Draft SOW.pdf

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STATEMENT OF WORK

MK 41 VERTICAL LAUNCHING SYSTEM

MISSILE ELECTRONICS BOX 1553 CIRCUIT CARD 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 Missile Electronic Box (MEB) 1553 Circuit Card Assembly (CCA).

This CCA makes up part of the MEB, which in turn, is part of the Launch Sequencer (LSEQ) for the MK 41Vertical Launching System (VLS). This CCA is a critical and required part of the MK

41 VLS.

3. SCOPE

The Contractor shall be responsible for the satisfactory and timely performance of all tasks 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 MK 41 VLS MEB 1553 CCA’s.

4. APPLICABLE DOCUMENTS

The Technical Data Package (TDP) consists of drawings 8652315-9 and all subcomponent drawings. The included drawings package provides detailed information, including all specifications, for the manufacturing of the CCAs. 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.

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4.1 Government Documents

Document Number Document Title

MIL-STD-109C Quality Assurance Terms and Definitions

MIL-STD-1686C Electrostatic Discharge Control Program for Protection of

Electrical and Electronic Parts, I Assemblies and

Equipment (Excluding Electrically Initiated Explosive

Devices)

MIL-STD-1553B Aircraft Internal Time Division Command/Response

Multiplex Data Bus

WS 20130 Production Environmental Test Requirements for VLS

TL130-AD-PLN-010-VLS

Configuration Management Program Plan for the MK 41

VLS,

Volume 1, Equipment (Hardware) Configuration

Management

MK 41 VLS Standing

Instruction 94-1F, Attachment 6

Marking for technical data

TL130-AD-PLN-030-VLS Firmware Configuration Management

MIL-STD-130 Identification Marking

MIL-HDBK-263 Electrostatic Discharge Control Handbook

NAVSEA Drawings 8652315-9 MEB 1553 CCA Technical Data Package

In addition, the attached TDP drawings 8652315-9 contain several subcomponent level drawings, including Parts List (PL), Notice of Revisions (NOR), Engineering Change Proposals

(ECP), Gerber files and release notes. These files are listed below. The Contractor shall thoroughly review all files to identify the latest drawing revision and parts.

MEB Interface CCA TDP (P/N: 8660408-9)

Drawing

No.

Related Files (.pdf) Description

8652314

8652314_NOR002_(NSWC2-1996R2)_appr_09112020 Notice of Revision 002

8652314_NOR001_(NSWC2-1996R1)_appr_06082020 Notice of Revision 001

8652314A_appr_09112020 Revision A

8652314rev-_(NSWC2-1996)_appr_05152020 PCB, 1553

8652315

8652315_NOR002_(NSWC2-1996R2)_appr_09112020 Notice of Revision 002

8652315_NOR001_(NSWC2-1996R1)_appr_06082020 Notice of Revision 001

8652315rev-PL_(NSWC2-1996)_appr_05192020 Parts List

8652315rev-_(NSWC2-1996)_appr_05192020 CCA, 1553

8652316 8652316_NOR001_(NSWC2-1996R2)_appr_09112020 Notice of Revision 001

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8652316rev-_(NSWC2-1996)_appr_05192020 Approved 05/19/2020

8652316 - Schematic, CCA, 1553 Schematic, CCA, 1553

8652317 8652317rev-_(NSWC2-1996)_appr_05192020 Approved 05/19/2020

8652317 - ATR, CCA, 1553 ATR, CCA, 1553

8660431 8660431_NOR 002_(NSWC2-1996)_appr_05192020 Notice of Revision 002

ECP

NSWC2-1959R2_(LAMP revisions to facilitate initial production of hardware)_appr_06122020

ECP NO. NSWC2-

NSWC2-

1996_(New_LAMP_1553_CCA)_appr_05192020

ECP NO. NSWC2-

NSWC2-1996R1_(New LAMP 1553 CCA

Revisions)_appr_06082020

ECP NO. NSWC2-

1996 Revision 1

NSWC2-1996R2_(New LAMP 1553 CCA

Revisions)_appr_09112020

ECP NO. NSWC2-

Revision 2

NSWC2-2006_MK57 UCEU PET REQ

UPDATES_appr_06192020 (CCB)

ECP NO. NSWC2-

Additional Files

Gerber

PCB_8652314-1_REV- Dated 4/24/2020 Updated 4/24/2020

8652314 Dated - 5/19/2020 Updated 5/19/2020

PCB_8652314-1_REV- Dated 6/25/2020 Updated 6/25/2020

PCB_8652314-1_REVA - Dated 9/14/2020 Updated 9/14/2020

Release

2020-06-

8652315-9 (1553 CCA) QA Pass 2020-06-23.pdf

8652315-9 (1553 CCA) QA Pass 2020-06-23.xlsx

8652315-9 (1553 CCA).AUDIT.xlsx

8652315-9 (1553 CCA).IPL.txt

8652315-9 Proprietary Readme.txt

QA/Audit Report files

4.2 Industry Documents

Document Number Document Title

ANSI/ISO/ASQC Q9001 Quality Systems – Model for Quality Assurance in Design, Development, Production, Installation and Servicing

ANSI/EIA-649 2011 National Consensus Standard for Configuration Management

ISO 9001 Quality Program Requirements

SAE Aerospace Standard

AS9102 Rev A

Aerospace First Article Inspection

ISO 14000 Environmental Management Systems Standards

ANSI/ESD S20.20 Protection of Electronic Assembly

IPC-J-STD-001 Requirements for Soldered Electrical and Electronic Assemblies

IPC-CC-830 Quality Electrical Insulating Compounds

IPC-A-610 Acceptability of Electronic Assemblies

PCI Local Bus-2.3 PCI Local Bus Specifications Revision 2.2

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5.0 REQUIREMENTS

The Government requires manufacturing of the MK 41 VLS MEB 1553 CCA in accordance with the TDP drawing 8652315-9. All the MEB 1553 CCAs shall meet all form, fit, and function requirements in accordance with the TDP drawings and associated specifications.

Part Number Description Brand Name QTY

8652315-9 MEB 1553 CCA N/A 455

Optional Requirement:

The Government has the option for Physical Configuration Audit of MEB 1553 CCA.

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 1553 CCA

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, 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 A002.

The audits will be conducted at the Contractor or subcontractor facility by NSWC

Dahlgren Division or other Government designated representatives.

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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 time frame specified by the Navy PCA lead in accordance with CDRL A003. 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 TDP drawings.

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’s 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.

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 1553 CCAs produced by the Contractor. The Contractor shall maintain a Contractor approved Configuration

Management Plan that complies with ANSI/EIA-649 2011. Notwithstanding ANSI/EIA-649

2011, the Contractor’s configuration management program shall comply with the VLS

Configuration Management Plans, TL130-AD-PLN-010-VLS, and shall comply with the following:

6.1 Configuration Identification

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The Contractor shall maintain identification of the product baselines throughout fabrication, testing, and delivery. The Contractor shall ensure that equipment is assigned identifying numbers, designators, and serial numbers in accordance with the TDP.

6.2 Manufacturing Certification and Traceability

The Contractor shall submit a Certificate of Conformance certifying that the VLS MEB

1553 CCA 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

A004.

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, the Configuration Management Plan for the VLS, Volume 1, Equipment (Hardware)

Configuration Management, TL130-AD-PLN-010-VLS, and the Configuration Management

Plan for the VLS, Volume 3, Firmware Configuration Management, and TL130-AD-PLN-030-

VLS.

7.0 GOVERNMENT TESTING, INSPECTION AND ACCEPTANCE

The Government shall perform all test requirements set forth in the Acceptance Test

Requirements (ATR’s) for all applicable parts. The ATR drawings below establish the test requirements for acceptance of the MEB 1553 CCAs.

I. Drawing No. 8652317 ATR for the MEB 1553 CCA, P/N: 8652315-9 (for schematic see 8652316)

ATR Testing and inspection of the MEB 1553 CCAs shall be performed at a Government and/or Government contractor facility in accordance with the applicable drawings, standards and specifications and factory test and inspection plans. The Government shall prepare specific written inspection and test procedures for each inspection and test operation to be performed by the Government. 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 Government shall maintain records of inspection results and quantitative test data for each deliverable end item.

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7.1 CCA Rework and Repairs

After delivery of the CCA’s, the Government shall conduct a series of PET and ATR tests and determine if the CCA’s require rework and/or repair. If at any point during testing the

Government finds it necessary for CCA rework/repair, the Government shall notify and coordinate the delivery of the failed CCA’s to the Contractor for rework and/or repair.

All deficiencies discovered during ATR and PET testing shall be corrected at Contractor’s expense prior to unit delivery to the Government. Once the CCA rework and repair is completed, the Contractor shall deliver the CCAs to the Government for re-testing.

7.2 Conformal Coating

Prior to the final series of ATR and PET testing, the Government shall perform conformal coating of the MEB 1553 CCA’s in accordance with the Quality Electrical Insulation

Compounds, IPC-CC-830. After conformal coating of the CCA’s, the Government will conduct the final series of ATR and PET testing. If the CCA fails after conformal coating, CCA rework/repair will take place as specified in Section 14.1. If required, the Government will re-coat the CCA’s prior to final testing and acceptance.

7.3 Production Environmental Tests

The Government shall perform all required testing in accordance with the Production

Environmental Test requirements for VLS, WS 20130. The purpose of PET is to provide a catalyst in surfacing manufacturing and assembly defects and weak or marginal parts/components within the units under test (UUT’s) prior to system integration.

8.0 GENERAL REQUIREMENTS

8.1 Risk Assessment and Management

The Contractor shall perform risk assessment and management. The Contractor shall use its own established Risk Management Program; however, the Risk Management Program shall at a minimum contain the following:

Risk management shall be a continuous process, analyzing program risks and individual mitigation plans on a sufficiently frequent basis to be proactive in preventing major Program problems. Major problems include, but are not limited to, not meeting delivery dates and nonconformance to specifications and drawings. The analysis shall identify the risks associated with each area, assess the probability of occurrence, identify the impact of each risk on the overall program, and develop and implement risk mitigation plans for identified risks. The risk analysis shall use metrics from the Contractor’s Risk Management Program.

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8.2 Right of Access

The Government shall have right of access to all facilities in which storage of raw materials, purchased parts, either finished or unfinished, and finished equipment may be established. Right of access shall include all areas in which VLS MEB 1553 CCAs are stored, manufactured, processed, aligned, assembled, and tested. Right of Access shall be interpreted to include access to records and documentation concerning the VLS MEB 1553 CCAs. Access includes specifications, purchase orders and subcontract documentation, receiving, inspection and test records for such purchase parts. Right of access shall include access at all tiers to vendors, Subcontractors and suppliers in accordance with FAR 46.405 and FAR clauses 52.245-

1(g) and FAR 52.246-1.

The Government may perform any necessary inspections, verifications and evaluations to ascertain conformance to requirements, and the adequacy of the implementing procedures.

9.0 QUALITY ASSURANCE

The Contractor Quality Assurance Program Plan shall be in conformity with either

ANSI/ASQC Q9001, or ISO 9001 for production. This applies to items manufactured or performed by the Contractor at the Contractor’s plant or all outsourced facilities. The Contractor shall flow down to the Subcontractors and vendors the quality requirements through subcontracts, purchase orders, or other contractual purchasing documentation by using

ANSI/ASQC Q9001 as a guide. The quality requirements include ANSI/ASQC Q9001 or ISO

9001, and relevant SOW and TDP requirements. The Subcontractors and vendors shall provide

Certificates of Conformance that the flowed down requirements are fulfilled.

10.0 MARKING FOR TECHNICAL DATA

The Contractor shall mark all technical data in accordance with MK 41 VLS Standing

Instruction 94-1F, Attachment 6. This instruction is applicable to new documents, revised documents or documents from file in response to a request for copy.

11.0 ENVIRONMENTAL COMPLIANCE AND REGULATIONS

The Contractor shall comply, and ensure that all Subcontractors comply, with all applicable environmental federal, state, and local laws and regulations and Navy policies, instructions and ISO 14000 Environmental Management Systems Standards.

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12.0 GOVERNMENT FURNISHED PROPERTY

12.1 Government Furnished Material

12.2 Government Furnished Equipment

12.3 Government Furnished Information

13.0 DELIVERABLES

NUMBER NAME

A001 QTY 455 MEB 1553 CCAs

A002 Configuration Status Accounting Information

A003 As Built Configuration List

A004 Technical Report Study/Services

14.0 ACRONYM LIST

ACRONYM DENOTATION

VLS Vertical Launching System

MEB Missile Electronics Box

ATR Acceptance Test Requirements

CCA Circuit Card Assemblies

TDP Technical Data Package

N/A

N/A

MEB 1553 CCA TDP#: 8652315-9