ML20198D819
| ML20198D819 | |
| Person / Time | |
|---|---|
| Site: | 07105450 |
| Issue date: | 04/28/1986 |
| From: | WESTINGHOUSE ELECTRIC COMPANY, DIV OF CBS CORP. |
| To: | |
| Shared Package | |
| ML20198D804 | List: |
| References | |
| NUDOCS 8605270070 | |
| Download: ML20198D819 (116) | |
Text
I O
ATDGMENT NO. 2 'IO IEITER DATED 4/28/86 Instructions for Replacement of Drawings in Attmeknant 12 Old Drawirn Mahar Replace with New Drawirn Maher SKC-86C11, Sub 1 SKD-86007, Sub 2 SKD-86008, Sheet 1 SKD-86008, Sheet 2 l
1 SKD-86008, Sheet 3 SKD-86009 SKD-86010 SKD-86011 SKE-85002, Sub 1 SKD-86012 SKE-85003, Sub 1 SE-85002, Sub 2 SKE-85004, Sheet 1, Sub i SKE-85003, Sub 2 SKE-85004, Sheet 2, Sub 1 SKE-85004, Sheet 1, Sub 2 SKE-85004, Sheet 2, Sub 2 SKE-86003, Sheet 2 SKE-86004, Sub 2 i O
- These are new drawings not included in original transmittal.
l l
O 8605270070 860428 PDR ADOCK 07105450 B
3 O
Westinghouse Electric Corporation Nuclear Energy Systems f
Application for Renewal of the Certificate of Compiiance for the RCC Shipping Containers Package Identification Number USA /5450/AF l
December 20, 1985 O
April 28,1986 (Revision 1)
U. S. Nuclear Regulatory Commission Docket 71-5450 e
l O
TABLE OF CONTENTS O
SECTION PAGE TABLE OF CONTENTS i
REVISION RECORD lii
1.1 INTRODUCTION
1 1.2 PACKAGE DESCRIPTION 1
1.2.1 Packaging 1
1.2.2 Operational Features 3
1.2.3 Contents of Packaging 3
2.0 STRUCTURAL EVALUATION 5
2.1 STRUCTURAL DESIGN 5
2.1.1 Discussion 5
2.1.2 Design Criteria 6
2.2 WElGNTS AND CENTERS OF GRAVITY 7
2.3 MECNANICAL PROPERTIES OF MATERIALS 7
2.4 GENERAL STANDARDS FOR ALL PACKAGES 7
O 2.4.1 Chemical and Galvanic Reactions 7
2.4.2 Positive Closure 7
2.4.3 Lifting Devices 8
2.4.4 Tiedown Deices 8
2.5 STANDARD FOR TYPE B AND LARGE QUANTITY PACKAGING 8
2.5.1 Load Resistance 8
2.5.2 External Pressure 8
2.6 NORMAL CONDITIONS OF TRANSPORT 9
2.7 NYPOTNETICAL ACCIDENT CONDITIONS 10 2.7.1 RCC Container 10 2.7.2 RCC-1 Container 11 2.7.3 RCC-2 Container 11 2.7.4 RCC-3 Container 11 2.7.5 RCC-4 Container 11
3.0 CRITICALITY EVALUATION
16 3.1 FISSILE CLASS 1 LIMITS 17 4.0 PROCEDURAL CONTROLS 17 4.1 OPERATING PROCEDURES 18 ACCEPTANCE TESTS 18 O
4.2 4.3 MAINTENANCE PROCEDURES 18 Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.i Revision Submittal Date:
4/28/86 Rev. No.]((
REVISION RECORD REVISION DATE OF PAGES NUMBER REVISION REVISED REVISION REASON 1
4/28/86 i,Ii Revised Table of Contents 1
4/28/86 4,10,11,16 Correction of typographical errors 1
4/28/86 4
Revised reference to drawing 1
4/28/86 9,10 Revised analysis for normal conditions of transport to reflect requirements of 10CFR71.71 1
4/28/86 17,18,19 Revised Section 4.0, Procedural Controls 1
4/28/86,
Changed references O
All Pages to drawings 1
4/28/86 2 Added drawings 1
4/28/86 18-4 & 18-5 Corrected errors 8 in Table.
1 4/28/86 19-1.to.19-8 Revised nuclear 19-32 criticality safety Added pages analysis to incor-19-42.1 thru porate additional 19-42.9 calculations to 9 support finite array accident analysis.
1 4/28/86 2, Added procedures for All Pages operation and maintenance 1
4/28/86 3, Added procedures for All Pages Quality Control Inspection O
Docket No. 71-5450 Initial Submittal Date: 12/20/85 PageNo.1 Revision Submittal Date: 4/28/86 Rev. No._1_
9 Neutron Absorbers, etc. - Neutron absorber O
plates; (1) consisting of 0.19" thick, boronated stainless steel containing 1.3 w/o natural boron, or (2) consisting of 0.19" thick, oxygen-free, high conductivity (0FHC) copper, or (3) consisting of carbon steel 0.035 inches in thickness, with 4 mils of Gd 0 23 2
(0.02gm - Gd 0 /cm ) affixed to each side 23 of the plate will be mounted in the packaging, i
when required. As shown in Westinghouse drawing SME85003 and SKE85004, these plates are restrained by the massive vertical structure separating the fuel assemblies, by a heavy end plate at one end, and by a clamp plate secured by two 1/2 inch bolts at the other. The installation is such that the presence of the neutron absorber plates may be readily detected by visual examination.
Specific data on O
assembly parameters which require the use of neutron absorber plates is included in Appendix 18 to this application.
Specific information concerning the Gd 0 neutron absorber 23 plates is presented in Attachments 20 and 21 to this license application.
Maximum Weight of Fissile Content - Listed in Appendix 18 Maximum Net Weight of Contents - Listed in Appendix 10 Maximum Decay Heat - Not applicable 1:2.3.2 RCC-1 CONTAINER - CONTENTS DESCRIPTION The description and discussions given in Section 1.2.3.1 will be directly applicable in all respects.
O Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No. 4 Revision Submittal Date: 4/28/86 Rev. No.J_
i NORMAL CON 0lT10NS OF TRANSPORT
)
O 2.6 Normal conditions of transport - The RCC fresh fuel shipping containers have been evaluated with respect to those conditions outIined in 10CFR71.
Each of the normal conditions outIined in 10CFR71.71 and their effect on the RCC containers is outlined below:
1.
Heat - The specified temperature and insulation conditions wiII have no adverse offact on the container since it is composed of structural steel. The shock mount system is designed to be effective up to 160 degrees F.
2.
Cold - As the shock mount system is designed for temperatures as low as minus 40 degrees F the specifled condition of cold will have no effect on the RCC coretainers.
3.
Pressure - The reduced external pressure of 3.5 psi or O
increased external pressure of 20 psi pressure will not cause any harmful stress state within the package.
4.
Vibration - Due to the nature of the design and construction of the RCC containers, any vibrations observed during transport will have no adverse effect on the package.
5.
Water Spray - Since the RCC containers are sealed from the environment, the water spray conditions described will have no effect on the RCC shipping container.
6.
Free Drop - As the RCC-containers weigh less than 10,000 pounds loaded, it must withstand a free drop of 3 feet.
From Attachment 1, a similar container withstood a 30-foot drop without opening or reducing the spacing between fuel assemblies.
It can, therefore be concluded that a drop of 3 feet will not damage the container i
sufficiently to reduce the spacing between fuel assemblies.
s O
Docket No. 71-5450 Initial Submittal Date: 12/20/8_5 Page No._9_
Revision Submittal Date:
4/28/86 Rev. No._1_
7.
Corner Drop - Not applicable to RCC containers.
8.
Penetration - For the conditions specified, the O-projectile does not possess sufficient energy to penetrate or deform the shell of the RCC shipping containers. Therefore, the effect of this incident is negligible.
9.
Compression - Not applicable to RCC containers.
2.7 HYPOTHETICAL ACCIDENT CONDITIONS 2.7.1 RCC Container The accident conditions specified in Part 71 will not credibly produce an arrangement more reactive than that analyzed under General Criticality Standards. The clearance between the massive vertical member of the Internal components and the shell of the container will be such that a fuel assembly wl!l not pass.
Any O
crushing due to the Accident Free Drop would only decrease the clearance.
It is not credible that the effectiveness of the neutron absorber material, when used, wIlI be appreciably reduced as the result of the Accident Free Drop, due to its location within the massive vertical member. The necesalty for evaluating the Accident Puncture and Water immersion conditions is obviated by the assumption of maximum moderation and fulI reflectlon. The necessity for evaluating an Accident Thermal condition is obviated by the limitation of the contents to clad fuel assemblies.
O Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.10 Revision Submittal Date: 4/28/86 Rev. No.1
2.7.2 RCC-1 Container O
The discussions presented in Section 2.7.1 are directly l
applicable in all respects to the RCC-1 container.
2.7.3 RCC-2 Container The discussion presented in Section 2.7.1 is directly applicable in all respects to the RCC-2 container.
2.7.4 RCC-3 Container The discussion presented in Section 2.7.1 is directly applicable in all respects to the RCC-3 container.
2.7.5 RCC-4 Container The accident conditions specified in 10CFR71 wilI not credibly produce an arrangement more reactive than that analyzed under General Criticality Standards for the following reasons:
The deformation of the container shell subsequent to the 30-foot drop for a similar type of container has been quantified by a series of tests, the results of which are documented in Attachment 1.
Due to the nature of the container shell design, the maximum shell deformat 9n occurs when the container is dropped onto its lid. TI:is drop configuration resulted in the container lid sustaining a three-inch depression along its entire length. The container shell fasteners remained intact and the container shell remained closed for the entire test sequence of 30-foot drops, including both flat and angular drops. The number of container shell closure fasteners has been increased in the RCC-4 container design to provide the same number, size, and i
Docket No. 71-5450 Initial Submittal Date: 12/20/85 Page No.11 Revision Submittal Date: 4/28/86 Rev. No.1
3.0 CRITICALITY EVALUATION
General Criticality Standards - The contents of each package will be so limited that, for a single container, with the contents maximumly moderated and fully reflected, the K,,, of the contents will obviously be less than the 0.95 on a best estimate basis with minimal additional uncertainties for the maximum credible accident (MCA) and also that k,,, is less than or equal to 0.98 for " optimum moderation" conditions on a best estimate basis with minimal additional uncertainties for the MCA. No consideration of dispersable material is required because the contents will be limited to clad components. See specific data in Appendix 18.
The calculations were made by the Nuclear Engineering Department using AMPX (1) modules NITAWL and EXSDRNPM along with Monte Carlo Code KENO-IV (2). The requiremeat that fuel be in assemblies in a fixed array assures that these calculations are accurate and directly applicable. The calculations include the effects of the neutron absorbing plates, when used. The criticality analyses are presented in 4 9.
Package Array Evaluation - Any number of undamaged, unmoderated RCC packages will be nuclearly safe, since uranium enriched to l
5 w/o or less in U235 is nuclearly safe in any quantity under any conditions. Any number of undamaged but flooded packages l
will also have a k,,, of 0.95 and there will'be a minimum of 12 inches of water between the contents of any two packages.
If the water drains away, the contents will also drain, so that I
the array returns to an unmoderated condition.
/1 N. M. Greene, et al, "AMPX: A Modular Code System for Generating Coupled Multigroup Neutron-Gamma Libraries from ENDF/B, "0RNL/TM-3706 (March 1976).
/2 L. M. Petrie and N. F. Cross, " KEN 0 IV - An improved Monte Carlo Criticality Program," ORNL-4938 (November 1975).
Docket No. 71-5450 initial Submittal Date:
12/20/85 Page No._1_6_
6 Revision Submittal Date: 4/28/86 Rev. No._1__
The maximum credible accident condition is conceived to involve O
only two packages, crushed top-to-top so that the spacing between the pairs of assemblies will be 4.0 inches, and aligned parallel to each other. This array is then assumed to be flooded. The heavy structural members of the base and the internal component support structures of the package will provide sufficient spacing so that any other package in the shipment will be isolated from this combination by a minimum of 12 inches of water.
1 Since only two packages will combine to form the MCA array with a k,,, less than or equal to 0.95 and any additional packages can only form similar isolated arrays, any number of the RCC package will be nuclearly safe under hypothetical accident conditions. An infinite array of packages can be combined under the MCA conditions with a k,ff less than or equal to I
0.98 wIth " optimum moderation".
O 3.1 FISSILE CLASS I LIMITS 1
The nuclear criticality safety evaluation demonstrates that any number of packages will be safe under both normal conditions and the hypothetical accident conditions with optimum moderation.
4.0 PROCEDURAL CONTROLS The user of this package, whether under a specific license or a general licnese, shall have in place a QA program approved by the USNRC under the provisions of Subpart H of 10CFR71 for use of this package. This program shall cover the following sections for operating procedures, acceptance testing and maintenance procedures. Current operating, maintenance and inspection procedures are provided in Attachments 22 and 23.
O These are provided to establish the information which must be l
incorporated into the detailed procedures which would have to be established under the users QA program.
Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.17_
7 Revision Submittal Date:
4/28/86 Rev. No.
4.1 OPERATING PROCEDURES Procedures for loading and unloading the fuel from the shipping l
container are provided in Attachment 22.
The QC inspection procedures are provided in Attachment 23. Since the material being shipped in these packages is clad low-enriched uranium, special provisions for contamination control are not required.
Normal health physics surveys of the interior and exterior surfaces of the packages shall be taken to assure compliance with U.S. D0T regulations for contamination limits prior to shipment of either full or empty packages.
4.2 ACCEPTANCE TESTS Visual inspections shall be performed on all model RCC containers to verify all welds and component dimensions, as identified by the drawings in Section 1.2, prior to the first use. Prior to each additional use (After routine maintenance),
O each container is reinspected in accordance with procedures outlined in Attachments 22 and 23.
The structural integrity of each container is then maintained upon completion of each visual inspection prior to loading.
Pressure and leak tests are not applicable to the testing of the RCC containers. The containers are not subjected to internal pressure since only unirradiated clad fuel is shipped.
1 Component testing (clamping, frame, closure devices) are accomplished prior to each shipment in accordance with 4
procedure's described in Attachments 22 and 23.
Testing of valves, rupture discs, and fluid transport devices are not j
applicable since these devices are not used in the RCC container design. Testing of the gasketed surfaces is not required since they are non-safety related and are only intended to maintain product quality.
Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.18 Revision Submittal Date: 4/28/86 Rev. No. 1
Tests for shielding integrity are not necessary since no shielding is incorporated into the RCC container design. There are no thermal acceptance tests required since there is no heat generating materials authorized for shipment.
4.3 MAINTENANCE PROCEDURES Maintenance procedures and QC inspection procedures are provided in Attachments 22 and 23 respectively.
These requirements are minimal due to the simplicity of the design and the nature of the material authorized for shipment. There are no structural and pressure tests, leak tests, subsystem maintenance, valves, rupture disks, gaskets on containment vessel, shielding, or thermal performance tests which are required to assure the safety of the package.
The maintenance program required prior to each use is necessary to assure proper placement of the internal components suitable for the fuel design to be shipped.
O O
Docket No. 71-5450 initial Submittal Date:
12/20/85 Page No.19 Revision Submittal Date:
4/28/86 Rev. No. 1
O ATTACHMENT 8 RCC-4 SHIPP1NG CONTAINER TOP AND B0TTOM SUPPORT ANALYSES 1 O i
O Docket No. 71-5450 Initiai Subelttal Date:
12/20/85 Page No. 8-1 i
Revision Submittal Date:
4/28/86 Rev. No.l
i l
t ATTACHMENT 8 RCC4 Shipping Container top and bottom support analyses 1
s l
l t
i l
l l
Hinge Plates Design Criterion Neither the top closure assembly hinge plates not the welds that secure them shall yield in the 6g minus x-direction acceleration.
Verification The loading and the shear area on the hinge plates are as shown.
Corner Assembly J'4 SKD-86008, it 20 O
1/8 inch weld f
9l O
Hinge Plate. -
P = 2732 lb
~~
/
s p
Corner Assembly Loads and Securing Welds l
The load P is one eighth of the total 6g inertial load 2
and the shear area in each hinge plate is 0.585 in The shear stress is thus:
2 t=
2 = 4.670 lb/in 5 n Each plate is welded in place with four 1.31 inch lengths of 1/8 inch filet. Weld stress is
)
t
= 5 M 4/in
- 4(1 3
(. 25/ J2)
Conclude that neither the top closure assembly hinge plates, nor the welds that secure them, yield in the 6g minus x-direction acceleration.
Re. Sion 1
O Top closure hinge pins
Purpose:
To detennine the shearing stress in top closure pins Assumptions: 6g loading 6(1720 lb) = 10320 lb P
v l
t
~
Pin A Pin B
]
/ sheared area of pin
= 10320
= 5160 _
= 5160 2
(.5)'(2)
'39
/
4 2
(2) 4 2
Shear A = Shear B = 13230.77 lb/in 2
Allowable shear for 1010-1020 carbon steel = 14500.00 lb/in
==
Conclusion:==
Allowable shear > maximum actual shear O
e
,~-- _ -.... -. -,, -,
--.,_-..n,
O Corner Post Design Criterion The bolts securing the top closure post to the top cross frame base tube shall not yield in a 6g minus x-direction acceleration.
Discussion The top closure post, SKD-86008 or SKD-86009, items 1 or 2 carries loads shown in the minus 6g acceleration case.
Reaction R is imposed on one of the securing bolts.
2 Loads F and F vary for the XLR and 414 loadings per the j
2 tabulation. The maximum bolt load R is imposed in the 414 2
case and is 13,136 lb. The required yield stress in the bolt material is 13,136 lb 2
= 66.900 lb/in (0.5in)2j4 Top Closure Post, SKD-86008 items 1 or 2
\\
F
\\
F2 A
R wi 2
E g
R P
R Shear Moment j
Loading. Shear and Mcments on Top Closure Post Due to 6g Minus x-Direction Acceleration
~
t F
j 2
XLR Top Closure 0
5463 414 Top Closure 2731 2731 Revision 1
O The bolt material is ASTM 354 grade BC which has a 2
minimum tensile yield of 109.000 lb/in,
Conclude that the bolts securing the top closure post to the top cross frame base tube do not yield in a 6g minus x-direction acceleration.
Design Criterion The top closure post shall not yield due to a 69 minus x-direction acceleration.
Verification The former diagram shows that the maximum beam moment occurs at the location of the R reaction. The moment 2
is maximum in the case of 414 shipments having value 30,696 in Ib. The moment of inertia of the section taking credit for the solid sections only is based on 3
the familiar 1/12 bh. The maximum fiber stress is,
,, (30,696 in 1b)(0.7 5 in)
= 44,077 0.522 in' 2.25 c
Tnp Closure Post SKC-86011
/
N.A^
4 1.53 I = 0.522 in
~ Top Closure Post Section at Point of Reaction R.,
The upright material is ASTM A572 grade 50 which has yield stress exceeding 50K.
(
Conclude that the top closure post will not yield due to ion.,ngs. sed in the 69.inus x.d,,ect,on acceleration case.
x,n.1
Jack Screw Buckling Load Design Criterion The jack screws that secure the fuel top nozzle shall not buckle in the 6g minus x-direction acceleration.
Verification The maximum inertial loading is on the jack screws that operate with the z-bars and is 5160 pounds on each screw. The actual and analytical equivalent loadings along with relevant dimensions are shown in the sketch. Buckling will occur at the critifal load, PCR, which Shames gives as Ip I, n,2 2
EI CR n 4L4 6
4
= (1)2,2 (30x10 )(w*.4056 )
4(3.42)2 64 l
(PCR); = 8,408 pounds l
P = 5160 lb i
I I a
L N
3.42 1 r l
'I f fle I//. 1/I f /
\\
l
[
l w 0.4056 Basic Minor Dia.
vC Analytical Equivalent Loading Actual Loading Actual and Analytical Equivalent Loading on Jack Screw in 6e Minus x-dir. Acceleration Conclude that the jack screws will not buckle in the 6g mi.nas x-direction acceleration case.
f Jack Screw Thread Strength Design Criterion The jack screw thread shell not yield in a 6g minus x-direction acceleration.
Verification Two jackscrews share the 6g minus x-direction inertial load from each fuel assembly. Each jack screw carries a maximum load of 5160 pounds.
R.C. Boucher tabulates shest area for threads of a 0.500130NC 2A bolt in " Strength of Threads",
contained in volum 32 of Product Engineering, dated 2
November 27,1961. The value quoted is 0.7821 in per inch of bolt length. Since one inch of thread engages with the applicable bar the thread stress is 5160 lb 2
2
= 6598 lb/in (0.7821 in )
d The jaca screw material is ASTM 354 grade BC which Ms 2
minimum tensile yleid of 109,000 lb/in. Minime shear yf eld 2
1s 54.500 lb/in by deduction.
Conclude that the jack screw threads will not shear in the 6g pinus x-direction acceleration.
1 Stress i
Desion Criterion Stress in the Z-bar shall not exceed material yield in a 6g minus x-direction acceleration, j
l O
1 I
sv
[eri f_ication Although the bar is a Z shape it is treated as straight in this analysis. The loading, shear force distribution and moment $1stribution are as diagramed. The center
' hub is assumed to transmit no portion of the bending acment along the beam, If the two side ligaments transinit the eritre load they are stressed to c. where 2
,, (19Ce6 in 16)(0.50 ini = 124.516 lb/in 1/12 tl in)O in)J
(
The caterial yield stress is quoted by note 4 of drawing SKO-86010 at 120K to 140K.
Conclue that.strets in the Z-bar will not exceed mater'ial yfeld in a 6g minus x-directi.on acceler6tihn.
4 f.
I-$ar Thread Strength Desten Criterion The thread through Z-t,Er tapped holas shall no't yield in a e
43 shs x-direction acceleration.
yerification__
Two jackscrews share the 69 minus x-direction ittertial lead free each fuel assembt/.
fach Z-bar(SKD-86010) h91e is loaded, thtrefore, to 5160 pounds.
R. C. Boucher tabulates shsar area for threads of a 0.50013UNC 23 hole in " Strength of Threads" contained in volume 32 of Froduct Engiceering, dated Novw.ber 27, 1961.
2 The value poted is 1.1231 in per inch of threaded hole length, since the Z-bar threaded hole is one inch long the 1
thmad stress is fh 3,2)
- 4M lb/in The material shear yield stress is 60,000 lb/in.
f 2
O Conclude that the thread through the Z-ber tapped holes will not yleid in a $g minus x.directica acceleration.
j i
Revision 1
Bgttgm.h229ft Bottom Support Plate Stress Design feiterion Stress iti the XL shipping container support frame' bottom support shall not exceed yield due to a 6g x-direction acceleration.
Veri /f ca tion Since it is symmetrical, consider only half of the bottom support plata. The plate edges are considered built in as shown in the sketch and the 6g loading is considered equally distributed over the plate surface, at intensity value q.
d a/b = 0.85 t
2 q = 97.4 lb/in 3
,' Sottou Support l
Plate S
= 1.455
/
y
/
/
8
= 1.419 g
= 1.151 1
l
[2 = 0.971
/
l
/
a
)
.c Hr/// u irrit a = 9.75
(/
Analyttcal Model for Bottom Support Plate Stress Calculation Definitions t = plate thickness = 0.75 in e, = bending stress in plate parallel to side a
= bending stress in plate parallel to side b eb R = reaction force nsrmal to the plate surface exerted by the boundary support on the plate edge.1b/in are functions of a/b given in the reference.
j 2 1 **d 2
B.8
p At y = 0 and z = b...
-s qb2 Q
2 2
-32.000 lb/in, and Max. o,
2 t
R2" 2qb = 1088 lb/in At y = a and z = o 8 qb 1
2
= -33.300 lb/in, and Max o b
2 t
R = 1289 lb/in The maximum stress in the plate is slightly over the commonly accepted yield value. The yield value is actually somewhat higher than 30 as Shames lists the value for annealed 2
1020 at 48,000 lb/in. In addition, the analysis neglects
'the stiffening effect of the gussets, SKD-86012, item 3, and any yielding in the plate would be local and of the self-relieving variety.
Conclude that the bottom support will not yield in the 6g x-direction acceleration.
Bottom Support Welds Design Criterion The welds and bolts which secure the bottom support must nct yield in a 6g x-direction acceleration.
Verification. Welds The weld along the y=o edge is a 3/16" fillet which has a strength of 1800 lb/ inch of weld. The normal reaction force along this weld has a maximum value of 1088 lb/in whic:,
is well below the 1800 lb/in allowable limit.
Revision 1
O Conclude that the weld along the side where x=o is clearly of sufficient strength.
The weld along the z=o edge (base plate to support plate connection) is a 1/4" fillet weld which has a strength of 2400 lb/in of weld. The normal reaction force along this weld has a maximum value of 1289 lb/in which is well talow the 2400 lb/in allowable limit.
Conclude that the weld along the side where z=o is clearly of sufficient strength.
Verification. Bolts The bolts, oriented on vertical axes (z-axes) running through the bottom support, and axle that restrain the half-plate shown previously are sketched below.
Q Support 10.5 g
Frane Centerline i
og L no n y
--- 1289 lb/in
-Bottom Support
//
//
'/
l 3_.
Z//W Xk l
e _.4_
N'_ /$f l -l >,.
fn i
y Axle
\\
Bolts
~
SKE-85004 Load and Restrainino Bolts on Bottom Support O
i Revision 1 I
O The bolts support a total load of 15.561 lb. which is assumed equally shared between the bolts. 7780 lb. The sheer stress in each is 2
t = 77
= 54.943 lb/in r
The bolt material is ASTM 354 grade BC which has a minimum 2
tensile yield of 109.000 lb/in. By deduction, the minimum 2
shear yield is 65.400 lb/in,
Conclude that the bolts which secure the bottom support will N t yield in the 6g x-direction acceleration.
O I
i O
l Raf. Roark & Young. Formulas for Stress and Strain. 5th Edition. p. 399 case 11a e
Y%
i f
5, E
N7 (iii) Uranium dioxide as Zircaloy clad unirradiated fuel elements, g
Two (2) neutron absorber plates consisting of carbon steel, 0.035 inches in thickness, with 4 mils of Gd203 (0.02 gm-Gd203/sq. cm) affixed to each side of the plate are required between fuel elements of the following specifications:
,_!1 14x14 15x15 14x14 15x15 17x17 16x16 16x16
-E ZR ZR SST SST ZR ZR ZR S
TYPE CLAD CLAD CLAD CLAD CLAD CLAD CLAD
.F
==------ -
cg r
Pellet diameter (nom), inches 0.344-0.367 0.384 0.384 0.308-0.322 0.325 O.367 O.322 gE Rod diameter (nom), inches O.400-0.422 0.422 0.422 0.360-O.374 0.382 j
o,E,,
O.422 O.374 gO Fuel length (max), inches 144 144 120 120 168 144 150 g
R*
Maximum rods / element 180.-
204 180 204 264 235 236 m
i m
03 \\
g k Maximum cross section, 7.8
- 8.4 7.8 8.4 8.4 7.8 7.98 j
m (nom), anch sq.
Maximum U-235/ element (kgs) 22.1 21.5 23.1 22.0 19.9 20.7 21.1 (144"L) 29 NS 23.3 i
(168"L)
U-235 enrichment (max),w/o 4.2 4.3 4.2 4.3 4.3 4.3 4.2 Ef l
A
/N Q
]
~
(iv)
Uranium dioxide om zircolay or etain1 con steal clad unirradiated fuel rods of the following specifications:
k TYPE SST CLAD ZR CLAD ZR CLAD ZR CLAD ZR CLAD ZR CLAD w
g J
Pellet diameter (nom), inches 0.384 0.344-0.308-0.322 0.3805 0.325 O.367 0.322 2
Rod diameter (nom), inches O.422 0.400-O.360-0.374 0.44 0.382 O.422 0.374 Fuel length (max), inches 120 144 168 144 144 150 U-235 enrichment (max),w/o 5g Note 1 4.0 4.0 3.65 4.0 3.85 1;;
Note 2 4.2 4.2 4.3 4.3 4.2
,E-Note 3 3.55 i g --
NOTES:
h (1) Two neutron absorber plates consisting of 0.19 inch thick, a_, ;;
full length stainless steel containing 1.3% (minimum) Baron or O.19 inch thick OFHC copper are required between the rod boxes.
g[J
,g-(2) Two neutron absorber plates consisting of carbon steel, 0.035 inches in thickness, with 4 mils of Gd203 E,g
[7 (minimum 0.02 gm-Gd203/sq. cm) affixed to each side of the 0-plate are required between the rod boxes.
(3) Two neutron absorber plates consisting of 0.19 inch thick carbon steel are required between the rod boxes.
t y PmE (2)
Maximum quantity of material per package E"
(i)
For the contents described in (1) (i), (1) (ii), and (1) (iii ) :
- f Two fuel elements.
gg (ii)
For the contents described in (1) (iv) :
~{
m Two inner containers containing not more than 80 kilograms U-235.
l
O ATTACHMENT 19 WESTINGHOUSE SHIPPING CONTAINER CRITICAL!TY ANALYSIS d
4 i
e-Y t
Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No._1.3-l Revision Submittal Date:
4/28/86 Rev. No.1
O WESTINGHOUSE SHIPPING CONTAINER CRITICALITY ANALYSIS INTRODUCTION in light of the improvements in the state of the art of criticality calculations in the last several years, a change in the Westinghouse criticality design methodology has taken place. Criticality calculations are now done using the AMPX-Il modeuls NITAWL and XSDRNPM for cross-section generation and KENO-IV for eigenvalue calculations. These methods have been benchmarked to various critical experiments and are now used exclusively for fuel assembly l
criticality calculations.
In addition to the standard RCC container (copper absorber plates),
an upgraded RCC container with Gd 0 coated carbon steel 23 absorber plates is analyzed.
Westinghouse has used two separate design criterion for the criticality of the shipping containers. The first criterion is that K,,, is less than or equal to 0.95 on a best estimate basis with l
minimal additional uncertainties for the maximum credible accident (MCA). The MCA for an RCC container is two flooded containers crushed together such that the assemblies are separated by four inches of water. The second criterion is that k,,, is less than or equal to 0.95 on a best estimate basis with minimal additional uncertainties for the MCA and also that k,,, is less than or equal to 0.98 for " optimum moderation" conditions on a best estimate basis with minimal additional uncertainties for the MCA. The MCA for an RCC container'with this criterion is an infinite number of containers crushed together such that the assembiles are separated by four inches of moderator on one side, sixteen inches of moderator on two sides and 24 inches of moderator on the fourth side. The O
container shell is assumed to be in place with adjacent container shells in contact with each other.
Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.19-2 Revision Submittal Date: 4/28/86 Rev. No. 1
O DESIGN METN00S As mentioned previously, the current Westinghouse criticality design methods employ the two AMPX( } modules NITAWL and XSDRNPM along with the Monte Carlo code KENO-IV.I2 The NITAWL code is used to add resolved resonance parameters to the 1227-group master l
library.(3) The XSDRNPM code then takes the revised group library and performs a cell calculation. The solution for this cell calculation is then used to collapse the cross-sections into a 19-group library (the group structure recommended by ORNL). This library is then used as input to KENO-IV.
Cross-sections for a shipping container are obtained from a cell calculation. The cross-sections for the structural material and the absorber are obtained by introducing trace amounts into the moderator in the cell. As far as has been determined, this procedure does not produce any bias in the results due to the fineness of the group structure.
O The geometric capabilities of KENO-IV are used to provide an essentially exact two-dimensional representation of the problem.
The problem is considered to extend infinitely along the length of the fuel assemblies, conservatively ignoring the benefits of axial leakage.
Each cell (or box type) is modeled explicitly as a fuel pellet, cladding, and associated moderator.
Thimble cells are also modeled explicitly. No credit is taken for the presence of U-234 or U-236; neither is credit taken for any structural material (grids, l
clamping frames, etc.).that does not extend the full length of the assembly.
A representation of the MCA problem for the finite array with two crushed containers is given in Figure 1.
The boundary conditions on z
the top and left are zero current, while those on the bottom and i
right are zero flux. A representation of the MCA problem with an infinite number of crushed containers is given in Figure 1A. The boundary conditions are zero current on all sides. The minimum spacing permitted by the tolerances is employed in both cases.
l Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.19-3 Revision Submittal Date: 4/28/86 Rev. No._1_
The Westinghouse criticality method has been benchmarked to a set of i
30 critical experiments from three sources. Two sets of the experiments were performed at Battelle's Pacific Northwest Laboratories (4'5); the third was performed at ORNL.I }
The PNL experiments were performed with LWR-type fuel in LWR-type geometries; the ORNL experiments were performed with dry highly enriched uranium metal cylinders. Table I provides general information about the critical experiments. Table 2 provides statistical information about the PNL analyses, the ORNL analyses, r
and the combined set. As is evident, there is very little difference between the PNL analyses and the combined set, indicating the wide range of applicability of the method. The results of the benchmark calculations show that there is essentially no bias to the experiments, with a 95/95 uncertainty of 0.013.
No critical experiment was eliminated on the basis of an anomalous result.
CONTAINER ANALYSES The RCC container (copper absorber plates) was analyzed for three
\\
different Westinghouse Optimized Fuel Assemblies (0FA) - the 14x14 0FA, the 15x15 0FA, and the 17x17 0FA. These assemblles were designed to maximize reactivity by optimizing the H/U ratio.
Each of these assemblies uses Zircaloy-4 cladding.
Figure 2 shows LEOPARO calculations of K,gg versus H/U for the 14x14 and 17x17 lattices (the 15x15 assemblies are already optimized, and no changes have been made to the H/U ratio between standard 15x15 and 15x15 0FA).
In both cases, the OFA is more reactive than the standard assembly, indicating that the OFA is limiting from a criticality standpoint. An analysis has also been performed for a 17x17 standard fuel assembly in a container in which the copper absorber plate has been replaced by a carbon steel plate of the same dimensions.
The Westinghouse 16x16 assembly was designed to fit the same envelope as the 14x14 assembly.
In shipping container analyses, therefore, the more reactive of the two assemblies is limiting.
O Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.19-4 Revision Submittal Date: 4/28/86 Rev. No._L_
Unit assembly calculations have been performed for both 14x14 standard and 16x16 assemblies under cold conditions. The 16x16 O
assembly is 0.007 delta-k less reactive than the standard 14x14 assembly which is 0.007 delta-k less reactive than the 14x14 0FA.
The 14x14 0FA is limiting, therefore, both for 14x14 and 16x16 fuel types. Table 3 indicates the fuel types that are covered by each of I
the 0FA types that will be analyzed.
Each of the three limiting fuel types was analyzed in the RCC container in KENO. The MCA problem used in this analysis consists of the two crushed containers as given in Figure 1.
A summary of the results is given in Table 4, the KEN 0 input listings are in Tables 5, 6 and 7 and the nuclide/nuclide number correspondence is given in Table 13.
In each case, the best estimate K,,, is less than or equal to 0.95 while the final K,gg with uncertainties is less than 0.96.
The 14x14 and 16x16 assemblies, therefore, exhibit no criticality safety problems at enrichments less than or equal to 4 w/o while the 15x15 and 17x17 assemblies behave similarly at enrichments less than or equal to 3.65 w/o.
The 17x17 standard fuel assembly with the carbon steel absorber plates is limited to an enrichment of 3.55 w/o. A summary of the KENO calculation results for this case is given in Table 4.
The KENO input listilg is given in Table 14, and the nuclide/nuclide number correspondence is given in Table 13. The best estimate K,,, is less than 0.95 while the final K,gf with uncertainties i
is less than 0.965.
The analysis for the CE-type fuel is given in Appendix 198. The same benchmarks and methods apply.
The MCA problem used in this analysis consists of the two crushed containers as given in Figure 1.
The limiting fuel types were also analyzed in the RCC container using the representation of the MCA problem with an infinite number of crushed containers (Figure 1A). A summary of the results is 23, 24, 25 O
given in Table 22, the KENO input listings are in Tables and 26 and the nuclide/nuclide number correspondence is given in Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.19-5 Revision Submittal Date:
4/28/86 Rev. No.[
Table 13.
In each case, the best estimate K-eff is less than 0.96.
O The 14X14 and 16X16 assembiles exhibit no criticality safety problems at enrichments less than or equal to 4/0 w/o while the 15X15 and therefore the 17X17 results exhibit no criticality safety problem at enrichments less than or equal to 3.65 w/o. The CE-type fuel is limited to an enrichment of 3.85 w/o, while the 17X17 standard fuel assembly with the carbon steel absorber plates is limited to an enrichment of 3.55 w/o.
Figure 3 shows the relationship (calculated by LEOPARD) between K,9f and rod pitch for atI three rod types.
In each case it is obvious that the drier the lattice, the less reactive it is. A square tight-packed lattice of individual fuel rods is, therefore, less reactive than those same fuel rods in a fuel assembly. The fuel assembly is, therefore, the limiting case for fuel rod shipments.
The upgraded RCC shipping container has two absorber plates made of O
carbon steel, 0.035 inches in thickness, with 4 mils of Gd 023 2
(0.02 g - Gd 0 /cm ) affixed to each side of the plate. The 23 MCA problem used in this analysis consits of the two crushed containers as given in Figure 1.
Four Westinghouse fuel assembly types were analyzed in this RCC shipping container. These were the 14x14 0FA,15x15,16x16, and 17x17 0FA. The applicable fuel types for the OFA fuel assemblles are shown in Table 3.
Table 8 summarizes the KENO calculated nominal K,99 for each of the four problems analyzed. The MEN 0 input listings are in Tables 9 through 12, and the nuclide/nuclide number correspondence is given in Table 13. The Westinghouse 17x17 0FA and Westinghouse 15x15 fuel assemblies with U-235 enrichments of up to 4.3 w/o can be shipped l
under MCA conditions and not exceed the criticality criterion of K,99 less than or equal to 0.95.
Furthermore, Westinghouse 14x14 0FA and Westinghouse 16x16 fuel assemblies with U-235 enrichments of up to 5 w/o can also be shipped under MCA conditions. Enrichments i
greater than 5 w/o were not considered in this study for those two fuel assembly types.
Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.19-6 Revision Submittal Date:
4/28/86 Rev. No.1
The upgraded RCC shipping container with the two Gd 0 coated 23 absorber plates was also analyzed using thr representation of the Og MCA problem with an infinite number of crushed containers (Figure 1a). An analysis was performed to determine which of the 17x17, 15x15,16x16 and 14x14 Westinghouse Standard Fuel assemblies would be more reactive, and therefore more limiting, under inifinite array and optimum moderation conditions. The 15x15 assembly is 0.001 delta-k more reactive than the next most reactive assembly. The 15x15 is therefore more limiting than the 17x17,16x16 and 14x14 fuel types. The applicable fuel types for the 15x15 assembly are shown in Table 15.
Five Westinghouse fuel assembly types were analyzed in this RCC shipping container with infinate array conditions. These were the Westinghouse 17x17 0FA,15x15,15x15 0FA,14x14 0FA and the C-8016x16 fuel assemblies. Table 16 summarizes the KENO calculated nominal K-eff for each of the problems analyzed. The KEN 0 input listings are in Tables 17 through 21.
The nuclide/nuclide number correspondence is given in Table 13.
The Westinghouse 17x17 0FA,16x16 and 15x15 0FA fuel assemblies with U-235 enrichments of up to 4.3 w/o can be shipped under the infinite array MCA conditions and not exceed the criticality criterion of K-eff less than or equal to 0.95 for full density water and K-eff less than or equal to 0.98 for optimum moderation conditions.
Furthermore, Westinghouse 14x14 0FA and C-80 16x16 fuel assemblies with U-235 enrichments of up to 4.2 w/o can also be shipped under the same conditions.
CONCLUSION A Monte Carlo criticality analysis of the RCC shipping container
(
under finite array conditions, with copper absorber plates has f
demonstrated that, at enrichments of 4.0, 3.65, 4.0, and 3.65 w/o, the 14x14,15x15,16x16, and 17x17 fuel assemblies, respectively, can be safely shipped without risk of criticality. The analysis has also shown that, since loose fuel rods in a tight lattice are less reactive than fuel assemblies, loose fuel rods of the above enrichments can also be safely shipped in the RCC container. With the carbon steel absorber plates, the Monte Carlo criticality
(
analysis of the RCC shipping container has demonstrated that, at an enrichment of 3.55 w/o, the 17x17 fuel assemblies can be safely I
shipped without risk of criticality.
Docket No. 71-5450 initial Subaittal Date: 12/20/85 Page No.19-7 Revision Submittal Date:
4/28/86 Rev. No.,_1_
The criticality analysis of the RCC shipping container under infinite array conditions with copper absorber plates has demonstrated that, at enrichments of 4.0, 3.65, 4.0, 3.65, and 3.85, i
the 14X14,15X15,16X16,17X17 and CE-type 14X14 fuel assemblies, respectively, can be safely shipped without risk of criticality.
Also, with the carbon steel absorber plates, the criticality analysis of the shipping container has demonstrated that, at an enrichment of 3.55 w/o, the 17X17 fuel assemblies can be safaely shipped without risk of criticality.
The Monte Carlo criticality analysis of the upgraded RCC shipping container under infinite array conditions, using Gd 0 absorber 23 plates has demonstrated that, at enrichments of 4.2, 4.3, 4.3, 4.2 and 4.3 w/o, the 14x14 0FA,15x15 0FA,16x16, C-8016x16 and the 17x17 0FA fuel assemblies, respectively, can be safely shipped without risk of criticality.
The Monte Carlo criticality analysis of the upgraded RCC shipping container under finite array conditions, using Gd 0 absorber 23 plates has demonstrated that, at enrichments of 5.0, 4.3, 5.0 and 4.3 w/o, the 14x14 0FA,15x15,16x16, and 17x17 0FA fuel assemblies, respectively, can be safely shipped without risk of criticality.
- O Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No. 19-8 Revision Submittal Date:
4/28/86 Rev. No._T_
TABLE 16
('
KENO CALCULATED RESULTS (INFINITE ARRAY MAXIMUM CREDIBLE ACCIDENT)
U-235 KENO Nominal K-eff Fuel Type Enrichment Mod. Density = 1 Opt.
Moderation Moderation W 14x14 0FA 4.2 w/o 0.926 i 0.0046(1) 0.961 0.0047 i.0048 W 15x15 0FA 4.3 w/o 0.908 1 0.0041 0.967 0
W 16x16 4.3 w/o 0.926 t 0.0046(2) 0.965 1 0.0036 0.0038(1) 0.969 i 0.0048 W C-80 16x16 4.2 w/o 0.933 t W 17x17 0FA 4.3 w/o G.908 t 0.0037 0.965 1 0.0037 (1) Calculated with 5 w/o U-235 (2) Not calculated, however, previous container analysis shows the Westinghouse 16x16 fuel is less reactive than the 14x14 0FA fuel.
l l
l l
l I
i l
' O Docket No. 71-5450 InltIal Subelttal Date:
12/20/85 Page No. 19-32 Revision Submittal Date: 4/28/66 Rev.No.1
TABLE 22 KEN 0 CALCULATt'3 RESULTS
]
(INFINITE ARRAY MAXIMUM CMDIBLE ACCIDENT)
U-235 Keno Nominal K-eff Opt.
Fuel Type Enrichment NM. Density 14X14 0FA 4.00
.923 1 0035 15X15 0FA 3.65
.918 i.0033 16X16 4.00
<.923 3 0035 17X17 0FA 3.65
<. 918 i.0033 17X17 STD(1) 3.55
.929 t.0030 14X14 CE 3.85
.939 +.0033 (1) Carbon steel absorber plates. All other cases for copper absorber plates.
O O
Docket No. 71-5450 Initial Subeittal Date: 12/20/85 Page No.19-42.1 Revision Submittal Date: 4/28/86 Rev. No. _L j
O TABLE 23 KENO INPUT DATE FOR THE 14X14 0FA INFINITE ARRAY CALCULATIONS INPUT DATA IMAGE LIST CARD 1
2 3
4 5
6 7
8 SEe.
5 0
5 0
5 0
5 0--~ 5---0--- 5----0-~ 5---0----5----O 1 SHIPPING CONTAIN(INFINITE) 4.0014X14 0FA W/ COPPER AT H2O 0.03 2 10 900 305 5 19 19 17 7 17 35 13 16 16 1 -17 1 0 1011 0 1 8 a0 0 3 -1.0 -1.0 -1.0 -1.0 -1.0 -1.0 41
-11261039
.0009290 51 11262039
.022031 61 11276
.045921 72 2128402
.043260 83 2128402
.003588021 93 31276
.00091705 10 3 31269
.001834 11 4 31276
.001000 12 4 31269
.002000 13 5 3119202
.061344 14 5 3119002
.006485 15 5 3119102
.016472 16 5 3119702
.000866 17 6 3129502
.084550 18 7 2128402
.004013152 19 7 31276
.00090723 20 7 31269
.001814 O
21 80X TYPE 1 22 CYLINDER 1 0.437388 381.00 0.0 19a0.5 23 CYLINoER 0 0.44627 381.00 0.0 19a0.5 24 CYLINDER 2 0.508 381.00 0.0 19*0.5 25 Cue 010 4 0.705612 -0.705612 0.705612
-0.705612 381.00 0.0 19*0.5 26 80X TYPE 2 27 Cue 010 3 1.411224 0.0 1.411224 0.0 381.00 0.0 19a0.5 28 BOX TYPE 3 29 Cus0!D 5 20.22856 19.757136 0.0
-0.4572 381.00 0.0 19a0.5 30 Cue 010 4 23.56037 19.757136 0.0
-38.5572 381.00 0.0 19*0.5 31 Cue 010 5 23.56037 19.757136 0.0
-38.68928 381.00 0.0 19*0.5 32 80X TYPE 4 33 Cue 010 5
1.411224 0.0 0.0
-0.4572 381.00 0.0 19*0.5 34 Cue 010 4
1.411224 0.0 0.0
-38.5572 381.00 0.0194.5 35 Cue 01D 5
1.411224 0.0 0.0
-38.68928 381.00 0.0 19*0.5 36 80X TYPE 5 37 Cue 010 5 21.14166 21.05276 1.411224 0.0 381.00 0.0 19a0.5 38 Cue 010 6 21.62426 20.57016 1.411224 0.0 381.00 0.0 19a0.5 39 Cue 010 4 23.56037 20.22856 1.411224 0.0 381.00 0.0 19a0.5 40 Cue 01D 5 23.56037 19.757136 1.411224 0.0 381.00 0.0 19a0.5 41 80X TYPE 6 42 Cue 010 5 21.14166 21.05276 1.411224 0.8128 381.00 0.0 19*0.5 43 Cue 010 6 21.62426 20.57016 1.411224 0.8128 381.00 0.0 19a0.5 44 Cue 0!D 4 23.56037 20.22856 1.411224 0.0 381.00 0.0 19a0.5 45 Cus010 5 23,56037 19.757136 1.411224 0.0 381.00 0.0 19a0.5 46 80X TYPE 7 47 Cus0!D 4
1.411224 0.0 25.6432 19.757136 381.00 0.0 19a0.5 48 CUB 010 5 - 1.411224 0.0 25.77528 19.757136 381.00 0.0 19a0.5 49 80X TYPE 8 50 Cue 010 5 20.22856 19.757136 24.9828 19.757136 381.00 0.0 19a0.5 i
--S 0
5 0
5 0
5 0
5---0--- 5---C 5----0-- ---O O
Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.19-42.2 Revision Submittal Date: 4/28/86 Rev. No. L
TA8LE 23 (CONTINUED) l INPUT DATA IMAGE LIST CAmo 1
2 3
4 5
6 7
8 SEQ.
-5 0
5 0
5 0
5---0----5 3----5----C 5---0----5----O 51 CUBOID 4 23.56037 19.757136 25.6432 19.757136 381.00 0.0 19=0.5 52 Cue 010 5 23.56037 19.757136 25.77528 19.757136 381.00 0.0 19a0.5 53 BOX TYPE 9 54 Cus010 5 21.14166 21.05276 19.148662 18.345912 381.00 0.0 19*0.5 55 CUBOIo 6 21.62426 20.57016 19.148662 18.345912 381.00 0.0 19*0.
56 Cue 010 4 23.56037 20.22856 19.757136 18.345912 381.00 0.0 19*0.
57 Cus0Io 5 23.56037 19.757136 19.757136 18.345912 381.00 0.0 19*0 58 eOX TYPE 10 59 CUB 010 4
0.0
-20.32 1.411224 0.0 381.00 0.0 19a0.5 60 Cus010 5
0.0
-20.45208 1.411224 0.0 381.00 0.0 19*0.5 61 BOX TYPE 11 62 Cue 010 4
0.0
-20.32 25.6432 19.757136 381.00 0.0 19*0.5 1
63 cue 010 5
0.0
-20.45208 25.77528 19.757136 381.00 0.0 19a0.5 64 80X TYPE 12 65 CUB 0ID 4
0.0
-20.32 0.0
-38.5572 381.00 0.0 19*0.5 66 CUBOID 5
0.0
-20.45208 0.0
-38.68928 381.00 0.0 19*0.5 67 50X TYPE 13 68 Cus010 7
1.411224 0.0 1.411224 0.0 381.00 0.0 19*0.5 69 1 2
15 1 2
15 1 1 1 1 0 70 2 4
13 3 4
4 1 1 1 1 0 71 2 6
11 5 6
6 1 1 1 1 0 0
72 2 4
13 9 7
7 1 1 1 1 0 73 2 4
13 9 10 10 1 1 1 1 0 74 2 6
11 5 11 11 1 1 1 1 0 75 2 4
13 3 13 13 1 1 1 1 0 76 3 16 16 1 1
1 1 1 1 1 0 77 4 2
15 1 1
1 1 1 1 1 0 73 5 to 16 1 3
14 1 1 1 1 0 79 6 16 16 1 2
2 1 1 1 1 0 80 7 2
15 1 16 16 1 1 1 1 0 81 8 16 16 1 16 16 1 1 1 1 0 82 9 16 16 1 15 15 1 1 1 1 0 83 10 1 1
1 2
15 1 1 1 1 0 84 11 1 1 1 16 16 1 1 1 1 0 85 12 1 1 1 1
1 1 1 1 1 0 86 13 8 8 1 8
8 1 1 1 1 1 87 -1 88 END KENO 5 - -C 5-0 5
0 5
0 5
0---5----C
-5 0--- 5 ----O O
Docket No. 71-5450 Initial Submittal Date: 12/20/85 Page No.JJ-42.3 Revision Submittal Date:
4/28/86 Rev. No. 1
TABLE 24
\\
KENO INPUT DATA FOR THE 15X15 0FA INFINITE ARRAY CALCULATION INPUT DATA IMAGE LIST CARD 1
2 3
4 5
6 7
8 SEe.
5 0
5 0
5 3-- 5 ---C 5 ----0--- S ---0--- 5 ----0 ---- 5 ----O 1 SHIPPING CONTAIN(INFINITE) 3.65 iSX15 0FA W/COPPEK AT H20 0.03 2 10 900 305 5 19 19 14 6 14 34 12 17 17 1 -14 1 0 1011 0 1 8*0 0 3 -1.0 -1.0 -1.0 -1.0 -1.0 -1.0 41
-11261039
.000848C 51 11262039
.022113 61 11276
.045924 72 2128402
.043260 83 2128402
.003855839 93 31276
.00091086d 10 3 31269
.0018217 11 4 31276
.001000 12 4 31269
.002000 13 5 3119202
.061344 14 5 3119002
.006445 15 5 3119102
.016472 to 5 3119702
.000866 17 6 3129502
.084550 18 80X TYPE 1 19 CYLIN0ER 1 0.464693 381.00 0.0 19*0.5 20 CYLIMOER 0 0.474218 381.00 0.0 19*0.5 21 CYLIMcER 2 0.53594 381.00 0.0 19*0.5 22 Cueolo 4 0.71501 -0.71501 0.71501
-0.71501 341.00 0.0 19*0.5 23 80X TYPE 2 24 Cue 010 3 1.43002 0.0 1.43002 0.0 381.00 0.0 19*0.5 25 80X TYPE 3 l
26 Cue 0ID 5 21.9075 21.4503 0.0
-0.4572 381.00 0.0 19*0.5 27 Cue 010 4 23.56037 21.4503 0.0
-38.5572 381.00 0.0 19*0.5 28 Cue 010 5 23.56037 21.4503 0.0
-38.68928 381.00 0.0 19*0.5 29 e0X TYPE 4 30 Cueolo 5
1.43002 0.0 0.0
-0.4572 381.00 0.0 19*0.5 31 Cue 0!D 4
1.43002 0.0 0.0
-38.5572 381.00 0.0 19*0.5 32 Cue 010 5
1.43002 0.0 0.0
-38.68928 381.00 0.0 19*0.5 33 e0X TYPE 5 34 Cue 010 5 22.8206 22.7317 1.43002 0.0 381.00 0.0 19*0.5 35 Cue 010 6 23.3032 22.2491 1.43002 0.0 381.00 0.0 19*0.5 36 Cue 010 4 23.56037 21.9075 1.43002 0.0 381.00 0.0 19*0.5 37 Cue 010 5 23.56037 21.4503 1.43002 0.0 381.00 0.0 19*0.5 38 e0X TYPE 6 39 Cue 0!D 5 22.8206 22.7317 1.43002 0.8128 381.00 0.0 19*0.5 i
40 Cue 010 6 23.3032 22.2491 1.43002 0.8128 381.00 0.0 19*0.5 41 Cueolo 4 23.56037 21.9075 1.43002 0.0 381.00 0.0 19*0.5 42 Cue 010 5 23.56037 21.4503 1.43002 0.0 381.00 0.0 19*0.5 43 80X TYPE 7 44 Cue 010 4
1.43002 0.0 25.6432 21.4503 381.00 0.0 19*0.5 45 Cue 010 5
1.43002 0.0 25.77528 21.4503 381.00 0.0 19*0.5 46 80X TYPE 8 47 Cue 010 5 21.9075 21.4503 24.9828 21.4503 381.00 0.0 19*0.5 48 Cue 010 4 23.56037 21.4503 25.6432 21.4503 381.00 0.0 19*0.5 49 Cue 010 5 23.56037 21.4503 25.77528 21.4503 381.00 0.0 19*0.5 50 80X TYPE 9 51 0-5 0
5 - -c 5
0 0 5
3----5 --0-5 ---O l
l Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.19-42.4 Revision Submittal Date:
4/28/86 Rev. No. I
O TA8LE 24 (CONTINUED)
V INPUT DATA IMAGE t.IST CARD 1
2 3
4 5
6 7
8 SEe.
5 0
5 0
5 ---0-- 5 ----C 5- ~ 0----5----O 5----0---S----O 51 Cue 01r, 5 22.8206 22.7317 20.82303 20.02028 381.00 0.0 19*0.5 52 Cue 0!O 6 23.3032 22.2491 20.82303 20.02028 381.00 0.0 19*0.5 53 Cue 010 4 23.56037 21.9075 21.4503 20.02028 381.00 0.0 19*0.5 54 Cue 010 5 23.56037 21.4503 21.4503 20.02028 381.00 0.0 19*0.5 55 00X TYPE 10 56 Cue 010 4
0.0
-20.32 1.43002 0.0 381.00 0.0 19*0.5 57 Cue 010 5
0.0
-20.45208 1.43002 0.0 381.00 0.0 19*0.5 58 00X TYPE 11 59 Cue 0ID 4
0.0
-20.32 25.6432 21.4503 381.00 0.0 19*0.5 60 Cue 010 5
0.0
-20.45208 25.77528 21.4503 381.00 0.0 19*0.5 61 00X TYPE 12 62 Cue 010 4
0.0
-20.32 0.0
-38.5572 381.00 0.0 19*0.5 63 Cue 0!D 5
0.0
-20.45208 0.0
-38.68928 381.00 0.0 19*0.5 64 1 2
16 1 2
to 1 1 1 1 0 65 2 4
7 3 4
4 1 1 1 1 0 66 2 11 14 3 4
4 1 1 1 1 0 or 2 9
9 1 5
5 1 1 1 1 0 68 2 6
12 6 6
6 1 1 1 1 0 69 2 4
14 10 7 7 1 1 1 1 0 70 2 5
13 4 9
9 1 1 1 1 0 71 2 4
14 10 11 11 1 1 1 1 0 72 2 6
12 6 12 12 1 1 1 1 0 73 2 9 9 1 13 13 1 1 1 1 0 0
74 2 11 14 3 14 14 1 1 1 1 0 75 2 4
7 3 14 14 1 1 1 1 0 76 3 17 17 1 1
1 1 1 1 1 0 77 4 2
16 1 1
1 1 1 1 1 0 78 5 17 17 1 3
15 1 1 1 1 0 79 6 17 17 1 2
2 1 1 1 1 0 80 7 2
16 1 17 17 1 1 1 1 0 81 8 17 17 1 17 17 1 1 1 1 0 82 9 17 17 1 16 16 1 1 1 1 0 83 10 1 1
1 2
16 1 1 1 1 0 84 11 1 1 1 17 17 1 1 1 1 0 85 12 1 1 1 1
1 1 1 1 1 1 86 -1 87 END KENO
--5 0
5----c 5---c 5
o---- 5 ---o---5 ----c 5 ---0---5 ----O Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.19-42.5 Revision Submittal Date:
4/28/86 Rev. No. 1
TABLE 25 Ab KENO INPUT DATA FOR THE CE TYPE 14X14 INFINITE ARRAY CALCULATION INPUT DATA INAGE LIST CARD 1
2 3
4 5
6 7
8 SEe. ---C 5 ---0--- 5 ----0---- 5 ----0---- 5 ----0-- S ----0---- S ----0---- 5 ----O 1 SHIPPING CONTAIN(INFINITE) 3.85 14X14 CE W/ COPPER AT H20 0.03 2 10 900 305 5 19 19 17 7 17 35 13 16 16 1 -17 1 0 1011 0 1 8'O O 3 -1.0 -1.0 -1.0 -1.0 -1.0 -1.0 41
-11261039
.0008940 51 11262039
.022062 61 11276
.045915 72 2128402
.043260 83 2128402
.004342975 93 31276
.0008996 10 3 31269
.0017992 11 4 31276
.001000 12 4 31269
.002000 13 5 3119202
.061344 14 5 3119002
.006485 15 5 3119102
.016472 16 5 3119702
.000866 17 6 3129502
.084550 18 7 2128402
.004019806 19 7 31276
.000907078 20 7 31269
.0018141 21 80X TYPE 1 22 CYLINDEA 1 0.483235 381.00 0.0 19*0.5 23 CYLINDER 0 0.5328 381.00 0.0 19*0.5 24 CYLINDER 2 0.5588 381.00 0.0 19*0.5
(
25 Cue 010 4 0.7366 -0.7366 0.7366
-0.7366 381.00 0.0 19*0.5 26 00X TYPE 2 27 Cue 010 3 1.4732 0.0 1.4732 0.0 381.00 0.0 19*0.5 28 BOX TYPE 3 29 Cue 010 5 21.082 20.6248 0.0
-0.4572 381.00 0.0 19*0.5 30 Cue 010 4 23.56037 20.6248 0.0
-38.5572 381.00 0.0 19*0.5 31 Cue 0!D 5 23.56037 20.6248 0.0
-38.68928 381.00 0.0 19*0.5 32 80X TYPE 4 33 Cue 01D 5
1.4732 0.0 0.0
-0.4572 381.00 0.0 19*0.5 34 CUBOID 4
1.4732 0.0 0.0
-38.5572 381.00 0.0 19*0.5 35 CUBOID 5
1.4732 0.0 0.0
-38.68928 381.00 0.0 19*0.5 36 BOX TYPE 5 37 Cue 0!D 5 21.9951 21.9062 1.4732 0.0 381.00 0.0 19*0.5 38 CUBOID 6 22.4777 21.4236 1.4732 0.0 381.00 0.0 19*0.5 39 Cue 010 4 23.56037 21.082 1.4732 0.0 381.00 0.0 19*0.5 40 Cue 01D 5 23.56037 20.6248 1.4732 0.0 381.00 0.0 19*0.5 41 80X TYPE 6 42 Cue 010 5 21.9951 21.9062 1.4732 0.8128 381.00 0.0 19*0.5 43 Cue 010 6 22.4777 21.4236 1.4732 0.8128 381.00 0.0 19*0.5 44 Cue 010 4 23.56037 21.082 1.4732 0.0 381.00 0.0 19*0.5 45 CUB 01D 5 23.56037 20.6248 1.4732 0.0 381.00 0.0 19*0.5 46 BOX TYPE 7 47 CUB 0!D 4
1.4732 0.0 25.6432 20.6248 381.00 0.0 19*0.5 48 Cue 010 5
1.4732 0.0 25.77528 20.6248 381.00 0.0 19*0.5 49 BOX TYPE 8 50 CUB 010 5 21.082 20.6248 24.9828 20.6248 381.00 0.0 19*0.5 5
.0 5
0 5
0
-5 0
5 0
5----o---s 0-- 0
\\
Docket No. 71-5450 initial Subaltta1 Date:
12/20/85 Page No.19-42.6 Revision Submittal Date: 4/28/86 Rev.No.[
TABLE 25 (CONTINUED)
IMPUT DATA IMAGE LIST CARD 1
2 3
4 5
6 7
8 S E Q. --5 ---0---- 5 ----0---- S ----0--S ----C 5 ---0---5 ----0---- 5 ---0---- 5 ----O 51 Cue 010 4 23.56037 20.6248 25.6432 20.6248 381.00 0.0 19*0.5 52 Cue 010 5 23.56037 20.6248 25.77528 20.6248 381.00 0.0 19*0.5 53 B0X TYPE 9 54 Cue 010 5 21.9951 21.9062 19.95435 19.1516 381.00 0.0 19*0.5 55 Cue 010 6 22.4777 21.4236 19.95435 19.1516 381.00 0.0 19*0.5 56 Cue 01D 4 23.56037 21.082 20.6248 19.1516 381.00 0.0 19*0.5 57 Cue 010 5 23.56037 20.6248 20.6248 19.1516 381.00 0.0 19*0.5 58 BOX TYPE 10 59 Cue 010 4
0.0
-20.32 1.4732 0.0 381.00 0.0 19*0.5 60 Cue 010 5
0.0
-20.45208 1.4732 0.0 381.00 0.0 19*0.5 61 BOX TYPE 11 62 Cue 010 4
0.0
-20.32 25.6432 20.6248 381.00 0.0 19*0.5 63 Cue 010 5
0.0
-20.45208 25.77528,20.6248 381.00 0.0 19*0.5 64 00X TYPE 12 65 Cue 010 4
0.0
-20.32 0.0
-38.5572 381.00 0.0 19*0.5 66 Cue 010 5
0.0
-20.45208 0.0
-38.68928 381.00 0.0 19*0.5 67 BOX TYPE 13 68 Cue 0!D 7
1.4732 0.0 1.4732 0.0 381.00 0.0 19*0.5 69 1 2
15 1 2
15 1 1 1 1 0 70 2 4
5 1 4
5 1 1 1 1 0 71 2 12 13 1 4
5 1 1 1 1 0 72 2 4
5 1 12 13 1 1 1 1 0 73 2 12 13 1 12 13 1 1 1 1 0 74 3 16 16 1 1
1 1 1 1 1 0 75 4 2
15 1 1
1 1 1 1 1 0 76 5 16 16 1 3
14 1 1 1 1 0 77 6 16 16 1 2
2 1 1 1 1 0 d
78 7 2
15 1 16 16 1 1 1 1 0 79 8 16 16 1 16 16 1 1 1 1 0 80 9 16 16 1 15 15 1 1 1 1 0 81 10 1 1
1 2
15 1 1 1 1 0 82 11 1 1 1 16 16 1 1 1 1 0 83 12 1 1 1 1
1 1 1 1 1 0 84 13 8 9 1 8
9 1 1 1 1 1 85 -1 86ENDgENO-C 5
0 5
0 5
0 5
0 5
- )----S 0--- -O O
Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No.19-42.7 Revision Submittal Date: 4/28/86 Rev. No. 7
TABLE 26 MENO INPUT FOR THE 17X17 INFINITE ARRAY CALCULATION INPUT DATA IMAGE LIST CAAD 1
2 3
4 5
6 7
8 SEe.
5 0
5 0
5 0
5 0 ---0---- 5 ----0--- 5 ---0---- $ ---O 1 SHIPPING CONTAIN(INFINITE) 3.55 17X17 0FA W/ CARBON STEEL AT H2O 0.03 2 10 900 305 5 19 19 15 6 15 34 12 19 19 1 -15 1 0 1011 0 1 8 a0 0 3 -1.0 -1.0 -1.0 -1.0 -1.0 -1.0 41
-11261039
.0008240 51 11262039
.022131 61 11276
.045913 72 2128402
.043260 83 2128402
.004049646 93 31276
.00090638 10 3 31269
.00181277 11 4 31276
.001000 12 4 31269
.002000 13 5 3119202
.061344 14 5 3119002
.006485 15 5 3119102
.016472 16 5 3119702
.nnnnAA 17 4 3119202
.083491 18 6 3127403
.003921 19 30X TYPE 1 20 CYLINDER 1 0.392176 381.00 0.0 19*0.5 21 CYLINDER 0 0.40005 381.00 0.0 19*0.5 22 CYLINDER 2 0.4572 381.00 0.0 19*0.5 23 Cue 010 4 0.62992 -0.62992 0.62992
-0.62992 381.00 0.0 19*0.5 24 som TYPE 2 25 Cus0!D 3 1.25984 0.0 1.25984 0.0 381.00 0.0 19*0.5 26 30X TYPE 3 27 CUB 0ID 5 21.87448 21.41728 0.0
-0.4572 381.00 0.0 19*0.5 28 CUB 0ID 4 23.56037 21.41728 0.0
-38.5572 381.00 0.0 19*0.5 29 Cus0!D 5 23.56037 21.41728 0.0
-34.68928 381.00 0.0 19*0.5 30 30X TYPE 4 31 Cue 0!D 5
1.25984 0.0 0.0
-0.4572 381.00 0.0 19*0.5 32 CUBOID 4
1.25984 0.0 0.0
-38.5572 381.00 0.0 19*0.5 33 Cue 010 5
1.25984 0.0 0.0
-38.68928 381.00 0.0 19*0.5 34 30X TYPE 5 35 Cue 01D 5 22.78758 22.69868 1.25984 0.0 381.00 0.0 19*0.5 36 Cue 0!D 6 23.27018 22.21608 1.25984 0.0 381.00 0.0 19*0.5 37 CU90!D 4 23.56037 21.87444 1.25964 0.0 381.00 0.0 19*0.5 38 Cue 0!D 5 23.56037 21.41728 1.25984 0.0 381.00 0.0 19*0.5 39 e0X TYPE 6 40 Cue 0!D 5 22.78758 22.69868 1.25984 0.8128 381.00 0.0 19*0.5 41 Cue 010 6 23.27018 22.21608 1.25984 0.8128 381.00 0.0 19*0.5 42 Cue 010 4 23.56037 21.87448 1.25984 0.0 381.00 0.0 19*0.5 43 Cue 010 5 23.56037 21.41728 1.25984 0.0 381.00 0.0 19*0.5 44 30X TYPE 7 45 Cus01D 4
1.25984 0.0 25.6432 21.41728 381.00 0.0 19*0.5 46 Cue 0!D 5
1.25984 0.0 25.77528 21.41728 381.00 0.0 19*0.5 47 30X TYPE 8 48 Cue 010 5 21.87444 21.41728 24.9828 21.41728 381.00 0.0 19*0.5 49 Cue 010
-4 23.56037 21.41728 25.6432 21.41728 381.00 0.0 19*0.5 50 Cue 010 5 23.56037 21.41728 25.77528 21.41728 381.00 0.0 19*0.5 5
0 5
0
-5 0
5 0
5 3---$--- 5-0 5----O
- l 1
- l l
f Docket No. 71-5450 initial Subelttal Dete:
12/20/85 Page No.19-42.8 Revision Submittal Date:,
4/28/86 Rev. NO.T
TA8LE 26 (CONTINUED) gU INPUT DATA IMAGE LIST CAAD 1
2 3
4 5
6 7
8 SEe.
5 0
5 0
5 3--- 5 ----0--- 5 ----0--- 5 ----0--- 5 ----0---- 5 ----O 51 00X TYPE 9 52 Cue 010 5 22.78758 22.69868 20.96019 20.15744 381.00 0.0 19*0.5 53 Cue 010 6 23.27018 22.21608 20.96019 20.15744 381.00 0.0 19*0.5 54 Cue 010 4 23.56037 21.87448 21.41728 20.15744 381.00 0.0 19*0.5 55 Cue 0I0 5 23.56037 21.41728 21.41728 20.15744 381.00 0.0 19*0.5 56 BOX TYPE 10 57 Cue 010 4
0.0
-20.32 1.25984 0.0 381.00 0.0 1G*0.5 58 Cue 010 5
0.0
-20.45208 1.25984 0.0 381.00 0.0 19*0.5 59 80X TYPE 11 60 Cue 010 4
0.0
-20.32 25.6432 21.41728 381.00 0.0 19*0.5 61 Cue 010 5
0.0
-20.45208 25.77528 21.41728 381.00 0.0 19*0.5 62 80X TYPE 12 63 cue 010 4
0.0
-20.32 0.0
-38.5572 381.00 0.0 19*0.5 64 Cue 010 5
0.0
-20.45208 0.0
-38.68928 381.00 0.0 19*0.5 65 1 2
18 1 2
18 1 1 1 1 0 66 2 7
13 3 4
4 1 1 1 1 0 67 2 5
15 10 5 5 1 1 1 1 0 68 2 4
16 3 7
7 1 1 1 1 0 69 2 4
16 3 10 10 1 1 1 1 0 70 2 4
16 3 13 13 1 1 1 1 0 71 2 5
15 10 15 15 1 1 1 1 0 72 2 7
13 3 16 16 1 1 1 1 0 73 3 19 19 1 1
1 1 1 1 1 0 74 4 2
18 1 1
1 1 1'1 1 0 75 5 19 19 1 3
17 1 1 1 1 0 76 6 19 19 1 2
2 1 1 1 1 0 77 7 2
18 1 19 19 1 1 1 1 0 78 8 19 19 1 19 19 1 1 1 1 0 79 9 19 19 1 18 18 1 1 1 1 0 80 10 1 1
1 2
18 1 1 1 1 0 81 11 1 1 1 19 19 1 1 1 1 0 82 12 1 1 1 1
1 1 1 1 1 1 83 -1 84 EMO KEM0 5
0 5
0 5
0 5----c 5---0---5 ----O --
5--0--5----O l
C
\\
l Docket No. 71-5450 Initial Submittal Date:
12/20/85 Page No._19_-42.9 l
Revision Submittal Date:
4/28/86 Rev. No. I i
I
\\
f ATDO9 TENT 22 OPERATING AIE) 10GNTElmHCE PPncyrunES i
4 i
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Docket No. 71-5450 initial Submittal Date: 12/20/85 Page No.22-1 t
Revision Submittal Date: 4/28/86_ Rev. No. T t
MECHANICAL OPERATING PROCEDURE FINAL ASSEWLY AREA O
PROCEDURE NO: M0P-730703
(/
ISSUE DATE: 8/1/85 i
REVISION:
7 FINAL APPROVAL:W / h f~ rxA m o PAGE:
1 of 3 CONTROLLED COPY:
TITLE: PREPARE CONTAINER FOR LOADING FUEL ASSEMBLIES
1.0 PURPOSE
To specify steps in preparing container for loading fuel assemblies.
2.0 REFERENCES
2.1 Replaces Procedure OP 730703, Rev. 6.
TEMS/ DEFINIT 10ES:i #6he. A..';-
3.0 4.0 RESP 0ldlBI feh:
g..-
4.1 Quality Control Personnel:
1.
Release shipping container for loading.
I 2.
Verify correct number of shock mounts installed.
4.2 Area Supervisor: Verify shock mounts, locking pins, and stabilizing bar.
5.0 REGULATORY REQUIREMENTS: None.
6.0 SPECIAL PRECAUTIONS: None.
7.0 PROCEDURE
1.
VERIFY SHIPPING CONTAINER IS QUALITY CONTROL-RELEASED FOR LOADING.
2.
REMOVE VALVE STEM AND ALLOW PRESSURE TO EQUALIZE.
3.
LOOSEN CONTAl'NER CLOSURE BOLTS.
4.
OPEN OUTRIGGER SUPPORTS AND LOCK IN PLACE, IF APPLICABLE.
(Adjust footpass for firm floor contact.)
5.
REMOVE COVER.
6.
OPEN PADS AND CLAMPS, VERIFYING CLAMP COUNT.
(1 set support plates and 1 clamping frame per grid.)
7.
OPEN CLAWING FRAMES AND SWING OUT PRESSURE PAOS.
8.
LOOSEN SWING BOLT CLAMP AND SWING CLEAR. AS NECESSARY.
9.
SECURE STA81LIZER BARS.
1
- 10. REQUEST GUAllTY CONTROL TO VERIFY CORRECT NUWER OF SHOCK MOUNTS INSTALLED.
- 11. REMOVE FLAT TYPE CROSS 8ARS FROM TOP CLOSURE FRAMES AND REPLACE WITH i
ROUND RECESSED TYPE.
(17 x 17 with spider type core components assemblies only.)
(Model C assemblies only.)
- 13. REMOVE LOCKING PIN AND SLIDE LATERAL CROSS 8ARS UNTIL RESTING ON SUPPORT O
PADS.
I WP-0095A t
MECHANICAL OPERATING PROCEDURE PROCEDURE NO: MOP-730703 FINAL ASSEMBLY AREA REVISION:
7 ISSUE DATE: 8/1/85 PAGE:
2 of 3
7.0 PROCEDURE
(Continued) 14.
TIGHTEN BOLT TO SECURE BARS.
(Use crane lift cradle, if necessary.)
- 15. ATTACH JACKING HUTS FACING PRESSURE PAD.
(See Attachment 8.1.)
- 16. RELEASE CLAMPING FRAME NUTS JUST UNTIL FRAME OPENS.
(See Attachment 8.1.)
- 17. REMOVE TOP PINS AND SWING TO OPEN POSITION.
- 18. ATTACH CRANE TO LIFTING EYE OF SUPPORT FRAME.
- 19. LIFT SUPPORT FRAME TO VERTICAL.
20.
INSTALL STABILIZING BARS AND SECURE WITH LOCKING PINS.
(Notify Supervisor if pins not easily inserted.)
- 21. REMOVE CRANE HOOK.
22.
INSTALL PROTECTIVE MAT AT STRJNG8ACK BOTTON.
- 23. OPEN EACH CLAMPING FRAME; RETRACT PRESSURE PADS AS FAR AS JACKING NUT ALLOWS ON SIDE TO BE LOADED.
(Start at top, work down.)
24.
INSTALL ALUMINUM SPACERS ON BOTTOM BASE PLATE SUPPORT FRAME FOR MODEL C ASSEMBLlES.
- 25. RECORD MOP REVISION NuneER, INITIALS, AND DATE ON ROUTING.
8.0 ATTACHMENT
8.1 Fuel Assembly Clamping Frame Sketch.
e O
WP-0095A i
i W CHANICAL OPERATING PROCEDURE PROCEDURE NO: MOP-730703 FINAL ASSEMBLY AREA REVISION:
7 l
ISSUE DATE: S/1/85 GE:
3 of 3 PA 4
8.1 Fuel Assembly Clamping Fraine Sketch.
WW 5
Y IOCKING NUT I
b f
7
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WP-0095A
MECHANICAL OPERATING PROCEDURE FINAL ASSEMBLY AREA f
PROCEDURE NO: M0P-730706 ISSUE DATE: 8/i/85 REVISION:
7 FINAL APPROVAL:
PAGE:
1 of 2 V
/
CONTROLLED COPY:
COM@
T T E: CLOSE SHIPPING CONTAINERS
1.0 PURPOSE
To specify steps to close shipping containers.
2.0 REFERENCES
2.1 Replaces Procedure OP 730706, Rev. 6.
3.0 TERMS / DEFINITIONS: None.
4.0 RESPONSI81LITIES
4.1 Quality Control Inspector; 1.
Witness centamer cover installation.
'2.
inspect locked bolts.
4.2 Final Assembly Area Supervisor: Furnish proper metal seals and seal O
iiiaenmentparts.
L' 5.0 REGULA1_0RY REQUIREMENTS: None.
6.0 SPECIAL PRECAUTIONS: Nci.t.
7.0 PROCEDURE
7.1 PREPARATION
1.
ASSEMBLE THE FOLLOWING APPROVED TOOLS:
a.
1/32-INCH DIAMETER, 1x19 STAINLESS STEEL WIRE OR EQUlVALENT.
b.
NICR0 PRESS #27-1-B SLEEVES OR EQUlVALENT.
c.
NICR0 PRESS CRIMP TOOL #17-2.
d.
WlRE CUTTER.
7.2 CLOSE SHIPPING CONTAINER:
1.
ENSURE T BOLTS AllGNED.
2.
INSTALL CONTAINER COVER.
(Ouality Control must observe installation.)
3.
TIGHTEN SWING OR T BOLTS.
(Until lock washers are flattened.)
4.
VERIFY CAMLOCK BOLTS SECURELY FASTENED, IF USED.
5.
REPLACE ALL DEFECTIVE BOLTS.
6.
REQUEST 00AllTY CONTROL TO INSPECT LOCKED BOLTS.
WP-0080A
MECHANICAL OPERATING PROCEDURE PROCEDURE NO: MOP-730706 FINAL ASSEMBLY AREA REVISION:
7 7s i
ISSUE DATE: 8/1/85 PAGE:
2 of 2 V
7.2 CLOSE SHIPPING CONTAINER; (Continued) 7.
OBTAIN SEAL AND SEAL ATTACHMENT PARTS FROM SUPERVISOR.
8.
ENTER REQUIRED INFORMATION IN SEAL LOGBOOK:
a.
SEAL NUMBER.
b.
CONTRACT IDENTIFICATION.
c.
FUEL ASSEMBLY SERIAL NUMBER.
d.
CONTAINER NUMBER.
e.
OPERATOR INITIALS OR BADGE NUMBER.
f.
DATE AND TIME.
9.
INSTALL 1 SEAL ON EACH END OF CONTAINER.
(Use approved Nicropress crimping tool.)
10.
CUT OFF EXCESS WIRE.
11.
PRESS ON SEAL COVER PLATE SECURELY.
12.
RECORD MOP REVISION NUMBER, INITIALS, AND DATE ON ROUTING.
7.3 ABNORMAL EVENTS:
1.
IF A SEAL IS DESTROYED:
A.
ENTER SEAL NUMBER ON SEAL LOG DISPOSAL SHEET.
8.
ENTER INITIALS OR BADGE NUMBER AND DATE ON SEAL LOG DISPOSAL SHEET.
2.
IF SHIPPING CONTAINER MUST BE OPENED AFTER SEALING:
(-'S A.
ENTER INITIALS OR BADGE NUMBER AND DATE ON SEAL DISPOSAL SHEET BESIDE PROPER SEAL NUMBER.
B.
REPEAT STEPS 7.2.7-12.
8.0 ATTACHMENTS
None.
(_ >
WP-0080A
UhCONTROLLED CO?X MANUFACTURING OPERATING PROCEDURE Fl,NAL ASSEMBLY AREA g)
(
k/
ISSUE DATE:
11/11/8 PROCEDURE N0: MOP-730713
/
REVISION:
19 e
FINAL APPROVAL:
()
PAGE:
1 of 4 i
/
CONTROLLED COPY:
TITLE:
LOAD FUEL ASSEMBLY INTO SHIPPING CONTAINERS
1.0 PURPOSE
To specify the steps to load fuel assembly into shipping containers.
2.0 REFERENCES
2.1 Replaces Procet re OP-730713 'Rev. 18.
2.2 Procedure OP 730712. " Wrap Fuel Assembly or Skeleton for Shipment."
2.3 Procedure OP 735502. " Handling Fixture Procedure" 2.4 Columbia Shipping Schedule.
3.0 TERMS / DEFINITIONS:
3.1 Accelerometer
Device placed in shipping container to record a significant jolt during shipping.
Gadolinium: Metal used in high enriched fuel shipping container to absorb
/ ) 3.2 neutrons and keep container critically safe.
'v' 3.3 Yellow Dot Shipping Container:S/C:
Shipping conta;ner marking for high-enriched fuel.
4.0 RESPONSl81LiTIES
4.1 Ouality Control inspector:
Verify torque readings.
4.2 Area Supervisor: Verify proper shipping container.
5.0 REGULATORY REOUIREMENTS: None.
6.0 SPECIAL PRECAUTIONS:
6.1 VERIFY PROPER SHIPPING CONTAINFR FOR CONTRACT BEFORE PACKING.
6.2 USE ONLY " YELLOW 00T" SHIPPING CONTAINERS WITH GADOLINIUM ABSORBER PLATES FOR HIGH ENRICHMENT FUEL, DESIGNATED BY ASTERISKS ON SHIPPING SCHEDULES.
6.3 ENSURE BALLAST IS EQUAL IN WEIGHT TO FUEL ASSEMBLY TO WITHIN 200 LBS.
6.4 00 NOT OVERTIGHTEN JACKING NUTS OR ASSEMBLY COULD BE DAMAGED.
6.5 ENSURE QUALITY CONTROL HAS REMOVED WRAPPER AND PERFORMED SPECIAL INSPECTION IF ASSEMBLV STORED LONGER THAN 6 MONTHS.
6.6 ENSURE BOTTOM SPACER 2654C60 IS ON BOTTOM SUPPORT FOR MODEL C'S.
6.7 ENSURE PLASTIC WRAPPER EXTENDS APPROXIMATELY 6 INCHES ABOVE TOP N0ZZLE.
7.0 PROCEDURE
O) 1.
ATTACH CRANE TO FUEL ASSEMBLY PER PROCEDURE MOP-735502.
(#
2.
RAISE ASSEMBLY AND INSPECT PLASTIC WRAPPE.R AND REPLACE IF NECESSARY PER PROCEDURE M0P-730712.
3.
PLACE ASSEMBLY SO "Y" CORNER IS IN SUPPORT FRAME CORNER.
(Except Model C)
WP-0192A
UNCONTROLLED 00PX PROCEDURE NO: MOP-730713 MECHANICAL CPERATING PROCEDURE REVISION:
19 FINAL ASSEMBLY AREA PAGE 2 of 4 (v)ggstsDATE:
11/11/95
7.0 PROCEDURE
(Continued)
ORIENT MODEL C ASSEMBLIES PER ATTACHMENT 8.1.
l 4.
LIFT ASSEMBLY UNTIL BOTTOM CLEARS CONTAINER SHELL, MAINTAINING 5.
ORIENTATION.
6.
MOVE ASSEMBLY INTO SUPPORT FRAME.
PRESS ASSEMBLY FLUSH AGAINST SUPPORT FRAME CORNER.
7.
(Press Against grid) 8.
LOWER ASSEMBLY TO CONTACT BOTTOM SUPPORT.
AllGN CLAMPING FRAMES TO GRIOS.
9.
ENSURE ONLY 1 THICKNESS OF PLASTIC BETWEEN PRESSURE PAD AND ASSEMB 10.
(No pressure pads used for Vantage V.)
11.
TIGHTEN PRESSURE PAOS AND SECURE CLAMPS.
OETACH CRANE AND MOVE LIFTING TOOL FROM ASSEMBLY.
12.
OPEN CLAMPING FRAMES AND RETRACT PRESSURE PAOS ON OTHER CONTAIN 13.
REPEAT STEPS 7.1.1-12 TO LOAD SECONO ASSEMBLY. AS NECESSARY.
14.
15.
INSTALL BALLAST IN OTHER SUPPORT FRAME, AS REQUIRED.
(Unless dummy is being shipped.)
ATTACH CRANE TO EYE ON FRAME TOP AND REMOVE SLACK.
16.
- 17. REMOVE DIRT AND FOREIGN MATTER FROM CONTAINER SHELL.
(Container must be clean.)
OETACH AND LOWER STA8ill2ER BARS.
18.
PLACE SUPPORT BAR ACROSS CONTAINER NEAR TOP ANO LOWER STRONG 8 19.
- 20. RESET SUPPORT BAR WITH FRAME SUPPORT HORIZONTAL.
(Crane cable vertical.)
]
RETRACT OUTRIGGERS AND LOCK IN PLACE i,
21.
s_
CLOSE TOP CLOSURE ASSEMBLIES AND INSTALL LOCF iNG PINS.
23.
CONTACT FUEL ASSEMBLY AND CORE COMPONENT WITH HOLD 00WN BOLTS.
24.
(Wrapper between clamp screw pads and components.l
'25.
LIFT SUPPORT FRAME AND REMOVE TOP LATERAL SUPPORT.
PIN STABILIZER BARS IN STORAGE POSITION.
26
- 27. MOVE CRANE. ATTACH TO LOWER END OF CRAOLE ASSEMBLY AND HOIST RETRACT LATERAL CROSSBARS AND INSTALL LOCKING PINS.
28.
TOROUE SIDE, THEN TOP PRESSURE PADS TO 48 INCH-POUNOS 29.
(Use dial torque wrench and cronfoot adapter SMA-2329.)
- 30. RETOR00E TO 72 IN-LBS.
- 31. SECURE LOCK NUTS AND TIGHTEN UNill JACK SCREW JAMMEO.
- 32. ENGAGE AND TIGHTEN SWING BOLT CLAMPS,
- 33. TOR 00E SWING 80LT CLAMPS TO 60 IN.-LOS.
- 34. VERIFY NO ACCEL.ER0 METERS TRIPPED.
- 35. RECORO REVISION NUMBER, INITIAL ANO DATE ROUTING.
- 36. CHECK "PACKE0': ON "F/A STATUS TICKET". INITIAL AND DATE.
- 37. PLACE TICKET IN HOLDER.
8.0 ATTACHMENTS; 8.1 Model C Assembly Orientation 8.2 Frame Joint Seating WP-0192A
UNCONTROLLED COP 1 PROCEDURE NO: WOP-730713 MECHANICAL OPERATING PROCEDURE REVISION:
tg O
FINAL ASSEWLY AREA PAGE 3 of 4 IS3UE DATE:
11/11/85 8.1 Wodel C Assembly Orientation G
c)/N 5/4 M
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LEFT ms4T BOTTOM END
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WP-0192A t
UNONTROLLED UUPJ.
PROCEDURE NO: MOP-730713 MECHANICAL OPERATING PROCEDURE REVISION:
19 FINAL ASSE W LY AREA 4 OI 4 ISSUE DATE:
11/11/85 8.2 Frame Joint Seating
=
CLAMPING FRAME FASTENER MIT (CCKING NUT (TIGHTEN FIRST)
JACKING NUT jg
/
o' N
i a
b PRESSURE P 0 7
"")
l c
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o g
x JACKING NUT O
WP-0192A
UNGUNIKULLLU1Ur_t MECHANICAL OPEPATlNG PROCEDURE FINAL ASSEMBLY AREA PROCEDURE NO: M0P-736902 O
ISSUE DATE: 11-11485 REVISION:
3 FINALAPPROVAL:{
PAGE:
1 of 2 CONTROLLED COPY:
REMOVE FUEL ASSEMBLY FROM SHIPPING CONTAINER TITLE:
1.0 PURPOSE; To specify steps for removing fuel assembly from shipping contup"Mf.
2.0 REFERENCES
2.1 Replaces Procedure OP 736902, Rev.
2.
M0P-735502, " Handling Fixture Pro::edure".
M0P-730708, " Moving Fuel Assembly in end Out of Storage Racks -- General" 2.2 2.3 3.0 TERMS / DEFINITIONS: None.
4.0 RESPONSIBILITIES; Receive debris from shipping container.
4.1 Ouality Control Inspector:
5.0 REGULATORY REQUIREMENTS: None.
SPECIAL PRECAUTIONS:..............................................................................
6.0 WATCH FOR DEBRIS FROM FUEL ASSEMBLY; COLLECT AND SUBMIT TO 00AllTY CON 6.1 WITH FUEL ASSEMBLY NUMBER...............................................................
7.0 PROCEDURE
BLEED PRESSURE FROM SHIPPING CONTAINER.
1.
LOOSEN CONTAINER CLOSURE FASTENER HARDWARE AND REMOVE C 2.
OPEN OUTSIDE OUTRIGGERS AND LOCK IN PLACE.
3.
LOCK IN PLACE USING HARDWARE PROVIDED.
4.
(Adjust as required to obtain firm contact with floor.)
REMOVE LOCKING PIN FROM LATERAL CROSS 8ARS.
SLIDE CROSS 8ARS FROM HOUSING UNTil THE REST ON SU 5.
6.
ASSEW LY.
TIGHTEN SCREW ON SUPPORT PAD BRACKETS.
7.
USE CRANE LIFT CRADLE ASSEMBLY, IF REQUIRED.
LOOSEN SWINCSOLT CLAMPS ANO SilNG FREE OF FUEL AS 8.
9.
ATTACH CRANE TO FORWARD LIFT EYE.
REMOVE TOP SECURING PINS AND SWING SUPPORTS FREE O 10.
11.
- 12. LIFT SUPPORT FRAME TO VERTICAL POSITION.
~
13.
INSTALL AND SECURE STABILIZING BARS: DISCONNECT CRANE H
~
4 WP-0082A 1
UNCONTROLLiu C0gEDURE NO:MOP-736902 MECHANICAL OPERATING PROCEDURE REVISION:
3 FINAL ASSEMBLY AREA PAGE:
2 of 2 ISSUE DATE:
11-11-85
7.0 PROCEDURE
(Continued) i CENTER CRANE HOOK 6-12 INCHES ABOVE FUEL ASSEMBLY.
14.
INSTALL FIXTURE LIFTING TOOL USING M0P-735502.
(Loop doubled nylon strap through eye bolt to crane hook.)
15.
REMOVE STRAP SLACK.
16.
OPEN ALL FUEL ASSEMBLY CLAMPING FRAMES.
I 17.
MOVE FUEL ASSEM8LY CAREFULLY OUT OF SHIPPING CONTAINE OR CONTINUE 18.
PLACE ASSEMBLY IN STORAGE RACK USING MOP-730708 19, PROCESSING PER ROUTING.
8.0 ATTACHMENTS
None.
1 e
O I'
l O
WP-0082A
UNCONTROLLEDQ1 MECHANICAL OPERATlNG PROCE FINAL ASSEMBLY AREA ISSUE DATE: 9-8-85 I
PROCEDURE NO: MOP-736904 REVISION:
1
"/
PAGE:
1 of 1 FINAL APPROVAL:
f v
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CONTROLLED COPY:
/
TITLE: LOADFUE(ROOBOXINTOSHIPPINGCONTAINER 1.0 PURPOSE _:_
To specify steps to load fuel rod box into shipping container.
2.0 REFERENCES
2.1 Replaces Procedure OP-736904, Rev. O.
3.0 TEfutS/ DEFINITIONS: None.
4.0 RESPONSIBILITIES
None.
5.0 REGULATORY REQUIREMENTS: None.
~~' -
6.0 SPECIAL PRECAUTIONS: None.
7.0 PROCEDURE
1.
ASSEWLE THE FOLLOWING APPROVED TOOLS:
a.
SPREADER BAR (SKC-1567) OR EQUIVALENT b.
6-INCH X 10-INCH X 1/4-INCH BOARD.
2.
PLACE R00 BOX ON SHIPPING CONTAINER STRONGBACK.
(Lid latches toward outside of containers.)
3.
PLACE BOARD BETWEEN ROD BOX HANDLE BASE AND CONTAINER BOTTOM SUPPORT.
4.
POSITION BOX FIRMLY AGAINST STRONGBACK CENTER AND BOTTOM SUPPORT.
(Width 1/4-inch spacer.)
5.
LEAVE LIFTING HANDLES VERTICAL.
6.
TIGHTEN JACK SCREWS AM) PAOS IN CLOSURE BARS AGAINST END OF A00 CC 3AINER BOX.
7.
LOATE CLAWING FRAMES SO PRESSURE PAOS CONTACT R00 BOX REINFORC"*cNT SPACERS.
(6 clampi frames.)
8.
TIGiTEN ALL PRE PADS FIRMLY AGAINST ROO BOX.
l 8.0 ATTACl4 SffS: None.
O WP-0802A
I MECHANICAL OPERATING PROCEDURE CONTAINER AND SHIPPING AREA ISSUE DATE: 8/3/85 PROCEDURE NO: M0P-755707 REVISION:
9 FINAL APPROVAL
- M Z E_
_A 7:rv Taun PAGE:
1 of 8 CONTROLLED COPY-L REFURBISHING SHIPPING CONTA dh TlTLE:
\\
1.0 PURPOSE
To specify steps to refurbish shippingM6Htainers.
2.0 REFERENCES
2.1 Replaces Procedure OP 755707, Rev. 8.
,,2. 2 MOP-755730 (OP 755730), " Installing Cork S;iacer on Container Strongback."
3.0 TEfWS/ DEFINITIONS:
3.1 Shim: Thin pieces of metal used for spacing and positioning.
4.0 RESPONSIBILITIES
4.1 Traffic Administrator: Determine type of assembly to be shipped next.
4.2 Fuel Assembly Quality Control:
Give approval for removal of red tags, as necessary.
5.0 REGULATORY REQUIREMENTS: None.'
6.0 SPECIAL PRECAUTIONS:
6.1 DO NOT REMOVE FED TAGS FROM CONTAINER WITHOUT APPROVAL OF AREA QUALITY CONTROL.
6.2 CLEAN AND PAINT ANY AREAS WELDED DURING PROCEDURE.
6.3 MOVE CONTAINER INSIDE BUILDING IF ANY REPAlRS ARE NEEDED TO INTERIOR OF CONTAINER BASE.
7.0 PROCEDURE
1.
VERIFY CONTAINER IS CLEAN.
2.
WASH CONTAINER AS DIRECTED BY SUPERVISOR.
A.
USE F0fELIFT TO MOVE CONTAINER TO WASH AREA.
8.
WASH CONTAINER WITH SOAP AND WATER.
(Use brush as necessary.)
3.
CHECK THE CONTAINER'S EXTERIOR CONDITION.
4.
REMOVE OLD PLACARDS AND LABELS.
5.
MAKE NECESSARY REPAIRS TO OUTSIDE OF CONTAINER.
(Refer to Drawings 617F (160") or 617F706 (137") for detail.)
6.
LOOSEN CLOSLEE FASTENERS AND REMOVE COVER.
i j
WP-0055A i
I MECHANICAL OPERATING PROCEDURE PROCEDURE NO: M0P-755707 CONTAINER AND SHIPPING AREA REVISION:
9 ISSUE DATE: 8/3/85 PAGE:
2 of 8
7.0 PROCEDURE
(Continued) 7.
CHECKCONDITIONOFFASTENERSANdhEPAIRASNECESSARY:
~
a.
T-BOLTS AND SWING-BOLT:
CHECK THREAD CONDITION, REPLAC' NG ANY THAT l
WOULD REQUIRE UNUSUAL TOROUE TO TIGHTEN; REPLAC
- 5. DEFORMED, DISH-SHAPED WASHERS OR ANY NUTS WITH ROUNDED b.
CAM-LOCK BOLT:
CHECK FOR BROKEN.
ISSING PARTS.
INCLUDING CAM LATCH SPRING UNDER 00 8.
CHECK CONDITION OF INSIDE COVER AND
- ESSARY.
9.
DETERMINE NEXT TYPE OF FUEL ASSE IPPED IN CONTAINER.
- 10. DECIDE NUMBER AND POSIT 10NING OF MOUNTS AND CLAMPING FRAMES.
- 11. USE A PAD GAGE TO LOCATE CLAMPlNG FRAMES.
- 13. CHECK PADS FOR PROPER AMOUNT OF CORK AND LOCATION.
(See attached ch' art for location.)
(Use space block in bottom of container for short assemblies, C9565014 and 2654C60.)
- 15. REFU98ISH, IF NEEDED, WITH 1/4-INCH CORK PER PROCEDURE MOP 755730.
..., 16. CHECK CORK ON STRONGBACK, REPLACING AS NECESSARY.
- 17. CHECK INTERNAL HARDWARE FOR DAMAGE AND REPLACE AS NECESSARY.
- 18. CHECK SHOCK MOUNTS FOR NUEER AND LOCATION.
(Refer to Attachment 8.1.)
CLEANING OR REPAIRING AS NEEDED.
\\
- 20. CLEAN CONTAINER.
- 21.. RECORD M0P REVISION NUW ER,. INITIALS, AND DATE ON ROUTING.
8.0 ATTACHMENTS
8.1 Shock Mount Designations Sketch.
8.2 Shock Mount Utilization Chart.
8.3 Fuel Assembly Container Condition Checklist.
8.4 Pad Identification Chart.
e f
U WP-0055A
ECHANICAL. OPERATING PROCEDURE PROCEDURE NO: MOP-755707
[
CONTAINER Afe SHIPPING AREA V SiON:
8/3/85 of 8 l
O ISSUE DATE:
8.1 Shock Mount Designations Sketch.
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q r
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A[ I5[ A lll l l I I 3 Iii IS[ 3 111 1(l l l I i l 4 lit ill 2 11l 11) 2 111 %) 1.- - 111 111 1 111 tl1 ~ n n n n '~ 3 u _ __ _ _._ _ J t __ _ _ _ _ _ _ _ a RCC-1 RCC -3 O 9 WP-0055A
l MECHANICAL OPERATING PROCEDURE PROCEDURE NO: MOP-755707 O CONTAINER Am SHIPPING AREA REVISION: 9 V ISSUE DATE: 8/3/85 PAGE: 4 of 8 8.2 Shock Mount Utilization Chart. ~ SHOCK MOUNT UTILIZATION The number of shock mounts required for each design is e ad regardless of presence or absence the fuel FUEL ASSEIER.Y TYPE MOUNTS UTILIZE 0 14X14 10 Ft. 14 14X14 12 Ft. STANDAR0 16 ~ 14X14 12 Ft. OPTIMlZED 16 15X15 12 Ft. 18 } 16X16 12 Ft. 18 17X17 12 Ft. STANDARD 18 17X17 12 Ft. OPTIMlZED 18 17X17 XL 14 Ft. N/A 14X14 8 Ft. 14 14X14 MODEL C 16 f l Shock mounts shall be removed only in opposing pairs. Single mount removal is i not permitted. Remove shock mount pairs to achieve " mounts utilized", above, according to the following tablec SEE FIGURE 1. l MOUNTS UTILIZED RCC-1 CONTAINER RCC-3 CONTAINER O 18 NONE AND V 16 A AND A i l WP-0055A 14 A&8 A AND B l l
MECHANICAL OPERATING PROCEDURE PROCEDURE NO: M0P-755707 CONTAINER A M SHIPPING AREA REVISION: 9 /O ISSUE DATE: 8/3/85 PAGE: 5 of 8 O 8.3 Fuel Assembly Container Condition Checklist, Page 1 of 2. Page 1 Of 2 p b C0r.TA I 1a N TE OPERATOR ma
- FUEL ASSEnELY CONTAINEA CON 0tflCM uV i T E Id '
INITIAL 1.) Verify Container Esternal Surface Cleanlinese i 2.) Check Fog Obvious Cefects Of Damage To Container Esterior 3.) Verify Acceptable Condetson: (a.) Container Base - Exterior And Interior (b.) Container Lid. Esterior And Interior 4.). Verify Container is Stenciled Properly Container Markings: (a.) Veri fy That D.O.T. License Plate is Present tone Eacn Side Opposste Ends) O y I\\ (b.) Veri fy That Name Pf ate is Present (5*
- 5*1 l
5.) Verify That Humidity anoicator Glass es Jainteo e t3tue .f Acolicable) 6.) Veri fy That The Air Valve Stem is Present And in Good Jondi tion 7.) Verify That Air Valve Slotted Type Cap is Present And in Good Condition 8.) Verify That The Reseef Valve is in Good Concation 9.) Verify Cover Plate is Secured setn The Fosicaing nardware: (a.) 2 - 5/16 18 SS Wingnuts 1 ...____________._________......i....-g (b.I 2 - 5/16 SS Lockwashers (c.) 2 - 5/16 SS Flatsashers l l I 0.) Skies - 4t. Oronen or rotten smids are to ne replacea. 14:os j nust be Uniform in Thickness. If Splits Are Greater Than 2" Oeen ; i l and Aun The Full t.enoth Of The Sk d. It *;st Be Ge=taced. I 8 11.) Veri fy That All Skid Bot ts Are Securea Taght 12.) Veri fy Outrigger... (a) Presence I (b) Condition (c) Pads Operable By Hand O WP-0055A
I MECHANICAL OPERATING PROCEDURE PROCEDURE NO: MOP-755707 i p CONTAINER AND SHIPPING AREA REVISION: 9 Q ISSUE DATE: 8/ V85 PAGE: 6 of 8 8.3 Fuel Assembly Container Condition Checklist, Page 2 of 2. j 1 l Page 2 Of 2 g 'FLEL ASSEMBLY CONTAINER CCNOIT:CN CHE~X LIST AO I TEW W intilAL 13.) 9egaer Defects On QCON From Site Surveis.a g W - 1a. verify That A Calibratec Accelerometer is Attacneo At Eacn End Of The. Container Stronceack 1 15.s varaty That Two Ciceer Or Gacolonium Absorcer Plates Are Present l Gadolinium Plates Wust Be painted Around Edoes to prevent Rustino. 16.) Checa Clamping Frames --- (a.s Position (b.) Cork Pads (c.) Condition 3f hardware I 17.) Veri fy Presence And Condition Of Lockerig Pins And dire 18.) Vers fy Presence And Condition Of Swingboits And Hardware (Acoly Lubriolate To Camlock Bolts And swing Bolts As Necessaryl 19.) vers fy Presence Ana Conds: son Of Support Pac Stacket Solts (% 20.) verify Presence Ano Condition Of vertican Stanelizing aar Solts j (u) I 21.1 Checa For sater in Bottom Of Container , 22.8 Top End Clamping Asaemoly-1 (a.) Condition 86olt Heads '60t Rounded And Threaos Not Stricce1 Or Burred) (b.) Bolts And Pads 14) (e.) RCC Soit And Pad 23.) Clean lasnet Slot On Base And Flange C f 1.id 1 24.) Verify Container is Clean And Ory -- ta. Base l i f (b ) Lid NOTE-WITHCUT 1AIS..'I i 40%C52Cx 25.7 ter ff Presence Of Holes For Seals Ah Container Enos Ano e..3 I Clamoine Channe6 26.1 ver fy Tnat Absorcer Plate Clancing Channel is Painted veti.:. one, i ,l 24 dol;nium Absorber Plates Are used. 27.i te rff That At. sorter Plate ;iamoing Charnel Has 3een Sea ea aten re. :n. Claros And Cadolinium Plates Are Being 'Ised. f Ihat 21/2 :cen Yellow Oot is painted On Container Sear Ine l 28.s te..f Canta ner Nuncer shen Gadolinium plates Are Used O WP-0055A
WECHANICAL OPERATING PROCEDURE PROCEDURE NO: MOP-755707 CONTAINER AND SHIPPING AREA REVISION: 9 p ISSUE DATE: 8/ V85 PAGE: 7 of 8 V 8.4 Pad Identification Chart, Page 1 of 2. PAGE 1 N k 1 CCNTAACT i ASSEMBLY TvPE i GRIOS I DAD _ s ( Bu. 6 fM 1 ht ALEF 17X17 12 FT STD i 8 ALFF 17X17 12 FT 570. 6 8 LK11 KUW" AP8F 17X17 12 FT. STD. l. Arm,P - APCF 17117 12 FT. STD.tu A.lBri, ARCF 17X17 12 FT. f,TD.1HF Blu ! ASAF 17X17 12 FT. bTD. " 8 8Lu ! AS8F 17X17 12 FT. STD. 8 8Ltt CAAF 17X 17 12 FT. OPT. 8 BL'.6 ANO sHITE C3F 17X17 12 FT. 570. 8 BLu1' COGF 15X15 12 FT. STD. T BLu ! CONF 15X15 12 FT. OPT. 7-BLui Am WHITE CaiF 15X15 12 FT. OPT. 7 BLUG ANO sHITE = CsGF 15X15 12 FT. STD. 7 BLUM CsMF 15X15 12 FT. OPT. 7 BLUNANDW TH CWIF 15X15 12 FT. OPT. 7 BLtfi AND WHITE OA8F 17X17 10 FT. OPT 8 BLUE AW StiTE 04CF t 17X17 10 FT. OPT. 8 8LUE A2 WHITE 08AF i 17317 12 FT, STO. 0 8LUE OCAF i 17X17 12 FT. OPT. 0 BLUE Am #44TE Ot.CF 17X17 12 FT. STD. 0 SLUE 3LOF 17X17 12 FT. f;TD. 8 i BLUE OLEF i 17X17 12 FT. 1,TD. 8 BLUE FFAF i 17X17 12 FT. STD. 8 i SLUE i FL,F 1 t$X15 12 FT. STD 7
- P.,
FL.F 15:15 121:T. OPT. 7 i SL'. ANO sHITE I FF'F i 15X15 12 FT. STD 7 8LL: i 7 BL'..E ANO sHI TE F3)F 6 ?5A15 12 FT. OPT FP4F i 15X 15 12 F T. OP T. 7 BL.E ANO eHITE INEF 15X15 12 FT. STO i 7 StuE 9-BLUE iP8F 15X15 12 FT. 4 P7 15X15 12 FT. 9 8LUE t K0DF 14X14 12 FT. STD 7 YELLCs MOEF 14X14 12 FT. ST). 7 YELLCe MOFF 14X14 12 FT. ST). 7 i VELLCs MO@ 14X14 12 FT. ST). 7 VELLCe MPAF 16X11 12 F" STO. 8 AED MF8F 16X1i 12 F" STD 8 AED MlWF 16X 11 12 Fr STD. 8 i AED i LEAF I TX17 12 FT.*!,TD 8 BLUE f t.53 F 17X17 12 FT. !,TD. 8 BLUE i LiCF 17X17 12 FT. STO. 8 SLUE i LECF 17X17 12 FT. STD l i ! BLUC 4 BLuti t0AF i 17X17 12 FT. f;TD 1 > LOSF 6 ITX17 12 FT. bTD 6 li i eLut shore BM and SHIM esds are used for 17:17 and 15x15 OM., the top and bottom grid pads are BJ_U.E and tne WHITE pode are for all center (Optimized) grids. Where SLACK and YELLOW pads are used for 14:14 OPT., the BLACK pads are for the center (Optimized) grids and the VELLOW pade re for the top and Dotton grids. l i \\\\ WP-0055A
I MECHANICAL OPERATING PROCEDURE PROCEDURE NO: WOP-755707 p CONTAINER Ale SHIPPING AREA REVISION: 9 Q ISSUE DATE: 8/3/85 PAGE: 8 of 8 8.4 Pad identification Chart, Page 2 of 2. .A CONrpACT i ASSEWLV TYPE GRIDS.A T LMBW" NDEF 14x14 WOCEL C 6. AKTM r - NOFF 14x14 WOCEL C a tm AJ'GIE.M NOGF 14:14 WODEL C MV GRER4 NOLF 14X14 to FT. 7 YELLOW NOW 14X14 to FT. 7 YELLOW NONF 14X14 to FT. 7 YELLOW %0F 14X14 10 FT. 7 YELLCW l PE8F 17X17 12 FT. STD 8 6LU' e PG8F 17X17 12 FT. STD. 8' 8LU ! l PGCF 17X'7 12 FT. STO. 8 BLU ! PN8F 17X17 12 FT. SfD. 8 BLU ! POEF 17X17 12 FT. STD. 8 SLU ! POFE I 1 X17 10 FT. STD. 8 Ellui ! i PSOF i 17 17 't FT. STO. 8 E.LU ! PSEF , 17X17 12 FT. STD. 8 ( LU ! PSFF i 17X17 12 FT. STD. 8 t.LU! ~ f s SAAF i 17X17 '2 FT. STD. t i. 8LUE 17X17 22 FT. 570. I L BLUE SCAF YELLOW O SONF i texte 'O FT. i l \\ sot.: 7 YELLOW . 14:14 'O FT. i i l TBAF i 17X17 '2 ST. STD. ! d SLUE TE3F
- 17X17 12 87. STD.
4 ! BL ' 7Gaf i 17xi7 14 FT tL
- 0 BL..
r4BF i 17x17 12 FT. STD. 8 BLJ 8 8L.E TVCF 6 17x17 12 FT. STO TsAF i 17X17 2 FT. OPT. 4 8LLE ANO sHITE TxAF i 17X17 2 FT. OPT. ! 8 .aLUE ANO eMITE UELF 14X14 Il FT. 6 fELLCW UE4F 14X14 4. FT. 6 YELLCe UEasF 14X14 < FT. 6 YELLCW UEOF 14X14 i i FT. t 6 YELLCe 6 VW 17X17 12 FT. 5T1). 8 BLUE VOCF 17X17 12 FT. ST1). 8 BLUE VIFF 15X15 12 FT. ST). 7 8LLE vi@ 15X15 12 FT. ST). 7 BLUE VP@ 15X15 17 FT. ST). 6 7 8LUE VFHF 15X 15 12 FT. ST ). 4 7 8LUE Vf4)F 17X17 12 FT? STD. e i 8LUE j VREF 17X17 12 FT. STO. i l l BLUE I sABF 17X17 12 FT. STD 4 l l BLUE ~ slBF 17X17 12 FT ;,70 i i i 8LUE sEnF i 14X14 12 FT. ? YELLCs l sELF ! 14X14 12 FT. OPT. I 7 BLACM & YELL 0s j sEMF 14X14 12 FT. OPT. 7 SLACK & YELL 0s ' steF
- 14X14 12 FT. STD.
7 VELLGW slaF e 14X14 12 FT. STD. 7 YELLOW sinF 14X14 12 FT. OPT, t 7 BLACM & YELL 0s l d WP-0055A
MECHANICAL OPERATING PROCEDURE CONTAINER AND SHIPPING PROCEDURE NO: M0P-755714 ISSUE DATE: 6/18/8 REVISION: 2 FINAL APPROVAL: 'f# M PAGE: 1 of 2 ( V / CONTROLLED COPY: TITLE: REMOVING CONTAINER INTERNALS
1.0 PURPOSE
To specify removal of internals from shipping containers.
2.0 REFERENCES
2.1 Replaces Procedure OP 755714, Rev. 1. 3.0 TERMS / DEFINITIONS: None. h[
4.0 RESPONSIBILITIES
None. h (gp/ 5.0 REGULATORY REQUIREMENTS: None. 6.0 SPECIAL PRECAUTIONS: None.
7.0 PROCEDURE
7.1 PREPARATION
1. ASSEMBLE THE FOLLOWING APPROVED TOOLS: 1/2-DRIVE AIR OR ELECTRIC IMPACT WRENCH a. b. 1/2-ORIVE 3/4-INCH-DEEP SOCKET c. SNAP RING REMOVER d. HAWER AND PUNCH 1/2-13 THREADING DIE AND DIE DRIVER e. f. 1/2-13 STANDARD NUT
7.2 OPERATION
1. REMOVE TOP AND SIDE LOCK NUTS FROM EACH CLAMPlNG FRAME. (Use impact wrench and socket.) 2. REMOVE PAD ASSEMBLIES. 3. REMOVE LOCKING NUT AND WASHER FROM CORNER CLOSURE BOLT ON EACH C FRAME. (Use wrench and socket.) 4. CHASE THREADS ON CLAMPING FRAME FASTENER BOLT USING THREADING D DRIVE. 5. CHECK THREAD WITH 1/2-13 STANDARD NUT. (No sticking permitted. Rechase thread as necessary.) O WP-0056A
MECHANICAL OPERATING PROCEDURE PROCEDURE NO: MOP-755714 CONTAINER AND SHIPPING REVISION: 2 ISSUE DATE: 6/18/85 PAGE: 2 of 2
7.2 OPERATION
(Continued) 6. REMOVE SNAP RINGS FROM ATTACHED PINS. 7. REMOVE PINS ATTACHING TOP Ci.0SURE FRAMES TO STRONG 8ACK WITH HAMMER AND PUNCH. 8. REMOVE CENTER LOCKING PINS. 9. REMOVE TOP CLOSURE FRAMES FROM SHIPPING CONTAINERS. 10 REMOVE INTERNALS. 11. RECORO M0P REVISION NUMBER. INITIALS, AND DATE ON ROUTING.
8.0 ATTACHMENTS
None. . [' f.,. q. %llCn [f) Oq O O WP-0056A
MECHANICAL OPERATING PROCEDURE CONTAINER AND SHIPPING ISSUE DATE: 6/18/8 PROCEDURE NO: M0P-755718 Qf REVISION: 2 / PAGE: 1 of 1 1 FINAL APPROVAL: v j w i CONTROLLED COPY: TITLE: INSTALLING CONTAINER INTERNALS
1.0 PURPOSE
To specify steps to install internal hardware on shipping cor. tainers.
2.0 REFERENCES
2.1 Replaces Procedure OP 755718, Rev. 1. h//l 3.0 TERMS / DEFINITIONS: None. h {0Pp
4.0 RESPONSIBILITIES
None. 5.0 REGULATORY REQUIREMENTS: None. 6.0 SPECIAL PRECAUTIONS: O 6.1 PLACE ".X" MARK ON PAD TOWARD CENTER OF STRONG 8ACK BASE.
7.0 PROCEDURE
7.1 PREPARATION
1. ASSEMBLE THE FOLLOWING APPROVED TOOLS: a. PRESSURE PAD ASSEMBLIES b. 1/2-13 STANDAR0 NUTS ( c. 2 PAIRS OF CLOSURE FRAME ASSEMBLIES d. A/R CLAMPlNG FRAME ASSEWLY e. 4 ATTACH PINS WITH SNAP RINGS f. 3/4-C0W INAT10N WRENCH g. SCREWDRIVER h. MALLET
7.2 OPERATION
1. PLACE CLOSURE FRAME ASSEW LIES AT TOP END OF STRONG 8ACK. ~ 2. INSTALL 4 PINS AT ATTACH POINTS AND SECURE WITH 2 SNAP RINGS PER PIN. (Install more frames, as necessary, for shipping a 9-grid fuel assembly.) 3. INSTALL 4 PRESSURE PAD ASSEWLIES ON EACH CLAMPlNG FRAME. 4. SECURE PRESSURE PADS WITH 1/2-13 STANDARD NUT. 5. RECORD M0P REVISION NUMBER, INITIALS, AND DATE ON ROUTING.
8.0 ATTACHMENTS
None. WP-0060A
MECHANICAL OPERATING PROCEDURE CONTAINER AND SHIPPING ( ISSUE DATE: 6/18/8 PROCEDURE NO: MOP-755719 FINAL APPROVAL: of 1 D / / / CONTROLLED COPY: TITLE: ADJUSTING CLAMPlNG FRAME ASSEMBLIES
1.0 PURPOSE
To specify steps to adjust clamping frames in shipping containers.
2.0 REFERENCES
j!C0h[g0 2.1 Replaces Procedure OP 755719, Rev. 3. Ll B( 3.0 TERMS / DEFINIT 10NS: 3.1 Pressure Pads: Clamping surfaces of hold-down devices in shipping containers, on strongbacks, and in fixtures.
4.0 RESPONSIBILITIES
None. 5.0 REGULATORY REQUIREMENTS: None. 6.0 SPECIAL PRECAUTIONS: None.
7.0 PROCEDURE
7.1 PREPARATION
1. ASSEMBLE THE FOLLOWING APPROVED TOOLS: a. PAD GAGE b. AIR OR ELECTRIC IMPACT WRENCH c. 3/4-INCH DEEP SOCKET AND EXTENSION d. 3/4-lNCH COMBINATION WRENCH j e. A/R 3/4-INCH FLAT STEEL WASHERS l 2. PLACE PAD GAGE INTO 1 SIDE OF SHIPPING CONTAINER. 3. CLOSE CLAMPlNG FRAMES, TIGHTENING CORNER CLOSURE BOLT. (No gap between frame halves permitted.) 4. LOOSEN CLAMPING FRAME WITH IMPACT WRENCH ATTACHED WITH 3/4-INCH SOCKET. 5. ATTACH NUTS. 6. ADJUST FRAME. (Pressure pads centered on pad gage grid.) l 7. VERIFY THAT BOTTOM OF PRESSURE PAD CLEARS ALUMINUM RISER ON STRONG 8AC (Install maximum of 1 washer per bolt as necessary for clearance.) 8. SECURE ALL CLAMPING FRAMES AND ATTACH BOLTS WITH IMPACT WRENCH. l 9. REMOVE PAD GAGE.
- 10. RECORD M0P REVISION NUMBER, INITIALS, AND DATE ON ROUTING.
8.0 ATTACHMENTS
None. WP-0089A l
MECHANICAL OPERATING PROCEDURE ISSUE DATE: 6/18/85 PROCEDURE NO: M0P-755720 REVISION: 2 FINAL APPROVAL: v' PAGE: 1 of 1 O { / CONTROLLED COPY / TITLE: DISASSEMBLING CLAMP ASSEMBLY 1.0 PURPOSE; To specify steps for disassembling clamp assembly.
2.0 REFERENCES
2.1 Replaces Procedure OP 755720, Rev. 1. .[ -] -) ~~ 3.0 TERMS / DEFINITIONS: None.
4.0 RESPONSIBILITIES
None. 5.0 REGULATORY REQUIREMENTS: None. 6.0 SPECIAL PRECAUTIONS: None.
7.0 PROCEDURE
7.1 PREPARATION
1. ASSEMBLE THE FOLLOWING APPROVED TOOLS: a. SNAP RING REMOVAL TOOL b. PUNCH c. HAWER
7.2 OPERATION
1. REMOVE SNAP RINGS FROM ENDS OF PINS USING SNAP RING REMOVAL TOOL. 2. REMOVE PIN, USING PUNCH AND HAWER, IF NECESSARY. 3. SALVAGE PIN, SPACER WASHER, EYE BOLT, NUT, AND CLAMP. 4. RECORD MOP REVISION, INITIALS, AND DATE ON ROUTING.
8.0 ATTACl4ENTS
None. O WP-0301A
MECHANICAL OPERATING PROCEDURE CONTAINER AND SHIPPING (' PROCEDURE NO: M0P-755721 6/18/8p ISSUE DATE: REVISION: 2 FINAL APPROVAL: [ M PAGE: 1 of 1 V CONTROLLED COPY: TITLE: REFUR8ISH " EYE" BOLT
1.0 PURPOSE
To specify steps for checking, refurbishing, or replacing eye bolt.
2.0 REFERENCES
2.1 Replaces Procedure OP 755721, Rev. 1. h 3.0 TERMS / DEFINITIONS: None. [
4.0 RESPONSIBILITIES
None. ,f J I 5.0 REGULATORY REQUIREMENTS: None. 6.0 SPECIAL PRECAUTIONS: None.
7.0 PROCEDURE
7.1 PREPARATION
1. ASSEMBLE THE FOLLOWING APPROVED TOOLS: a. BENCH VISE b. 3/4-lNCH COMBINATION c. 1/2-13 THREADING DIE d. DIE FILE e. 1/2-13 STANDARD NUT
7.2 OPERATION
1. CLAMP EYE BOLT IN VISE. 2. REMDVE NUT. (Use 3/4-inch wrench, as necessary.) 3. REMOVE BOLT FROM VISE. 4. CHECK BOLT FOR STRAIGHTNESS. (Do not use if bent.) 5. CLAMP BOLT IN VISE AND CHASE THREADS. [ 6. DEBURR EYE BOLT WITH DIE FILE. 7. CHECK THREAD WITH 1/2-13 STANDARD NUT. j (No sticking permitted; rechase as necessary.) 8. LEAVE NUT ON BOLT. 9. RECORD MOP REVISION NUMER, INITIALS, AND DATE ON ROUTING.
8.0 ATTACHMENTS
None. WP-0062A l
UNCONTR01ED C0?X MECHANICAL OPERATING PROCEDURE CONTAINER AND SHIPPING AREA REVISION: 2 FINAL APPROVAL:1 49 Lg-_ N m t < t vm PAGE: 1 of 2 CONTROLLED COPY: TITLE: ASSEELING PRESSURE PAD ASSEELIES
1.0 PURPOSE
To specify steps to assemble pressure pad assemblies.
2.0 REFERENCES
2.1 Replaces Procedure OP 755722, Rev. 1. 3.0 TEfteS/ DEFINITIONS: None.
4.0 RESPONSIBILITIES
None. 5.0 REQJLATORY REQUlREMENTS: None. 6.0 SPECIAL PRECAUTIONS: None.
7.0 PROCEDURE
i
7.1 PREPARATION
1. ASSEWLE THE FOLLOWING APPROVED TOOLS: a. PRESSURE PADS b. EYE BOLTS WITH JACKING NUTS AND ELASTIC STOP NUTS c. PINS I d. SPACERS e. LOCKING CLIPS f. MALLET g. SCREWDRIVER
7.2 OPERATION
1. ASSEE LE MATERIALS FOR 1 SHIPPING CONTAINER. 2. A m amLE PRESSURE PAD ASSEW LY PER SKETCH. 3. FEC0ft) MOP REVISION NUWER, INITI ALS. AND DATE ON ROUTING.
8.0 ATTACMENTS
8.1 Pressure Pad Assembly. O WP-0102A
1 UNCONTROL<=ED MV N EQEDURE NO: MOP-755722 WECHANICAL OPERATING PROCEDURE CONTAINER AND SHIPPING AREA REVISION: 2 ISSUE DATE: B/ 3/85 PAGE: 2 of 2 8.1 Prassure Pad Assembly. f A ELASTIC STOP NUT L JACKING NUT si ll EYE BOLT SPACER LOCKING CLIP ~ ~ 1 u .'-[ PIN PRESSURE PAD ( J O WP-0102A I l O m
MECHANICAL OPERATING PROCEDURE ISSUE 9 ATE: 6/18/8 PROCEDURE NO: MOP-755723 REVISION: 2 PAGE: 1 of 2 FINAL APPROVAL: u j CONTROLLED COPY: TITLE: DISASSEMBLING AND REFUR8ISHING CLOSURE FRAME ASSEMBLIES
1.0 PURPOSE
To specify steps to disassemble and/or refurbish closure frame assemblies.
2.0 REFERENCES
2.1 Replaces Procedures OP 755723, Rev. 1 and OP 755724, Rev. 1. 3.0 TERMS / DEFINITIONS: None.
4.0 RESPONSIBILITIES
None. 5.0 REGULATORY REQUIREMENTS: None. 6.0 SPECIAL PRECAUTIONS: None. f
7.0 PROCEDURE
7.1 PREPARATION
1. ASSEMBLE THE FOLLOWING APPROVED TOOLS FOR DISASSEMBLY: 3/4-INCH COMBINATION WRENCH a. b. ALLEN WRENCH c. HAWAER d. PUNCH e. SNAP RING REMOVER 2. ASSEMBLE THE FOLLOWING APPROVED TOOLS FOR REFURBISHING: a. 1/2-13 TAP AND TAP DRIVER b. 1/2-13 DIE AND DIE DRIVER c. 1/2-13 STANDARD BOLT d. 1/2-13 STANDARD NUT
7.2 OPERATION
A. OlSASSE WLY: 1. REMOVE RODS FROM END OF CLOSURE BOLTS AND SALVAGE. 2. REMOVE LOCK NUTS AND CLOSURE BOLTS AND SALVAGE. 3. RECORD MOP REVISION NU WER, INITIALS, AND DATE ON ROUTING. O WP-0070A
T PROCEDURE NO: MOP-755723 MECHANICAL OPERATING PROCEDURE REVISION: 2 O. CONTAINER AND SHIPPING ISSUE DATE: 6/18/85 PAGE: 2 of 2
7.2 OPERATION
(Continued) 8. REFUR8ISHING: 1. TAP HOLES IN FRAME. 2. CHECK HOLES WITH BOLT. (No sticking permitted; retap as necessary.) 3. CHASE THREADS WITH DIE AND ole DRIVER. 4. CHECK THREAD WITH NUT. (No sticking permitted; rechase as necessary.) 5. RECORD MOP REVISION NUMBER. INTITAlS, AND DATE ON ROUTING.
8.0 ATTACHMENTS
None. 's,.s Q[<], ./3 'Q) O WP-0070A y
HANICAL OPERATING PROCEDURE ONTAINER AND SHIPPING AREA h PROCEDURE NO: MOP-755803 i REVISION: 1 g\\ N( M kAL APPROVAL:/Ac?M_ 6 h <, e c.. c y PAGE: 1 of 2 CONTROLLED COPY TITLE: REPLACEMENT OF ABSORBER PLATES IN SHIPPING CONTAINER
1.0 PURPOSE
To specify steps for removing and replacing shipping container absorber plates. 2.1 Replaces Procedure OP 755803. Rev. O. 3.0 TERMS / DEFINITIONS:
3.1 Gadolinium
Metal used in high enriched shipping container to absorb neutrons and keep container critically safe.
4.0 RESPONSIBILITIES
4.1 Quality Control: Inspect gadolinium on absorber plate as necessary. 5.0 REGULATORY REQUIREMENTS: None. 6.0 SPECIAL PRECAUTIONS: None.
7.0 PROCEDURE
7.1 REMOVING ABSORBER PLATE: 1. OPEN SHIPPING CONTAINER. l 2. REMOVE ABSORBER PLATE CLAMPING CHANNEL. I 3. USE CRANE TO LIFT STRONGBACK HIGH EN0 UGH TO ENGAGE LOCKING TUBES. l 4. PULL OUT THE 2 COPPER ABSORBER PLATES. l (Store plates until enough have been collected for disposal.) 7.2 REPLACING COPPER PLATES WITH GAD 0LINIUM PLATES: 1. REMOVE GADOLINIUM ABSORBER PLATE FROM PACKING CONTAINER. 2. PLACE ABSORBER PLATE FLAT ON WORK TABLE. (Ensure plate is supported over its fulI length.) 3. CHECK BOTH SIDES OF PLATE FOR PEELING OF GADOLINIUM. (if peelin'., extends more than 1/4-inch in from edge, submit plate to Quality Control for acceptance.) 4. CHECK PAINT AROUND EDGES. A. NEW PLATES: 1) PAINT EDGES WITH BROWN PRIMER WHILE PLATE IF LAYING FLAT 2) FINISH EDGES WITH C0AT OF BLUE PAINT. B. USED PLATES: 6 l 1) CHECK FOR PAINT PEELING AND FOR RUSTING. 2) REPAINT, AS NECESSARY. WP-0300A
MECHANICAL OPERATING P E PROCEDURE N0: M0P-755803 CONTAINER AND SHI 4G REVISION: 1 (V] ISSUE DAT A M -L I PAGE: 2 of 2 lh\\JW ACING COPPER PLATES WITH GADOLINIUM PLATES: (Continued) 5. INSERT GAD 0LINIUM PLATE INTO ABSORBER CHANNEL. (Use 2 people to lift plate off work table. being careius not to allow plate to bend smaller than a 3-foot radius.) 6. LEAD PLATE INTO ABSOR8ER CHANNEL. 7. HAVE 1 PERSON GUIDE PLATE INTO EACH CHANNEL BRACKET, WHILE OTHER PERSON PUSHES PLATE INTO POSITION. 8. STRING SEAL WlRE THROUGH 1/2-INCH-DIAMETER HOLE IN EACH PLATE. (Leave ends out far enough to alloa threading through clarrping channel.) 9. LEAD END OF SEAL WIRE THROUGH CENTER HOLE ON CLAMPING CHANNEL. 10. PLACE CLAMPlNG CHANNEL ON 2 STUDS PROVIDED. 11. SCREW ON 2 NUTS TO SECURE CLAMPING CHANNEL IN PLACE.
- 12. CRIMP SEAL.
13. LOWER STRONG 8ACK.
8.0 ATTACHMENTS
None. O e* ,a
O ATDOIMENT 23 QUALITY CONTROL DEPECTION PROCEDURES O O Docket No. 71-5450 Initial Submittal Date: 12/20/85 Page No. 23-1 i "*1' ' ' *" 8"* ' "' ' "*i' : 8' 86
001 REVISION COVER LETTER 001 938602 REVISION 37 NOTES:
- 1) DESTROY ALL COPIES OF PREVIOUS REVISIONS TO THIS OCl!
- 2) No reinspection required for parts in-process and/or released parts; exceptions shall be handled by Special Routing.
CHANGES MADE BY THIS REVISION: Pages 1 & 2 -- Deleted reference to a ' log'. Page 5 -- Deleted item 15 requiring verification of clamping frame position. Renumbered items 16 through 28 (pages 5 through 8) as 15 through 27. -- Deleted Attachment 3 and renumbered Attachment 4 to 3. -- Changed reference in item 11. from Attachment 4 to 3. Page 10 -- Changed number of Attachments from 4 to 3. O Prepared by: M d Auality Control Engineer Date , /, d t Approved by: Wfv w P ' d0ct ' Assurance Manager / Gate o Concurrences: I~/0-f4 Trai 1 kt zur 6/-d-f4 P. A. Engineerin'g Manager Date
- 0. C. Iqppedtion Map 6ger Date h
I \\qllk 1 a Area 0. C. % pervisor Date l 41760:3 O i l L
WESTINGHOUSE NUCLEAR FUEL DIVISION OUALITY CONTROL INSTRUCT 10N Page 1 of 10 OCl No.: 938602 Rev.: 37 Rev. Date: 1/20/86 Engineer: J. Bond
SUBJECT:
FUEL ASSEMBLY SHIPPING CONTAINER INSPECTION SCOPE: INSPECTION AFTER REFURBISHMENT DRAWING: N/A CHARACTERISTIC OPERATION DESCRIPTION FREQUENCY Read OCl 000198 and comply with the applicable paragraphs. In case of conflict between OCl 000198 and this 0C1, this 0C1 will prevail. Applicable JSA procedures: N/A GENERAL Inspect all shipping containers after refurbishment for 100% INSTRUCTIONS acceptability per items listed in this OCI. Before inspecting, check the container folder to verify all OCON's issued as a result of FOR's have been cleared. Initiate a container check list, Pages 2 through 8 of this 001, and indicate inspection results as inspection steps are completed. If the container is not acceptable, notify Manufacturing that repairs are needed. Place the inspection check list with the container routing to identify the needed repairs to Manufacturing. When notified by Manufacturing that repairs have been made, reinspect the repaired items and check the ACC block if they are acceptable. When all items of the container check list have been accepted or properly reworked and accepted, stamp the container routing and check list. i l 1 i 41760:3 ' - ' - * * ^ " " ' ---..y-y
Page 2 of 10 001 No,: 938602 Rev.: 37 CHARACTER 4STIC OPERATION _ DESCRIPTION FREQUENCY EVEL ASSEMBLY SHIPPING CONTAINER INSPECTION CHECK Ll_ST Container Serial No. Length 137" or 160" inspector Date Accepted INSPECil0N OF CONTAINERS REFURBISHED WITH CORK SPACERS If the container has received the initial inspection after curk installation, proceed to Step 6. If the container has not been inspected after cork installation, proceed with Steps 1 through 5. ACC REJ R/W 1. Inspect cork surface for flatness using a straight edge and.030" feeler gage. Lay straight edge parallel to the clamping frames and scan surface. Check gaps with.030" feeler gage. Gage must not go. 2. Check distance of cork edges from the corner of the strongback with a steel scale. Distance should be .350 Max. See Sketch. OMoMGd M. fW NE50Rs tu y: f CORK ~ _r 350 wx .;5 r: . :!.*.: N. *.* t g-a i \\ 4 g __ 3. Check cork spacer overall length with a tape measure. The distance should be 158.840/158.960 (nearest fractional equivalent is 158 27/32 / 158 61/64). This measurement is not required for 137" containers. 4. Check cork width with a steel scale. Width should be 8.720/8.950. 5. Check length from bottom end support (without 1/16" cork liner) to top edge of cork spacer with a tape measure. This distance should be 159.275/159.400 (nearest fractional equivalent is 159 9/32 / 159 25/64). For 137" containers refurbished with continuous cork, see Attachment 2. Check overall length from bottom end support (135.875/136.00) and gap of cork from bottom end support (.375/.500). 41760:3
Page 3 of 10 001 No.: 938602 Rev.: 37 CHARACTERISTIC OPERATION DESCRIPTION FREQUENCY INSPECTION OF CONTAINERS REFURBISHED WITH CORK SPACERS ACC REJ R/W Any outages should be documented on a OCON. Specify location and degree of outage on the OCON or an attachment if necessary. Location should be described as viewed from the top end of the container. 6. Visually inspect cork spacers for damage or mislocation. Reinspect suspect areas using the criteria for initial inspection (Steps 1 through 5). 7. For cork that has been repaired, verify the following: a. No more than two splices (seams) per cork surface. b. 1/32" maximum gap at splice. c. New cork and spliced joint are flat within.030" d. Splice is not under a clamping frame location. e. Coih meets width & length requirements defined above. f. Cork edge to corner of strongback is.350" maximum (item 2 above). Enter N/A beside steps which do not apply. For initial inspection, Steps 6 & 7 do not apply. After initial inspection Steps 1 through 5 will not apply unless damage is found. CONTAINER INTERIOR Visual 100% 1. Verify that the clamping frames, pressure pads, Unless and interior of the container lid is clean, Otherwise painted, & free of rust or other particulate. Noted 2. Verify that the interior of the container base does not contain gross amounts of rust or other particulate. This inspection may be performed without raising the strongback. 3. Verify that the container base flange, gasket slot and U channels for swing arms are clean, painted and free of rust, loose hardware or other particulate. ~ 4. Visually inspect bolts and verify that the nuts are not excessively rounded, washers not bent or burred, and bolt threads not stripped or burred. 41760:3
7 -_. [ Paga 4 of 10 0C1 No.: 938602 Rev.: 37 T CHARACTERISTIC OPERATION DESCRIPTION ~ FREQUENCY ACC REJ R/W ~ Visual 100% Unless CONTAINER INTERIOR n Otherwise Noted 5. Verifythat;allballlockpinsinsidethecontainerare attached to the container-by a wire. Verify that each ball t loc %pifis functional by installing the pin and manually pulitng on it. A. Top closure pins. B. Stabilizer pins'.v r, C._ Cross bar pins. '( D. For stabilizer bar pins, check length'of shank portion. Length should be 1 1/2" minimum. 6. Verify the presence of twc absorber plates of the same type f in strongback, i.e.,4 copper, steel, or cermet co,ated. Yellow dot containers (see 3 tem 9 below) must contain cermet coated absorber plates. This may be. verified by the O rough surface as compared to the smoother surface of the ~ copper and steel plates; also, the edges of the cermet coated, plates are painted blue. 7. Cermet coated plates must be secured in the strongback by a yellow clamping channel and a, visible security seal which prevents removal of the plates without destroying the seal. 8. The copper or' steel plates are to have a blue clamping channel without a security seal. 9. For containers having cermet coated absorber plates, verify the presence of a painted yellow dot (approx. 3" dia.) next to the serial number on both the top and bottom sections of the container.
- 10. Obtain 2 calibrated accelerometers from Tool & Gage to replace the ones that are on the container and verify that an accelerometer is attached at each end of the container strongback. The calibrated accelerometers must be serialized and sealed.
If inadvertently tripped, return it to Tool & Gage for resetting. Return old ones to T & G. O 41760:3 l
Page 5 of 10 001 No.: 938602 Rev.. 37 CHARACTERISTIC OPERATION DESCRIPTION FREQUENCY ACC REJ R/W Visual 100% CONTAINER INTERIOR Unless Otherwise Noted
- 11. Verify the top closure jack screws and lock nuts are in good condition with bolt heads not rounded and threads not stripped or burred. Verify proper location of jack screws by comparing to the provided sketch. See Attachment 1 (Attachment 3 for Model C).
Verify that the neoprene rubber pads are in good condition and not cut or severely gouged. Verify the allen head shoulder screws (not applicable to Model C) holding the pads to the jack screws do not protrude beyond the neoprene rubber pad and that the pressure pads spin freely on the shoulder screw. 4
- 12. Verify that each pressure pad is covered with one layer of cork that is cut flush with the pad. Cork must be within 1/8" of end but must not extend beyond end of pad.
- 13. Verify that the pressure pad eye bolts are not bent and that the jacking nuts are regular nuts and not n(j setf locking nuts. Either regular or seIf locking nuts may be used as lock nuts.
14. A. For pressure pads with grooved pins, verify that lock clips are present at both ends of each pin at every pressure pad. B. For pressure pads with ungrooved pins, manually check to see that pins will not slip. (Pins without grooves / lock clips must be held in place by a force fit at their center.
- 15. Verify the presence and correct orientation of a stamped "X" on all white, blue, red, green, & black pressure pads. The pressure pad end with the stamped "X" must be oriented toward the strongback.
.-r-- m
Paga 6 of 10 0C1 No.: 938602 Rev.: 37 CHARACTERISTIC OPERATION DESCRIPTION FREQUENCY ACC REJ R/W Visual 100% Unless CONTAINER INTERIOR Otherwise Noted
- 16. Verify correct color coding of pressure pads:
A. Green pads for Model C 8. Blue pads for 17x17 and 15x15 ] } C. Yellow or red pads for 14x14 ] Except Optimized Fuel ] D. Red pads for 16x16 ] E. White pads for 15x15 or 17x17 Optimized Fuel, except first & last clamp frame from bottom end support to have standard pressure pads. F. Black pads for 14x14 optimized except first & last clamp frame from bottom end support to have standard pressure pads.
- 17. Verify that each pressure pad will rotate freely to line up with a grid.
If the pad will not rotate e freely to align with a grid. the pad and bolt assembly and/or swing arm must be replaced. I f pad will not clear horizontal surface of strong back it may be necessary to add a washer to raise the swinq arm assembly. No more than one washer per position may be used.
- 18. Verify that the tack welds at each swing crm Solt are sound and that the bolts are not stripped or burred. Also verify that the nuts are not excessively rounded.
(Minor cracks in these tack welds are permitted so long as the bolt does not turn.)
- 19. Verify that the swing arms will open far enough to allow a clear path to the strongback. Open each clamp and inspect visually. Use a straight edge held against the strongback if in doubt. Swing arm should open approximately 30' beyond the minimum clearance.
- 20. Verify that lock clips are present at both ends of each pin at every swing arm.
41760:3
Page 7 of 10 001 No.: 938602 Rev.: 37 CHARACTERISTIC OPERATION DESCRIPTION FREQUENCY ACC REJ R/W Visual 100% Unless CONTAINER INTERIOR Otherwise Noted
- 21. Veri fy that the swing bolts holding the strongback to the cradis are in good condition with nuts not rounded and threads not stripped or burred.
- 22. Visually verify that the swing bolt brackets are not bent downward more than 1/8".
If in doubt measure or use functional gage drawing 603C04GA01, Gp.1.
- 23. Verify that the welds on the strongback brackets and on the swing arm bolt brackets are not cracked.
24. A. For grooved pins, verify that lock clips are present at each end of each swing bolt that holds the strongback to the cradle. B. For ungrooved pins, manually check to see that pins do not slip. Pins without grooves / lock clips must be held in place by a force fit at their centers.
- 25. Verify that the container gasket is not broken or damaged.
- 26. Verify that the correct number of shock mounts are present for appropriate fuel assembly types and that they are in good condition.
Number of Mounts Fuel Assembly Type 18 16x16 & 17x17 - 12' 18 15x15 - 12' 16 14x14 - 12' 14 14x14 - 10' 14 14x14 - 8' 16 14x14 - 12' ModeI C Shock mounts are to be removed only in opposing pairs. When two shock mounts are to be removed from RCC-1 containers, they shall be the fourth pair from the bottom. When four shock mounts are to be removed, they shall be the fourth and fifth pair from the bottom. When four shock mounts are to be removed from the RCC-3 containers, they shall be the third and ninth pair from the bottom. When six shock mounts are to be removed, they shall be third, fifth, and ninth pair from the bottom. When eight shock mounts are to be removed, they shall be O-the third, fifth, sixth, and ninth pair from the bottom. 41760:3
) Paga 8 of 10 OCl No.: 938602 Rev.: 37 CHARACTERISTIC OPERATION DESCRIPTION FREQUENCY l ACC REJ R/W Visual 100% Unless CONTAINER INTERIOR Otherwise Noted
- 27. Verify that a 1ifting device is present on the container internals to allow raising the internals to adjust the lateral crossbar. The device may be any one of the following:
A. Eyebolts mounted on the pillow blocks on both sides of the internals (above the lateral crossbar). B. U bolts mounted on the end of the internals (above the lateral crossbar). C. A single bolt mounted on the end of the internals (above the lateral crossbar). O
Paga 9 of 10 0C1 No.: 938602 Rev.: 37 0 CHARACTERISTIC OPERATION DESCRIPTION FREQUENCY ACC REJ R/W Visual 100% Unless CONTAINER EXTERIOR Otherwise Noted i Verify that the container closure bolts or camlocks are 1. not damaged. For camlocks, verify that the heads are not excessively rounded and that a lock device is present at each required location. 2. Verify that the exterior of the container lid is well painted, free of loose rust and peeling paint. 3. Verify that the exterior of the container base is well painted, free of loose rust or peeling paint. 4. Verify that the serial numbers stenciled on both halves of the container match. 5. Verify that container name plates are present at the bottom end of the container and all information is legible. 6. Verify that the lifting holes at each end of the container O lid are identified at 5 and 6 by 1" high stenciled l lettering in a 2" circle or by 2" high stenciled numbers. 7. Verify that " LIFT HERE" is stenciled between each pair of lifting holes in 2" high stenciled lettering. 8. Verify that " CAUTION: HANDLE WITH CARE - CONTAINER SHOCK INSTRUMENTED" is stenciled along each side of the container lid in 2" high lettering, d 9. Verify that a 7" x 8" ! decal is located in the black area near the container name bracket & is in good condition.
- 10. Verify that 11" x 13" ! decal is located in the black area opposite the container name bracket and is in good condition.
- 11. Verify that a permanent license plate is present on each side of the container lid. Raised letters must be painted white against a blue background. Verify that information on plate is: FISSILE RADI0 ACTIVE MATERIAL N.O.S. UN2918 USA /5450/AF 4
- 12. Verify that a 8" square black area is painted just above each permanent license plate.
41760:3 i . -, -,,,,,,,,., _ -, -,. -,, - - -, -,,, -. - -. - - - -, + - -, - -.,, - - - -, - _ - -,, - -. - - - - - - - - - -, -,, -,, - - - - - - -,
Pags 10 of 10 0C1 No.: 938602 Rev.: 37 0 CHARACTERISTIC OPERATION DESCRIPTION FREQUENCY ACC REJ R/W Visual 100% Unless CONTAINER EXTERIOR Otherwise Noted
- 13. Verify that an unpainted stainless steel cover plate is present at the bottom end of the container and is secured with stainless steel wing nuts, lock washers and flat washers.
14. Verify that the wooden skids are in good condition. If splits in skids are greater than 2" deep and run the length of the skid, the skid must be replaced. If the shank portion of a skid bolt is completely exposed due to wood deterioration that skid should be replaced. Also, if the wood if predominantly rotten the skid should be replaced. If metal skids are used verify that they are free of any deformation that causes the container to rock or sit unevenly.
- 15. Verify that the four (4) stacking bolts if present on top of each container are in good condition with threads not stripped-or burred, and that the nuts are not rounded.
Os
- 16. Verify that our return address has been stenciled midway along the container lid inside the name plate bracket.
- 17. Outrigger pins - Verify that all ball lock pins are attached to the container by a wire. Verify that each ball lock pin is functional by installing the pin and manually pulling on it.
- 18. Verify presence of holes at container ends on outer edge of flange to be used for wire seals during shipment.
(Minimum of one hole at each end required.) i
- 19. Check container file to verify that all Field Discrepancy Reports (FDR) against container have been cleared.
l Attachments: (3) \\ 41760:3 O i
m ,a ,27 -) N..] N., ATTACHMENT 1 (QCI 938602 & 938603) Top Closure' Jack Screws Must Be Oriented As Shown Location of Jack screws as shown are for 15x15 and 17x17 fuel NOTE: assemblies. Jack screws must be moved to the adjacent hole locations for 14x14 and.16x16 fuel,assembifes. TOP RIGHT A I;. fTrry- ] ~ TOP LEFT ed 1 4 i ) a lll A ,i ! k ~ j, ur .m: - y l l l / . rr[.L i BOTTOM RIGHT BOTTOM LEFT LNh;1 _ 1.. ii !~ I s 8
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f3 QCI REVISION COVER LETTER QCI 938603 REVISION 42 NOTES:
- 1) DESTROY ALL CCPIES OF PREVIOUS REVISIONS TO THIS QCI!
- 2) No reinspection required for parts in-process and/or released parts; exceptions snall be handled Dy Special Routing.
CHANGES MADE BY THIS REVISION: Revision 42: - Incorporated handwritten revision 41A with some modifications - pg. 7, Item 7. - Clarified requirements when a ballast weight is used - pg. 5, Item 14. - Added requirement to verify serial numbers of top nozzle and component - pg. 3. - Clarified use of clows 'aot adaptor for torquing - pg. 6. I Prepared by: / Quality Control Engineer Date 4 [Ad 7/2,/r Approved Dy: Qtf i'ty Control Manager'/ Date Concurrences: l hY / vru1( we 7-30-/S~ Date Q.' C. Inph$tition Margger Date / Q. C. Engineerin @ ger di8 7 I.ulo' Area 0.C.jSupefvisor- ' Date 4175Q:3 l
O ESTINGHOUSE NUCLEAR FUEL DIVISION QUALITY CONTRO<_ INSTRUCTION Page 1 of 8 QCI No.: 938603 Rev.: 42 Rev. Date: 8/4/85 Engineer: J. Bond SUEDECT: FUEL ASSEMBLY SHIPPING CONTAIER INSPECTION (LOADED & TEN) SCPE: GENERAL ORAWING: GEERAL CHARACTERISTIC PERATION DESCRIPTION FREQUENCY Read QCI 000198 and comply with the applicable paragraphs. In case of conflict between QCI 000198 and tnis QCI, this QCI will prevail. Applicable JSA procedures: WA INSPECTION The following inspection sequence applies to this QCI: 100% O SEQUENCE A. Wrapper inspection of assemblies from storage. 8. Verify documentation, cleanliness, and fuel assemoly orientation. C. Before torque inspection. D. Complete torque check. E. After torque inspection. GEERAL Initiate a container check list, pages 2 thru 8 of this QCI, and INSTRUCTIONS indicate inspection results as inspection steps are completed. If the container is not acceptable, notify Manufacturing that repairs are needed. Place the inspection check list with the container routing to identify the needed repairs to Manufacturing. When notified by Manufacturing that repairs have been made, reinspect the repaired items and check the ACC block if they are acceptable. .When all items of the container cneck list nave been accepted or properly reworked and accepted, stamp the container routing and check list. O 4175Q:3
Page 2 of 8 QCI No.: 938603 Rev. 42 CHARACTERISTIC O'ERATION DESCRIPTION FREQUENCY FUEL ASSEMBLY SHIPPING CONTAIER CHECK LIST Container Serial Nc. 137" or 160" Inspector Date Accepted ACC REJ R/W WRAPPER INSPECTION Verify that wrappers of previously stored assemblies are free of visible marks or tears that may indicate assemoly damage. If wrapper damage is found, assemoly must ce unwrapped & reinspected at indicated area for damage. DOCUENTATION VERIFICATION 1. Verify that the fuel assemblies in tne container nave been Q. C. Released for shipping. 2. Verify the completeness of the fuel assemoly route card. 3. Verify that any core components in the fuel assemblies have O been Q. C. Released for shipping. 4. 01eck the component loading chart to confirm that the fuel assentalies contain the correct core component. Verify correct drawing and group numer. Record core component serial number below. NOTE: When a core cvinponent is removed and then reinserted in an asseely, verify that the identity and orientation is correct. 5. Verify the completeness of tne core component route cards. 6. Verify that ALL QCON's have been cleared / accepted. For reference se7eI 000112. 7. 01eck the "Columoia Snipping Schedule" to determine if assemblies are to be shipped in a " Yellow Dot" container. If so, verify the presence of the yellow and channel and security seal at the cottom end of tne strongeack.
- Also, verify that the contairer and the lid have a yellow dot painted next to tne serial runber.
CONTAIER INTERIOR CLEAM.IESS With the strongback upright, inspect the container interior for cleanliness. In particular, check the base for dust, dirt, rust, loose nuts, Dolts, wasners, and other debris. 4175Q:3
Page 3 of 8 QCI No.: 938603 Rev. 42 CHARACTERISTIC G'ERATION DESCRIPTION FREQUENCY ACC 'REJ R/W 1005 Unless Otherwise Noted FLEL ASSE2LY ORIENTATION After the strongback has been lowered, verify that the fuel assemblies have been loaded with the Y-corner in the corner of the strongback and that the core component, if required, is correctly oriented per core component loading cnart. 1. Viewed from the top end, the fuel assemoly on Contract Fuel Core Comp. VN the left should have the top nozzle clamp with Assy (if applicable) the engraved serial nuncer in the lower left WN hand corner. For Model C the serial nuncer on the flower should be at the lower right corner. For assenclies 1193E92 & 685J872 verify that the serial number is on the right side of the top nozzle top plate. Verify that the serial numbers of the top nozzle and component agree with the associated routing. 2. Viewed in the above manner, the fuel assembly Contract Fuel Core Comp. W N on the right should have the engraved spring Assy (if applicable) clamp on the upper left-hand corner. For WN Model C the serial number on the flower should be at the upper left corner. For assenclies 1193E92 & 685J872 verify that the serial number is on the bottom side of the top nozzle top plate. Verify that the serial nuncers of the top nozzle and component agree with the associated routing. 3. Stamp and Date G'EN CONTAIER INSPECTION EEFORE T0fGUING 1005 lk11ess ^ ACC REJ R/W Otherwise Noted 1. Verify that the top and clampinc frame assemblies are closed and latched properly and are neId in place with two locking pins attached to the container by wire.' Verify that plastic i's ' secured between the top closure bo' t ~ l 2. pads and nozzle corners. 3. Verify that top closure assembly bolts are in their proper location by comparing to the provided sketch. (Attachment 1) (Attachment 4 for Model C) 4. Verify that a rubber pad is present on each of the pads on the 4 bolts (single plate for Model C) of the top closure assembly. ~ ~ MSVi\\e
Page 4 of 8 QCI No.: 938603 Rev. 42 CHARACTERISTIC P ERATION DESCRIPTION FREQUENCY PEN CONTAIrER INPECTION 8EFORE T0fGUING ACC REJ R/W 1004 Unless Otnerwise Noted 5. Verify that a ruDoer pad is bonded to the hold down bolt (or plate) and that a piece of plastic is secured oetween tne pad and core component. 6. Verify that a plastic sheet nas been placed between tne bottom nozzle feet & strongback Dase (spacer block for Model C) for each assembly. 7. Verify that pressure pads are properly located. a. For 17x17,16x16, & 15x15 fuel assemolles, tne pads must be located so that no springs show in eitner direction. A maximum of one spring window may show at the end of the clanp. D. For 14x14 fuel assenclies, no portion of the spring may l show in the long direction of the spring but a maximum of one spring may show at either end of tne clamping pad. c. Verify the presence and correct orientation of a stamped "X" on all white, blue, red, and green pressure pads. The pressure pad and with the stamped "X" must be oriented toward the stranguack, f 8. Verify correct color coding of pressure pads. j a. Green pads for Model C. b. Blue pads for 17x17 and 15x15. ] c. Yellow or red pads for 14x14. ] Except Opt-Fuel d. Red pads for 16x16. ] White pads for 17x17 & 15x15 Optimized Fuel except 1st & e. [ last clamp frame from bottom and support to nave standard pressure pads. f. Black paos for 14x14 Optimized Fuel except first &,last clamp frame from bottom and support to have standard pressure pads.
- 9. Verify that the pads ao not interfere with eacn otner cr tne strongback.
O i 4175Q:3 l w -e -,..--,---=,------,---------ewm-..- .-,--..-,-----,-,.-m---.-, -m---.-- .w-. -~..-----.,v.-- ..., ~. - - - - ' -
= -. Page 5 of 8 ^ QCI No.: 938603 Rev. 42 CHARACTERISTIC P ERATION DETRIPTION FREQUEfCY PEN CONTAINER INSPECTION BEFORE TOR;)UING 100% Unless ACC REJ R/W Otherwise Noted
- 10. Verify that grids do not extend beyond the aluminum or cork spacer plates (or continuous cork spacers if used) attacned to tne strongback.
- 11. Verify that each assemD1y is enclosed in a plastic Dag whicn has been cut or folded back with excess at top nozzle end clamped under top closure colts. Also verify that the excess i
plastic has been pulled out at the corners between clamping pads and is not folded over and clamped between the pad and assencly. NOTE: Slits at bottom nozzle end are permissiole in the area between the nozzle legs & below the bottom nozzle plate, i.e., slits cannot extend over the ootton nozzle or any portion of the fuel assencly.
- 12. Verify that no tape is present at any grid location.
- 13. Verify that one layer of cork is present on each clamping pad and aluminum spacer, if applica01e.
- 14. In cases wnere a single fuel assemoly is being snipped, verify tnat a dummy assembly or other callast is snipped with the assencly.
If a dummy assemoly is used, verify that it has the sa:ne configuration as the fuel assenoly (17x17, etc.). If ballast is used, request a weight from Manufacturing and verify that it is within 200 pounds of tne fuel assemoly weignt listed in Attacnment 2. If the assenoly being shipped is a dummy assencly, a Dallast is unnecessary. If tne fuel assemoly being snipped contains a core component, weigh the component and verify the ballast is within 200 pounds of the total assenoly and core component weight. t I i t 1 5 f 4175Q:3
Page 6 of 8 QCI No.: 938603 Rev. 42 CHARACTERISTIC (PERATION DESCRIPTION FREQUENCY ACC REJ R/W 1005 Unless Otnerwise Noted TORJUE Visually verify tnat all Jackscrews are tigntened in tne sequence described below. The value indicated on the torque wrench must ce within 10 lbs. of the required value. Verify tnat grid pressure pads remain properly aligned and the plastic properly located during and after torquing. The below " crows foot" torque values are based on using an 8 inch " effective length" torque wrenen and a 2 inch crows foot adaptor. Any other comoination is unacceptacle as an incorrect torque may result. 1. Side clamps are to be tightened first, starting at the bottom grid and working to the top, tightening clanps to 60 in.-lbs. (48 in.-lbs. reading when crows foot is used.) 2. Top clamps are to be tightened second, starting at the bottom grid and working to the top, tightening clamps to 60 in.-lbs. (48 in.-lbs. reading wnen crows foot is used.) 3. If an error is found when side or top clamps are being tigntened to 60 in.-lbs., apply additional torque if value is below specified range or loosen and retorque if value is above the specified range.* 4. Repeat steps 1 and 2, tightening to 90 in.-lbs. (72 in.-lbs. when crows foot is used). 5. If an error is found during the tightening to 90 in.-10s., 7 retorque as follows: If indicated value is below the specified range apply a. necessary additional torque. b. If the indicated value is above the specified range, loosen top and side clamps at that grid location and retorque both clamps first to 60 in.-10s. and then to 90 in.-10s. (48 *in.-lbs. and 72 in.-10s. respectively if the crows foot is used.) i Top closure bolts are to be tightened to 60 to 120 in.-10s. ' 6. (48 to 96 in.-lbs., reading when crows foot is used). This also applies to tre center Dolt, for nciding the core components in place, except fnr the 17x17 & 16x16 core components having the long spider body, where a center nub is used. If torque value exceeds 110 in.-10s. (88 in.-lbs. when crows foot l
- NOTE:
1s used) issue a QCON for the affected fuel assembly. l i 4175Q:3 i
V Page 7 of 8 QCI No.: 938603 Rev. 42 CHARACTERISTIC PERATION DESCRIPTION FREQlENCY PEN CONTAINER INSPECTION AFTER TOFCUING ACC REJ R/W 1004 Uniess Otherwise Noted 1. Verify that the core component hold down bolt (or plate) is securely tightened against tne core component (if present) oy checking manually with a wrench. 2. Verify that the two halves of the clamping frames are securely fastened oy cnecking the nuts manually with a wrenen. 3. Verify that tne swing bolts which secure tne strongoack to the cradle are securely fastened by checking the nuts manually witn a wrench. 4. Verify tnat the two lateral cross Dars nave been retracted into tne lock tube and secured with an operable locking pin attacned to the container oy wire. Verify that tne bars are O secured by pull testing each bar manually. 5. Verify tnat the two hex need colts which are used to secure the lateral cross bars are nand tightened to prevent them from falling out during the shipment. 6. Verify that the two vertical stabilizing bars are secured to the container with hex need bolt, washer, and nut at one end; and an operable locking pin attached to the stacilizing bar with wire at the other end. The snank portion of tne locking pin must be 1-1/2" long minimum. See Attacnment 3 for correct l position of car and locking pin. 7. Verify that one serialized and tamper sealed accelerometer is secured at each end of the strongback. If the accelerometer is tripped or the seal is broken, return it to Tool & Gage for a replacement. l i. 4175Q:3
( N Page 8 of 8 QCI No.: 938603 Rev. 42 CHARACTERISTIC CPERATION DESCRIPTION FREQLEPCY CPEN CONTAINER INPECTION AFTER T0fGUING 1004 Unless ACC REJ R/W Otherwise Noted 8. Verify that tne correct numDer of shock mounts are present for appropriate fuel assemoly types and tnat tney are in good condition. Number of Mounts Fuel Assemoly Type 18 16x16 & 17x17 - 12 feet 18 15x15 - 12 feet 16 14x14 - 12 feet 14 14x14 - 10 feet 14 14x14 - 8 feet Shock mounts are to be removed only in opposing pairs. Wnen two shock mounts are to be removed from RCC-1 containers, they shall De the fourth pair from the bottom. Wnen four snock mounts are to De removed, tney shall be the fourth and fifth pair from the bottom. s Wnen four shock mounts are to be removed from the RCC-3 containers, they shall be the third and nintn pair from the bottom. Wnen six snock mounts are to be removed, they snail De third, fifth, and ninth pair from the bottom. Wnen eight snock mounts are to be removed, they snall be tne tnird, fifth, sixth, and ninth pair from the bottom. 9. Before container closing operations, verify the following: l a. Container base interior cleealiness using a mirror to see under the fuel assenclies. b. Container lid interior cleanliness. Container gasket in proper location & in good condition. c. ~ d. No water or moisture present inside the container. NOTE: Cnce a snipping container has oeen inspected, continuous Q. C. surveillance must be maintained until tne container is closed. If an inspector nost l 1 eave the area Defore tne container is closed, eitner a second inspector I must continue the surveillance or the container must be reinspected. O 4175Q:3
,ry ,/m, ,r i ) \\ ) \\u) ATTACHMENT 1 (QCI 938602 f. 938603)- Top Closure' Jack Screws Must Le Oriented As Shown NOTE: Location of Jack screws as shown are for 15x15 and 17x17 fuel assemblies. Jack screws must be moved to the adjacent hole locations for 14x14 and.16x16 fuel, assemblies. g 4 g-O 'k. TOP RIGHT TOP LEFT A eis .[Il~i l I .l dw ew 1 i 'II I' -( -}- -(b / e - i + v u %5: Q\\ l l 1 I \\ f I l MA BOTTOM RIGHT I BOTTOM LEFT y, .ii: - i - s i ii' i in li 1 ) ,!'t! i i, c.f-M [Of .s [! O l [ 'u g
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ATTACHENT 2 TO QCI 938603 Fuel Assent)1y Dwg. Weight 685.3872 1066 1598E42 1232 1193E92 870 1101E76 1467 1559E05 1365 1559E13 1467 1559E98 1467 1462E82 1453 1189E17 1310 1598E40 1443 1224E29 1210 1222E31 1440 1541E98 1197 1553E80 1135 1598E38 1310 1222E32 1274 1557E27 1310 1541E26 1467 0 O 4 O 2404Q:3
.u ucv:en t w 4. un ATTAC EEST 3 STABILIZER BAR & LOCK PIN CRIENTATICN IN I-BOLT T M CONTAINERS THE STABILIZER BAR SHOULD BE PLACED IN THE BRACKET Ale TE LOCK!!IS PIN INSERTED WITH THE RELEASE BUTTON END OUTSIDE THE'.BAACgN. (TOWARD THE CENTER OF THE CONTAINER). SEE FIGURE 2 BELOW. IN OTHER CONTAINERS THE ORIGINAL BRACKET IS TOO CLOSE TO THE OUTER SHELL AND A REPAIR PROGRAM IS IN PROGRESS. FOR REPAIRED CONTAINERS THE i STABILIZER BAR SHOULD BE PLACED IN THE SLOT CREATED BY THE REPAIR. THE LOCKING PIN SHOULD BE INSERTED WITH THE RELEASE BUTTON END TOWARD THE CENTER OF THE CONTAINER AND THE LOCKING BALLS TOWARD THE CONTAINER SHELL. SEE FIGURE 1 BELOW. FOR UNREPAIRED CONTAINERS THE STABILIZER BAR SHOULD BE PLACED OUTSIDE THE BRACKET (TOWARD CONTAINER CENTER). THE LOCKING PIN SHOULD BE INSTALLED WITH THE RELEASE BUTTON END INSIDE THE BRACKET (TOWARD THE - CONTAINER SHELL) AND TE LOCKING BALLS OUTSIDE TE BRACKET AM) THROUGH THE STABILIZER BAR (TOWARD THE CENTER OF THE CONTAINER). SEEFIGuaE',[.
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QCI REVISION CD/ER LETTER QCI 938604 REVISION 14 NOTES: 1) DESTROY ALL C03IES OF PREVIOUS REVISIONS TO THIS QCI!.
- 2) No reinspection required for parts in-process and/or released parts; exceptions shall be handled by Special Routing.
CHANTS MADE BY THIS REVISION: Page 2 - Revised item 3 to include new containers which have 2 out-riggers only. O
- 'M~#f Prepared By:
l Kality Control Engineer Date Approved By: 1,[b // / I ality Control Manager / Qdte j ( Concurrenc l'b k-2/4r 9(.-/ /w L- +/n W Date Q. C/ Inspan Manager Q. C. Engineering Manager Date h.$460 i./.u/h* Area Q. CL Supervisor Date i O l 4275Q:3
ESTINGHOUSE NUCLEAR FUEL DIVISION QUALITY CONTROL INSTRUCTION Page 1 of 2 QCI No.: 938604 Rev.: 14 Rev. Date: 11/21/85 Engineer: J. Bond SUWECT: FUEL AS:EMELY SHIPPING CONTAINER SCPE: AFTER CONTAINER CLOSING DRAWING: CHARACTERISTIC P ERATION DESCRIPTICN FREQUENCY Read QCI 000198 and comply with the applicable paragraphs. In case of conflict between QCI 000198 and this QCI, tnis QCI will prevail. Applicable JSA procedures: N/A GEERAL Visually inspect all shipping containers after closing 1004 INSTRUCTIONS for completeness and acceptacility per the items listed 'q in this QCI. g Initiate a container checklist, Page 2 of this QCI, and indicate inspection results as inspection steps are completed. If the container is not acceptable, notify Manufacturing that repairs are needed. Place the inspection checklist with the container routing to identify tne needed repairs to Manufacturing. When notified by Manufacturing that repairs have been made, reinspect the repaired items and check the ACC block if they are acceptaDie. When all items of the et.tainer cnecklist have been accepted or properly reworked and accepted, stamp the container routing and enecklist. O 4275Q:3 i
i Page 2 of 2 QCI No.: 938604 Rev.: 14 CHARACTERISTIC (PERATION DES'RIPTION FREQ TNCY FUEL ASSEMBLY SHIPPING CONTAltER INPECTION CHECKLIST Container Serial No. Length 137" 160" Inspector Date Accepted Closed Container Visual 1005 Inspection Unless Otherwise ACC REJ R/W Noteo 1. Verify that container lid is properly seated on the container base. 2. Verify that all closure colts are present, in acceptable condition and have been securely tightened by checking manually with a wrench. Verify that T-bolts are positioned crosswise with slot. 3. Verify that all four (4) or two (2) out-rigger mencers, as applicaole, are present. 4. Verify that all out-rigger members have been secured to the container by operable locking pins attacheo to the container with wire. 5. Verify that the leveling pads on the out-riggers are in good condition, operable oy hand and have been raised. 6. Verify that hex head nuts have been tack welded to the end of the Jackscrew. 7. Verify that the air valve and cap are present. Re-place cover plate and tighten nuts securely. o O 4275Q:3
G QCI REVISION COVER LETTER QCI 938606 REVISION 6 NOTES: 1) DESTROY ALL COPIES OF PREVIOUS REVISIONS TO THIS QCI!
- 2) No reinspection required for parts in-process and/or released parts; exceptions shall be nandlec by Special Routing.
CtWES MADE BY THIS REVISION: Page 2 - Item 3.A. - Expanded requirements. t be v e t t N F-7~/ MI Prepared by: tydlit? Control Engineer Oate Approved by: d#dt /I[ eve.) 7.X 44 Date pafity' ContfoY /anager Concurrences: lA$NaNr?#w f . &nd) f$t-zur 9-/9.f4 Date Q. C. In$ tion ManJK er D.ite 3 Q.C.AngfpringManager ft Eill 9 YN bk ~A Manufacturfnt) Date Area Q.~C. Supervisor Date 3479Q:3
ESTINGHOUSE NUCLEAR FUEL DIVISION QUALITY CONTROL INSTRUCTIONS Page 1 of 3 QCI No.: 938606 Rev.: 6 Rev. Date: 9/24/84 Engineer: J. Bond SUNECT: ' FUEL ASSEH8LY SHIPPING CONTAIER INSPECTION SCCPE: LOADED WITH R00 CONTAINERS ORAWING: 1215E34 CHARACTERISTIC OPERATION DESCRIPTION FREQUENCY Read QCI 000198 and comply with the applicable paragraphs. In case of conflict between QCI 000198 and this QCI, this QCI will prevail. Applicaole JSA Procedures: N/A 1004 OPEN CONTAINER Visually inspect all snipping containers after rod oox O INSPECTION loading for completaness and acceptaoility per the items O AFTER LOADING listed in this QCI. The container must ce refuroisned and released oy Quality Control. Initiate the Container 01ecklist, Q.C. Torin 481 and indicate 1004 inspection results. 01ecklist must be 41th the inspector at all times. Checklist must be completec for items required. Initiate QCON for items tnat are not acceptacle and record 1004 QCON number on checklist. After container nas been repaired, entec acceptance oate 1005 and inspector stamp on checklist. Also, check the reworked (R/W) olock next to the rejected item. 1. A. Verify that the four Dolts are ecurely tigntened 100% against the rod ooxes. B. Verify that a ruocer pad is bon.so to eacn of the 1004 pads on tne four oolts, and Dolts are secured against the rod oox. 1006 2. Verify tnat tne two vertical staoiltzing cars are secured to the container with a hexnaad oolt, washer, and nut at one end; and an operaole locking pin attached to the staoilizing oar with wire at the otner end. The snank portion of tne locking pin must ce 1-1/2" long ( ininimum. 3479Q:3
/" % Page 2 of 3 QCI No.: 938606 Rev.: 6 CHARACTERISTIC P ERATION OESCRIPTI0rd FREQUENCY PEN CONTAIfER 3. A. Verify, that.the grid clamping' frame assemolles 1004 INSPECTION are properly. located against'tne rod oox on or as AFTER LOADING near as possiole to tne rodoox reinforcing bars, (Continued) and are secured in place on the strongoack. B. Verify that the clamping frames are securely 1004 fastened -- i.e., cap screws tightened. 4. Verify that twenty-two (22) snock mounts are present. 1004 5. A. Verify tnat the two lateral cross bars nave been 1004 retracted into the lock tuce and secured with an operaole locking pin attacned to tne container oy wire. 8. Verify tnat the oars are secured by pull testing 1004 each car manually. 1004 N 6. Verify that the two hexhead Dolts are present and in [\\ good condition on the two (2) support pad Orackets used to secure tne lateral cross cars in their extended position. 1004 7. Verify that the container gasket is in proper location and in good condition (not broken ut taped). 1004 8. Verify that the interior of tne container is clean, dry, and free of all particulate. 1004 9. A. Verify tnat one (1) acceleromet-:r is secured at each end of tne strongeack in t u 137 inch and 160 inch snipping containers. 1004 8. Verify tnat tne green color cocid spring is located in the lower portion of tne pla ic enclosure and is in position oetween the two 2) green color coded points. Verify tnat the yellow color coded spring is located 1004 C. in the upper portion of the plastic enclosure and is in position between the two (2) yellow color coded points, 1004 D. If eitner the green or yellow spring is not in the n proper position or if it is questionaole, notify I ) the Q.C. supervisor immediately. 3479Q:3
T O Page 3 of 3 QCI No.: 938606 Rev.: 6 CHAHACTERISTIC 03ERATION DESCRIPTION FnEQlENCY
- 10. Visually inspect rod ooxes and verify the following:
1004 A. No oroken or spring hinges or latches. 6. No open spaces along edges of lid,
- 11. Verify tnat no foreign material is present inside tne 10tX shipping container at the time the snipping container lid is positioned and closed.
Q.C. inspector must ce present.
Attachment:
Q.C. Fonn 481 i lO l l 4 0O l 3479Q:3 l L
O Q.C. Form 481 Attachment to QCI 938606 Revision A Page 1 of 1 FUEL ASSEMBLY SHIPPING CONTAItER INSPECTION CHECKLIST (Rod Snipments) ACC REJ R/W l _l l l l l 1. a. Four bolts securely tightened. l l l l l l 0. Rudoer pads on four Dolts, and bolts secured against rod box. l l l l l l 2. Vertical staoilizing cars secured. l l l l l l 3. a. Grid clamping frames properly located and secured to strongoack. l l l l 1 1 0. Clamping frames secured -- cap screws tigntened. I I i l l l 4. Shock mount quantity. l l 1 l l. l 5. a. Lateral cross cars retracted and secured. l l l l l l 0. Manual pull test. l l l l l l 6. Two (2) hexhead bolts condition as sepport pad brackets. ) l l l l l 7. Container closure gasket location and condition. l l l l l l 8. Container interior clea1, dry, free of all particulate. l l l l l l 9. Accelerometer springs a e correctly positioned. l l l l '.) l
- 10. Visual inspection of rod ooxes.
l l l_,1 I i
- 11. Container lid closure verified in presence of Q.C. Inspector.
3479Q:3 s
T O April 28, 1986 U.S. Nuclear Regulatory Ocentission Division of Fuel Cycle and Material Safety Office of Nuclear Material Safety and Safeguards Washington, D.C. 20555 Attention: Mr. Charles E. MacDonald, Chief L nsportation certification Branch subject: Suhaittal of Additional Information for Application for Renewal of ROC shipping W, certificate of Ocagliance No. 5450, ~ Docket 71-5450
References:
- 1) West 4PM Intter Number IA 85-101, dated narwnhar 20, 1985 frcet A.J. Nardi to C.E. MacDonald
- 2) USNRC Iatter dated February 28,1986 "Icet C.E. MacDonald to A.J. Nardi The Wes+4 P M Electric Corporation hereby subnits this additional information to styport the application for rensual (Reference No.1) of certificate of Otagliance No. 5450 for the ROC shipping Package. This information is in response to the USNRC questions (Reference No. 2).
The information is provided in the fo::st of revised pages to the consolidated l application and as revised drawings. Attachment No.1 to this letter provides a response to each question given i' by Reference 2 to aid your review of this information. Attachment No. 2 to this letter provides the information p aary to tpdate the set of l l L. a
drawings included in Attachment No. 12 to the consolidated application. The Revision Record included in the application doctaments the other pages which have been revised. Each page of text is further marked in the margin to identify the specific area where changes have been made. If you have any questions commig this application, please contact me at the above address or telephone (412)256-6054. Very truly yours, A. . Nardi, Maplager NES License A&ninistration ATN/pe l l O
OVERSIZE . DOCUMENT ~ l PAGE PULLED l SEE APERTURE CARDS i l NUMBER OF PAGES: $5 l ACCESSION NUMBER (S): 8906Q70076 X/fo6&7C/ 46 7F /60 i s% /65 1 89 9(o /05 /& /29 /97 /3& /82 /4 A l APERTURE CARD /MARD COPY AVAILABLE FROM RECORD SERVICES BRANCH,TIDC FTS 492 =S989 i l- - -}}