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STATEMENT OF WORK
VERTICAL LAUNCHING SYSTEM
MISSILE ELECTRONICS BOX AND HAZARD ELECTRONICS BOX
BACKPLANE HARNESS ASSEMBLY
1. INTRODUCTION
The Naval Surface Warfare Center (NSWC), Corona Division, Measurement Science & Engineering Department, Interface Engineering & Assessment Division (MS20) builds and maintains Navy Interface Gages for ship-launched missiles, surface and underwater munitions; air-launched missiles and strategic weapons including fleet ballistic missile systems and subsystems.
2. BACKGROUND
Naval Sea System Command (NAVSEA) Integrated Weapons System (IWS) Code 3L has a requirement to procure HEB and MEB Backplane Harness Assemblies. These harnesses make up part of the HEB and MEB, which in turn, are part of the Launch Sequencer (LSEQ) for the MK 41 Vertical Launching System (VLS). These Backplane Harnesses are a critical and required part of the MK 41 VLS.
3. SCOPE
The Contractor shall be responsible for the satisfactory and timely performance of the requirements defined in the Statement of Work (SOW). This SOW, with its supporting attachments and referenced documentation, describes the total requirement for the manufacture, assembly, test and delivery of VLS MEB and HEB Backplane Harness Assemblies.
4. APPLICABLE DOCUMENTS
The Technical Data Package (TDP) consists of drawings 8660446-9 and 8660527-9, and all subcomponent drawings. The included drawings package provides detailed information, including all specifications, for the manufacturing of the harness assemblies. In addition to these drawings, the following documents form a part of this SOW to the extent specified herein, including all applicable terms, conditions, clauses, attachments and exhibits. The Contractor shall apply the latest version of the documents in effect at the time of award of the contract.
4.1 Government Documents
| Document Number |
| Document Title |
| MIL-STD-1686C |
| Electrostatic Discharge Control Program for Protection of Electrical and Electronic Parts, Assemblies and Equipment |
| TL130-AD-PLN-010-VLS |
| Configuration Management Program Plan for the MK 41 VLS, Volume 1, Equipment (Hardware) Configuration Management |
| MIL-STD-130 |
| Identification Marking |
| MIL-HDBK-263 |
| Electrostatic Discharge Control Handbook |
| WS 19202 |
| Test Requirements for Electrical Harness and Interconnecting Network |
| WS 19179E |
| Process Specification for Fabrication and Installation of Cable Assemblies and Wiring Harness Rev. E |
| WS 19185 |
| Marking of Items, Process Specifications |
| WS 19167A |
| Process Specification for Coding, Fabrication, and Inspection of Riveted Joints Rev. A |
| NAVSEA Drawings 8660446-9 |
| MEB Backplane Harness Assembly Technical Data Package Drawings |
| NAVSEA Drawings 8660527-9 |
| HEB Backplane Harness Assembly Technical Data Package Drawings |
In addition, the attached TDP drawings 8660446-9 and 8660527-9 contain several subcomponent level drawings, including Parts List (PL) and Notice of Revisions (NOR). These files are listed below for each Assembly. The Contractor shall thoroughly review all files to ensure the latest drawing revision and parts are used.
MEB Backplane Harness Assembly TDP (P/N: 8660446-9)
| Drawing No. |
| Related Files (.pdf) |
| Description |
| 8660446 |
| 8660446_MEB BP Harn Assy_NOR 1_181107 |
| Notice of Revision 001 |
| 8660446rev- PL |
| Parts List |
| 8660446rev- |
| Harness, Backplane, MEB |
| 8660428 |
| 8660428rev- |
| ATR, Harness, Backplane, MEB |
| 8660447 |
| 8660447_MEB BP Harness CCA_NOR 1_181107 |
| Notice of Revision 001 |
| 8660447rev- PL |
| Parts List |
| 8660447rev- |
| CCA, Backplane Harness, MEB |
| 8660449 |
| 8660449_MEB BP Harness Schematic_NOR 1_181108 |
| Notice of Revision 001 |
| 8660449rev- |
| Flex Harness, Backplane, MEB |
| 8660448 |
| 8660448_NOR001 |
| Notice of Revision 001 |
| 8660448rev- |
| PCB, Flex Harness, Backplane, MEB |
| 8660454 |
| 8660454_NOR 1.pdf |
| Notice of Revision 001 |
| 8660454_RevA.pdf |
| Revision A |
| 8660454rev-.pdf |
| Pin, Short |
| 8660445 |
| 8660445rev- |
| Support Bracket, PWB, MEB |
| 8660453 |
| 8660453_NOR 1.pdf |
| Notice of Revision 001 |
| 8660453_RevA.pdf |
| Revision A |
| 8660453PL_revA.pdf |
| Parts List Revision A |
| 8660453rev- PL.pdf |
| Parts List |
| 8660453rev-.pdf |
| Receptacle Pin |
| 8660509 |
| 8660509_NOR 1.pdf |
| Notice of Revision 001 |
| 8660509rev- PL.pdf |
| Parts List |
| 8660509rev-.pdf |
| Cable, Ground, HEB/MEB |
HEB Backplane Harness Assembly TDP (P/N: 8660527-9)
| Drawing No. |
| Related Files (.pdf) |
| Description |
| 8660527 |
| 8660527_HEB BP Harn Assy_NOR 1_181105 |
| Notice of Revision 001 |
| 8660527rev- PL |
| Parts List |
| 8660527rev- |
| HEB Backplane Harness |
| 8660474 |
| 8660474rev- |
| ATR, Harness, Backplane, HEB |
| 8660528 |
| 8660528_HEB BP Harness CCA_NOR 1_181107 |
| Notice of Revision 001 |
| 8660528rev- PL |
| Parts List |
| 8660528rev- |
| CCA, Backplane Harness, HEB |
| 8660530 |
| 8660530rev- |
| Schematic, Flex Harness, Backplane, HEB |
| 8660529 |
| 8660529 NOR001 |
| Notice of Revision 001 |
| 8660529rev- |
| PCB, Flex Harness, Backplane, HEB |
| 8660454 |
| 8660454_NOR 1 |
| Notice of Revision |
| 8660478 |
| 8660478rev- |
| Support Bracket, PWB, HEB |
| 8660453 |
| 8660453_NOR 1 |
| Notice of Revision 001 |
| 8660453PL_revA |
| Parts List Revision A |
| 8660453rev- PL |
| Parts List |
| 8660453rev- |
| Receptacle Pin |
| 8660509 |
| 8660509_NOR 1 |
| Notice of Revision 001 |
| 8660509rev- PL |
| Parts List |
| 8660509rev- |
| Cable, Ground, HEB/MEB |
4.2 Industry Documents
| Document Number |
| Document Title |
| ANSI/EIA-649 2011 |
| National Consensus Standard for Configuration Management |
| ANSI/ESD S20.20 |
| Protection of Electrical and Electronic Parts, Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices) |
| IPC-J-STD-001 |
| Requirements for Soldered Electrical and Electronic Assemblies |
| IPC-J-STD-005 |
| Requirements for Soldering Pastes |
| IPC-A-610 |
| Acceptability of Electronic Assemblies |
| IPC-CC-830 |
| Qualification and Performance of Electrical Insulating Compound for Printed Wiring Assemblies |
| ASTM B16 |
| Standard Spec for Free -Cutting Brass ROD, BAR and Shapes for Use in Screw Machines |
| ASTM B488 |
| Standard Spec for Electrodeposited Coatings of Gold for Engineering Uses |
| A-A-56032 |
| Commercial Item Description INK, MARKING, EPOXY BASE |
5.0 REQUIREMENTS
The Government requires manufacturing of MK 41 VLS MEB and HEB Backplane Harnesses Assemblies in accordance with technical data package drawings 8660446-9 and 8660527-9. All the MEB and HEB Backplane Harness Assemblies shall meet all form, fit, and function requirements in accordance with the drawings and associated specifications.
Optional Requirement:
The Government has the option for Physical Configuration Audit of MEB Backplane Harness Assembly and HEB Backplane Harness Assembly.
5.1 Physical Configuration Audit (Option Item, if exercised)
The Government will perform a Physical Configuration Audit (PCA) of an assembly built in the first production lot of the following items:
a. MEB Backplane Harness
b. HEB Backplane Harness
The PCA purpose is to verify the as-built configuration matches its technical documentation and validate supporting processes. The PCAs shall be conducted in accordance with Section 7 of TL130-AD-PLN-010-VLS, Configuration Management Program Plan for the MK 41 Vertical Launching System, Volume 1, and Equipment (Hardware) Configuration Management.
The Contractor shall provide qualified engineering, technical, manufacturing, administrative, management and other support as necessary for these Government audits. Technical personnel shall be required to have necessary tools, measuring devices and other equipment necessary for equipment disassembly, dimensional & tolerance verification and performance verification. The contractor shall provide an area for audit conduct that is well-illuminated, temperate and low noise level. The audit work area shall contain worktables, print copies of all pertinent drawings, telephone and easy access to a copy machine.
The Contractor shall provide during the PCA, at a minimum, individual parts that make up the configuration item, completed assembly(s), an as-built list delineating all Engineering Change Proposal (ECPs) (either requested or approved). Hardcopies of production specifications and technical drawings, complete shortage list, manufacturing instructions, acceptance test procedures and data, purchase order documents and associated certificates of conformance from suppliers or appropriate documents indicating compliance with material or drawing requirements in accordance with (CDRL A003).
The audits will be conducted at the Contractor or subcontractor facility by NSWC Dahlgren Division or other Government designated representatives.
Each audit will be performed after assembly completion (including acceptance testing) and prior to DD 250 Acceptance. For planning purposes, each complete PCA will require approximately two weeks for pre-audit preparations, three weeks for audit conduct and three weeks for post audit close-out efforts.
Following the conduct of the PCA, the Contractor shall generate the necessary documentation to resolve all audit findings and provide these to the Navy audit team within the period specified by the Navy PCA lead in accordance with (CDRL A004). This documentation shall be evaluated by the PCA team to assess the corrective action taken to close the audit finding. This necessary documentation may include but not be limited to, revised manufacturing processes, engineering change proposals, Notice of Revisions, Specification Change Notice and revised drawings.
The Government and Contractor pre and post PCA activities are described in sections 7.4 through 7.7 of the VLS Configuration Management Plan TL130-AD-PLN-010-VLS.
All deficiencies discovered during the PCA’s that affect form, fit, function or performance shall be corrected at Contractor expense prior to unit delivery to the Government.
5.2 Government Technical Data Reviews, Quality Audits
During the performance of the contract, the Government shall have the right to perform technical data reviews and quality audits consisting of evaluation of records, processes and products to verify the Contractor's compliance with the respective quality programs. The Government audits may include evaluation of effectiveness in implementing the Contractor's and Subcontractors' or suppliers' audit programs to promote prevention of defects, which includes schedule of audits, evaluation of operations, notification of required corrective action with follow-up and means of notification to top management concerning audit results.
5.3 Testing, Inspection and Acceptance
The Contractor shall perform and meet all test requirements set forth in the Acceptance Test Requirements (ATR) for all applicable parts in accordance with Test Requirements for Electrical Harness and Interconnecting Network, WS 19202. The ATR drawings below establish the test requirements for acceptance by the Government of the MEB and HEB Backplane Harness Assemblies.
Drawing No. 8660428 ATR for the MEB Backplane Harness Assembly, P/N: 8660446 (for schematic see 8660449)
Drawing No. 8660474 ATR for the HEB Backplane Harness Assembly, P/N: 8660527 (for schematic see 8660530)
Testing and inspection of the VLS MEB and HEB shall be performed at the Contractor's facility in accordance with the applicable drawings, standards and specifications and factory test and inspection plans. The Contractor shall prepare specific written inspection and test procedures for each inspection and test operation to be performed by the Contractor. These inspection and test procedures shall be reviewed by the quality assurance organization and maintained current in accordance with the change control system requirements. The inspection and test procedures shall clearly identify the item through part number with revision and nomenclature, and include detail instructions and/or operations to be performed.
The Contractor shall maintain records of inspection results and quantitative test data for each deliverable end item and make them available to the Government upon request.
6.0 CONFIGURATION MANAGEMENT
The Contractor shall maintain a configuration management program, which shall provide for the administrative and functional systems necessary for configuration identification, control, status accounting and reporting, to assure configuration identity with the MEB and HEB Backplane Harness Assemblies produced by the Contractor. The Contractor shall maintain a Contractor approved Configuration Management Plan that complies with ANSI/EIA-649 2011, and shall comply with the following:
6.1 Configuration Identification
The Contractor shall maintain identification of the product baselines throughout fabrication, testing, and delivery.
6.2 Manufacturing Certification and Traceability
The Contractor shall submit a Certificate of Conformance certifying that the VLS MEB and HEB Backplane Harness meets the requirements of this contract. The Contractor shall retain and provide upon request inspection and test results associated with certifying the units in accordance with CDRL A005.
6.3 Substitution of Sources of Supply
The TDP contains source control or vendor item drawings that specify approved or suggested sources of supply. The Contractor shall submit all proposed changes to approve or suggested sources of supply as indicated in the source control or vendor item drawings to the Government for approval.
6.4 Configuration Status Accounting
The Contractor’s configuration status accounting shall be in accordance with ANSI/EIA-649 2011. The Contractor shall provide a system that documents the exact delivered configuration of each unit. The Contractor shall provide the as-built configuration data to the Government upon request.
7.0 GOVERNMENT FURNISHED PROPERTY
7.1 Government Furnished Material
N/A
7.2 Government Furnished Equipment
N/A
7.3 Government Furnished Information
MEB Backplane Harness TDP # 8660446-9 and HEB Backplane Harness TDP # 866027-9
8.0 DELIVERABLES
| A001 |
| QTY 455 MEB Backplane Harness |
| A002 |
| QTY 62 HEB Backplane Harness |
| A003 |
| Configuration Status Accounting Information |
| A004 |
| As Built Configuration List |
| A005 |
| Technical Report Study/Services |
9.0 ACRONYM LIST
| VLS |
| Vertical Launch System |
| MEB |
| Missile Electronics Box |
| HEB |
| Hazard Electronics Box |
| ATR |
| Acceptance Test Requirements |
| CCA |
| Circuit Card Assemblies |
| TDP |
| Technical Data Package |
ADDITIONAL INFORMATION
A. PERIOD OF PERFORMANCE / REQUIRED DELIVERY DATES
20 weeks after date of award (DOA)
B. PLACE OF PERFORMANCE
TBD
C. SHIPPING ADDRESS
Naval Surface Warfare Center Build 519 1999 Fourth St Norco, CA 92860
D. INSPECTION AND ACCEPTANCE
E. TECHNICAL POINT OF CONTACT
NAVAL SURFACE WARFARE CENTER, CORONA DIVISION
CONTRACTS DEPARTMENT
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