ML24260A171
| ML24260A171 | |
| Person / Time | |
|---|---|
| Site: | 07105086 |
| Issue date: | 09/09/2024 |
| From: | Freudenberger R BWXT |
| To: | Document Control Desk, Office of Nuclear Material Safety and Safeguards |
| References | |
| 24-046 | |
| Download: ML24260A171 (1) | |
Text
L eWXr BWX Technologies, Inc.
September 9, 2024 24-046 ATTN: Document Control Desk Director, Division of Spent Fuel Management, Office of Nuclear Material Safety and Safeguards U.S Nuclear Regulatory Commission Washington D.C. 20555-0001
References:
NRC (Document Control Desk) Storage and Transportation Licensing Branch (Doyle) to BWXT (Ward) - Certificate of Compliance No. 5086 Revision NO.
16, for the Model NO. UNC 2600 Transportation Package
Subject:
Request for Renewal of Certificate of Compliance No. 5086 for the Model UNC 2600 Package
Dear Sir or Madam:
BWXT Nuclear Operations Group, Inc., requests that the referenced Certificate of Compliance, for the UNC 2600 shipping container be renewed. Renewal is being requested prior to the expiration date of December 31, 2024 for Certificate of Compliance No. 5086, Rev. 16. No other changes are requested at this time. The Safety Analysis Report for Packaging (SARP) for this container is enclosed.
If you have questions or require additional information, please contact Daniel Ashworth, Manager of Licensing and Safety Analysis, at dlashworh@bwxt.com or 434-522-5472.
Sincerely,
,u.....J.,~~
Richard J. Freudenberger Manager, Environment, Safety, Health & Safeguards BWXT Nuclear Operations Group, Inc. - Lynchburg Enclosure cc:
NRC, James Downs, Senior Project Manager NRC, Resident Inspector NRC, Region II BWXT Nuclear Operations Group, Inc.
2016 Mt. Athos Road Lynchburg, VA 24504 USA t: +*1.434.522.6000 www.bwxt.com People St r ong INNDVATIDN DRIVEN >
BWXT Nuclear Operations Group, Inc.
ENCLOSURE (27 Pages) 2016 Mt. Athos Road Lynchburg, VA 24504 USA t: +1.434.522.6000 www.bwxt.com People Strong INNDVATIDN DRIVEN >
UNC 2600 Safety Analysis Report for Packaging Application for License USA/5086/B(U)F BWXT Nuclear Operations Group, Inc.
Lynchburg, Va.
March,2016
Table of Contents Page I of 2 Page I.
General Information 1.1.
Introduction 1.2.
Package Description 1.2.1.
Packaging I
1.2.2.
Operational Features 2
l.2.3.
Contents of Packages 2
- 2.
Structural Evaluation
- 2. 1.
Structural Evaluations 3
- 2. 1.1.
Discussion 3
2.2.
Weights and Center of Gravity 4
2.3.
Mechanical Properties of Materials 4
2.4.
General Standards for all Packages 4
2.4. 1.
Minimum Package Size 4
2.4.2.
Tamperproof Features 4
2.4.3.
Positive Closure 4
2.4.4.
Chemical and Galvanic Reactions 4
2.5.
Lifting and Tiedown Standards for All Pkgs 5
2.5.1.
Lifting Devices 5
2.5.2.
Tiedown Devices 5
2.6.
Normal Conditions of Transport 5
2.6. 1.
Heat 5
2.6.2.
Cold 5
2.6.3.
Pressure 5
2.6.4.
Vibration 5
2.6.5.
Water Spray 6
2.6.6.
Free Drop 6
2.6.7.
Corner Drop 6
2.6.8.
2.6.9.
Compression 6
2.7.
Hypothetical Accident Conditions 6
2.7. 1.
Free Drop 6
2.7.2.
Puncture Test 6
2.7.3.
Thermal Test 6
2.7.4.
Water Immersion 7
2.7.5.
Summary of Damage 7
2.8.
Special Form 7
2.9.
Fuel Rods 7
- 2. 10.
Appendix 7
L
Table of Contents (cont'd)
Page 2 of 2
.).
- 2. 10.1.
- 2. 10.2.
Thermal Evaluation Current Package Design Drawings Original Package Design Drawings
- 4.
Containment
- 5.
- 6.
4.1.
4.2.
4.3.
Containment Boundary Requirements for Normal Conditions of Transport 4.2.1.
Release of Radioactive Materials 4.2.2.
Pressurization of Containment Vessel 4.2.3.
Coolant Containment 4.2.4.
Coolant Loss Containment Requirements for Hypothetical Accident Condition 4.3. 1.
Fission Gas Products 4.3.2.
Release of Contents Shielding Evaluation Criticality Evaluation
- 7.
Operating Procedure 7.1.
7.2.
7.3.
Procedures for Loading Package Discussion and Results Procedures for Unloading Package Preparation of Empty Packages fo r Shipment
- 8.
Acceptance Tests and Maintenance Program 8.1.
8.2.
Acceptance Maintenance Program 8.2.1.
Structural and Pressure Tests 8.2.2.
Leak Tests 8.2.3.
8.2.4.
8.2.5.
8.2.6.
8.2.7.
Subsystem Maintenance Valves, Rupture Discs, and Gaskets on Containment Vessel Shielding Thermal Miscellaneous 7
7 7
7 8
8 8
8 8
8 8
9 9
9 10 12 13 14 14 14 14 14 14 14 15
CERTIFICATE OF COMPLIANCE 5086; Page 1 UNC-2600 PACKAGE March, 2016 1.0 General Information This package consists of an outer steel drum and an inner steel cage assembly which centers and firmly locates an inner steel box. This box contains the fuel elements authorized for shipment. All aspects of design modification, fabrication, and use are controlled under the QA Plan approved under Docket 71 -0088.
1.1
==
Introduction:==
The UNC 2600 package is used to ship fuel elements with U-235 enrichments up to 100%. Fuel elements are clad components with no exposed fissile material.
Each package is limited to a maximum of 375 grams. U-23 5. The loading wi ll not exceed the A2 values and will be verified prior to shipment.
No credit is taken in analysis for the shipping container. It is assumed to fail completely under the hypothetical accident condition. As a result, a Criticality Safety Index (CSI) of 50 is being assigned to the package.
1.2 Package
Description:
1.2.1 Packaging
(1 )
(2)
W eights:
Nominal empty container Max. weight of contents Nominal gross weight Materials of Construction:
840 lbs 265 lbs 1105 lbs The package is constructed of mild steel, using two high strength steel bolted closure flanges to retain the fuel box in an inner steel cage. The fuel box is also of mild steel construction. An oak wood block measuring at least 2-1 /2" long is positioned at each end of the fuel box to prevent product damage and keep the product from moving during normal transport. Additionally, rubber bumpers are used at both ends, external to the cage, also to distribute the axial loads. The construction details are shown in Drawing 8-2600-2, Sheets 1, 2, 3, 4, 5, and 6, Rev. 3 which is provided in Appendix 2.10. 1.
CERTIFICATE OF COMPLIANCE 5086; Page 2 UNC-2600 PACKAGE March, 2016 1.2.2 1.2.3 (3)
==
Description:==
(All Dimensions are Nominal)
The fuel box (inner container) is an 11 gage steel box with inside dimensions of 2-5/8" x 7 11 x 96". It is supported in a 22-1/2 11 I. D. by 102-1/2 11 long 14 gage steel drum by a welded reinforced insert cage. This cage is 97 11 long, and is formed by nine 21-1/2" diameter by 3/8 11 thick steel plates (disks) spaced approximately 12" apart by 1-3/4 11 x 1/4 11 steel strips welded radially to each of the nine disks. The 12 11 sections at either end of the cage are further strengthened by eight I II x 1" (1/8 11 angle) welded to the structure.
A channel to hold the fuel box is formed through the center of the cage by 1-1/2 11 x 1-1/2 11 x 1 /8" angle irons which are also welded to each disk. Four additional l II x l II x 1/8 11 angles are used to further strengthen this fuel box slot. The fuel box is retained within the cage channel by two 1/2 11 thick diameter high strength 4130 steel closure flanges which are secured to each end of the cage with eight 7 /8 11 SAE Grade 5 steel bolts.
The outer container closure is a 14 gage drum lid which is secured to the drum with a 12 gage bolt locking ring with drop forged lugs, one of which is threaded, having a 5/8 11 diameter bolt.
(4)
Pressure Relief:
Pressure buildup is precluded because the drum lid has no gasket, facilitating pressure equalization.
Operational Features Use of the package is simple, with minimal operational features. Proper use of the package is described in Section 7.
Contents of Package
( 1)
Type and Form of Material The UNC-2600 package is used to ship unirradiated fuel elements.
The element is a clad fuel component. The contained uranium may be enriched up to 100% in the U-235 isotope. Each element may be wrapped in protective plastic.
CERTIFICATE OF COMPLIANCE 5086; Page 3 UNC-2600 PACKAGE March, 2016 (2)
Maximum Quantity of Material Per Package:
375 gram U-235 as clad fuel elements.
(3)
Fuel Geometry Constraints:
The inner 11 gage steel box confines the uranium materials to a 2-5/8" x 7" cross section.
2.0 Structural Evaluations 2.1 Structural Evaluations:
2.1.1 Discussion
Section 1.2 identifies the principal construction details of the package design. Drawing B-2600-1 details the original design which had been drop tested, and is provided in Appendix 2.10.2 The current design, specified in Drawing B-2600-2 has been analytically evaluated using Finite Element Analysis (FEA).
The current design improves the mechanical retention of the fuel box within the cage, using a 12" 0.0. x 1/2" thick 4130 AMS 6370 heat treated steel closure flange secured with eight 7 /8" SAE Grade 5 steel bolts to each end of the cage. The use of these closure flanges adds less than 40 lbs. to the empty weight of the original package, and this is offset by a reduction in the product loading from 308 lbs.
to 265 lbs. Additionally, the current design specifies that the bumper disks at each end of the cage be fabricated of a 60 durometer, 2:_ 2500 psi rubber with a Bell Brittle Point temperature of at least -?OF.
A prototype package (Drawing B-2600-1 ), representative of the original design has been previously tested as described in Section 2.7. The current design (Drawing B-2600-2) has been additionally evaluated for the drop test conditions using FEA. This evaluation is also described in Section 2.7.
2.2 Weights and Center of Gravity:
The center of gravity is essentially the center of the package in both the loaded and empty conditions.
CERTIFICATE OF COMPLIANCE 5086; Page 4 UNC-2600 PACKAGE March, 2016 2.3 Mechanical Properties of Materials:
The package is primarily fabricated of mild steel, and the 12" diameter closure flanges are 4130 AMS 6370 heat treated (Rockwell C = 28-33) steel. The properties of these steels, the SAE Grade 5 steel bolts, and the Rubber disks at each end of the cage are provided in Appendix 2.10.4.
2.4 General Standards For All Packages:
2.4. l Minimum Package Size:
The package dimensions shown in drawing B-2600-2 exceed the minimum package size specifications of 10 CFR 71.
2.4.2 Tamperproof Features:
A tamperproofseal is inserted in the end of the bolt wh ich secures the cover ring seal closure at the front of the package.
2.4.3 Positive Closure:
The inner box which contains the fuel is held closed with steel banding. The banded box is constrained by the angle iron channel within the welded cage assembly. This cage assembly is retained within the outer container, as demonstrated by the accident test sequence and the ana lysis discussed in Section 2.7. The outer container lid is held closed by the ring seal which is bolted closed.
2.4.4 Chemical and Galvanic Reactions:
2.5 The steel package construction is not vulnerable to degradation from uch reactions during shipment, or as a result of accident conditions.
Lifting and Tiedown Standards For All Packages:
2.5.1 Lifting Devices:
Packages are lifted to and from the transport vehicle using appropriate slings, and other normal techniques. These are engaged with fork lifts or other standard mechanisms.
CERTIFICATE OF COMPLIANCE 5086; Page 5 UNC-2600 PACK.AGE March, 2016 2.5.2 Tie Down Devices:
No tie down devices are incorportated as part of the package design.
2.6 Normal Conditions of Transport:
2.6.l Heat The low carbon steel construction of the package drums and internals, and the design and construction of the fuel elements retain ductility through a temperature range of -40 to + 130 degrees, F. The rubber bumpers have a Bell Brittle Point at or below -70 F, and are serviceable at the specified -40 F. The package design imposes minimal stresses, and fracture of the steel construction or the non-brittle zirconium fuel cladding will not occur.
2.6.2 Cold See Section 2.6. 1
2.6.3 Pressure
The package is closed with an ungasketed lid, and will not retain pressure differentials. If a gasketed lid were incorrectly applied, the outer drum may dimple, but the containment of the uranium contents will remain unimpaired.
2.6.4 Vibration
No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
CERTIFICATE OF COMPLIANCE 5086; Page 6 UNC-2600 PACKAGE March,2016 2.6.5 2.6.6 2.6.7 Water Spray:
No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
Free Drop:
No credit is taken for the ability of the package to protect the content during transport; therefore, this ection is not applicable.
Corner Drop:
No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
2.6.8 Penetration
2.6.9 No credit is taken for the ability of the package to protect the content during transport; therefore, this ection is not applicable.
Compression:
No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
- 2. 7 Hypothetical Accident Conditions
- 2. 7.1 Free Drop:
No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
2.7.2 Puncture Test:
No credit is taken for the abi lity of the package to protect the content during transport; therefore, this section is not applicable.
2.7.3 Thermal Test:
No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
CERTIFICATE OF COMPLIA CE 5086; Page 7 UNC-2600 PACKAGE March, 2016 2.7.4 Water Immersion:
No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
2.7.5 Summary of Damage:
2.8 The criticality safety analy is does not credit the ability of the shipping container to protect the contents in any way. The assumption is that during the HAC, the fuel is ejected from the shipping container and attains an optimum configuration.
Special Form:
ot applicable 2.9 Fuel Rods:
Not applicable 2.10 Appendix:
2.10.1 Current Package Design Drawings 2.10.2 Original Package Design Drawings 3.0 Thermal Evaluation No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
4.1 4.0 Containment Containment Boundary:
No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
CERTIFICATE OF COMPLIANCE 5086; Page 8 UNC-2600 PACKAGE March, 2016 4.2 Requirements For Normal Conditions of Transport:
No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
4.2.1 Release of Radioactive Materials No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable. It is assumed that all radioactive material is released.
4.2.2 Pressurization of Containment Vessel o credit is taken fo r the abi lity of the package to protect the content during transport; therefore, this section is not applicable.
4.2.3 Coolant Containment No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
4.2.4 Coolant Loss No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
4.3 Containment Requirements For Hypothetical Accident Conditions No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
4.3.1 Fission Gas Products This section is not applicable since the material being shipped is unirradiated.
CERTIFICATE OF COMPLIANCE 5086; Page 9 4.3.2 Release of Contents UNC-2600 PACKAGE March, 2016 No credit is taken for the ability of the package to protect the content during transport; therefore, this section is not applicable.
5.0 Shielding Evaluation The content of the shipping container is an unirradiated uranium fuel element. This does not result in any external dose.
6.0 Criticality Evaluation As noted in the previous sections, no credit is taken for the ability of the package to protect the content during transport. The a sumptions are: 1) the fissile material is released from the package, 2) the cladd ing fai ls, 3) the uranium becomes finel y divided, 4) mixes optimally with water in a spherical geometry and 5) is full y reflected by water. To assure subcriticality in this configuration, the total amount of U-235 must be below the minimum critical mass.
The minimum critical mass of U-235 is about 820 grams'. To provide a safety margin, the maximum allowable amount of U-235 in a shipment wi ll be limited to 750 grams. If the maximum number of shipping containers is limited to two per shipment, each container can have 375 grams U-235 with a CSI=50.
1LA-I 0860, 1986 Revision, "Critical Dimensions of System Conta ining 235U, 239Pu and 233U" by H.C.
Paxton, N.L. Provost.
CERTIFICATE OF COMPLIANCE 5086; Page 10 UNC-2600 PACKAGE March, 2016 7.0 Operating Procedures The UNC-2600 Package is used to ship up to 375 g U-235 of fuel elements in non-decomposable form, and up to 100% enrichment in the U-235 isotope. CSI=50 per package, thus limiting two to a shipment. Maximum payload weight is 265 lbs. The detai led loading and unloading procedures are given below and are in compliance with subpart G of 1 0CFR 71. All operating procedures for the UNC-2600 shipping package are approved by NOG plant management. These procedures have been prepared to meet the intent of NUREG/CR-4775, "Guide fo r Preparing Operating Procedures for Shipping Packages".
7.1 Procedures For Loading Package Discussion and Results Unacceptable shipping packages shall be marked accordingly, and appropriately repaired before use.
PROCEDURE
- 1.
Assure that the package is to be loaded in accordance with the Certificate of Compliance as specified in written procedures and check lists.
Compliance with these procedures and completion of the check list shall be recorded on appropriate shipping documentation.
- 2.
Each UNC-2600 package shall be inspected prior to each use. The fo llowing requirements are to be checked; That the maintenance inspections required by Section 8.2 have been conducted within the 12 months of use.
Compliance with the requirements of Section 8.2.7. 1.
That the package is in unimpaired physical condition.
Inspect inner box for damage.
Inspect bolts for thread condition.
Inspect the top closure flange surfaces fo r damage. Inspect drum lid, ring seal, and locking bolts for damage, and replace as necessary.
CERTIFICATE OF COMPLIANCE 5086; Page 11
- 3.
Requirements for Loading Box:
UNC-2600 PACKAGE March, 2016 Verify that the shipment consists only of fuel elements. Each element may be wrapped in protective plastic.
Verify the total U-235 per package is less than 375 grams.
Verify that the A2 values ar not exceeded based on the actual isotopic values for the loaded contents.
Elements shorter than 91" may be positioned with longer oak wood spacers at the ends of the box to prevent their movement during transport. This bracing protects the element from shifting.
Verify contents do not exceed 265 lbs. consisting of elements, wrapping, and wood spacers.
Each loaded box is to be strapped closed with three (3) 0.02" tk. x 1/2" wide x 24" lg. (approx.) steel bandi ng straps.
- 4.
Requirements fo r Loading Box into Package:
Slide the sealed box into the channel, assuri ng the end is flush with the face of the disk.
Locate the 12" diam. 1/2" thick steel closure flange to align the bolt into the bolt holes, and secure each bolt with a nut. These are to engage the bolts welded to the backside of the disk, and tightened to a snug closure.
- 5.
Requirements For Sealing Package:
Place the rubber disk into the package to fi ll the free space at the front end of the package.
Close the front of the package with a 14 ga. drum lid which has no gasket.
Secure this lid with a 12 ga. ri ng seal, and secure the seal by torquing (40-45 ft. lbs.) the locking bolt into the threaded end of the ring seal.
Tighten jam nut against the locking bolt, and apply the tamper-safe seal to the locking bolt.
CERTIFICATE OF COMPLIANCE 5086; Page 12 UNC-2600 PACKAGE March, 2016 7.2
- 6.
Survey Requirements:
Removable surface contamination
_:s 2200 (beta and gamma) dpm per l 00 sq. cm.
_:s 220 (alpha) dpm per I 00 sq. cm.
Radiation levels _:s 200 mrem per hour on contact.
Radiation levels < 10 mrem per hour at 1 meter.
- 7.
Each shipment of the UNC 2600 package shall require the preparation of, and retention for three years, of those records specified in 1 0CFR 71. 9 1 as appropriate.
- 8.
Verify that each package has a proper metal identification plate welded to the outer drum.
- 9.
All shipments shall be Exclusive Use.
Procedures For Unloading Package The UNC-2600 package is designed to be unloaded with commonly avai lable tools and equipment in accordance with the fo llowing procedures:
PROCEDURE
- 1.
Prior to unloading, verify that the following documentation is included with the shipment.
Radiological survey data Packing list
- 2.
Conduct a survey prior to unloading to assure that:
Removable surface contamination
_:s 2200 (beta and gamma) dpm per 100 sq. cm.
_:s 220 (alpha) dpm per I 00 sq. cm.
CERTIFICATE OF COMPLIA CE 5086; Page 13 UNC-2600 PACKAGE March,2016 7.3 Radiation levels_::: 200 mrem per hour on contact Radiation levels < l 0 mrem per hour at I meter
- 3.
Remove the tamper-safe seal, drum lid, and the rubber disk to expose the bolted closure fl ange.
- 4.
Loosen and remove the eight closure flange bolt nuts and remove the flange.
- 5.
Remove the inner box from the package using a manual or mechanical means. Remove the three steel closure bands from the box, and remove the elements from the box in accordance with applicable criticality control limits.
- 6.
Replace the empty box into the package, and resecure the closure flange with the eight bolt nuts finger tightened. Replace the drum lid with the ring seal, and secure.
Preparation of Empty Package for Shipment Empty UNC-2600 packages will be prepared for shipment by verify ing the absence of fuel, closing all closure bolts, and securing the lid with a ring seal. The locking bolt is to be tamper-sealed, and appropriate labels are to be affixed to the package exterior to signify that it is empty.
A survey shall be performed on the outer package surface to ascertain that the removable surface contamination is _::; 2200 (beta and gamma) dpm per I 00 sq. cm or _::;
220 (alpha) dpm per I 00 sq. cm.
CERTIFICATE OF COMPLIANCE 5086; Page 14 UNC-2600 PACKAGE March,2016 8.0 Acceptance Tests and Maintenance Program 8.1 Acceptance Tests o new fabrication is allowed; therefore, Section 8.1 is not applicable.
8.2 Maintenance Program 8.2.1 Structural and Pressure Tests A general inspection of the shipping package shall be made annually while in service. See Section 8.2.7.1. Maintenance shall be performed prior to placing containers back into services once removed.
8.2.2 Leak Tests Not applicable.
8.2.3 Subsystem Maintenance Not applicable.
8.2.4 Valves, Rupture Discs, and Gaskets on Containment Vessel Not appl icable.
8.2.5 Shielding Not applicable.
8.2.6 Thermal Not applicable.
CERTIFICATE OF COMPLIANCE 5086; Page 15 8.2. 7 Miscellaneous The fo llowing inspections are to be conducted; UNC-2600 PACKAGE March, 2016 8.2.7.1 Within 12 Months Before Use, and Annually while in service The outer surface of the drum shall be visually inspected for rust and scratches. Such defects shall be sanded off and repainted. Any significant dents will be reworked.
The inner cage will be removed from the outer drum and inspected for rust and broken welds. The former will be sanded and repainted, and the latter repaired.
The bottom closure flange shal I be inspected to assure that the bolt nuts are properly secured.
8.2.7.2 Prior to Every Shipment Inspect inner box for damage.
Inspect bolts for thread condition.
Inspect the top closure flange surfaces for damage.
Inspect drum lid, ring seal, and locking bolts for damage, and replace as necessary.
CERTIFICATE OF COMPLIANCE 5086; Appendix 2.10.1 Appendix 2.10.1 Drawing B-2600-2, Sheets 1,2,3,4,5 and 6 Current Package Design UNC-2600 PACKAGE March,2016
\\(>
SIDE Pi.ATE BLOCKS Tl'P. (2 PLACES)
DAN DING STRAP ( I / 2")
(3 l'UCES)
HINGE ASSE,IBLY ID LID DAND STRIP CG)
END PLATE LOCK CLIP (G)
BOTTOM PUTE srnE ANGLE SCRAP BOX ASSEMBLY 102 - 1 /2"
[_,_____ _ _ _______ u, CLOSURE TLAHGE BOLTED AS IN FRONT RUBBER BUMPER
§)@
BARREL ASSEUBLY RING SEAL PER 4g CTR 17 8.IOJ - 5 (1908 EDITION)
TORQUE rn-t5 TT. UIS. AT CLOSURE Vl[ll A-A SCRAP BOX ASSEMBLY PER ITEMS <G THRU @
Rrv1s;ons/Da te REV I 8 SJ 1.) ADD SHEETS 4,5 2.) GRIP WIRE REV. TO 3/111" DIA. AIRCRAFT WIRE ATTACHED 111TH PAD EYES, OR EQUIV.
3.) END VIEW RtV. TO SIIOW ANGLE.
t,) BOLTS TO SAE GRADE 5 5.). IIJPROVED ASSEllBLED VIEWS ran CLARIFICATION Rf visions/Do. tf' REY 2 9 94 GRIP IIIRE IS 3/tfi" DIUI. AIRCRAFT CONTROL Wl*RE, APP. I 8" LG.
USE Of WIRE ON BOTII ENDS OF BOX OPTIONAL WIRE CDNHECTED USING 1/4" TK. 9/16°13/4" STL TABS WELDED TO BOX. I/ t" FILLET WELDS SPACED TO ACCOIIODATE WIRE IN 5/18" IIOLE.
WIRE SECURED USING SWAGED BAU AHO SINGLE SIIAHK. TABS MAY BE PROTECTED Willi TAPERED PROTECTOR TO USE PUC£NEHT IHTO CAGE.
GRIP lflRE ASSEllBLY DETAIi. ON SIIEET 8 CAGE DISK (9 PLACES)
EQ. S'!A,.CED AND TO FIT ITEIJ ~
§ LID CLOSURE Fl.ANGE AN GLE (n) 15/16" DOLT 1101.ES 10* DIA. BOLT CIRCLE
'!rt--~-"'-
\\JRIUED TO FIT LOCATION or WELDED BOLTS WIRE ASSEII BOLTS LOCKll ASIIERS. A< NUTS BOLTS ARE SNUGGED BUT HOT TORQUED.
END VIEII: RUBBER DISK RtlfDVED TYPICAL (2 PUCES)
THOMAS GUTMAN.CONSULTANT W. HARTFORD, CT.
JG/21/9)
UNC-2600 DEFINITION TO REPUCE PRIO REFERENCES TO "AIRCRAFT GRI WIRt:" AND "AIRCRAFT CONTROL IIRt:".
ID/MJ UPGRADED PACKAGE ONE GRIP WIRE ASSEMBLY PER BOX.
NOT TO SCALE 0WG.# B-2600-2 SIIEET I OF 6 REV.
3
(SEE NOTE I I I i'
NOTE:
I.) TYPICAL l'[lDIIENT AS SHOWN FOR INNER I< OIJTCR 3/rf I 21 - 1/2" DIAMETER DISC.
2.) ANGLE IRON AND BOX NOT SHOWN IN SIDE VIEW TO PRESERVE CLARITY.
3.I 12* 0.0. X 1/2°" 4130 AIIS 8370 STEEi. IIEAT TREAT TO ROCKWELL C HARDNESS :
28-33 FLAHCE COVER TO 8£ PIIYSICJ.LLY MARKED TO 511011' STl:£L GRADE, HARDNESS 3d 11 - 45/ 84 (TYP.) 8 PLACES Re:visioni:/Dole REV I 8 113 1.) ADD SHEETS 4,5 2.) GRIP.WIRE REY. TO 3/te*
DIA. AIRCRAn WIHE ATTACHED WITII l'AD EYES, Oil EQUIV.
3.) END VIEW-REV. TO SIIOW ANGLE.
4.) BOLTS TO SAE GRADE 5 5.) ltJPROVEO ASSEMBLED VIEWS FOR CI.ARlflCATION 2 I - I /2" DIA. 3/8" PLATES EQ. SPACED MILD STEEL (SEE NOTE f3 ON THIS SHEET)
BOLTS 15/16" HOLES FUEL nox FRONT VIEW WITH 12'" CLOSURE FLANGE AND RUBBER DISK REMOVED Revisions/Dale iU ***~"- Revi,ion, /Dalt W F.lf THOMAS REV 2 11-08-114
~V 3 10-18-Bt
/d/;3.:-/47P GUTMAN CONSULTANT GRIP WIRE IS 3/te* DIAM. AIRCRAn "GRIP WIRE ASSEMBLY-USED AS W.. IIARTFORD, CT.
CONTROL WIRE, APP. 18° LG.
USE DEFINITION TO REPLACE PRIOR Drown BY RH Dole IOllf/11*
OF WIRE ON DOTH EHDS OF BOX REFERENCES TO
- AIRCRAFT GRIP UNC-2600 OPTIONAL. WIRE CONNECTED USING WIRE:" AND "AIRCRAFT CONTROL A~grav,~ llY TG [!gl, 10ll1{9 UPGRADED PACKAGE 1/4" TK. 8/ltl 0 s3/4" STL TADS 11111£".
!!*llf*w*A BY WK nnl* 10/ll~
WELDED TO BOX. I/ 4* FILLET WELDS ONE GRIP WIRE ASSEMOLY PER I n~v.
SPACED TO ACCOMODATE WIRE IN BOX.
NOT TO SCALE OWG.I n-2600- 2 5/18" IIOLE.
WIRE SECURED USING SIIAGEP BALL AND SINGLE SIIANK. TADS IIAY DE PROTECTED WITH TAPERED PHOTECTOR TO EASE PUC[IIENT INTO CACE.
SIIEET 2 OF 6
0 VIEW A-A SHOWING BOLTS LOCK WELDED ON THREE SIDES TO END DISK.
+
+
+
+ +
END VIEW -
LID AND RUBBER BUMPER REMOVED FRONT & BACK R*v1s10ns/Da. te REV I 8-27-B3 I.) ADD SHEETS 4,5 2.) GRIP WIRE REV. TO 3/18" DIA. AIRCRAFT WIRE ATTACHED WITH PAD EYES, OR EQUIV.
3.) END VIEW REV. TO SHOii ANGLE.
4.) BOLTS TO SAE GRADE ~
5.) IMPROVED ASSEMBLED VIEWS FOR
- CLARIFICATION 0
,- 1-3/4" TYPICAL (B PLACES) 19"
-j 12-1/2" l-1/4"
'I.
BOLT HEAD POSITION LOCK lTELDED 1/4" FILLET THREE PLACES ON EACH BOLT. COOL BETWEEN EACH FACE WELDED.
ll-=! /
FUEL BOX
~
END DISK OF INNER CAGE r RUDDER PARTS TO OE DURABLY MARKED TO IDENTIFY RUBBER SPEC.
DETAIL OF RUBBER BUMPER tr R*vlsiOns/Oo.t*
Ill.. -,.~, Rov1sions/D11to /vrK THOMAS GUTMAN CONSULTANT REV 2 9 08-94
-jEV 3 10- 18 114
- w. HARTFORD, CT.
GRIP WIRE IS 3/18" DIAII. AIRCRAFT "GRIP WIRE ASSEMBLY' USED AS CONTROL WIRE, APP. ta* LG.
USE DEFINITION TO REPLACE PRIOR Drown BY RH Dole 10/21/9]
OF WIRE ON BOTH ENDS OF BOX REFERENCES TO
- AIRCRAFT GRIP Aoorov* d BY TG n,,. 11/21/93 UNC-2600 OPTIONAL WIRE CONNECTED USING WIRE" AND
- AIRCRAFT CONTROL UPGRADED PACKAGE 1/4" TK. 11/18"s3/4" 5TL TABS WIRE".
R*viewed RY \\/K n,,
- 18/21/9]
, WELDED TO BOX. I/ 4* FILLET WELDS ONE GRIP WIRE ASSEMBLY PER I Rr SPACED TO ACCOMODATE WIRE IN BOX.
NOT TO SCALE DIYG.# B-2600-2 5/18" HOLE.
WIRE SECURED USING SIIAGED BALL AND SINGLE SHANK. TABS MAY BE PROTECTED WITH TAPERED SHEET 3 OF 6 PROTECTOR TO EASE PUCEIIENT INTO CAGE.
Scrap Assembly Box Item #
- Reqd.
Name of Part Stock Size Material 1a 1
Bottom Plate 11 Ga. X 7" X 96" LCCGS 1b 2
Side Plate 11 Ga. X 2-5/8" X 96" LCCGS 1c 2
End Plate 11 Ga. x 2-5/8" x 7-1/4" LCCGS 1d 1
Lid 11 Ga. x 96-1/4" x 7-9/16" (Approx.)
LCCGS 1e 1
Hinge MS-35830-2D,(or Equiv.)
Steel 0.093,. tk. x 96" lg.
1f 2
Side Angle 1" x 1" x 1/8" x 96-1/4" Angle LCCGS 1_g 2
End Angle t ~-x.t"x-1 /8" ~ 7-1/4" Angle LCG,;;&_.
fh-_,
2 Wood Positioner 2-3/8" x 2-1/2" x 6-3/4"
'Oak-wood:
t i 1
Grip Wire Assy.
3i1-S--diam:-wire--x-Approx. 16" lg Gal. or stainless including swaged ball shank.
steel 1 i(a) 2 Tab Ball retained by 1/4" tk. x 9/16" x 3/4' steel tabs welded to box.
5/16" hole in tabs to engage swaged ball.
1 i(b) 2 Tapered protector 1/4" tk. x 9/16" high x 2-1/2" lg.
Steel (optional) tapered at both ends to 1/4" land on top to help guide box into cage.
1j 3
Banding Straps 0.02" tk x 1/2" x 24" (approx)
Steel With 0.02" lockclips Box seam welds are continuous. Side angle welds 1/8"-fillet, 3" lg. every 6" for the 96" lengthwise runs. Welds for packages procured on or before 10-9-92 are visually inspected.
Welds for new construction are per AWS D-1.3.
Matl. LCCGS is low carbon, commercial grade steel, also referred to as "mild steel" Barrel Assembly Item#
- Regd. Name of Part Stock Size Material 2a 1
Bottom Drum 14 Ga. 22-1/2" 0. D. x 52" lg. Drum LCCGS 2b 1
Top Drum with 14 Ga. 22-1/2" 0. D. x 52" lg Drum LCCGS no bottom 2c 1
Lid with no gasket 14 Ga. for 55 gal. Drum LCCGS 2d 1
Ring Seal with 12 Ga. For 55 gal Drum LCCGS 5/8" Bolt Closure Bolt is torqued to drilled for tamper 40-45 ft. lbs.
seal.*
Ring seal per 49CFR 178.103-5, 1988 edition.
Welds are continuous. Welds for packages procured on or before 10-9-92 are visually inspected. Welds for new construction are per AWS D-1.3 Matt. LCCGS is low carbon, commercial grade steel, also referred to as "mild steel"
.II AP vl SIQnS / Oci t*
APv1s.ont/ Dci t f
'%I........ Rpv;s.ons. / Oca't* H/~
THOMAS GUTMAN CONSULTANT r
REV I e-27*0~
REV 2 o-oe-o,
~f:v ~ 10-1e-8'
- f t:'{;2.'f ('t'I W. HARTFORD,. CT.
1.) <lDD SHtETS 4,$
CRIP 1ITRE IS :J/18" DIAM. AIRCIUf"T RIP lr!RE "5SEVBLY" SED AS
~. ) GRIP lrlRE REV. 'I' *. :I/ Ill'" CONTROL lrlRE. I.PP. I S" LC.
USE DEF!NmON TO REPLACE PRIOR Drown BY RH Oolo IQ/211'1.l UNC-2600 CIA. AIRCliFT mu:
OF lrlRE ON BOTH ENDS OF BOX REFERENCES TO "AIRCRAFT CRIP Ann-- BY TG nn,. )ll/cll'J'.l ATTACHEI) 'll'ffll PAD OP'T10NAL lrlll CDNNEcn:D USINC 11111£" AND "AIRCRAfT CONTROL UPGRADED PACKAGE
. EYES, OR EQUIV.
1;,* TIC. D/ IS"x:1/ 4" T1t. STL TABS 11'111£".
R*---*~ BY \\JK n~,. )Q/211'1.J
,.) END VlEY REV. TO SHOW'
'fl:UIED TO BQL 1/4' nuzr 'll'ELDS ONE.GRIP 111RE ASSEMBLY PER DWG.j 8-2600,-2 I ~-
~CLE.
SPACED TO ACCOMOD4ff l'lll IN BOX.
NOT TO SC>.IZ 4.) BOLTS TO Sil CIUllE '
6/111" HOLE. lrlRI: SECI/JIEII USINC S114CEll BAU..UCD SlftCU SIWIL Tl.BS
$.) IMPROV!D ASSEWBUD M4 Y BE PROTECTED l'ITB TAPERED SHEET 4 OF 6 VlE'll'S,oa CUJUFICATION P1IOTICTOa 'Ill USE l'UCZIIIIIT llffl) CAC:L
Cage Assembly Item#
- Reqd. Name of Part Stock Size Material 3a 9
Cage Disk 3/8" x 21-1/2" diam LCCGS 3b 8
Rib 1/4" x 1-3/4" x 97" bar LCCGS 3c 4
Support angle 1-1/2" x 1-1/2" x 1/8" angle, 97" lg LCCGS 3d 16 Stiffener angle 1" x 1" x 1/8" angle, 11-45/64" lg.
LCCGS 3e 4
Support angle 1" x 1" x 1/8" angle, 97" lg.
LCCGS 3f 16 Bolts 7/8" diam x 1-3/4" lg, with SAE Grade 5 lock washers and nuts to fit 3g 2
Closure Flange 1/2" tk x 12" diam 4130 AMS 6370 stl, Ht trt to Rock. C =28 -33 3h 2
Rubber bumper 19" diam x 1-3/4" tk 60 Durometer,
~ 2500 psi Rubber BeU Brittle point, -70 F.
Welds are 3/16" fillet. Welds for packages procured on or before 10-9-92 are visually inspected.
Welds for new co_nstruction are per AWS D-1.1.
Matt. LCCGS is low carbon, commercial grade steel, also referred to as "mild steel" Closure flange bolts with lock washers are snugged, but not torqued.
Closure flange and rubber bumper to be physically marked to identify the steel or rubber, to show the steel hardness, and to identify the drawing number. Cognizant QC to mark.
Name Plate Item #
- Reqd. Name of Part Contents of Plate Material 4a 1
Name plate 1/16" tk, and sized to fit lettering LCCGS or SST Plate spot welded to drum, engraved with 1/2" high lettering to show at least:
Model UNC-2600 Gross weight of package: 1105 lbs.
Weights Package Gross Weight:
Maximum Weight of Contents:
1105 lbs 265 lbs.
Inspection and.Acceptance Criteria Cert. of Campi. number 5086 1/8" l~ttering to show Yepf of manufacture Serial#
All parts to be free of raised metal, burrs, or significant dents and.rust.
Vercif'y~ine. l~E!l'ltifi~.tion on the 9,JOSUf~,fl~nges and 1th1f R;ubbet aisf?s:,*,, ~ese shall:-' li>i:Hlj~a9le ta, tne* maiena! identification, ana':the'tteaf' tr_!3at p11oeessir39,.,.,:. *,.,., ** *
- Verify weld inspections for new packages. These must oe certified to AWS D-1.1 or 0-1.3.
For packages procure9 by B&W prior to 10-9-92, verify that all welds are visually acceptable.
Verify the presence of a name plate showing the model number and maximum gross weight.
,ll R* vis;ons/ 0~
R*viSk>ns / Do'tP
~ " *** Lll'-lf'Yi SIOns/ 0Gtf' 1£/'&,J('
THOMAS GUTMAN CONSULTANT REV I e-27-93 REV 2 g-08-94 litV 3 10-18-94 11)/~'IY W. HARTFO~D, CT.
) ADD SHEETS 4.5 GRIP lflRE JS 3/115" DIAM. AIRCRAfi "GRIP ll'IRE ASSEl,IBLr USED AS
.. ) GRIP 'll'IRE REV. TO 3/ 111" CONTROL lf!RE. APP. 16° LC.
USE DtrINmON TO REPUCE PRIOR Drown BY RH Dole 10/zv,)
UNC-2600 DIA. AlRCRAfi ll'IRE OF lflRE ON - BOTH ENDS OF BOX REYERENCES TO
- AIRCRAFT CRIP A--*-~A RY TG nato 10/zv,)
ATTACHED lfln! PAD OPTIONAL WIJU: CONNECTED USING
'll'IRr ANO
- AIRCRAfi CONTROL UPGRADED PACKAGE EYl:S, OR EQUIV.
1/4" TX. g/lll"x3/4" TX. ST!. TABS WIRE".
R-'----' BY w'K,,_,. 10/21/93 3.) END Vltlf REV. TO SHOW 11ELDED TO BOX. 1/4" FlUXI' irt:LDS ONE GRIP ll'IRE ASSOIBLY PER D1TG,# B-2600-2 I ~-
ANCU:.
SPACED TO ACCOUODATE 11IJU: IN BOX.
l'jOT TO SCALE 4.) BOLTS TO SAE GRADE !I
!1/115" HOU:. WIRE SECURED USING SWACED BAU. AND SINGLE SIIANL T>.BS 5.) IMPROvtD ASSEMBLED MAY BE PROTECTED 'lflT!I TAPERED SHEET 5 OF 6 VIE11S FOR CURlnCATION PROTECTOR TO WE PUCEIIDfT lllTO C.ICL
3/ll!" DIAM I APPROX. Ill" LG. INCL'D, SRANI[
fROII AIRCRAFT SfRUCI! CAT.
GAL. OR ST. STEEL 11:d 7 CABLE (P1. 105).
ITEII IIS2011114C (P1. 104) BAU. SHANI( SUPPLIER SWAC!D TO EACH END OF WIRB.
@ PROTECTOR (2) PUCES 41, 8/le"s :l/4"s l/4"TL NJLD STL. TAB Wlm 5/111" ROLE, HLDEO TO DOI R*vts10ns/OCl te REV I 11-27-83 I. ) lDD SHEETS 4.11 2.) GRIP WIRE REY. TO 3/llt' DIA. AIRCRAFT WIRE ATTACHED WITH PAD tns. OR Equiv.
3.) END YlBll REV. TO SHOW ANGLE.
4.) BOLTS TO SAi! GRADE Ii
- I. ) IMPROVED ASSEMBLED YIElfS FOR CURIFIC.ATION TAB~
lllnt I/ 4* FIUET 1181.DS.
WELDS NOT TO INTERFERE WlTH BOLB FOR lllRE.
ROUND CORNERS.
BREU: EDCES Otm:R m.&.N 111!1.D EDGE. AND BOLE TO APP. 1/111" RAD.
@ 1/4"U.ll 11/lll"ll 2-1/1:LG. TAPl!RED PROTECTOR WElllED ON TOP OF TAB WITH 1/8 FlUET WELDS NOT TO INTERFERE WITH TAB OR GRIP WIRE.
GRIP WIRE me BAU. SHANK SECTION A-A ITEM II. GRIP WIRE.ASSEMBLY, ll(a) TAB, AND OPTION.ALLY ll(b) PROTECTOR GRIP WIRE ASSEMBLY TO PULL BOX FRON CAGE.
11! *11-'/II NOT FOR unlNG R*v1,1ons/Oo. ti' R*;;.,ons/D~t*,Vr-11\\.
THOMAS GUTMAN CONSULTANT REV 2 8-08-114 I V :I 10-111-84
/O/-:i_'ff {s,'1'f
- w. HARTFORD, CT.
GRIP llJRE 19 3/lir° DI.AM. AJRCR.trr "GRIP WIRE ASSBIIBLY" USED CONTROL lllRE. APP. Id° LG.
USE DEnNfTION TO REPLACE PRIOR Drown BY RH Dole I0/21/93 Of WIRE ON BOTH ENDS or DOI REFERENCES TO
- AIRCRArr GRIP Annr-*-~ Ry TG n-** I0/2)/'IJ UNC-2600 OPTIONAL. lllRB CONNl!CTBD USING WIRI!/' AND
- AIRCRAFT CONTROL UPGRADED PACKAGE l/4" TI. l/lll"d/4" Tl'.. STL TlBS llJRI!/'.
R*vl*w*d BY \\JK n-*
- IG/21/93 RLDED TO BOX. 1/f" FIUBT llELDS ONB GRIP WIRB.ASSEMBLY PER I
R~Y.
SPACED TO.ACCOIIODATS WIRE llf BOX.
HOT TO SC.ALE DWG.# B-2600-2 li/18" HOLE. WIRE SICURID USING SUCl!D e,u.utD SINCll SIWIK. TABS KAY BB PROTECTED WlTH TAPEIIISD Pllllnt'TOR TO !l!IS PUCllllNT IIITO CAGE.
SHEET 6 OF 6
CERTIFICATE OF COMPLIANCE 5086; Appendix 6.1.1-3 Appendix 2. 10.2 Drawing B-2600-1 Original Package Design UNC-2600 PACKAGE March,2016
(Tri')
- 1rt
- l'Urt: (SH:t:L) 11 GA. -
2-!*/8 111111:: X !lti I.ONG 121 l!~Q*n lllOO;s -
IIIAIWll'OODJ
.!-J/R rt x 6-a/*
(2) P.[Q'D.
/-
'J\\
,.7---------, --, - ---------------
-~
I I
- ---- - -- ___ J ---------*------ --- - --
SIDE ANGLE CSTl:.EEL) -------
llilH/8 At-c.LE -
Ob-1/i LG (21 Rl:.Q'D.
IIANOIHG STIIAP (S11.. )
."l.!TI, -
1/211.J li :?* LG IH'Pl!OXJ 131 REQ' D.
I
- --- - -- - - - --- - - - - ---1----- - ------ - - - - - --
t11r-:i;1, AS:'t:,1111 Y -
Srt*
.JUJTI( X Ob 1.0:-;c,
~ 1, Rt:*ru
.I
'- IIA!'llLE (!".H:1::1,)
l/4TK ~ l~U X 1mo
(.!I llt::Q*D.
I X I X 1/e A~c;t.E -
97 LOHC.
ENll l'LHt; (SHEL) 11 G.4.-..!-~/8 l\\"ll;L ); 7
\\.!' IWQ' II.
1-7/8 Tli'.-lilO.D -10 I.D.
I RUUDER DUMPl::R
/
(21 REQ'D.
rr 2-5/8 i: 7.- C6 INSIDE Dlllt::NSION 11 GA. (!:TEEi.i
,;r.1uP uot A:..,;t::UUL\\'
HJ HEQ*o.
\\
21-1/'.! f\\lA. J/C Pl.HE I li I X 1/8 MIGI.E -
11-t~,
(Cl HEQ'D.
r-(ll;J REQ'U.
l:.Q. SPA<:l::D
/
1-J/~ l\\"IUI:: X I /4 Pl.~
~
DARREL ASSt:MOLY U C.l.(IIIH) 3/4 0.0.
102-1/2 O.H. -
(I) Rt:Q'D LID IIING ASSY 12 UA. li.2:J - ;J/4 O.C.
(II HEG'IJ
\\ ~ ~~~:::::,~' 07 1.G (fn Rt::Q*u.
X 1-1/~ E 1/8 Ar-:LL~
~
~
I.G. H) P.EQ'U.
6 ); 1-J/e I II.TL *-
f.tJ.RElflJ.
t:ITllt:11 1/:!-IJ X 1-1/2 LONG DOLT!'. r.HII 1/.? 11.\\SIIEI:
STll &. l/~-13 !':UT::-: TU 'dt:
usn, IJII l'i/8-11 >.: 1-1/ I I.ON,.;
~r*Rn,s TilTII 5/1: 'iTU l.'.lCK IIA:>>111::P.S -
(B)Rl::Q' U.
END lilt:l\\': COVt::R l:ING & Dt.:ldl'EH ll1::~10v1m DIA DOI.T ~ LONG 11 NUT THOMAS GUTMAN CONSULTANT Pev1s1ons/Oot W. HARTFORD. CT.
1-...::..:._:.:..::.::..:..:....:....::...:..:..::,....:-_U.:....N.:....C ___
2 5-=--0=-o=--=p:-A::--:C:::I-;-( A:-:G:::, E:;-1
, *.,..... by T.G.
o.,,-11/J/9!
NOT TO Scale: scA1.~:
AS n:sTEn "2
D\\./G# 0-2600-1 t_Q__ S