ML20135J146

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Application for Rev 13 to Certificate of Compliance 9073 for Model OH-142.Changes Alleviate Inconsistencies Between SAR & Controlling Drawings & Cover Minor Mfg Deviations.Revised Pages to SAR Encl.Fee Paid
ML20135J146
Person / Time
Site: 07109073
Issue date: 09/06/1985
From: Temus C
NUCLEAR PACKAGING, INC.
To: Macdonald C
NRC OFFICE OF NUCLEAR MATERIAL SAFETY & SAFEGUARDS (NMSS)
References
25780, QQ4523, NUDOCS 8509250314
Download: ML20135J146 (36)
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Text

{{#Wiki_filter:. ~ h b /D b,. i.a NtKLEMR(SO - ~65 SEP -9 sq NM$d5 September 6, 1985 File: WOfJO OH-142 Ref: 004523 Mr. Charles E. MacDonald, Chief Nuclear Regulatory Commission RETURN rTO 396-SS Transportation Certification Branch Washington D. C. 20555

Dear Mr. MacDonald:

l Enclosed please find eight copies of the revised pages to convert ~ i Revision 12 of the OH-142 Safety Analysis Report (Certificate of Compliance No. 9073) to Revision 13 of that report. A check in the amount of S150 is enclosed to cover the cost of a minor il amendment. I The changes made for this revision are minor. They have been made to alleviate a few minor inconsistencies between the Safety Analysis Report and the controlling drawings, as well as to cover very minor manufacturing deviations which are considered to have no structural significance. These minor inconsistencies have raised some concern with our customer, so we felt that it might be profitable to resolve these inconsistencies. Significantly, we believe that in reality no licensing issues are involved and that the changes in no way af fect the ability of the package to i meet the requirements of 10 CFR 71. This revision, including the revised drawings, has been copyrighted. This entire submittal contains proprietary information per the notice on the flyleaf of this report. We are aware of your requirements to place this submittal in the Public Documents Room. This may be done with our permission; however, j this permission should not be construed as a waiver of or in any way prejudicial to our lawful proprietary rights to this material. It is done only.to facilitate the issuance of a Certificate of Compliance. i Photontatic copies of this copyrighted material may be made by l NRC review personnel for convenience and for record purposes within the Commission's files; however, permission to copy the material is expressly denied to persons other than Commission personnel or for any other reason. Copies of the material may t not be released by the commission except to the Public Documents Room p-p# N' / lc Y ! N l M 73 D .mn, s a n i........ .........c raa G ava. a u. a. k........ am an...L. ice categor S.1/m j gz SEP1ap395y 2 ,,, x yea, M,y.a ,y 9, u w.: e x.x ne 'd,u C...' . J/ f.m d IiUCdU d C/. 4,C. .t h..

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~ p. [-~ / DOCKET NO. >67[ CONTE 0L NO. Ok/d[7[7 DATE OF DOC. MY/ !!#[ DATE RCVD. FCUF PDR FCAF LPDR WM ISE REF. SAFECUARDS VrfUR_ FCTC OTHER DESCRIPT10M: Av a L a m tn %a&- %nha-~ 17 v/Ak DH-/W AHk'i lim &uw ' /%P 'l>d//8/ff nuTut OSb '/'/

t W September 6, 1985 Mr. Charles E. MacDonald, Chief Nuclear Regulatory Commission Transportation Cortification Branch Page 2 Thank you very much for your help in this matter. Your timely review of this submittal is greatly appreciated. If you have any questions, please do not hesitate to call either myself or Stephen Goetsch. Very truly yours, NUCLEAR PACKAGING, INC. [f ~~_ Charles J, Temus Technical Director

Enclosure:

Eight Copies, OH-142 Revision 13 pages Check # 12883

NmPas CH-142 SAR Ray. 13, 9/85 Insert / Delete Instructions for Rev. 13, OH-142 SAR Delete Patos Insert Panes 0-4 0-4 0-6 0-6 0-7 0-7 1-2 1-2 1-8 1-8 1-11 1-11 1-12 1-12 1-76 1-76 1-108 1-108 Dwg. AL-20-202 2ev. I Shts. 1-3 Dwg. A1-20-202 Re v. L Sht s. 1-3 Dwg. Y-20-202D Rev. L Shts. 1-2 Dwg. Y-20-202D Rev. M Shts. 1-3

  • Dwg. Y-20-201D Rev. P Shts. 1-2 Dws. Y-20-201D Rev. Q Shts. 1-3 Dwg. AL-20-203 Rav. H Shts. 1-2 Dws. AL-20-203 Rev. J Sht s. 1-3 The drawing revision number was incorrectly stated on the last submittal of this drawing as revision M.

The correct drawing revision for this application is Revision Q. a I r -

NaPa2 OTI-142 SAR Rsv. 13, 9/85 The lower impact limiter in the Mark II version is retained in place by ratchet binde rs which are attached to the upper imprct limiters in 8 locations. This causes the lowe r and uppe r impact limiters to be pulled toward each other and against the ends of the cask effectively securing them in pl ace. This arrangement allows the removal of both the lowe r and uppe r impact limiter for top or bottom loading. The l ower impact limiter in the fark I version is fully welded to the cask outer shell and bottom. This version can only be top loaded. Material on the Mark II is A516 and uses.1 inch plate on the external skin vs. the 1-1/8in 4-26 used on the baseline package. In all other respects the R!a rk I and TI are identical with the baseline configuration. All Mk II casi welds are designed as full penetration and are made in accordance with weld procedures qualified to ASME, Section IX requirement s. This is verified on al l longitudinal welds via full radiographic inspection. All circumferential welds joining the inner and outer cask shells are made utilizing groove configurations, that assure full penetration. Integrity of these welds is verified via magnetic particle or liquid pene trant inspection. The various configurations are summarized in the figures given on the following three pages. l i l 0-4

V NsPaa OH-142'SAR i Rav. 13, 9/85 0.2.1.5 Peckaee Weleht .4 Gross weight for the package is approximately 64,000 lbs. This includes an estimated payload weight of 10,000 lbs. d 0.2.1.6 'Recentacles There are no internal or external structures supporting or protecting receptacles. 0.2.1.7 Drain Port The cask is provided with a NPT pipe plug and drain system. -It s use is for i removal of entrapped licluids, i.e., rain, decontamination fluids, etc. 0.2.1.9 Tiedowns i Tiedowns are a structural part of the package. From the attached general arrangement drawing it can be seen that four reinforced tiedown locations are provided. Refer to Section 1.4.4 for a detailed analysis of their structural integrity. 1 4 i '0-6

Iterne OE-142 SAR Rev. 13, 9/85 0.2.1.9 Liftina Devices Lif ting devices are a structural part of the package. From the general ~ arrangement drawing it can be seen that three reinforced lugs are provided in the Mark II configuration and two or three reinforced lugs are provided in the Mark I configuration. i 0.2.1.10 Pressure Relief Systes There are no pressure relief valves. i t 0.2.1.11 Eg.31,Dissination ' There are no special devices used for the transfer or dissipation of heat. j The package maximum design capacity is 400 watts. However, this value may be j exceeded if it can be demonstrated that actual equilibrium temperatures with the higher heat load are still within allowable limits. l l 0.2.1.12 Coolants j There are no coolants involved. 0.2.1.13 Protrusions There are no outer or inner protrusions except - the external ratchet bindsts described i n 0.2.1.2, above, and these are located within the envelope protected by the overpack. f ) i i 3 i e I 0-7

_. ~ _ -.. _.. j NmPas OH-142 SAR Rav. 13, 9/85-l substantiate their integrity. Liners are placed within the combined transportation shield and overpack. j The. shield top and bottom are constructed to two-three inch thick steel plates I I laminated toSether to provide a full 6 inches of solid steel. Cylindrical ,t side. wall s ~ have an external skin of 1-1/8 inch steel plate (1 in. when i i f 1 manufactured from A516 grade 70) and an. internal skin of 1/2 inch thict plate. 1 These two plates encase 3-1.2 inches of lead resulting in a total side wa l l thickness of 5-1/8 inches. I i An overpack or impact limiter provides localized protection to those critical [ areas of the assembly, one of which is the primary lid to body interf ace or j seal. This area must receive minimum deformation during impact, as well as 0 not exceed a maximum temperature of 500 F. Due to the design of the seal i area, direct compression, or crushing of the seal is not possible. From the drawing it can be seen'that the seal is recessed below the 1-1/3 inch thick [ j plate. Use of a thick silicone seal will allow the joint to open more than l 1/2 inch before sealing is lost. I L i M We i ght s and Cente r p.,[ Grav i ty i i I The weight of the overpack, cask and liner (or payload) will not exceed l 64,000 pounds. ne overpack and cask weight is approximately 54,000 pounds. The center of gravity for the assembled 1 i l I i r L i l I t i j i I l h i 1-2 l -f [ L i

NmPas OH-142 SAR - Rav. 13, 9/85 1.4 General Standards for all Packanes This section demonstrates that the general standards for all packages are met. 1.4.1 Chemical and Galvanic Reactions The materials from which the packaging is fabricated (steel, lead, and polyurethane foam) alon5 with the contents of the package (disposable steel containers) will not cause significant chemical, galvanic, or other reaction in air, nitrogen or water atmosphere. 1.4.2 Positive Closure The positive closure system has been previously de scribed in Section 0.2.1. In addition, each packa5e will be sealed with an approved tamper indicating seal and suitable locks to prevent inadvertent and undetected opening. 1.4.3 Lifting Devices Two or three lifting locations are provided for the Mark I and three for the Ma rk II. Both have identical t us s. Total load for two lugs is: P = ( Pk g if t) (3g's)/No. of Lugs P = (6400 lbs) (3 's)/(2) = 96,000 lb/ lug 5 1-8 t

NmPaa 09-142 SAR R:v. 13, 9/85 The capacity of each lug can be determined from the following: 1 \\ ~ / l'/t wxx parx y ~ za b l d /,q P \\ - 3"4 Pz 7 I 1 g % / 7 3 Using the standard 40 shearout equatlon: P = F,,2 t (E.M.-d/2cos40) = (35,000 psi) (2) (1-1/2) [2-(.766)) ~ = 129.570 lbs. Margin of Safety is:

~

MS = 129,570/96,000-1 MS = +. 3 5 The capacity of the lug to cask interface can be calculated as follows: f Lun weld Area (fillet only) Weld Area A = (6) (2) (.0.5 in.) (sin 45") t A

  • 4.24 in P=F A ty

= (36,000) (4.24) = 152,740 lbs/lus M.S. = 152,740/96,000-1 4 = + 0.60 (for 2 lug configuration) i 1-11 t

MmPas 0E-142 SAR Rev. 13, 9/85 Therefore, it can be concluded that the lifting points are more than capable of reacting a load equal to three times the package weight. Should the lugs experience a load greater than 129,570 pounds, they will shear out l oc a l ly. His will have no detrimental effects on the package's ability to meet other requirements of the subpart. The lugs will be covered during transport. Magt 1 Overnack Liftina Lugt Since the Mark I configuration has a removable overpack separate lifting lugs are provided. These will be covered during transit. } i \\ ed / Vz. W e I /d Sfd RArd / a 1-12 i

18mPas 0H-142 SAR R2v. 13, 9/85 The lug capability in net area is: P=F A t tu Where: F = 110,000 psi (ASTM A 517) tu A = (3.75 - 1.625)(1.5) = 3.19 g 2 P = (115,000 psi)(3.19 in g P = 366,850 lbs. (Net Area) yton% g 34 / Lug to lid attachment 4 \\ 3 fmk[ 4 i P Weld Shearing (counting' bevel weld only) P, 'F A weld Whe re : 'F, = 35000 psi A = (1.50 in)(3.0 in) = 4.$.in2 2 P =,(35000 psi) (4.5 in ) P = 157,500 lbs. 1-76 (

s Nurae OR-142 SAR Rav. 13, 9/85 I l the. foam is repl aced by an equiv a l ent air gap a t 400,F. Gases generated from i decomposition of the foam (temperature 600,F) are vented through at least four (two in each everpack) 1-1/2 inch diameter ho l es in the externa l skin. These vents are c l osed with a standard AB S p l astic pipe pl ug that nel ts wel l before of f gasing starts. The cylindrica l sheet of the shie l d is therma l l y protected from fire by a 3/16 t inch nominal thickness of A l bi-C l ad 39 Intumescent paint which exhibits a 4.1 1 expansion upon exposure to fire (a t 300 F). A comprehensive discussion of the g experimental demonstration of this coa ting's therma l performance is summarized l in Union Carbide Report No. K-1661, ' Fissile Ma teria l Container and Packaging I D e v e l opme n t and Testing Program', April 1, 1966. The experimental therma l response of the container discussed in this re ference c omp a re s c l ose l y with tha t predic ted by the O H-142 shie l d therma l ana l ysis. j Sol ution of the t ransien t ( fire) case is achie ved by a conv entio na l the rm a t. analyzer program, 171AN, based on the well known Lockheed Thermal Analyzer. t i 1 4 i 4 i i ) J 1-108 ___m..__ .,,,m., ,..,,,,._7 _g.,,., .r. .e. ..m_. .y-

_ NOTES: UNLESS OTHERWISE SPECIFIED i 1. PATERIAL: LOW CARBON HOT ROLLED ETEEL:

PLATE & SHAPES CONFORM TO ASTM-ASIS, GR70

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SHEETS CONFORM TO ASTM - A415. A569. A570. A36. OR 304 SST PER ASTM - A240 WHERE NOTED.

r- ' ' D 2. PATERIAL : ASTM-A514 oR A517 .C. i .m l .r : 3. FOAM: 1,000 PSI CRUSH STRENGTH RIGID POLYURETHANE. PER NUPAC FOAM C'.' g SPECIFICATION NPI-F6. REVISED FO AM PROPERTIES ALLOWED Ah", FOR 16 INCH DI AMETER CENTR AL LID OPTION. Y'

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4 4. LEAD: PER FEERAL SPECIFICATION GQ-L-171E, GRADE A OR C. h Ol 5. REMOVD

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"5-6. REFERENCE DATA: CASK WT: 54,000Las. PAY LOAD: 10,000Las. GROSS WT: 64,000Las. 7. REMOVED ocTAtt-K 8. ALL WELDING PROCEURES AND PERSONNEL SHALL BE QUALIFIED IN ACCORDANCE WITH ASME CODE, SECTION IX. l C 9. ALL WELDS SHALL BE INSPECID VIA NDT METHODS AS FOLLOWS: LIFTING LUG AND CIRCLFERDTIAL CONTINUQUS TOD VIED SHOWING OPTIONAL WELDS: PAGNETIC PARTICZ PER AS".E CODE SECTION III, DIVISION I, SGSECTION NB, ARTICE NB-FC00 AND SECTION V, ARTICS 7. L!OUID PENETRANT NOT SHALL BE SUBSTITUTED FOR MAGNETIC PARTICLE ON STAINLESS STEEL WELDS. LONGITOINAL SHELL WELD: RADIOGRAPHIC PER AS"E CODE SECTION III, DIVISION I, SUBSECTION NB, ARTICLE NB-5000 AND SECTION V, ARTICG 2, OR UITR ASONIC PER ASME CODE. SECTION 131. DIVISION 1. SUBSECTION N8* ~ DETAIL.$} [DEWL ARTICLE NS-5000. PAR A NB 5330.

10. AS A5 OPTION,12 GA. NO. 304 STAINLESS STEEL CL5DDING MAY BE INSTALLED ON THE INTERIOR & EXTERIOR SURFACES OF THE FLASK BODY & INTERIOR SURFACES OF k,

THE UPPER LID, a SEAL WELDED ALONG ALL EDGES & SEAMS. [ GSf s a -e- \\ s 'L - t I IW' hl6 -

11. PAINT ALL EXPOS 8 CARBON S* EEL SURFACES WITH ONE CDAT CARER 0 ZINC II 1 ONE CDAT PHD0LINE 305, OR ONE PRIMER COAT (3-5 MILS).

l MOBIL CFEM EP0XY NO. 89 a ONE FINISH COAT (3-5 MILS) MOBIL CHEM E? OXY NO.89..

12. COAT ALL EXPOS 8 EXTERIOR SURFACES OF FLASK BETWEEN UPPER AND LOWER OVERPACKS WITH ONE (1) COAT (MIN 3/16 THK) "ALBI-CLAD" NO. 89. AS AN PARTIAL SECT A. A SHOWING OPTION OPTION, A 10 GA. NO. 304 STAINLESS STEEL THEPIAL SHIELD MAY BE INSTAf ' A BETWEEN THE OVERFACKS.
13. FLASKS FABRICATED PRIOR TO 3/84 PAY BE MADE USING ASTM-A36 MATERIAL. '

(FLASK BODY O'JTER SHELL SHALL BE 11/8 IN. THICL WITH FULL PENETRATION DOUBE SIDED V GROOVE WELD FOR VERTICAL SEAM.) NOMINAL AIR GAP (MINIMUM.05, MAXIMUM.42 Irt) 15, eAcuar mau. se===eo a ce<rvuo a AcConouct werw ne neousummers or to cm 7tassa l(s. ennaurr a secoNOurf UDS & ORApf SHAu. BE EcurPED wrrH Tats"ER socAroso OeMCES = ACCORD eCE wrrH to Cm 7t.4am] It JOINTS & SEAMS SHOWN ARE PREFERRED CONFIGURATION. DUE TO VARYING FABRICATOR CAPABILITIES SPECIFIC JOINT / SEAM CONFIGURATION SHALL BE CONTROLLED ONLY TO THE EXTENT THNT IT AGREES DIMENSIONALLY WITH THE DESIGN & THAT MATERIALS SHALL BE AS SPECIFIED. e i y I a i s

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NOTES: UNLESS OTHERWISE SPECIFIED i 1. MATERIAL: LOW CARBON HOT ROLLED STEEL: ~

PLATE & SHAPES CONFORM TO ASTM-ASIS, GR70
SHEETS CONFORM TO ASTM - A415. A569. A570. A36. OR 304 SST PER ASTM - A240 WHERE NOTED.

D h MATERIAL : ASTM-A51tl CA A517 FOAM: 1,000 PSI CRUSH STRENGTH RIGID POLYURETHANE. PER NUPAC FDAM i SPECIFICATION NPI-F5. I hLEAD: PG FEERAL SPECIFICATION QQ-L-17tE. GRADE A OR C. 5. RE?'0VD PRE 8ERENCEDATA: CASK WT: 54,000Las. PAY LOAD: 10,000L3s. GROSS WT: 64,000Las. 7. RE"0VED %sTM-cu "am:::.' 70. ATTRtha.s CONF 06?MS 7 A i C 9. ALL WEDING PROCDURES AND PSSONNEL SHALL SE QUALIFID IN ACCORIAtlCE WITH AS?.E CODE, S~CTION IX. lQ ALL WE!.DS SHALL 3E INSPECTC VIA NDT METHODS AS FOLLOWS: LIFTING LUG Atc CIRCTFE?IITIAL CONTINU0US WEDS: MAGNETIC PARTICG PER A2E CCDC SECTION III, DIVISION I, SUBSECTION NE, ARTICM NE-ICOO AND SECTION V,' ARTICG 7. LlQUID PENETRANT NOT SHALL BE SUBSTITUTED FOR MAGNETIC PARTICLE ON STAINLESS STEEL WELDS. LONGITUDINAL SHELL WED: RADIOGRAPHIC PG ASPE CODE SECTION III, DIVISION I, SU3SECTION NE, ARTICLE NE-5000 At:D SECTION V, ARTICG Z. OR UlTR ASONIC PER ASME CCCE. SECTION lit. OlVISION 1. SUBSECTICN NB. ARTICLE N8-5000. PAR A N8 5330. I 1. AS AN OPTION,12 GA. NO.104 STAINGIS STEEL CL DDING MAY BE INSTALLD ON THE INTERIOR & EXTERIOR SURFACES OF THE FLASK BODY a INTERIOR SURFACES OF THE UPPG LID, & SEAL WELSD ALONG ALL EDGES & SEAMS. ~l'2. PAINT ALL EXPOSD CAR 20N sic.:. SUP5 ACES WITH ONE CDAT CARER 0 ZINC II g & ONE CDAT PHENGLINE 305, OR ONE PRIMER CCAT (3-5 MILS) MOBIL CHS E? OXY NO. 89 s ONE FINISH CDAT (3-5 MILS) MOBIL CHD E30XY NO.89.. COAT ALL EXPOSD EXTERIOR SURFACES OF FLASK BETWEEN UPPER AtlD LOWER OVERPACKS WITH ONE (1) CDAT (MIN 3/16 THK) "ALBI-CLAD

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PLATE a SHAPES CONFORM TO ASTM-A516, GR70
SHEETS CONFORM TO ASTM - A415. A569. A570. A36. OR 304 SST PER ASTM - A240 WHERE NOTED.

D % MATERIAL :ASTM-A5184 oR A517 FOAM: 1,000 PSI CRUSH STRENGTH RIGID POLYURETHANE. PER NUPAC FDAM SPECIFICATION NPI-F6. % LEAD: PER FEERAL SPECIFICATION 00-L-171E. GRADE A OR C. I 5. REMOVD REFERENCE DATA: CASK WT: 54,000as. PAY LDAD: 10,000as. GROSS NT: 64,0000s. 7. REMOVD 8. ALL WELDING PROCCUTIS AND PERSONNEL SHALL EE CUALIFIED IN ACCORDANCE WITH AS".E CODE, SECTION IX. C 9. ALL WEO S SHALL EE INSPE.i u VIA NDT METH0 S AS FOLLOWS: LIFING LUG A?Q CIRCU"PEFSTIAL CONTINUUUS WELDS: MAGNETIC PARTICLE PER ACME CCEE SE TION III, DIVISION I, SUBSE7 ION NE, ARTICLE NE-5C00 AND SECTION V, ARTICLE 7. LICUID PENETR ANT NDT SH ALL BE SUBSTITUTED FOR MAGNETIC PARTICLE ON STAINLESS STEEL WELDS. LONGITCINAL SHELL WELD: RADIOGRAPHIC PER ASME CODE SECTION III, DIVISION I, SUBSECTION NE, ARTICLE NE-5000 AND SECTION V, ARTICLE ', OR UCR ASONIC d PER ASME CODE. SECTION lll. DIVISION 1. SUBSECTION NB. ARTICLE NB-5000. P AR A NB $330.

10. AS AN OPTION,12 GA. NO. 304 STAINLESS STEEL CL DDING MAY BE INSTALLED ON THE INTERIOR EXTERIOR SURFACES OF THE FLASK BODY INTERIOR SURFACES OF THE UPPER LID, a SEAL WELD D ALONG ALL EDGES s SEAMS.
11. PAINT ALL EXPOS S CAR 30N STEEL SUFIACES WITH ONE CDAT CARER 0 ZINC 11 s ONE CDAT PHENGLINE 305, OR ONE PRIMER COAT (3-5 MILS)

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PLATE a SHAPES CONFORM TO ASTM-A516, GR70
SEETS CONFORM TO ASTM - A415. A569. A570. A36. OR 304 SST PER ASTM - A240 WHERE NOTED.

2. PATERIAL : ASTM-A514 on A517 D l'3. FOAM: 1,000 PSI CRUSH STRENGTH RIGID POLYURETHANE. PER NUPAC FDAM SPECIFICATION NPI-F6._ 4. LEAD: PER FEERAL SPECIFICATION CQ-L-17tE. GRADE A OR C. 5. REMOVD 6. REFERENCE DATA: CASK WT: 54,000as. PAY LOAD: 10,000as. EROSS WT: 64,0000s. 7. REPOVD 8. ALL WELDING PROCELRES AND PERSONNEL SHALL EE CUALIFIED IN ACCORDANCE e WITH ASME CODE, SECTION IX. C 9. W. WE.DS SHALL EE INSPECTC VIA NDT METHC:S AS FOLLOWS: JFTING LUG AND CIRCUPEE:ENTIAL CONTINUGUS ELDS: PAGETIC PARTICLE PER AS"E CODE SECTION III, DIVISION I, SUESECTION NE, ARTICLE NE-EC00 AND SECTION V, ARTICLE 7. L!OUID PENETR ANT NOT SHALL BE SUBSTITUTED FOR MAGNETIC PARTICLE ON STAINLESS STEEL WELDS. LONGITUDINAL SELL WELD: RADIOGRAPHIC PER AS"E CODE SECTION III, DIVISION I, SUESE TION NE, ARTICLE NE-5000 AND SECTION V, ARTICLE 2, OR UD'R ASONIC PER ASME CODE. SECTION lit. OlVISION 1. SUBSECTION NB. ARTICLE NB-5000, PAR A NB 5330.

10. AS AN CDTION,12 GA. NO. 304 STAINLESS STEEL CLdDDING MAY BE INSTALLED ON THE INTERIOR & EXTERIOR SURFACES OF THE FLASK BCDY a INTERIOR SURFACES OF THE UPPER LID, a SEAL WELDED ALONG ALL EDGES & SEAMS.
11. PAINT ALL EXPOSS CARZON STEEL SUPJACES WITH ONE COAT CARER 0 ZINC II

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