material or 8 products processed shall be performed for each work operation 11 t l I'
where necessary to assure quality. . . If' mandatory inspection ' holdpoints ,which require witnessing or inspecting by the appli- ' 7 n cants'<iesignat5d representative and beyond which work shall not
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proceed 'with'out the consent of its d5signated representative are required, thef specific hold points shall be indicated in appropriate ' j. g documents . " '
}
Criteria Xi TEST CONTROL. "... Test procedures shall include ~ provisions for assuring that all prerequisites for the given test have been met, that adequate test instrumentation is available and used. . . Test results shall be documented and evaluated' to assure that test requirements have been satisited." Criteria XIV INSPECTION, TEST, AND OPERATING STATUS
' Measures shall be established to indicate by the use of markings such as stamps, tags, labels, routing cards, or other suitable means, the status of inspections or tests. . . . These measures shall provide for the identification of the items which have sat-isfactorilly passed required inspections and tests."
Criteria XVII QUAIITY ASSURANCE RECORDS " Sufficient records shall be maintained to furnish evidence of activities affecting quality. The rerards shall include at least the following: oper; ating logs and the results of reviews, inspections, tests, audits, ! monitoring of work performance. . . Inshection and test records L shall, as a minimum, identify the inspector or data recorder, the
- 12 1
O type of observation, the results, the acceptability, and the action taken in connection with any deficiencies noted." 3.4 fk The short review of appendix B was presented to ask and answer the questions:
+ Are inspection records of welde qualification testing re-quired at nuclear power facilities? ,
+ Does the welder qualification test have hold points that must be inspected before the' test can be allowed to proceed?
+ If a QC inspector performed an inspection of a mandatory hold point, would that ' inspector be required to document the re-sults of such an inspection?
In thirteen years of welder qualification testing at Diablo Canyon, has no one attempted to audit the inspection records for verifica-tion to the requirements of 10 CFR 50, Appendix B? PG&E's own FSAR states in chapter 17 Quality Assurance para.17.1.10 "All suppliers and contractors on the Diablo Canyon Project are required to employ a program for inspection of their work to verify conform-ance with approved drawings, specifications, and procedures. . . Both process monitoring and inspection of final products are em-ployed to confirm the quality of work. Records of inspections are maintained to demonstrate the quality of work. Suppliers and con-tractors routinely establish hold points on shop travelers or similar documents to be signed off by the suppliers' or contractors' inspectors." 13 l
Federal law and PG&E's own FSAR indicate that records exist and shall v.be maintained to indicate hold points have been examined
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- and rbt:orded .by quality assurance personnel. Yet, in December of 1983 I requested inspection records of welder qualification test-ing and was refused twice.
3.5 A false statement made before the ASLB in the affidavit 'of C. M. Neary, F. J. Lyautey, and J. P. Watson is the statement:
". . . Mr. Lockert admits he was shown records of welder qualifi-cation for the days in question (December 7,8, and 9,1983) which documented the inspections performed by Mr. Watson on welder qualification tests." I state emphatically I was not shown inspec-tion records for welder qualification testing. I had requested the records because I had observed that many of the inspections that were supposed to happen did not. I had observed a problem and was performing my duty as a QC inspector when the records were denied to me. I was obligated to report the problem and in at -
tempting to do so was fired. I have read the above 14 page affidavit and it is true and correct to the best of my knowledge and belief.
. .. _ . - . . ___..Stavan .Tnck e.rt__ .-. .... . .
[T^ ou kT[orALIFOSM Luis Obispo j , on_M/_2B4 before me, the undersigned, a Notary Public in and for said State, personally appeared _ k ,
. .; personallykn wn to me(o p ved to me on the basis of a s
**-*"-*"*C 7 factory evidencel to be the person (s) whose name(s)is/are sub-
. CU3#.?! HAW:GMS b?h4di j 47 SANr:oTtr.Y PFSIC.?A'. o.rfiCE IN LUIS OBISPO Coutim FU5Uc CAUFCAND.(
he/she/they enecuted the same. d f.*y C;nen':s!cn Ebrmem.ra 23, trf. 14 WITNESS my hand and official seal. L*.;;35.7Ct**7* ' lar-r* *:3;u.0.4.J;4 r.;;;J i t t (This area for official notarial sea Signaturp. M[vM Nb e . -
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) Derl;nition: A 307 - 823 0 ^ 3o7 ANSI Bl.1 Unified Screw Threads 5.2 Resulfurized material is not subject ac ANSI Bl8.2.1 Square and lien Bolts and rejection based on product analysis for sulfur.
Screws 5.3 Bolts are customarily furnished from
- 3. Ordning Information stock,in which case individual heats of stee cannot be identified.
Standard Specification for 3.1 Orders for enternally threaded fasteners 5.4 Application of heats of sacel so whicig (including nuts and accessories) under this bismuth. scienium, tellurium. or lead has bees specification shallinclude the following: CARBON STEEL EXTERNALLY THREADED STANDARD ! 3.I.I ASTM designation and date orissue, intentionally added shall not be permitted foe' j FASTENERS' Grade B Isolfs. *i 3.1.2 Name of product, that is, hea or heavy 5.5 Clwmical analyses shall be performed in hen. Tbs oror stand;rd es mued under the Gaed designateon A 307. the sumtws isnmediately rolloesos the designation endicaeas the accordance with Methods A 751. ycar reapprova inaladopenom or. sa tbe casc orrevannoa.the year otease revisana A sumber en parentheses endicases A superscnps cpulon see madecases an eJaurialchange unce the lau reviseos or reapprowal 3.3.3 spcCsfied. Grade, tbe yeas ortant Grade thatareis,furn,shed. A bolts A or B t (1f no grade is
- 6. MGChaEICal E89"e 3.l.4 Quantities (number of pieces by size 6.1 Bolts 'shall not exceed the maaimum
- 1. Scspe including nuts). hardness required in Table I. Bolts less than optional nature is provided, which describes 1.1 This specification
- covers the chemical 3.l.5 Fastener size and length, three diameters in length, or bolts witl* drilled additionalrestrictions to be applied when bolts i and mechanical requirements of two grades of are to be welded. It shall apply only when 3.1.6 Wa:Acrs-Quantity and size (separate or undersize heads shall have hardness values from bolls),
czrbon steel externally threaded standard fas- specified in the inquiry, order, and contract. . not less than the minimum nor more than the tenirs, in sizes % in. (6.35 mm) through 4 in. 3.1.7 Galranising-Specifyhot dip, mechan. maximum hardness limits required in Table I; (104 mm). This specification does not cover
- APP ** * * * " " ' " ' ' ical(4.41 or other unish required, as hardness is the only requirement.
requirements for externally threaded fasteners 2.1 ASTM Standards: 3.1.8 Specify ifinspection at point of man. 6.2 Bolts 1% in. in diameter or less, other
; having heads with slotted or recessed drives or ufacture is required, A 36 Specification for Structural Stect' than those excepted in 6.1, shall be tested fuQ for mechanical expansion anchors. The fas. 3.1.9 Specify if certified test report is re. size and shall conform to t!.c requirements fos l A 153 Specification for Zine Coating (flot- quired (sec 9.2). and seners covered by this specification are fre- Dip)on Iron and Steel ifardware' tensile strength specified in Table 2. ~
queitly used for the folidwing applications: 3.1.10 Specifyadditional esting(9.3)or spe. 6.3 Bolts larger than 1% in. in diameter, A 370 Methods and Definitions for Mechan- cial sequirements. I.I.I Grade A Botts,forgeneralapplications, ical Testing of Steel Products' r other than those excepted in 5.1. shall preferai aid A 563 Specification for Carbon and Alloy bly be tested full size and when so tested, shall 4 Materials and Manufacture 1.I.2 Grade B Bolis, for flanged joints in Steel Nuts' conform to the requiremsats for tensile strengt
. piping systems where one or both flanges are A 706 Specification for Low-Alloy Steel De- 4.1 Steel for bolts shall be made by the open-sPecified in Table 2. When equipment of suf,
' cast iron. hearth, basic-oxygen, or electric-furnace proc. ficient capacity for full-size bolt testing is not formed Bars for Concrete Reinforcement' ess.
1.2 If no grade is specified in the inquiry, A 751 Methods, Practices, and Definitions available,or when the length of the bolt makes contract, or order, Grade A bolts sha!! be fur- f r Chemical Analysis ofSteel Products' g 4.2 Bolts rnay be produced by hot or cold full-size testing impractical, machined speci,
, gished. e4 forging of the heads or machining from bar mens shall be tested and shall conform to thel
- B 454 Specification for Mechanically Depos- stock.
1.3 Nonheaded anchor bolts, either straight ited Coatings of Cadmium and Zine on requirements shown below:
' 4.3 Bolt threads may be rolled or cut. (
cr bent, to be used for structural anchorage Ferrous Metals' Te s.i, Eloosa-purposes, sha!! conform to the requirements of
" 4.4 When specified, galvanized bolts shall 2.2 American NationalStandards: swearth tai d be hot-dip zine coated in accordance with the Specification A 36 with tension tests to be made , on the bolt body or on the bar stock used for g requirementsofClassCofSpecification A 153. crade A and c,we a boli.
8'#*l L'*as s g ,g,,, , ,,,, ,, 60t oisi Is i miking the anchor bolts. p,,, ,, ica When specified by the purchaser to be mechan, crwe a bosu osty 100 lsect .c.: . ca..,uce F.le on Faseepers.and as she direit re ponsab iny h Ically galvanszed bolts c vered Iry this specifi. 1.4 Suitible nuts are covered in Specifica. or suhm.sasssee F 16.02 on $seel Botung - In the event that bolts are tested by both full 4 d d cation shall be mechan tally zinc coated and
' tio2 A 563. Unless otherwise specified, the. ,,d'oa"7,'Q"6 "*l,2s ap,b ,,A;.g ,, 2 2 -
the coating and coated 'asteners shall conform size and by machine test specimen methods,'
' grade and style of nut for each grade of fas- 47 T. Lasi previous edition A 507 aa teier,of all surface finishes, shall be as follows: *F* ^
,,,,',,,5, soi .o to the requirements for Class 50 of Specifica- the full-size test shall govern if between the two methods exists.
j, ram Prge
. jdeage g
s ei tion B 454, or to the coating thickness, adher-Fastener Grade and $sre Nut Grade and Sayle'
*19ff AaawaI Aee4 efASTM Standards.Vol0104. * "3CC' and qua! sty requirements for Class C of 6.4 For bolts on which both hardness and'
^ ' h i"- ^ 6" **" '
8 tension tests are performed, acceptance based! 4.over aw so 4 u. B. l'. s2 4 so. A. besty bes a, athISTYSNas.'vY0IoIOiO2. 0103. 0104. 05 Os. and 15 og O on tensile requirements shall take precedence A. besvy ben 1981 Aaamar Joe 4 ef ASTM Ssaadards. Vol 08 01 and
"* S. Chemical Reqeiennents so the event that there is controversy over low
- N1:s oroiber grades and asyles havnag specsfied proar 01 04 ,
. IoaJ s.rcues ISpec rnation A 563. Table 3; gresser than the w 5.I Stee] shall conform to the following readings of hardness tests.
' 8' d*""8I 8**4 of A STM Ssaaderds. Vos 0104.
speafied grade and ssyle oraus are also suitable. H43 Aammal Aeel ofASM SrsaJards. Vot 04.01.04 02. l chemical re9uirements: 7. Dhnensioes 010s.0104.0 Os. and u).05. 1.5 The values sisted in inch-pound units ' pas Aaa t 8,oA of ASTM Ss dards. Vot 04 04 and csade A crede 7.I Unless otherwise specified, threads shall
.cre to be regarded as the standard. 3,,a.
"May be olisalow fro. Amerkan National Sunderds be the Coarse Thread Series as specified in the 1.6 Supplementary Requirement SI of an Isaanna.s.c, 430 erowwsy.New York.N Y. lfuls
, Phos e.u.phorus. 0 06 O ne latest issue of ANSI Bl.1, having a Class 2A,
..- sna a. 9 - '
L .. 7.2 Unless othIrwise specified Gride A stock.and the mtnufacturershall make sample furnished in accordance with this specifiestion. 12. Rejeetles bolts shill be hem bohs with dimensions es inspections to ensur that the product conforms All tests end inspections required by the spec-gisen in the latest issue of ANSI B 18.2.1. Iln- to the specified requirements. Additional tests 12.1 Unless otherwise speedied, any seja less otherwise specified. Grade B bolts shall be of individual shipments of material are not ilication that are requested by the purchaser's tion based on tests specified heroen shaB l heavy hem bolts with dimensions as given in the ordinarily contemplated. Individual heats of representative shall be made before shipment. reported to the manufacturer within 30 eorkis I latest issue of ANSI B 18.2.l. and shall be conducted as not to interfere un- days from the percept of samples by the pu ,l 7.3 Unless otherwise specified, bolts to be steel are not identified in the finished product. 9.2 When specified in the order, the manu-necessarily with ale operation of the works. chaser.
' used with nuts or tapped holes which have been facturer shall furnish a test repost certified to tipped eversize,in acccrdance with Specifica- be the last completed set cf mechanical tests for tion A 563, shall have Class 2A threads before each stock size in each shipment. SUPPL.EMENTARY REQUIRElbEENT hot dip or mechanical galvanizing. A."ter gal- 9.3 When additional tests are specified on <
vuizing. the maximum hmet of pitch and ma- the purchase order, a lot, for purposes of se- , h following supplesneatery requirement shall' apply caly when speedied is el jor di: meter may exceed the Class 2A limit by lecting test samples, shall consist of all material purchase order or contract: the following amount: offered for inspection at one time that has the ' 3,, ,, , oveense umis. i. following common characteristics: SI. Balts Sakable for Welding - product described sa this supplementary sq taan 93.I One type ofitem. q ,;,,,,,g, Upio Un. et eonsoat 9JJ One nominalsize,and St.l The material desenbed in this section ca,s e se s. ei s I 9.3.3 One nom nallength of holts- is intended for welding. This supplemental sec. Maassaae I en t. [' f 86 'o I. m , , ' ! ' ,,* nese vatues a,e she same
- tion, by additional cheniical composition re-strictions and h a cah e@alent famula, 7 "
,,ed to, s.i... ,c4 a.iiin spranc.e.oa a sal. as sheeach maai===imnapp=s requiremnt shan k as fog ows- s.=se aso s. mas I
provides assurance of weldsbility by chemical 7.4 The gaging limit for bolts shall be veri. Number dPwcas ia t cd Namber a sampi,, composmon comrd St.5.2 Carboe Egiseleat (Seesne-A.ITJ fled during manufacture or use by assembly of sno end .. der a . SI.2 Welding technique is of fundamental Spergicesion A 7061-in addition to the hea a nut tapped as nearly as practical to the sos io s axe 2 importance when bolts produced to this sup- chemical analysis requirements in St.5.1. th l amount oversize shown above. In case of dis- o' *", g a l i P ementary section are welded, h is presuP" W mal # shah be such a m provsde pute, a calibrated thread ring gage of that same p sr.d that suitable welding procedures for the carbon equivalent (CE) not esceeding 0.5 size (Clus X tolerance, gage tolerance plus) 9.5 If any machm.ed test specimen shows j steel heing welded and the inter.ded service will when calculated as follows-shall be used. Assembly of the gage.or the nut defective machining it may be dncarded and be selected. 1 described above, must be possible with hand another specimen substituted.
. CE = % C + + -+
' SI.3 All of the requirements of th,s supple-i 6 20 effort following application oflight machine oil 9.6 Should any samp!e fail to meet the re- mental section apply m addition to ail of the quirements of a specified test, double the num- , + .,. _ chemical, mechaascal, and other requirements 10 50 10 e ti ns, when rform to re v ber of samples from the same los shall be tested, of the base specification. A 307 for Grade B. SI.6 Analr fs Reports-1f requested on sh
. disputes, shall be performed at the frequency in which case all of the additional samples shall ,
ol.4 Because of the embrittling effects of order or contract, the chemical composition e I ar;d quality described in Table 3. meet lige specilication, welding temperstures on cold-forged sacel, this each heat of steel used and the calculated ca t
- 8. Test Methods supplemental section is hmited to hot-forged boa equivalent for each heat shall be report
- 18. Marking bolts, or,if not forged, then to bolts produced to the purchaser.
8.1 The material shall be tested a.n accord-10.1 Bolt heads shall be marked (by raised from hot-rolled bars without forging or , SlJ Product (Check) Verification Analy depressed mark at the option of the manu- threaded bars, bars studs, or stud bolts pro- sis--A Chemical analysis may be made by tim 82 nda 59ua ad t ly facturer) to identify the manufacturer. The duced from hot-rolled bars without forging. purchaser or his representative frosa bolts se bc tested y wed n n h Cold-forged bolts, or cold-drawn threaded lected from each heat ofsteet The analysis t manufacturer may use additional marking for
" bars,if they are given a thermal treatment by determined shall not enceed the values spe body or threads of the bolt withous any fracture *2nn8 8 8 8cmPerasure of not less than fled in St.5.2 by more than the follown j at the junction of the head and body. Other ( an air e am also s,mta-j , headed bolts shall be tested by the axialtension g g, g,,,,,g,, amounts.
) method. 11.1 ff the inspection described in II.2 is St.5 ChemicalRegenrements: +e j 8.3 Speed of testing as determined with a required by the purchaser it shall be specified 3 . c,arta.
,,,,,,, ,ss .
free running crosshead shall be a maximum of in the inquiry, order, or contract. pbmpherw, d oes I in. (25A mm)/mm, for the tensile strength n testsof bolts. 11.2 The inspector representing the pur-chaser shall have free entry to all parts of the Hsh M k M w mhm N dh,,$ manufacturer's works that concern the manu-
- 9. Nrmher of Tests and Retests facture of the material ordered. The manufac- lN 9.1 The requirements of this specification avrer shall afford the inspector all reasonable O
) shill be met in continuous mass production for facilities to satisfy him that the materialis being
*I
TABI E I ttweness measmerenness ser mens T4:3.s 2
.s ,ne si,es.t-b and tece, hers s= De: Ignition: A 320-82 Bois sire.
,,,,,,c,s Rn weg a"
-. t ~ r.a. r;. c.,.3
. ore.4, (W ,
Grade a act I's size sample L,e*
- A",'
g [ ; mue
- ~ - - - - - ~
sana mas 2 so 90 33. ..- . .l - An A -323-mas 141' 69 10e* 911o 15o 20 2 ;
- j a 123 212 49 93 R$l eo 2so 32 3 2
- 18o 500 M 3
' :=re . hen ies=a by . age ==.o. .e..
, g8y g :$ d Standard Specification for 3 20lso to coo $no g4 J
usu 2 T,.sae 'o oo8 *ad o - iis
- . . , r, si.e n.eps u ALLOY STEEL BOLTING MATERIAL $FOR LOW-
- se=Pk e of narpuna ambus m esuwwd r=.
i Bda seress -Te.ou- s- - . ,,b.ihe. TEMPERATURE SERVICE' reads single semipling Plan fue Normal laspec ior Table 114. sue. pas wh Area
- c,.4,. c,,J. Mit sTD-loSD
, ca. ,, E' A and 3' 3 only. * ! aspect all Isoles is the los it the los ssre a less them she Thas standard is issued usder 'he Seed densgnesion A 320t she sumihre " i fallmeing she " men
- may sangs nee, indicaans she .
~-
-- year or ongssel adopsion or. se the case or reviseas. ehe yest or less revisaae A member sa paseesheess eedsanes she year ofle j
!,,. seapproval. A seperscnpa epaalce gelindacanes se edssonal theage siese the last sewuses er reappse al. -
- '- 54
- Ikt **"** b** b"* '9P'"dl** *** br *e*mnes of she Depennant af & endfe, hung h sh, DsD M af
. % 16 00775 ## " 4 650 772 #""*"# } % 14 08063 6 35o lo 63o l I. Scope (
'"* ' 58' " "' for Steel Bars. Carbon and Alloy. Hos-j s Wrought and Cold-Finashed' i.
F-80 o$ e nd
N n3 20 oso n *e
- l. I This specification' covers alloy steel bolt.
ing materials for pressure vessels, valves, A I94 S P8Cif' cation for Carbon and Alloy-e 0 442 271m 46 2io Hanges, and fittings for low-semperature ser- Steel Nuts for Bolts for High-Pressure and vice. The term
- bolting materiar* as used in High-Temperature Service
- i a e se6 36 350 1 *- 7 ao ano thi> specification covers rolled. forged.or sirain A 276 Specification for Stainless and Hess-0 763 45 soo 76 3<o 8% 7 8 '** Sa sm , e6 we hardened bars, bohs, screws, studs, and stud Resisting Steel Bars and Shapes ,
sk 6 bolts. The bars shall be hot-wrought. The ma. ( 1.855 ** 3m tis $<n , A 325 Specification for High-Strengsk Bolts c serial may be further processed by centerless for Structural Joints
- 1%
- 405 s4 300 Ho 500 i l 5 s.*o I:4 nuo iao o"'
grinding or by cold drawing. Austenitic stain. A 370 Methods r.nd Definitions for MacInse-less steel may be solution annealed or annealed ical Testing of Steel Products' ' !.'. , Is $$ 'n" $ jy[ and strain-liardened. 2.2 Ameriras Natiosief Standards lassiasse i 25 4 e 00 l.2 Several grades are covered, including S8cadards.* 24o coo am om
- both ferritic and austenitic steels designated L7 B18.2.1 Square and Hex Bolts and Screws
$ [* j si. 4 2 so 2 4x coo 43 7:o coo 88, etc. Selection will depend on desi6n. service Bl8.3 Hexagon Socket and Spline Socket conditions, mechanical properties, and low. Screws 3 35 4 sn 49, soo an ono temperature characteristics. B18.22.1 Plairt Washers 34, 4 , og 37,6uo 966 sino Nort I-The cosnniistee formulating this speci-d 4 11 o8 664 son I los oc 3. Ordering leformation ficacia has meluded several grades of matenal that [
- Area calcuinted freen the formula: have been rather ennensively used for the present 3.1 The inquiry and order for material moder purpose. Osher composition 'will be considered for this specification shall include the followtag as f
j .bere: A. - 0 7sH l D - to 9743/esl. y m e
]tQt a asa e required to describe the material adequately:
A. - uress nea. - hardenshility of wsne of the grades mensioned may 3.l.1 ASTM Designation A 320 latest issue.
- ,D - my; ameur or bok. *=d resencs she meninnuai sire as which the required and analy .is by grade as selected front Table I, mechanical properties are obtainable.
'
- s ist . 4 44:N. 3.1.2 Minimum mechanical properties re-
' O l.3 Nuts for use with this bolting material
' sueda 60isitoi4 w r. *
, a: ice on toin i tas, urai. are covered in Section 9. ' The s 3
W I A SuPPl ementary R'9uirement SI of an C'","',"",pearamesse
,,4 is sederstesseed b,,,',',,"e,^
- s=ct.seemismseest.and she je A
. De A were, serwerfor Ten.=g .ad w, ruse =4<s O OP ional nature is provided. It shall apply only v.s.es a vnomen.p hei ry or s.% Aos.22 em ,.
.e ,re .wa =r n,= _ - 2 nu u d.,4 vwr,.r:4,.non== respurnee, s.rs.,, ,.pr nt.sac ret,s,rr ys,,,r.,
.sm,s,4., r nre.ie regas nuernes i ef e. =4 vera, ngari. d en, me .f af=g, , ,./ n.ra nsa ,.. .re ,.i.,.i ,4,n .. ,,,n,,,,3,inr ,, ,j ,4, f,s , ; when specified in the inquiry, contract and C seiy n tes2. rebenhed Sep.
,",",,",*E
, ""**' *d'une w order. 2'do'*p* s
['"* ' * *' ^ '" na n.*s u .6jere e. ,,nu ., , r $. es, ,,in. i, ,,,4,,,,, , 1.5 The values stated in inch. pound units
- hr AsME, Soder and Premuse Venert Code apphse.
.odf.not renws. ,ns,r renpyreseder asundr. men 3 our commente are anverd,uartjer verruen vf tan su.nJ.nrJer
,,, e .,,,, 3, ,,o,,,s ,."' I
- a'"
are to be re arded as the standard-for .J.'nen.l
'"*'- P"#**" s4 32e is samen is er chan h Code.'" "'*"d S n.ne rds end ekooIJ hr .Jdreis,d s. 45 TM il,edqueers,va. 3 *e* <enem,n,s edlenenr e.rrfuirenaerr.,u,n.e . nwrumg ol see respeeu6tescrh.ur.f remaurace. 4ere i.e no.r.rsend if swer t,rtsase n.or somments 4. e noe rerne,J /.ur 4,.r.ng i u .4, JJ y. Applicable Docamients *.s,es s*s3AAanannine.h af ASTM Sanaderer.Vel StR5.
naner even news an.mn oe uer A STM t'enenenwe en St.nderde. tvi6 Jtere se . Phdadelpen P 1o10 t ' t a a .fASrar se d rde.ves east. 2.i ASTM Standardt. * "*,,',,. ea'*.a.n"i, ****4.,,',',, W # *
#,4,**
y,,,",,",', 5 i,,',,,,,, A 29 Specification for General Requ,remenis i H3e nn.edway. Hee Yak. N Y.109ts.
~
l
- . ,, _ . - . -_ - a_. {
i EXH1 BIT 2, 21 pages (313-326.8)l Msn b N-71 -7 cases or Asw.non.ni no riassi ne uwa.mns (1644-7)
'.lleeting ofSeptember 16, I977
,1pprorecr 21, !9R0 uniess previously unnulled or renffirm.~d.
Case N 717 (1644-7) ~ nor on material 3 to Sperification* AsT.\1 A51 l-7:5 amt Additional Materials for Component Supports SA 'i92. nor s.n the Irre toachining' aterls permitted in Section III, Division 1, subsection NF Class 1,2,3, and (3)Irlow. MC Component Supports
% ,< (3) % hen the Nominal Conqu>>itiihi rohann refer-rners AISI gradr>, only materials meeting the themical Inquiry: What materiala, in aildition to tijou listralin romgmsition requirements of .the operific AISI grades Tal,lre 1 11.0,1-12.0, and 1 13.0 of Appendix I of Sertion - liste i 3 hall be nsed, with the exrrption that 0.60 maxi-111, Disi> ion 1, may be used for Cla3s I,2,3, or SIC com-mum silicon is penuittrd for castings. Free inachining 2 inment Supports con >tructed to the trquirrments of Sub-rttion NF? minlifications of the specific AISI grades listed may be n,rd at the 3.une design > tress intrn itir>, allowahic sin u-Reply: it is the opinion of the Committer that the es awl 3 i cid strengths of Ilm referrnre grades but their additional materials, dr>ign tress intensity and allowable u.c is limited to 400 l' masimum temperature.
strn.e salurs, the >irld strength, and the ultimate tensile (4) When~ welding on A487 76 Grade 10Q, SA-508 otrrngth values', listed in Tables I,2,3,4, aml 5 of this (1 ass 4, A50th76 (.1aw 4a aml A5Kk74 Class I,2, and 3, Cule Case may be used in the run truetion of Cla+ 1,2, 3, and SIC Comgament supports for Section ill, Division the following additional requirements shall apply: (a) Welding proced'nre qualification and wchler 1 in addition to tho.c listed in Table NF.2121(a) 1- and welding operator qualification > hall be made in ac-The fullowing additional rrquirement > hall apply: (1) All other requirements of Sub*ction NF shall be ronlante with Section IX as mmlified by Section ill and a:6 gisen herein. mrt including NF.2586, w herc applirahlr. (2) Until rules are added, webling is not permitted (b) Separate webling procedure qualification on carbon and low alloy steels containing more than of Section IX , hall be required for three material, and combinations of other materials with the c 0.35 percent carb<m, nor on Pil: or age-hardened2 etrels, materials. When joints are made between two diffrn nt
,The tabulated valuca of ten 41r etrength and ty[ws or gradre of base material, a procedure qualificalion are tho.e which the t'ommotre brhrses arr muita{rld strength e for use m mu3t be made for api di cal,le combinations of materials de,ign cJeulations required by Section lit. thision 1. At the armperaturca ahuve room trmtwraturr, the naturs of tenste even though procedur, qualification tr>ts hase twen
.trrngth ir 4. muchtend as 10%toward antenste atant the airrage or ritrrtrd strength irrnd runesalue a which ma4 mad he rarh of the two ha e Inalerials wrbled to juated to the minimam stvrified nium temperature trn itself (materials ..I the name nominal chemical anal} sis strength. At temperatures alnne truem temirraturr, theidyw,41r d udmial iniIirrtir> I range, cVen thouEh of different attrngth satur> rorrrapsmd tu the >ichl strrngth trrnd rurer ad-V ju frd tu ihr_ Ininimuns pperifie d nuun trentwrattur )irhl pnnhwt forni, may he ram idered a$ the name type or '
altrugth. Nrithrt the ten >ile strrngth nor the jirld stren,pth Erdd")- talure corrrepond exactly to rither "aterage" or minimum as I r$r r applied au a ntati.tical treatment of a honwgenr- (r) The following, in addition to the variabica in Sec. IN, QW-250, shall be considered a, r> ential vari. Neither the AS\lE nr ASUI Alaterial 8pecifications nor the Itutes of Srction lit, thei4un 1, require rievated temperature ables n quiring re-qualification of the welding procc s.
-treting for tensic or yictd strengths of production material for uar in, Gale components. It is not intended that results of nurh J. A change in filler metal SFA rlarification tr.ts, if rrformrd, i he romparrd mth thcar tabulatrd trunte and )irld strength talurs for ASME Gale arreptantr/rrjrrtion or to a wa Id n id M roven d b an Y SFA eIwcification. <
i purpo rs for materials. If s mw clesated temperature test results 2. An inrrease in the maximum or a decrease in on prmlurtson matrnal appear lower than the tabulated valurs h) a large amount (more than the typical sarialulity of material Llw minimme1n4ified 1 in In at or interIsa3s temIwratures. nuggrating the pouilaility of some rrrur)furthrtimestigation by The ogwrified range of prehrat temgwratures > hall not retryt or other encans should he run*nlered. pgpppg gr,g p, 21hc desigrwr sha'l camsider ihr effects of temperature, en-i,iomnwnt and applird strean on the material prnprrtirs of per- .3. A change in the heat treatment (pneredure ripnahon or aste hardrmng allu)s, on other high alrrngth brat iiualification trots shall he sub'rcledI to heat treatment _ treatrd alloys, or on irrrmachining trels. casentially reptivalent to that encountered in fabrication 313 SUPP. 3 - NC l
**MS g -W + pgim _. , ~
cass(c=,imed) "7 I " * *Y'O N-71 -7
'(1644-7) cases or asm: nounsn meSscu nessti. cons C of the vessel or ve,psel parts including the masimum total Thickness of aggregate time attiemperature or temperatures and cool. Specimen, in. A in. B in. C in.
' D in.
I"I' ra tes). .
;,j,, gy 3y 378 l ,gi,
- 4. A changein the types of current (ACor DC) 2 4 86 polarity, or a change in the s,pecified range for amgwrage, s 6ji 3ji a j i + j 4 j i + ,';;.
soll, or travel speed.
- 5. A change in the thicknra(T)of the weldi" (g) The finA p.>,tweld in at en atnn nt .hWI be at a procedure qualification tr t plate a4 follows:
mininnun b mpemtun of 1075 F and a masinnnn t m. perature limited only by ihe ability to meet the specified (a) For welded joints which are quenched mechanical properties. Minimum hohling time at the y and tempered after welding, any increa3e in thickness (the final g=>stwehl heat treating tenq= rature sliall he one minimum thicknra qualified in all ra3es is % in.). hour lwr inch of wrid thi kncs.s, one hour minimum. (b) For welded joints w hich are not quenched (5) When the ASTM specification referenced in and tempered after welding, any change as follows: Tables 1 through 5 does not specify minimum tensile aml 3ichi >trength.s, the valuca listed umler the appropri. 7 are cohnnn.4 > hall be met by the material. leu than 5/8 m.. Any decrease m. thickness (The (6) Materials in Taldes I through 5 whose nominal masinmm thirkness qualified .n composit.um
- referenerd as an AISI com >osition ma .
he arrrpted a, nati fying the requirements of the ASTM 5/11 in. a.n d in er Any departure from the range of operification provi. led the themical requirements of the AISI reiGreion an widdn du prifid qc of tie 5/8 in. to 2T. desipab d AS'DI yn.rifiMiom W a nifidm of dm material whall be in accordance with the requirements of s (d) Welding I'dler metal containing more than O.06 gwn ent vanadium 3 hall not 1.c n rd. NCA.3867.1 (c) or (f). The term "rach piece of stock material" in NCA. ll!67. l (c) may be taken to refer to (c) In addition to the requirements of Nil-1410 that portion of the material of the same heat and tot of Scotion 111, Divi > ion 1, the materials may require re. which has trarrability r>taldir' .d by the Manufacturer haking in order to minimiec moisture. The prorrdures through his program. B hrre Certificate,, of Gunpliance for doing thin for roscrrd are wrkling r!rrinnies are are gisen in 8 wrifications SFA.S.1 and SFA .i .. arrrptable umler Subsretion NP, testing of ruch pirre is not n pdrril. (f) The radius of the mandrrl or die uard in the (7) All >nprorts aml component stamlan! ,,upport.4 gui. led I.cnd trots of Fertion IN. Figs. QW 166.1, .onstructr.1 nmler the pnnisions of this Case shall bc VW-166.2, and QW-166.3 hall 1.c: identifird oith ihis Case nmn!,rr. r i l j 3It l SUPP. 3 - NC i i I
y ( ( ( TABt.E1
, Desiyi Stress Intensity Values, Sm . for Ferritic Steels and Copper Alloys for Class 1 Plate and Shell Type Component Supports A
Min 5 Min Ultimate Design Stress intensity, ksi (multiply by 1000 to obesia poil i Type Yield Tensile for metal temperatures F, not to exceed * ' *
; Nominal P. Group Product Specifica- or Class Notes Strength. Strength, 4 Composstion No. No. Form tion No. Grade ksi hsi 100 200 300 400 500 600 650 700 750 000 3
Carbon Steels
. liar A108 73 1015CW -
6.9 AIS11015 1018.1020 liar Itar Alt 473 A108 73 1018CW 1020CW 6,9 6,9 J (/ 40 60 20.0 20.0 20.0 20.0 - - - - - - j AISI l043 - - I:ar A 108 73 1085CW - 2 100 120 40.0 40.n tius 40.0 _ _ - - - _ p e - g AISil030 - - Itar A108 73 1030CW - 2 123 140 46.7 46.7 46.7 46.7 - - - - -
- jQ-j AISI 1013 Tule A313 76 1013CW 6,9 55 63 21.7 21.7 21.7 21.7
= a AISI 1020 - - Tule A313 76 1020CW - 6.9 60 70 23.3 23.3 23.3 23.3 - - - - - - *- :- AISI 1025 - - lute A513.76 1025CW - 6.9 63 75 23.0 23.0 25.0 25.0 - - - - - - y Tulw A319 76 10lat'W{ - 5,7.9 50 70 23.3 23.3 23.3 23.3 - - - - - - M AISI 1018 1020,1022 1022CW l 5 f Tulw A519 76 1020113 l - - 32 60 20.0 20.0 20.0 20.0 - -- - - -
- (:
! 1022111t I . 4 i' AISI 1026 Ji Ti.ls A319 76 1 02 61111 - -
-10 70 23.3 23.3 23.3 23.3 - - - - .- -
?,.
AISI1026 - - Tulw 4519 76 1026CW - 5.7.11 60 80 26.7 26.7- 26.7 26.7 - - - Ilar SA.675 63 - - 32.5 65 _ 21.7 21.7 21.7 21.7 21.7 21.7 21.7 - - - h, Itar St.675 To - - 35 70 23.3 23.3 23.3 23.3 23.3 23.3 213 - - - Ilar A675 77 75 - - 37 75 25.0 23.0 25.0 25.0 25.0 25.0 25.o - - - 5: m AISI 1022, 1030 - - I'orgine A668 72 - 11 - 30 60 20.0 20.0 20.0 20.0 20.0 20.n 2H.0 - -
- Ij" Low Alloy Steels m .
AISI 4130, L 4330 4 2 Casting A148.73 90.60 - 8 60 90 30.0 30.0 30.0 30.0 30.0 30.0 30.0 30.0 - - 5 Q;Is AIS14130, ~ - Casting Al l8 73 IU3M - 2 85 105 33 0 35.0 35.0 33.0 35.0 33.0 35.0 35.0 - - 5 , b-4140,4330, 4340 Casting Ca> ting Al48 73 AI48 73 120.93 150 125
' 1,2 1,2 93 125-120 150 40.0 40.0 40.0 40.0 40.0 40.0 10.0 40.0 50.0 50.0 50.0 50.0 50.0 50.0 50 0 50.0
;Q O :' N 8, 2%Cr 1 Mo 5 2 Casting A 487-76 -
8Q - 83 103 35.0 35.0 34.6 33.8 33.6 33.6 33.8 33.1 - - p = Un to I sue H
*- A e4
. ^ O .r
=
g z. u ,- i A N e d g C bH b w i@ V
. j
(
*n TABLE 1 (Cons *d!
.h O 8d Dessen Stress Intensity Values. m S . for Ferritic Steefs and Copper Alloys for Class 1 Plate and Men ShellSupports
..ac..nt Type C:
^{D
@ g, m o Men Ultimate Design Stress Intensity, k si Imultiply by 1000 to obtain poil '
A w fut #. Nominal , Type Yield Tensite A, P- Group Product Specifica- or for metal temperatures. F, not to exceed m Composition No. No. Class Notes Strength. Strength. a n Form teon No. Grade kse ksa N q-O Low Alloy Steels ICont'd) 100 200 300 400 500 600 650 700 750 800 w
- 3
* ~'
- 4 e =
Ni Cr.Mo - - Casting A487 76 - l(H,9 I 100 Ni-Cr.Mo Fe,reing 125 41.7 41.7 41.7 41.7 41.7 41.7 41,7 41.7 _ _ C A503 76 - 4a 100 115 8 1 33.3 33.3 38 3 37.9 37.(, 37.I - _ - - g, l'! ate A318 75 All - I.2.3 500 llo
. Plate A314 75 36.7 36.7 36.7 36.7 36.7 36.7 36.6 35.9 ' -- -
All - 1.2.1 90 AIFI 4140, ~ jTule A"> I 9 76 100 ~ 33.3 33.3 33.3 33.3 33.3 33 3 . 33.2 32.6 . - - 4142
~~ 41 toOV l. -
2 100 124 40.0 10.0 40.0 10.0 n I Tule A319 76 41420V { - 2 100 120 10.0 80 0 10.0 40.0 g 2'iCr.1 Mo 3 2 Plate A512 77 3 m, 75 9~. 31.7 31.7 31.7 31.7 31.5 3 I. 30.8 30.1 ti 2%Cr.1 Mo 5 2 Plate A342 77 4 - - 60
=
!!5 Ni-Crato Plate A343 77 23.3 23.3 28 3 211 3 28.2 27.8 27 ~. 27.2 - -
[ A.II 1 - 8" lui 31.0 3~* .o 35.0 3 83* 38.4 3U8 - N.Cr-Ma -- - Plate A343 77 A.ll 2 A I Ni.Cr.Mo - - Plate A513 77 A.Il 3 - l#Me To ll1 90 33 3 38.3 38.3 37.9 . 37.6 37.1 30.0 30.0 30.0 29.7 29 1 29.I ( Plate Shapr> A572 77a 42 - - 12 60 u Plate,Shapen A572-77a 50 20.0 20.0 20.0 20.0 20.0 20.0 20.0 20.0 - - y 50 65 E SNi-Cralo V - - Forging A179 76 23.7'23.7 23.7 23.7 2I 7 23.7 21.7 23.7 - -
?
12a - I .2 144 150 Plate A~88 774 50.0 49.5 48.0 47.0 47.0 87.0 46.0 48.o - -. Mntr Cu4, 4 .11 - 12 12 63 Plate 21.0 21.0 21.0 21.0 21.0 21.0 21.0 2I.o - - "I Mn.N i.Cr-Cu.). A388 77a A.ll - 13 86 67 ::: Plate.Shaprm A388 774 A.!! 22.3 22.3 22.3 22.3 22 3 22 3 22.3 22 3 - - 2/. 11 50 To i.
\ln4h - -
Plate A633 75 A . - 23.3 233 233 23 3 233 2:13 23.3 23.3 - - 3
\lnd 12 63 E 114tr Ar.33 75 I: - - 21.0 21.0 21.0 21.0 21 0 2l 0 2I n 20.n -
a Mnib 7 {- - 114tr A633 75 C.i t - 3 58 70 233 23.3 23.3 23.3 23 3 233 23.3 23.1 - - 4 WCr.Ni-Cu ) ~ - I' late \633 75 C.i t - l 16 60 Mn.V.N Plate 20.0 20.0 20.0 20.0 20.0 20.0 20.0 19.8 - -
-[
A63375 F. - 5 60 80 AISI8620 3 3 Forpng 26.7 26.7 26.7 -26.7 26.7 26.7 26.7 . 26.8 - 46ft." K Io P' AISI 4140, - - Forging 3663 72 - K 2.10 100 33.3 33.3 33.3 33.3 333 33.3 33.3 33.3 - - N 4340 - - 9 AISl4Ilo, - -
' * (-
4380 AISI 1330 -
- Forging A668 72 - 1, 2.10 H5 Ilo 36.7 36.7 36.7 30.7 36.7 36.7 36.7 36.7 - -
4310 - - Forgine A663 72 -
\l I.2.10 110 131 15.0 15.o' 45.o 85.0 45.0 81.0 85.o 85.0 M
AISI 4380 - - Forging %fAl.72 - N I .2.l o 13o 160 53.3 53.3 333 53.3 33,;l 53.3 53.3 53.3 n 9 W
>s W
l V' N 0% 1 V . I$
\ \
( TABLE 1 (Cont'd) - Design Stress Intensety Values.mS . fo' Ferritic Steers and Copper Alloys for Qass 1 Plate and Shell Type Component Supports Min Min Ultimate Design Stress intensity, ksi (muttiply by 1000 to obt'ain psi) Nominal Type Yield Tensele for metal temperatures, F, not to exceed n P. Group Product Specifica. or Class Notes Strength, Strength, ?- Composition No. No. Form tion No. Grade k si ksi 100 200 300 400 500 6C0 650 700 750 800 s V' Copper and Copper Alloys . C w.* Alum. Itronxc - - liar Fil.150 682 - - 23 70 16.7 18.3 13.3 13.2 80 10 10 Casting Sill.8 l
- g 937 - -
12 30 8.0 7.I 6.7 6.5 -. - F f O Notes =
- 1. I-
$ The maximum tennile strength shall not exceed the minimum specified len de strrngth I,y more than 40.48 ksi. Where the Specification durs not hmit hardnes , the
-a maximum 370. surface hardncm s. hall not exrred Ihr hardecu+ salue, corre>ponding to the masimum sensde sterneth, as determined from ihr applicable Taldes [ in SA.
2
- 2. Until rules for welding on thi, material are added. thi3 matenal i not for wrided construttuen. O
- 3. I!p to 2% in. incl. E
- 4. Oser 2% in. to 1 in.
5. 3y The>r materials are limited for u c only for >mshbers and rem
- tant >upporta.
- 6. Max It!!N 215. --
- 7. Max IllIN 225.
8. 5 The rioncation and rc<lurtion of area rrquirement, for this matrnal ma> le >perified a- l 7% and 35') minimum renserti rly. ,U
- 9. When welding is requirrd. the allowalJe strr*. valur* of A319. In20llit whall apriv. i
- 10. >
For cach forging 1810 lim. net weight and Iro. the marking rrepurrments of AM>3 72 may le met by a suitabic rewir or :.)mle.J identified by the \lanufarturre ?! in 11. his Certificate of Complianer. The hardnr3, trat requirement shall le pertornwd only on the tensdr trat ,perimen. When weldme is required. the allowaleir > tree s a'uc, of A319,1026 fili shall apply. .,,
- 12. Over 5 en. to 8 in. 5
- 13. O cr i in. Io 5 in. C -
I 1. M I'latra up to I in. inre. and all *trurtural shap ,. b' Ch N wI 4A i , N m - i. A i. y, ^ co --a do lr
. g 2 =3 *
==.
2 i: to i. w
- 2 I
A N'C ==d e I ) O e C^[ v N' v& N H j 1 w N .i
.m 4 r -
v .-
\ l'd
EXH1 BIT 2, 21 pages (313-326.8l CA51i (scntin:;cd) N-71 -7 ()h44-7) CMES OMSME BOH.ER MD PRESSURE VESSEI. CODE l t i l i i l i i I i I i l i i 4 i i 1 1
-1 } l 1 i i i i i I i i I f I i i i t I I i J. .
l I i l 1 i i i q et e. n l 1 I I i i i C.
i.ra. e 1 i -e as ,= c e- e - e 9. e n e i A. a es M m -a e es es es I! je C, arg ef =,aq ej eg eg q C
'l i i t 1 1 t i I e Is h
E I I io -
- e,s oes.m-c M n en ne e es en e- e. s
.g 4, d .M C =, 0, s'; si te q C eq C, C, eq ?Q C q 8*t et *. eq C v.
y C e [
> e e.i.
ce $ .@. 8 - CC = t= M B* O to e4 -
?f 4C8* t*
e4 es M M e4 81 et e4 e4
-. c0 8* ea
- - gE e, C, e Pg g eq .q e, .q C. e .
.a sq e, C iq c. eg e. .q C 3 .3 e n - o- e. c= e.. o O en e e - c - ce s - n, M
- -- . - e.
. ca i.e se es e n ce n ce en ce
{ c. 2 C *1 sq cc, q C eq C C. q et C, q et et e,
, a E.
c n. e i nM .e. .t -cc e.. - in r- ee.-in
- eg cet e e n n- c. n- ce.
e e
- q-
- e. ena C.
f O O O. t-C, C, eq q CC q o e. c r. ec t C t't C CQ aq q C, q f7 el 4 aq C, - e - to m - - - .. Li C to e4 4 O 8- @ == CC 1- LS
- . t.=. ce - ea es M r1 es ei es ce ca 2
e g Se5-g e o e n e q eeq n 2 ;~g$ .e.m
,3 c s.
-e s.e. 4 s=.s- s- % t. oc e g =s n=e 6. ,,s e .. e - - - - -
e -oe e g 3 M 2 g (,) l c*2C211. 3
. e2 p
e
** e P3 O ., Oe wq d- e=.- e. M eeo
** @ fi
= . ., n . 3 - ee 4 0 @ eI
= = = =
. CO -3O .D @ .
ad
.J .3 b q E
- e 4 * @ 2 M **
3 es en #e. e. * **. e .: H =s 1 1 ,; I :: es el et i .- ej ei ( z ' 7 i* 3 h y i I f I I I I I I l e a l i l E J l 1 0 - e
. [,3 N. F i.S. E M
.s I.S, M 18, 38 F.,. E E E W.
-- - . _ ,, , . P,
)
**- CE6G%C 'e' 2 58 8;l24' 4q$2iii4%
H U CC- C E O r u --- .C. -C - .O - .C. e -- C O -O O - O O ta e p --. 48 g h hf 42 MMM 8 7 8*8* f* 8 M O8* 4 @ C 87 87 87 C 8
@ @ el 8* 87 8*
M M M fS C C 8* @ si e9
-c g
..g g' _ 8gM
- 7 8
- 8 .* 8 .* 8 7 3*
87 8 .* 87 _ .--M M @
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+
E4
---.<nren e
ee e
< < < <<*<<<<n
---- - - .E.
a U M u uuu u ed W 3 .h
= 3 = 3= .h .h
-,b i 2:
- a. .
.,.,. 6, m, t- H H t-.
=
H
= .I= 3= h.
HH6 ".,",".,'.,,'.,6 (A wv= , e e EE e 3* *
$zd
- i I i i i I I II I i i es i I es i t i 1 Q
d i l i 1 i i 1 11 1 1 I e 1 1 o I i l I C e C $ g c
* -C es C C IM
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.6 .d n = =CLa=COI C
=
- d.
e4
*d es j M M .M,
- d d- .*
**. O C C C-C C C
- < .e .et .i. C.
O = -
- ---- - ca - e ,,,,,, p 7 zE .E. _S EE .E E .E E _S.
EEE
--- E EE
- .O. .O _ .
O e w 313 SUPP. 3 - NC
r i
'I gg M* a.
p s'I m%= eWM h
~C. v D ,
n3m,^oO323ceev ( Z-N* N ng @ S.g % g 5M;>.C3~~i3Mm.mJn,2 : c 2 . Q0M 3 . t . m e. &h.b.eN*.. 0 0 8 l lu - p 0 5 7 in . ed em ts e oen 0 24 7 0 2 0 2 0 7 7 5 6 3 9 8 0 5 7 0 0 - 2 0 4 7 1 5 6 3 5 67 5 7 1 19
- - - 5 7 3 0 oo 7 2 2 2 2 2 1 1 3 1 1 1 1 1 1 2 2 3 4 t
0ot 1 7 I. 5 5 0 2.57 7 t s 0 0 to 0 5 - 3 0 5 7 *1 5 8 50 0 3 5 8 0 5 7 0 r 5 6 8 5 6 7 5 7 5 0 6 7 8 5 7 3 0 o p 1 6 2 2 2 2 2 1 1 3 1 1 1 1 1 1 2 1 1 1 2 2 3 4 p y r
- n. .
tF S u y s. 0 0 - 3 R4 8 R0 2 3 0 1 7 7 5 8 5 0 n. 3 58 0 5 7 0 t n l per it u 6 2 2 21. 27 21 5 1 1 6 5 5 3 1 1 6 7 1 5 1 7 5 nf 7 8 1 1 2 I 1 1 5 2 7 3 0 2 3 4 e ~ n o lu ta 0 7 1 8 2 1 0 2 I. 7 '7 5 8 50 u. 3 5 8 0 5 7 0 ( p I mrep 0 5
- 3 1 5 8 2 5 61 5 5 6. 17 5 7 5 0 1 17 8 5 7 3 0 2 2 2 2 2 1 3 1 1 1 1 1 2 1 1 2 2 3 4 m isme o
C k.sr t 0 0 0 0 8 3 0 4 3 0 2 I. 7 7 5 8 50 n. 3 5 8 0 5 7 0 e p y t se et r e 4 3 3 2 21 62822 25 61 I M15 6 1 7 1 5 1 7 1 51 0 6 7 8 2 1 1 1 5 2 7 3 0 2 3 1 T l Sm 0 0 R3 2 7 50.2 0 7 7 5 8 5 0 0 3 5 8 0 5 7 0 l e ler 0 0 3 6 8 2 5 6 6 1 5 6 71 b fo 1 5 7 5 0 6 7 1 1 5 7 3 0 h 3 3 2 2 2 2 21 3 1 1 1 1 1 2 1 1 1 2 2 3 4 S a w d o 0 8 3 2 7 5 0 2 1 7 7 5 n ll 0 0 0 8 J. 0 0 3 5 8 0 57 0 a 3 1 6 8 2 5 61 7 1 5 6 7 5 7 51 0 6 7 8 1 5 7 3 0 e A 2 3 2 2 2 2 2 3 1 1 1 1 1 2 1 1 2 2 3 4 t Pla 0 0 R3 2 7 50 25 7 7 5 R 50 0 3 5R 0 5 7 0 0 0 3 1 6 8 2 5 6 7 5 6 7 S 7 5 0 6 7 l 5 7 3 0 C 1 3 2 2 2 2 2 1 1 3 1 1 1 I 1 1 2 1 1 l I 2 2 3 4 M , d e et t h n n ad gi 0
- a. e msns 2 5 5 1 9 8 0 3 0 1 9 60 G0 ( 5 3 676 7 0 6 3 0 )
7 Mfin5 6 in5 7 0 0 H 5 n 3 6 3, Min ek 1 1 1 1 1
) lt er 1 1 1 1 d
't 2 uTtS n es os h 5
- C s ndtgi 0 5 0 5 0 0 2 0 n2 6 Hi 2 0 I 0 2 5 ? 5 5 0 0 I la elen s 0 7 6 8 0 7 4 5 4 1 5 4 5 I 6 3 3 l. 7 8 1 3 2 Cr Miek Yrt 1 1 l 1 1 E o S L f B sy s 0 0 e
A t 2 - - - -
- - 2 2 3 i - - 3 5 - . - 0 0 0 1 1 Tt o 1 - 1 o 1 1 1 1 1 1 1 2 2 At N 2 2 1 1 r
e u p p o C lo 3 4 1 2 3 - - - - - - - - - - - - - - K A1. % N I C d n WR a e prd e CC l I D. D. i G o 1 l 1 ls yoa r 04 2 - - I. B. J 2 50 2a 1 I. 1 I e e 8 A A A 1 I T A ( A I CCl ( T 3. - - - - - S t T G l i 4 1 ic it r . a a a a a ca o. r e 6 6 7 7 7 7 7 7 7 6 7 7 7 5 5 5 5 5 F f iN 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 7 5 75 77 67 272 72 7 2 2 7 - r icn 9 9 2 2 3 3 3 2 2 9 8 8 8 3 3 3 1 3 e 5 8 8 - 8 l 8 o 1 I 8 4 1 1 4 7 7 7 8 8 8 3 3 3 3 3 r. d t f eo pi St 3 S 5 3 5 5 3 5 5 5 3 3 5 6 A A A A A A AA AAA A A A A A A A S f> 6 6 6 MA S A 7 6%6A A6 A 6 A6 6 f f f
> f S, s . .
s e pe e e p p u a a a te t h b g h ' g g g g V c n um e e e e e e e S. e e S. n n n n n s s dr b b S. ig ia r e e e r e e r ig ig ig ig ig e o rF o u u a a a a a t t t t t ta a r t ol f la t a t ta ta t t ia r r r r r r r r S t r P { TT1 P1 P P P P P l l l l f l F P P l' P P la l l P la P P lal I i l a ia F F l o o F o%oF 1 [( le p b u o . a o l
- 2 2 - - - - - -
w rN d
't lo l
A G.o C n o P- N ( - 5 5 - - - - - - - - - - - - ~ - - - - - s le 2 0 01 0 e 4
- 8 5 t 1 V. 3 3 3 n S 4 V. u u tsr o V. C. C 1, 8 1 _
ni t lo y 0 4 WW W u r n 0 0 0 n 2 3 1 i Wo aV.. 3 W C.Ci is _ t V. mo op l A 1 4 1 r I. . . r r :r I. h r r b h %. r \. 6 l1 8 i 1 3 8 a t. Nmo 1 C
- r 4 C C. S. 4 A '4 C. 4
% 'h C.
4 C. i I 1 I w S d - S 5 S I S 1 8 C L o I A 2 2 Ni NNWWNi o S WWWWWWW !A 1AA I I A A 1 S*
"5;1 2o
un "g,
^ Z'M> e g
.N.M
-z .._ sa :
o q ~Nn#a e
., v
. . 3
+
2. 2 C TABt.E 2 (Cont'd) S Allowable Stress Values, S, for Ferritic Steels and Copper Attoys for Classes 2,3, and MC Plate and Shett Type Component Supports g v Min Min Ultimate Attawable Stress, ksi Imultiply by 1000 to obtain pail Type Weld M Nominat P. Group Product Tensde for metat temperatures, F, not to exceed ,# Specifeca- or Class Notes Strength, Strength, f3 Composation No. No. Form tion No. Grade 100 200 300 400 500 600 650 700 750 800 Q hsi ksi i Copper and Copper Alloys .e . AIuln. IlrorUr .s
- = ltJr .El!.158 612 m 25 70 16.7 I t.0 15.", 11.0 - - - - .'
30 10 10 - - Casting Siti.fi l 937 m 12 30 27."> 7.0 6.6 6A - - - - -
.:n Notra _9 1
- 1. !=s a The masimum sensde strength hall not escred ihr minimum specified ten ite strength b) more than 40.0 Lai. Where the Specification dors 3 not limit hardnes
*i madmum surfare hardnew shall not rsreed the hardnew saturn torrc*pondin:: to the masinmm ten dr >trength, an delennined from the apphrable Tabirn in SA.
370.
~
- 2. ?, .
l ~niil ruirs for wchhna on this matrrial are added, t!n* material i* not for wohled construetism. -
- 3. L'p to 2% in. incl. 4
- 4. Iher 2% in. to Iin. =
5. fe.
'Ihow materut,are lismtrd for u-r ml) for snubbrr and run tant suppore .
\tas lillN 215.
Q 1- i
- 7. %s ItllN 225. i:i .
!!. M
- 9. 'lhe rhmgation and rrdurtiim of arra rrquirrnu ni for shi material rnas in >gwrified a I74 arul 3VJ minimum, re persnels. < j H hen wrldmg sa trquared. the allowahic trra sahar,of A319. In2tilll6 hall appis. '
10. Q i his Certificate of Comphanre. The hardnr>> tv t trquirement > hall be performed onl3 c the tensile tr>t *prrimen.For ' rach b
- 11. % hon weldmg is rrqmrril. the alhewahir otrr > saturn of A319.11t2t.ll14 -hall .sppl).
- 12. Oscr 5 in. to 8 m.
[F -Q n
- 13. t hrr l in. to a m. 2 e W glj I 4. 11atr* up to i m. incl. and all >trurtural .hapr . I m Q!
'rO e N
ea ; y sn W ea i .
~
Os
* \
%e
.i
_} EXH1 BIT 2, 21 pages (313-326.8) CASE (continued)
- Y N-71 -7 cases or asue non.en en enesscne ma. cone 1I I I I i (1644-7) l I a i l i i l i i i 3 i a l I i i l i j '{ l rI i l I I i i i i i i I I I i i i i i i I lI b I I I i ! i i i i i i i i I i e, e, - e t.g ,, 3 e W m* 1 i f e m n e. I I I I o
9I I l l l 6 i l I i i I i
.~.*n- '
g E 6 I . ..i = H ,:i l ' I I I I I I g E.
- es n M es y
a S } l' l ( l l
= = e
>* i 1 1 1 I I i i t a' es e nW es e l ( I 3 @ == l '1
- I I e
I-3 t 3* M ee y y' eg l l 6 ) { l i j l 4 1 i i ! C3 N I .l M- 4 8 l e n n e. l \ l I a U j 3-{ 4 E i i e, ce,;c ee e,
- ne, v.e, e se e,q s. e
. .- m E.e,* = m -
- e,.3 q , e g .*,
co ==e ee ese ne e==e i,,, m 3
-- m es es e 4 e m=n e* .o . -ao as e.
es c' m e, g 8 i ! e C! C ** e9 -$ @ L1 9 S. 9$?
- e.! =M- E #ee$9 9 9 C.
e M .$. (1 ==-ee-eg # 4 == e t. .e. a e4 = es es M M 4 M g t* as e ff
~
= m .
== tt) es .O 8 99C ai
- *O. re cQ e, 9 9 9. E e, M CA % ej li f9
.2 @{ e
> I I- e-o e ee ei es c*e *) 98i=
sw ca - e e -- e e. n es elce es3 e- EJ - M o na i- 4 a
$en to 8 E9 O, 9 E O
]g '"
ta es et= CC. 1 es eg == O.
= g .E C9 . *. .g *.
J == f. 81555O et : e
$ E .O. O.
e O O. O M, S m
- _
- = -
?"S s . c0 e .O M et* .. et c'i * -* M ti *3w2 4*
."J el = =
81 *@ ei. e* a e c = e = e se .=ee c =. m es - x === s.e. i:. e e :: eg a see 4.- s. e eo e *t = s= 2 ;E ,J - - = es e .i- .. e. i.
=
e i. x
=c 5"G E
U e2 5' = =
.. T g >.e j',g e e r. co - e. ; .e -
m ng - e. - eer e
- -e i . -=.4 p=, n= ees2 .*-*ei
- nn z..3 en e =
w- :: n m *e J $ M D ,el O
<3 pq
. 5 g ~
--- e - e. e.
o- 2f f I l - m. es e; *. . 4. *. ~4- 1 1 1 l I i .+ 2 ad - ,:,:,-- en en en . n cs n 9 1 s-3 & es eee cm e s
~ e e 5
h i l l l 4 1 4 I I I i l i I i 'M i
'E 0 l l l 1 1 1 l l l l l l 1 j - AMM M M Am d, U,4 --
k&Y 3 y v = i = .; 1 M E FMMeRs gMdREE = T. E E E3 A r G " "4 o A
==2 E E 5. 5:
u, s '* . , 3 3 c = = = = =
= u m ==no=u
== = = = = = = = = = n u
*g e. e-s e n e -- nn ne B 3z e a =- e r: it *: i: it it *:
.- : e : ee.e. eeece: ee
-e . g g, g
_ g .-g g----e g 5 g g .ap -,g p '.- '::'=': = =_e m ------- neeeeyeee
. ay ': i t i: it tri:iriririt it i x o .s _e = s.= .,.a p. n_
<<<<<<<<<e w e - < <e_<n <e n-<<<<=r*<<.-
w to, C
= = s. w ., e n m e e r . <-
3
~4
> t v= u e 3 = i i .:
ii. ]o[ d' 6 3 E1 1 h #*
==-
DD......E. " ' ' ' ' ' l . b . m 6 m 6 " " st ' O. ;I.20 ' ' ' ' ' ' ' g --v--.- ' 's S ? 5 $ G E ? d N Wv 555555 5 i s t.
.2 o O gi l i I i a I i i i i 1
> 62 - - 1 I i l i l i i O. -
4 1 dj h; ) 1 i ! 4 l l 1 l l l l l - - I I i l l 1 1 l l *
- d. i c=
L' kg 2= .c3. a .g 75 .c g- 3 c .*
.Q e
- a. u .g 4- eg e. - - - n=m
- es
*3 A. 2. E e O * * * " " - te et du -
e E , g ."". C .O II- = C O ee o == - - ' C z s. s.
.s -- 3 w ,= r ,
wy www
.O o
=- a q 3 . , www w ...
O6 ;; < E U -C < < *C < <
--- .=
3.' l SUPP. 3 - NC j L. . . . , , , . . . . _ . . _ . , _ . . . . . . -
. EymBIT 2, 21 page3 (313-326.8) I CASE (co'ntinued) N-71 -7 . (1644-7) CMES OMSME H0H.EMNMESSUHOUSD. CODE V, p 3 . iti i i i , i , ,
, 1 i l i i , I i , ! , , , , I l i , , i l l l l' ) J l 8 1 'l IIIil1111IIIllIlllIIl
@d@d O CE4 Pi C e{ C e4 eg M M ea M elc es
~3 g, 9% ' .J C .4 9 c. $.
e8 e t F*
%=g.
& 9ggE Me. E $. :*g* E 3
g9$. f. C% r1
$ ". 4 N C. N O. 9 ". O N$
oo "P s. O t. e - - L- 31
- CO 8= e e.3 ** C M -M e@
o = e e' e-
" E C e e e CQ 4 8-o I" om eg; 4pge npm.; eg c :c - eg.;.; egese. 'a e
M q e. R R . C. . -- O et :C e. 4 O 9 4 #
- E 5
-c Es es n e =. 6x
=* I c-O ee.-ee
- t. a 9 e e-e ce cc 1. s4 cO es - c
I
>- - *C C. :: r= 8 -
eg *; e=; e. =; *- S a d E .. e -: es es e G e.;s e el ;es.;::se e:d es - e. e e se E e, - :. e M. O. eM - e e, q q -* 4
- e ee
.S g.* . i . ca : xc . q e e eescc es :q $. ey e: e. ez-m r-Dh d e: se. c eaccz.
'5 e 5'. fi
.,; e*@ 64 q e- ed el 4* fa *- *-
n- 8-C 9 Pe " EO r- cO=**e-SM$ I*! O ** N *I " I * "". N ** ** g E 1'
- ca es 4 -c Es ei es Es c MO
- -e-e em * " c' **o as b*-c2 e **
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TABLE 3 ICont'dl y Yield Strength Values. S . for Femtic Steels and 'We Alloys for Classes 1,2,3. and MC -..tLinear SupportsType Comw Mm Mm Ulbmate Nominal Type. Yield Strength, ksi Imultiply try 1000 to otstein poil P. Group Product Specifics. or Vield Teneile for metal temperatures. F, not to encoed Composition No. No. Form Class Notes Strength. Strength. , teon No. Geode ksi kai 100 200 300 400 500 600 650 700 750 800 Forting A 47170 1,2 . 2 85 105 Forging A47170 - 3 1.2 85.0 80.1 77.5 75.8 74.6 73.3 72.2 71.2" 1 - 3Ni-Cr Mo V 95 110 l'orging A47170 - 4 1,2 95.0 89.5 86.6 84.7 83.4 81.9 80.7 79.6 - - 105 Forging A47170 - 5 120 105.0 99.0 95.8 93.7 92.1 90.6 89.2 88.0 - -- - 1.2 115
- Forging Al7170 - 6 130 115.0 103.4 104.9 102.6 100 9 99.2 97.7 96.4 - -
1.2 125 140 125.0 117.8 ! !4.0 111.5 109.7 107.8 106.2 10lE - Forging A47170 - 7 1.2 135 n 3Ni-Cr.Mo.V Forging 150 135.0 127.1 123.0 120.3 118.3 116.2 114.8 113.1 A 171.70 - 8 12 145
- g Forging A171.70 9 160 145.0 136.6 132.2 129.3 127.1 124.9 123.2 12l E - - F; 1.2 155 170 2%Cr 1 Me 5 2 Casting 155.0 116.0 141.2 138.1 136.0 133.5 131.!! 130E -
Ni.Cr.Mo Casting A487.76 - 8Q
~
85 105 85.0 78.5 76.1 74.5 73.2 71.7 70.9 70.0
- Q A 887 76 -
100 100 1 125 r. Ni Cr.Mo - Forging 100.0 97.0 93.2 88.0 83.5 83.0 113.0 83.0 - er A508.76 - 44 1 100 115 m Plate A314 75 All 100.0 91.2 91.2 89.2 117.7 86.1 - - - - - I .2.3 100 Plate A314 75 All 1.2,4 110 100.0 95 5 92.5 89.8 87.6 85.5 88.3 83.0 - w 90 100 AIS14140 90.0 86.0 83.3 80E 78E 77.0 75.9 74.7
'2 Tub- A319.76 4140Cu -
4142 - - Tube - 2 100 > A319 76 4142rn 120 100.0 93.5 90.2 87.8 - - - - -
- y 2% Cr.l Mo 5 2 Plate A312 77 -
3 - 75 95 = 2% Cr.1 Mo 5 2 Plate A512 77 75.0 72.0 70.3 68.9 67.7 66.4 65.6 6 8.11 - - = 4 - 60 83 Ni.Cr.Mo 60.0 37.6 56.2 55.1 54.1 53.1 52.5 31.f1 Plate A3 83 77 A.It 1 - 11 5 los
- h Ni.Cr.Mo - -
Plate A513 77 A.It 85.0 110.0 77.5 75.8 78.5 73.2 _ - -
- E 2 I luo 115 Plate A383 77 A.It 3 100.0 98.2 41.2 ft9.2 fl? 7 116.1 - - - -
".f 70 90 Pla tc. liar. 70.0 65.4 63.n 62.1 61.4 60.3 59.5 58.7 - -
7r. Shale A572 774 42 - - 42 60 m Plate. liar, 42.0 40.0 3fl.3 36.8 33.2 33.5 32.7 31.8 - - b, Stule A572 77a 50 - - 50 65 $ . SNi.Cr Mo.V Forgma 50.0 47.5 43.6 43.8 41.8 39.9 38.9 37.9 - m g A579 76 124 - 1.2 1 80 Plate. Ilar A388 77a A.Il 13 150 140.0 138.6 134.0 129.5 127.7 126.3 123.5 117.6 - - H 42 63 H Mn-Cr.Cu.V - - Platc. Har A388 77a A.H 14 42.0 40.0 38.3 36E 35.2 33.5 32.7 31.8 - - O 46 67 y M t Mn.Ni.Cr.Cu V - - liste. ilar, 46.0 43.8 41.9 40.3 38.6 36.7 35.8 34E - - - Slupc3 A388 77a A.Il m 15 50 70 N Forgina S \.592 AI,F - 1.2 100 50.0 47.5 45.6 43.0 41.8 39.9 38.9 37.9 - - m m 115 100.0 95.5 92.5 89.8 89.6 85.5 81.3 83.0 c, Mn.C V Forgine Tul-8t.592 A.1:5 - 1.2 90 105 90.0 86.0 83.3 . 80.8 78E 77.0 75.9 78.7 m
$ 3
- o w Mn.V Tule
.wi8 7 8 11 - -
50 70
. - Os 2, 3
* $m l
A418 7I Ill - - So 65 50.0 45.8 81.7 38.0 31.6 33.9 33.6 33.I A - Mn.Cb - 3 2 0 Mn.V Pla te Ah33 75 A - A N C ^ Plate Ah33 75 1: 12 63 42.0 38.2 35.1 31.9 29.1 28.5 2 11. 2 27.8. - - vq N 78 EL d w v N !t
- e.
v .
r. l . . l I l i i C A Y w Z . n. p z o Ohm A w m A e n a N .q o n v 3 TABLE 3 ICont'd) .o Yield Strength Values y S , for Ferritic Steels and Copper Attoys for Classes 1,2,3, and MC Lineer Type Component Supports { C Men e
- Mm Ultimate R.
Nominet Type Yield Yield Strength, ksiImultiply by 1000 to ostein hl v P. Group Product Specifice- or Tensate for metet temperatures, F, not to encoed Composation No. No. Form Class Notes Strength Strength, tion No. Grade k si ksi 100 200 300 400 500 600 tiSO 700 750 800g
%In.Ch
{~
%!n-Cr-Ni-Cu ) -
Plate A633.75 C.1) - , 3 50 70 50.0 45.l 41.7 38.0 34.6 33.9 33.fi 33.I 114tc A633 75 C.lb - 4 4te 60
%In V.N -
114:e 46.0 41.8 38.4 35.0 31.8 31.2 30.9 30.4 - 5 A6:ta.75 E - 6 60 im 60.0 54.5 50.1 AISI 4140, 4380.8620
- f Forging
- ( Forgir.g A668 72 is -
2.9 no lui 15.6 41.5 40.7 40.3 39.7 80.0 78E 72.3 70.3 68.1 611 63.1 '60.9
- M A668 72 K -
2.9 75 100 AISI 4140 Forging 75 o 70.1 67.7 65.8 63.0 61.0 59.0 57.0 A668 72 1. - 1.2.0 ifG 125
- - 5 4340 - -
Forging 105.0 98.1 94E 92.2 89.4 85.5 82.9 "9.8 A6f4172 L - I .2.9 115
- Q U forging A668.72 4 ~.
95.0 88.5 85.4 83.0 80.6 77.0 74.6 72.0
~ L -
2.4 35 110
- [
AISL4330 Forging A6fdl. 2 ft3.0 79.5 76.8 74.6 72.4 69.1 67.0 68.6 11 - 1.29 120 14~.
- 2 8340 - Forging
- f Forgmg writ.72 \1 -
1.2.9 115 120.0 112.1 108.4 105.2 102.1 97.6 91.6 91.1 lin 115.0 107.5 103.8 101.0 98.0 93.6 90.0 87.5
-3 AeW1.72 11 -
i.2.9 110
- [
135 l'orgine A 66tl.72 % 1.2.9
!!0.0 102.9 99.4 96.6 93.6 80.5 86 8 83.6 - 1 llo 170 AI5I1380 - - Forging At f.fl 72 \ I .2.** I r. IfC 180.0 131.tl 126.3 123.0 119.1 114.0 110.4 106.3 -
-5 Forging Ar.v.it.72 N 135.0 126.1 121.9 118.5 115.0 103.9 106.5 102.7 -
1.24 130 160 High Alloy Steels 130.n 121.5 117.2 IIl.I i10,7 loi 7 1u2.5 98.8 -
- 5 Precipitation Hardened Steers '5 tm 15Cr.lNi.4Cu 'h ! g$
Ilar. Forg. A348 74 \\ll2 - 1.2 1 15 155 $ i I 15Cr:lNi.lCu - - Ilar. Forg. A348 74 185.0 136.0 130.7 125.8 121.7 III.2 II5 2 112.9 - - M
\ 1112 -
1.2 125 1 15 s
- 13Cr4Ni.2%)o - - Ilar. Forg. A~.6 8 74 \\lla 125.0 117.1 112.6 103.3 104.8 101.0. 99.5 97.2 - -
1.2.5 ItG 175 165.0 158.6 148.5 143.0 138.1 133.8 131.1 128.4 E Stainless Sieets - -
.N. j AISI 302,30 8, Wire A380 76 d-II -
2.16 100 125 310.317 - - 100.0 83.3 75.0 69.0 - - - - - - l.i! i m I tn e-a Y u i y t 0% 00 V l
' ( ( (. (
.~g.
TABLE 3 (Cont'ct) . Yield Strength Values,Sy, for Ferritic Steels and Copper Alloys for Classes 1. 2,3. and MC t.ineer Type Component Supports Notes > V-
- 1. The maximum tensile strength shall tml exrced the minimum agreified tensile strength I,) more than 40.0 kni. Rhere the iS rcification dors not limit hardnce, the 5 e
maximum surfare hardnesa shall not exceed the harduras values corrr>p.mdmg io the maximum ten >ile strength, as determined from the applirahic Tahics in SA.370. ' ' -
- 2. I!ntil rules for welding on this material are added, this anatrrial is not for welded rimstruction.
- 3. lip to 2% in. incl.
- 4. Over 2h to 4 in.
, y.
=
- 5. A564 Type XM 13 shall be modified so that age hardenmg treatment shall tw 10~20 F only.
- 6. Theme materials are limited for use only for snublern and constant supports.
S Ie. y 7. Max BIIN 215.
'ct 8. Max IlllN 225. [
g
- 9. For carh forging 100 lbs net weight and less, the marking requirementa of AWI.72 may le mrt by a suitaur code or >ymisolidentified in the Manufacturerin his ' ;
Certificate of Complianer. The hardncas tr>t requirenwns shall tw perfornwd ont> on the tensde test spreinwn. =
- 10. The riongation and reduction of area requirements for this material may tw perified at 17% and 3W minimum, rrepertisely.
- 11. When welding is required, the allowable strem ialues of T519.1020111t shall apply. h
- 12. When welding is rrquired, the allowabic strem salur> of A319.1026111t chall apply.
O
.G.
- 13. Over 5 in. Io it in.
l1. Over 4 in. to 5 in. Q*r
,j
- 13. 11ates up to 4 in. incl. and all structural shagen. Q
.g.
- 16. This material may be used ont> in fully constrained apptirations >uch as thread inwrts, no tha; failure of the wire would not affcci the function of the component support. g
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- 9 7 6 1 1 1 l 1 l St AT A A 1 1
1 1 l l 6 S S S S A 4 5 A A A A LA b0 A b b. S S S S S S 8S SS p u _ o rN o _ G - - - - - - - - - 1 I 1 1 i 1 1 I I i s fe e
.o.
t s S PN - - - - - - - - le e de - t 8 8 8 B 8 8 8 ! n S t 8 8 e s s ls 0 dr e 4 a le n ts e 1 H n _ e n%tiS
, t o a
- lai ni s t te 5 0 S 4 5 4 4 1 5 1 s i 0 S 4, y7 0 8 ~i 5o , 0
. 0, 8 0 o2 imo no10 10 l
8 _ l 1 2 l 0 lo3 03 0 101 3 43 4 it a i ic 8 8 . _ op l 1 1 l l 1 1 1 it N it 0 0 1 6 7 .. 6 6 1 1 6 7 1 A4 4 n3333333333 1 i l , 4 1 2 2 0 5 - Nmo t 1 r S S S S S I i I I i S I S I 5 5 I 0 I 0 ip 8 r e aI I S t I C CA A IA A A IA I I I oI I 4 IS 38 r 3 c C e s S SS S S 1 I I I I 1 S Sl IS 1 1 A L wlS A A1S0 30 1 4 IA4 I A$P 1 u I AA AA A I I I I S S I A A IAAAA I I g* . nc i 3$
( c t ( d TABLE 4 (Cont'd! Yeeld Strength Vafues. Sy . for Botting Materials for Classes 1,2,3, and MC Supports' Min . Min Ultimate ' Yield Strength ksi (muttiply by 1000 to obtain psil %y Type Yield Tenssie Nominal P. Gro,sp Specifica- for metal temperatures, F, not to exceed 3 Composition No. or Class Notes Strength, Strength.
- No. tion No, Grade k si ksi 100 200 300 400 500 600 650 700 750 800 $ C AISI 316 8 1 SA 19 8 11 8 \ 1 -
In - - - - - - n AIS1321 8 i SA.19 8 Il8T 30 - - - - - o
.- -. - - - - =
Notes m 5 [
~~ I. All A307 bolts shall. in a<fdstion, meet Exilh ihr chemical and mechanical requirement < for SA.36 bar material. Welding is permittrd.
- 2. No welding permittrd. $
- 3. A561. Type \%13, shall 1.c naulified so that a::e hardening treatment dull le 1070 F. only. =
- 4. %1mimum Tempering Temperaturc . hall be 350 F. $
j
- 5. Allowable tensile, shearing and tending stres s for the Imle and threaded part material- of Table 4 shall not exterd the saturs si gnen in paragr
- 6. The muimum tensile >trength
- hall rme excred the minimum spenrwd sen ile ,trrngth by nuire than 10.0 Loi. Where the Specification dora not lim maimum surfare hardarm chall not exrced the hardnr>s value. rorresporalms tu ihr maximum tensile strength, [ a4 determined by g
- 7. No yield or tensile strength specified. Amume to ler the umr as A32513 pr I liolt, for nut dr*ign calculations.
' 8. 3 in. mnimum diameter, cold drawn and temperrd. us -
9 10 in. maximum diameter. $ 10 No yield strength or tenJe strength specified. Amune to bc Ihr name strength as SA.193 liolting material of the equivalent grade forQ nut design calculati $' g Q; ta
=
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m A-A
- ^ 0 #
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s in A s -
Aq o 4C1 u'
y e v 8
. s, EXHIBIT 2, 21 pages (313-326.8) ,
CASE (continuad) N-71 -7 (1644-7) CASES OF ASME 110ll.ER AND PitESSI.'ItE VESSEI. CODE g' { l i i i l I i i I i I i i a i a i i i i i I i i 1 o
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m . ok 4f t. M- - M I' M I* M MI" Mi* MI" M @ 4, Y2 8* C
- I* i M @ @8* C c to t, mCI*48*cccc@ c
.> -= 4.:
. ,e, --m eq - - -
'a* E
.: a I'.
I* I* 8* I* 8 I 8 l I 8 8__ 8----0a' 8 8 8. -. eg -e a'* pi ce e. 2 n.:. s e' n me e en ., a a s m s s s' _s" _s' _s' s'
%=.-i; .o _=e
< < <<<<<<e< u,<
- m m u: v. < < < < < < m<<<<<nn ., n n- -.
i < < ne <<
$a=
>7 c y = . .
9e2 w_ o. m N x=0 N N NN NNN .Q in *= = = =N Se= = = = c:= m"8_-,,,. s s m s s s s s s s s s s s e a
- a. -
g j I l I I I I I I I I I I i i l o C I I l l l l
- s. o
-3 43. gi i i i i s 1 i i i -- i i i i i i i a . i i i g
a e. d ( ,o e. s s! s ca 7 =
- 8
!.4 m-e
.E
.4 8 e,
.-1 w a= = =. ,eo- e e'.=
~
e - -d-~~ n_ v _c- e, e E
$gE ENa 2 -.
- - .. _e. e.,
co
= e
=u d03 N$E 4E8 EEEGE ZEE Z8
=
dE8dE" EEEEE REE E~ E E 326.2 SUPP. 3 - NC l l l l
c c EXH1 BIT 2, 21 pages ' (313-326.8) < r CASE (continued) o
\' N-71-7 ases onsus nonnusn nassnie ussa. cone (1644-7) g i,iiiiiiiiiiiiiii i i i i i i i i i i - , i i , i i i P -
,e1, $. 30 i i ii i I i i i i. i i l i i i i i i I I I l I l I I l I I I I I ja3 E ei $ $ E O. ** $ 9 $ $ $ $ k $ $
m o .= u n i i i i i 'i .I f* I i i ' i i i i = - e = es e i e .= .e.s- e ca- - E. o
---.eQ 2 " &" -----
- n e"ee -
- c" O.
t- o g - 3 i i ei i 1 =- . = , = . = e. =. ooo2 C. = = =. c. o
- g I g- i e i i t i 6 = e==
a 0*
- g" = 0 es ei cc ca e
- 1 ==e_= 5-e ===e
- = f1 ?4-e
=====-- 0 2,~ E =- =. = =. = = =
=.
>J @ : i i ; e i i - 1 i i i i 1 g 6 = e: i o .o =. = =. = =.=o = =
6 gee e= n. =ee C I.
-- e .=- e n =n== :: .e. -
.es - . .e=.
-. . = = = .
a 3 = s v E = _E g .. 8 e i i i i i g- i i i i i i i 5
= r==
$ 5 =. CC -e 9 i C :.99O $$$$$
gM e .- c en e = u g e =---e. e w ..6.==.,, e .n. e.e . . . h C= = = c=C =
> e- 8 ci s4 = 3
=0 = EE E E . E S E C. C. O. $$$55$$
e e.ed '4 oe ee oisee.i ei e6 ee so cc e. ee a. -=es-
-7 . e = i-== ~e = ei oe ee e cc e : es t- 0
~
--- co - e _- c3
- - - e e e= -n= - - es -- - = -
E "-
! E 8 CC==
W * * = =- * * * * "'*
= e.*- .9 e=- - r- * **********-
w.: ei : -: 4
- eee-eeec m -
8 s. 2c e:s :3 si e @E 3 e s:*c =e= s=. .*i
, el, ". .B -
.d e=s e=:o - F .e e g e.c - e o .m e s -
'.! 8 e o .4 e 4ecioec:6 = = c c = c = c.e ce =. c. c.
e e4 eei.jja =o q = . = . = . @ C. A43 =. C =.=.C. 99* l O"I 7 e es e e cc .c q% t- e ,-$ e= en. = e== e .= es- e :c - e e e : o +- eeeF -m oe
- - .cf. .e. es e - ce "g
- 8 ccccC C = C C C = =c ci W .4 ci y si ei ci =' ::s 4 4. e.i-c. Q e4 . E C. E $ C. C. C C. = 9 C. O O. c. C. O.
= .= e e =e.ece.=
=n=0 n =
= eeee s e c N. ..
** Ti e e. c5 e w e o e a: eee cc 4 e=.s .
. - e, = o m -0 3.I .
*i
- e*
- E 's E c
- o e e'a e 5 e e e o c:- e e es cc e e q e. c: ia 4 s=. e- e e== ce -
- l. 3 2 .= g ,a : ca e-e i
.;; oee e = g 02 5 '- G es
_=_-.e e-5 - .e e . =8 .eeee-- es --- -
'v .5 E e
- c >3 e= e
-C3 5 m t. e n=3 ea C f9 a C = **
o n en n e e e6 m n .*t ememoM r4 M= et ta I- 0-o o 80 2 >3 g ,g ,=: ** e9 a9 o et c eS =e a se e9 c: = u=- t =c e -es c 5 e. e= co
- s. etosec -- e :c
-ea 4t .O m w
a [l a. . 80 f J k O wig v 0s ' ' 9 9; iiii1 - **
-
- 1 1 1
.o 0 - 1 I l I i i ! =O EE O MU mm=c=UUUU ===m
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. 'e wl t
> a lt- i :
*i u_.
.. e P.
- ;- e - e. c_::
A
=
-.v
'g g >= 0 ey......
=
w *
- i i , , - -
- ** * = .d e=s e= 'J _- e.
w c i i i i i e i i i i s A = --= c: 4
*E[ hd c. 9 .8 .4eee e t.1 si es e4 e4 *8 4 M
- MM @ 9I*e@
+2 t. *
.P W tw $= 0* 4*. f*. 1* t *! e l* 1*l'8* 8* B* e@I*@8*@ e@ C g g g , y. t eonii4 2 2
'E .$ $ . . . , .ec-.4 4=:
. l .a 8* 8* 4* f*
'g*. >
- - - 1*
+g, a a a a a a a a' I*a a a' l
C l O=
* .9 e e e n .c - e o$m a a u 5 a.s ,ennm m n n n mnm
%.7 3g
< < < < v. v5 < < < <e <3 <e <mi< - ---
< - << v.<<<<<
-M M * - - - ------
e<<<<<
~
>g.l.
.- U wwuu c e== u ee es u u uuu u A Ig 3 = =c c = = = = =
- S O h hk k Jaiib b i
.e -
. g
- a. u. .- .o. o-.c p .e. m
- *: ,e .c
.p. . .. *
- 6 6
.a a- .a 6
----m-aaaaaaaaaa
.3.,.5 .3
=
2
- t. w n. e. *. m w w a m 6 5 e% - - -------
EU *
. o. I i i ==.
I i l l i l i .= el I el I I 5 0= el ! I l i l l I I i I l E
- st j .i i i i i i i i : -- i - i i 5 e i e i i i i i i e i i e=
f$ M m = =' **
. == g faF9 -
C ' t-r4 e ** 9. .=. . 0
. t.6. =
4 'o
.C C e eg C C ta > =. = M C = =
. .=. n.eg=
e$ c = e ea es es M O e =q ra .=: to eg at
- C.
2 C C = = - ** =4 M *P, . cc. M ** ** Z =. e-c.C. . m
" - 4
.*.e-*ee=. ** cQ
- O a O n -* .= =.
v=..=. ---va m 1-5.a m
-- v. n .c.
m v. --
-.1. . .-1. .m, .m.
.. m
< < < < -r- e<<< - . '
< m.e 326 3 i
SUPP. 3 - NC I
EMHBIr 2, 21 pages (313-326.8) CASE (contlnccd) . N-71 -7 (1644-7) c'sEs or ts"E no" Emo ms"E "ss" cooE l l $ $ $ $ i I l I I l l 0 l l I I I I l l l l l l l l I l l' l l I I l l I I I I I ~ l l l l I i l I $ $ l I l j t C. O EC E. E El ** I l k C. 89, b. 9 @. ** 4 Q Q Q Q CC, ti C C sa io ** eg r* es e3 =. = c. = - = = CO g8 3; @
- f. l l is C C, = C o3 - .e. .fi. .M. . .=. ..
.e.s M. - - .e. .se. cc CD -= -?8 :C E0 m - .C. & @
s.S t1 se
=* tS M
O C = C = = = = t. PS CC .P @ ta 4 4 - C = 0 ** O O C I"$, i4 C e is d i si= .* .4 C C C C
.it. .m .e .e.9. .m. . -
ese4
. - - . n *re o.ei e es ce cei=- ei -
is d d =' =i d= 6 I I id
.e.s.:: :c -= - . - -
c 4 e. is t4
.m fe ,. A u.' C. C. C. C. E: 8* * "
E " 'I ?. ""! * **
> =*. h m e = m* = - g i-E. O EE"3
- O. C. C. E cg en
..g Li st to 9 ed
.M
= . .e. e toit*e4e==-re a
C C = l : = ===---- --=
-- C = l i e e i.* =a o - - - - - - - -- O rd gk 2 **
C C. O E E '9 " C. CC, f. (*{ rj eq q c e-si Es qg .E
- i eM =*P ta e m= g Ce r. s, t. e. f. .- - ~ Qe Q= Q= eg == Q Q e m = c I i sa C' O*t Q ' O u9 . .=- -CS .M. -* -- e e .-
8 h
- - #4. .M - i. c Cd C .=. e.l 30 :C- = . - - .=. . -= .C. .e '.
=* M 12
> z- C. C. C EC E 8* ** 'i
- f* E a O. E E E O. O EEEC C C C p] g n e .e i2. e c=E m g e: C c - - i- O.
.a.n e -e et M .ce
.i.c,e. qer c =- e e e sC *2 r
,, g ., . - - . - - -
-e = ~ m s = es => - -= $ .. e=s w "e *J. "m cs es. .! *E C Cr. C.
- C. C. =. 0 C. =. 3 C. C C. C E.. = . =.=.0 =. =. C. O. C. C. =.
eeC n eo C e C = a * .. 3 = o C. C. C. e-
] N. a,
.&. .i. .. en. " .M.
M
- .C. =.- . . -
et M in
- t. cd CO- =- el = CO .d. .e 3=.=.= peC e in e.?
e h"
- e s .e 4-4
- .e 4 - c.1 l g C C C. C. C C C . 9EEC EC C e e= a .s eenC
.- = e c .= =. -ce-te. ce e. cd E ..= eEenE:=cE c=e .E 9en.E.=.CdE C C C C
-ne- . m n .c.s.
i-c -- . .-es .e. , e. m e e
". 0 - - - . - 5 .e Ce.s es 2. e '.
n 3 8 C = C C C = == coo C C = = c 3 = =c===c C = e u, .,
.4 =e..6,is
.m -n- 6 .n. .4e-- e d. n. e 6
- m. .e e .e. .a:s ce 64 = e-4. 4 6. 6eW.. .4 e ied.e 6W e .i.,.is .4 .4
'" "5 *
. - - . .i
.m.
f -c * ,g # 3g 3.[3h,a " C C C O Ce - O C
-'4' -m-'O- - - .4.se
.c 2 , on = F C- es O O
- O. c O
- e* *s x c: .*5.- -C ECC et
'9 D ';f
- .e. .e '"6 *c '= te e
- 5&G -
.e.s .ce .e .ic. - .e.k
.g c
.4.i
'V J' c >3 e 3 '- C = = e- .- -
_ y, g Q.. e = j cse e i .- e i e e- - i. - -
.e. .= e .m. 4. .e. ei sa :d 5 O e U O ,g g
2 n. .e.4
. .=. .. es -
e= 5 cd ,O,,,,o .$ 5 .di ,e -c,, ,G,, ,4
,c,,m, e ., *4w in a ,,,,
a.=. my 4M IC
.2 gn IE O J
< ur [ = = = = = *
*7g = Ci 0 " " " * * * ' " ~ " # ""# f f .-
- E 4 " ~ ~
' ' ' '~ " ~
3 g _5 y . .* .* .w .* u. vg 13 $ es =. =en en et et
=. ==es ee es et en xa g[
,5*- 0 i i i a i i e i e i i i i i i i i i 5 5 .;y -
U es:".:n $s= es=er .:",.m=. 3 es = es g et :q en O *e ** EC C E 2*. bU
.$ g .k x CI C @ to4 t.
- t. CCC E Et. O OI. Ot. O Et. E #
.> ~2 4 0 t. 8 6 I t. t. # * *J O#
p 44 4 4 CO gM l'I. t. 4. I . = to = c g ce m *re
- 444.s.
c. r.e. e. 2
. = 4s 4s 4e 4 4. e.a 5 5.
4 s
=* *
.c i*= N ,5,:, , :i e'
t. d44 sd
- - ?r
=
?,
=
=
fy -
< < < < < # < < << < < ? *Jo
'J. < < '/5 'b 'Is ? * < ne-
.c s- e e- -
e 2N < < *J 'f. V; &
>5 g.'-
s, E u
.5 vvvvu
= .= .= =evu 5 ==u= - =u =u =avvv u u E= = ="
m& b b '=
.4 L.a d' 6" ~0 "
g *= , u. g 2'.
.b b, . . I. . I. I d'.
. . . 0 k s
,A g" g g". g . .g'..y' aigh 5 w
*ic*2 ll*. 2*,. CO = :.a 6 6 6 6 6 6 6. 'w3 'w.s
' .J w 6 6 "w. 6 2. A M l=. O M
h, M h,
=
s,. Y F*O 0 a e O 8"z.
~ i i i i i i - e es een i i i i i 1 e i E
- O' *e 6
- i. Z i i t 4 i i = n i nm I l t i i
.C - i i i I es
. .o* .e
* =.
. c,
** f$ r$ m M
=.
.= g4 e-n*
** 9 e -
3
=
=.
.M.
f.- v. O C -0 0 *= 3 = m
= e. e.
9' C =
.c. ** *.
k P
.N # ~
$TTT T
*. rg ec.
= en.
p c.3 9 zE_Q 4 P"* * ,
** =r e ~4 4
,a '4
= ~ ~ -
.9 9 ~.^<. w ^< .".w
.=* :. e a /. /. /,. /. . ' /. ".O, ^=.t/. ^< w U "l* 7 , . . w-TS *
.** *I" ** .*" .f 3.Mi.1 SUPP. 3 - NC 4
I i 1 1
EXH1 BIT 2, 21 pages P (313-326.8) ; 6 CASE (continued)
% N-71 -7 casts onsuo non.auso enesscne vossa. cone (1644-7) l l t 4 I I l I i ) I i i l i i i t i i l i i l i l l I i 1
, o '
d 1y I I e i t 4 i l e i l n 6 a 1 1 i t i i i i l i i i ii1 i I
.o
- 3 b8 C. t-
$"I n e 89 *. b c. C. =. =. = 4 =. ri * - **
- -*Cm@ y =- q i.2 Mes r- s 9 e e eesm .oe*9.dc.
g ,g e4 e es
- a a = =. C C =9 -
, ,, .-=
. . w w
-. e e 8- = e e -ease es =e ee .e .== r*.m o
E $ C. ". 4 *@.9 9 c. =. S 8- $ ==
== -
---.8==..- . .. - . = .9
,3,, 3 e o -ece ; e e
= =. 5$$MO S =. = $ $ $ =.
1 '2 ca C'* C8* d* k,O o o 3
@ CC
- C =
..- .".8*
"* - C = "C ** =4 8*= C= 0 = 'e 'e = "E E
.=.-.".-i e8 "*
= *S*
ea g> .: e E in o em-M9e N *. e
- e
=.
e =. C. =. =. 4 i-4ea==
=.
e e C. =. 9 C # o eee e . = = c. c, = =. =, c, c. gr ., t es
- e cc -- e e e es- - = e. e e e e. e= e e cee.e= .4c.r.2 Q ik 33 e o
o e o q - e, e,
- c. o =. =, =.
- c. =. q =. =. = o ---
c =
= =-~~-
=.= e, ,- = =, c =.
g Ea .,E g* - e, ,-* e+ "= .et. $ o e 4 . e"
. . F-ee=. " "
= a=.w -
G "ee" i .= 9. 'd c= es" o **='c"4 .+ .e Ey i. -t c m =. = = e - =.
=. =. =. =
---~~---
p[ 3 e o e C .e- m os = .e e -e e= e= = =. = =. =ra=.eo =. = = = = = c.c.=.
- .e.n .e -- cc e -
e e s=. c. a. -=-e s-3 Ej E c o comeo o eo=c= e ee.e .u 5 e.3iee.4.c.e.- - - . . . .m a.-g',;, G, .a. M oi o dsu .4 ci a. ==c==oceoccooeco
- .e e e .c. .5 .g e ss 4- r4ee. e d. e '
.4 .i = .4eee C C
- - en r4 i. .e 8 8 4 -ei ss -e n4' d.c . '
- .r.4 E oC C C C =, C, tag =, c, Q e- n. e o
e d .e m. e, 8 o re e e, Q Q Q Q o Q Q C, = QQ=,QQo
.e e .a e e. =. . .e
= .=. ~ e m te =
- .s2 -
- e ~
-- e i. e
.O ci. O- E C =
e c. nneoe C. == C C. C :. E
- c. =. C. c. C.
c .d- .=. e--
= s. n. = .4 c. .a N **, ,'" e.
= et @ CC --C -e o e 4 .o i
eee8 a s. = 9 e e o o= oc o.-o io .e =. c.= = c C. dC et -n -
*. - =. .d- i . r ce reee@ i.@
* - n.* .=*Mn
-ea* ,a, e w - ==
=- = = = = . = - . = = .
c -
" o g 2.E c .F,a = *4r* =
es
- e" e" --d-*" " e= e 'e" 8es - =. 't
** =
= i . J*
- r1 e r*e i=. .q .8 @ e.ei_at .c.
- - e .=, *e*
0 .,. . -------
*q =
o..c e y c ~j e2 - i.eec
;; pty.F.a, e e . e :o = =. es ne = es e
- - - e= ; =
- 3. =, =t u
- u. - - -
- - ee= =n.e,s -e, ne e e= e. g- ,e .. o .a e e d ei - -
gi <t - --- hJ ] a . m
*0 .
4 E n e m 1l fM
=
- es e i i i i i i i i i i i i e i i l i ! i l g- el at et e n = es =t Gl ~~
< T ". m' ww
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< -e .e ei
* = e". =
n <, =< .e; 4 4e-- = - 4 Ci. . .--- Uvd2.
.= E -- - --
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ir a: '- aperi -e in io .e se es es ei ei ei ei + e. a so = <
,7
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w w n e se e
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- 3
< <<<<< mz<<<eoeeceeecoe
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a a u s as {3 -
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& a. = = .
J E .A t.2. AJ .2 A .2 A D'J a. 7J6AA 6 C = =
- 9 k= b= E E .2 y C C C C C C C C g t.
W6466666 5 M WV e
>0 I gf I I es es i I i i e
C 1 1 I i S. i i l i i 1 i i ! I I i t I i 5 sf I I no o 1 i l i i t i i l I I i i i i l I t i i l i 1 S S m e 2.I* g g o o : . m ^-e n m EE o- -o 6 * e o. e. = =. D
- t - e
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"$ [ -3 s
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- .n. .e.
1 1 es
- -= - ea - n= 1 i t = =
.n. i I
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- i ji C C # C 4 *e .e.
* ' ' ' ' " = 9 90 i
y i E.1 3c . . e" e-e.. .es "na- ..e. - c'o a
= = "e s "- e
= I I 8 e=
e , g ag oeo w q =, q z- oqg m. =. =. q =, =. =. c, o, o c, =. c. =, / p]. 3 t.=. - w, w M e -.veto.e* 8.e. M n.
.d
- e ira e is el e = ne s- =ee-=
C et .= te *a d & e =t. c.
- - - - .C - .=. - .O ------
la C=O S ee. G ., 2 o. l 6 :4 8.* C C 6
= C C = = =
s4 6 s' M "
-- .'.# Oif if is l'
=
6
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cc =. = = = c:. =. =. M = = =
$l*
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- 3 .e r o.
a: e= n
=. =. =c = = . = = . =. =.
.c0 --- - -----
e -
=n o e
.a e
egie- e: n. ee = =en: e = = i.
"5.
g oco C. = c.=.=.=
= =.
------- e- -
g. e o e J- e e e - .-.4 e.e
- se.-
M
= e
=.
.- e n
= =
e .e
= =o=====.
= .e e = e.
= =.=
ei = e e. es .= ce - s - e es .-d c=, .= 3 . f,
. - - - s "y ;3 --e
- 3 gi = -
m = 2 ee .; i e. A
- e. 4 = :: .-= ..., ye e ee e---,---e .=.
32 2 =E .e , ,.s e n - = = es e =i .e = e i- ..
--- - -- --- en e
.= .e r e.i 08' 5 '- G .
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o eg ** M M = - e4 * ?8 4 = M 4 i .
= .d.
e
=s.p3e . eea . .. i. = ..
u =o =8 2' * >* :C
-- - tj t si .f*
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