SOW_SPS49PBLO DCMotor_Rev02.pdf
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- DC Motor Evaluation and Repair
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- N0016426Q0131
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This is a Statement of Work (SOW) for the inspection, evaluation, overhaul, and delivery of PBLO AN/SPS-49 Elevation Drive Direct Current Motors (P/N 914104), with Naval Surface Warfare Center (NSWC) Crane Division designated as the overhaul point. The contractor must furnish all equipment, parts, and labor necessary to test, overhaul, and repair the motors, with assets returned to the Government on FOB Destination to NSWC Crane, Building 3168.
The SOW specifies a Level I Standard Overhaul that includes mandatory component replacements per SE110-A2-MMD-010 Tables 9-4, 9-5, 9-6, and Figure 9-3, along with tachometer brush, connector, and hardware replacements. Additional overhaul levels (II through VI) address more extensive repairs including brush holder assembly, rotor/stator repairs, armature assembly, frame assembly, and back end bracket replacements. All work must comply with Drawing 914104 Rev M, Drawing 914321 Rev D, and Repair Manual SE110-A2-MMD-010. The contractor must conduct initial inspection and evaluation, submit evaluation reports (CDRL A002) for Government approval before proceeding with extensive repairs, perform comprehensive coating removal and application following NSI 009-32 FY22CH1 standards, and execute post-reassembly testing per SE110-A2-MMD-010 Section 6. Deliverables include Engineering Change Proposals, Evaluation Reports, Unit Test/Inspection Reports, Certificates of Conformance, and Certificates of Compliance. The contractor must maintain ISO 9001-2008 compliance or equivalent quality standards, implement counterfeit material avoidance procedures per SAE standards, and ensure configuration control per EIA-649-1.
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Distribution Statement A: Approved for Public Release; Distribution is unlimited.
STATEMENT OF WORK
DIRECT CURRENT (DC) MOTOR OVERHAUL
21 JANUARY 2025
1. BACKGROUND AND SCOPE
1.1. This Statement of Work (SOW) establishes the requirements for the inspection, evaluation, overhaul, and delivery of PBLO AN/SPS-49 Elevation Drive Direct Current Motor (P/N 914104).
Naval Surface Warfare Center (NSWC) Crane Division is the designated overhaul point for the AN/SPS-49 Antenna.
2. APPLICABLE DOCUMENTS
914104 Rev L Elevation Drive Motor 914321 Rev D Servomotor Tachometer Specification 94R11276-000 Rev - SE110-A2-MMD-010 Overhaul & Repair Manual AS-3262/SPS-49(V) MIL-STD-129P Military Marking for Shipment and Storage MIL-STD-130N Identification Marking of US Military Property MIL-STD-2073-1E Standard Practice for Military Packing
NSI 009-32 FY-22CH-1 NAVSEA Standard Item (NSI) Package 009-32 FY-
22CH-1 Cleaning and Painting Requirements
SAE AS5553A Fraudulent/Counterfeit Electronic Parts; Avoidance, Detection, Mitigation, and Disposition SAE AS6081 Fraudulent/Counterfeit Electronic Parts: Avoidance, Detection, Mitigation, and Disposition - Distributors SAE AS6174 Counterfeit Materiel; Assuring Acquisition of Authentic and Conforming Materiel SAE AS6301 Compliance Verification Criterion Standard for SAE
AS6081, Fraudulent/Counterfeit Electronic Parts:
Avoidance, Detection, Mitigation, and Disposition – Distributors
3. REQUIREMENTS
3.1 GENERAL REQUIREMENTS
3.1.1 The contractor shall furnish all equipment, parts, and labor necessary to test, overhaul, and/or repair the AN/SPS-49 Elevation Drive DC Motor (P/N 914104).
3.1.2 The contractor shall be responsible for shipment of all assets submitted to the contractor for evaluation and overhaul. Assets submitted for overhaul shall be returned to the Government per FOB Destination to NSWC Crane, building 3168.
3.1.3 All assets to be delivered to the Government, the contractor shall perform marking for shipment and storage processes using MIL-STD-129P.
3.1.4 All assets to be delivered to the Government, the contractor shall apply equipment markings and identification processes using MIL-STD-130N.
3.1.5 All assets shall be packaged IAW MIL-STD-2073-1E Method 54 and cover all external electrical ports with plastic protective caps.
3.1.6 The contractor shall maintain a configuration control program that meets the requirements of EIA-649-1 Configuration Management Requirement for Defense contracts.
3.1.7 In the event it is necessary to deviate from the drawings provided based on obsolescence or diminished manufacturing sources and material shortages (DMSMS). The contractor shall formally request the change in an engineering change proposal (ECP) and submit it to the government for approval. The government will require adequate time to review ECP's based on the magnitude of the change. Furthermore, an updated technical drawing package reflecting the changes must be provided to the government. The updated TDP may or may not need to accompany the ECP for approval depending on whether or not it is needed to adequately describe the change. (CDRL A001)
3.1.8 All SPS-49 Antenna Elevation Drive DC Motors overhauled or manufactured shall meet Drawing 914104 Rev M, Drawing 914321 Rev D, and Repair Manual SE110-A2-MMD-010 Chapter 9 and Appendix C upon delivery to the Government.
3.2 Overhauls – 914104 – Direct Current Motor
3.2.1 Evaluation and Inspection (CDRL A002)
3.2.1.1 When subassemblies are received for overhaul, the Contractor shall perform an initial inspection and test paragraph 3.3 of the assembly or subassembly. All discrepancies beyond the scope of a standard overhaul shall be documented in an Evaluation Report (CDRL A002) with accompanying documenting photograph(s). After initial inspection and test of the subassembly, the Contractor shall disassemble the subassembly IAW SE110-A2-MMD-010 Manual Sections II (9-2 Disassembly), III (9-3 Cleaning and Examination), Table 9.3, and Appendix C. During cleaning, the Contractor shall remove all sealant from exterior casing and hardware. The contractor shall perform detailed inspections, tests, and/or measurements of all parts not already designated as mandatory replacement items as part of a standard, Level I, overhaul. Items that require repairs and/or replacement beyond a standard overhaul (paragraph 3.2.3, Level II through Level VI), are defined as extensive overhauls. Repairs not within the scope of an extensive overhaul, are defined as supplemental repairs. The Contractor shall document these non-mandatory repairs/replacement parts, which fail inspections, tests, and/or measurements, on the evaluation report and designate the failed parts as supplemental repairs.
3.2.1.2 The evaluation report shall include the additional level of overhaul/repair beyond standard overhaul required.
3.2.1.3 The contractor shall provide evaluation reports to the Government for each subassembly submitted for overhaul. The contractor shall overhaul subassemblies which have no repair requirements beyond standard overhauls. For subassemblies which have extensive overhaul and/or supplemental repair requirements above and beyond standard overhauls shall NOT be overhauled until the Government approves the evaluation report. If the Government does not approve the evaluation report, the contractor shall take disposition actions for the subassembly in accordance with the Government’s evaluation report response. When the Government approves evaluation reports, the contractor shall execute the subassembly standard overhaul and extensive repair and/or the supplemental repair.
3.2.2 AN/SPS-49 Pedestal DC Motor Level I Standard Overhaul
3.2.2.1 A subassembly standard overhaul includes: the replacement of all components that are identified as mandatory (marked by asterisk “*”) in Tables 9-4, 9-5, 9-6, and Figure 9-3 of SE110-A2- MMD-010; and in accordance with (IAW) Drawing 914104 and Specification 914321.
3.2.2.2 The Contractor shall replace tachometer brushes, J1 and J2 connectors/pins, and associated hardware parts that are identified as non-mandatory in Table 9-4, 9-5, 9-6, and Figure 9-3 of SE110-A2-MMD-010; and IAW Drawing 914104 and Specification 914321.
3.2.2.3 If the tachometer brush holder assembly and tachometer stator assembly currently installed is not model M35000-003 and M35002-301, the contractor shall replace the tachometer brush holder assembly and tachometer stator assembly with model M35000-003 and M35002-301.
3.2.2.4 Coating Removal and Application (CDRL A003)
3.2.2.4.1 General Requirements
3.2.2.4.1.1 Accomplish the applicable requirements of NSI 009-32 FY22CH1 for all components to be coated. All components shall be treated as Critical Coated per NSI 009-32 FY22CH1. Small parts prepared and coated together with the same preparation and coating system requirements can be defined as a batched for QC/QA sampling.
3.2.2.4.1.2 All coatings must be mixed and applied per NSI 009-32 FY22CH1 paragraph 3.1.13.1 and the NAVSEA-reviewed ASTM F718 data sheets. Copies of the NAVSEA-reviewed ASTM F718 data sheets are available from the Naval Surface Treatment Center (NST Center) website: http://www.nstcenter.biz. Thinning is authorized to enable spraying of coatings with high volume low pressure (HVLP) paint spray equipment if airless spray equipment is unavailable. Follow coating manufacturer product data sheets/directions as to the types of thinners to use and the maximum amount of thinner that should be added. Use the minimum amount of thinner that will result in the deposition of a uniform, even coating without extensive orange peel appearance. Do not exceed the Volatile Organic Content (VOC) levels allowed by local paint permits.
3.2.2.4.1.3 QA inspection steps shall be performed by listed QA personnel and results recorded in applicable QA Appendices B through H1 of NSI 009-32 FY22CH1.
3.2.2.4.1.4 Upon receipt of abrasives and coatings, ensure requirements of NSI 009-32 FY22CH1 and TABLE XIV are met. Materials not meeting requirements shall not be used without written authorization from NAVSEA.
3.2.2.4.1.5 Before using any paint, thinner, or other chemical product, ensure that the shelf life and storage requirements of NSI 009-32 FY22CH1 are met. Paint or chemical products that are past their shelf life/expiration date shall not be applied without written authorization from
NAVSEA.
3.2.2.4.1.6 Mask critically machined metal surfaces with appropriate protective sheets, films, or other material to prevent abrasive blast media or tools used to prepare the metal substrates for coating from causing impact damage critically machined metal surface. Masking shall overlap the metal substrate between ¼ and ¾ inch such that abrasive media does not impact on critically machined metal surface. Critically machined surfaces are bare metal surfaces identified in the part/assembly spec control drawings.
3.2.2.4.1.7 All internal surfaces within Drawing 914104 Rev M are considered critical surfaces and shall only be addressed in corrosion areas. For critically machined steel surfaces, power tool clean to a SSPC-SP 11 cleanliness level. The profile requirement for SSPC-SP 11on critically coated areas in NAVSEA Standard Item 009-32 FY-22CH-1 is waived. Only corrosion shall be removed. Pretreatment of these surfaces shall be achieved IAW SOW para 3.2.2.4.2.2.9 OR 3.2.2.4.3.2.10 depending on substrate type.
3.2.2.4.1.8 The coating colors specified in this document refer to the colors defined by FED-STD-595.
3.2.2.4.2 Steel Substrates
3.2.2.4.2.1 Prepare and coat steel in accordance with NSI 009-32 FY22 CH1, Table 2, Line 1 or 2, Columns A, B, and G amended as follows.
3.2.2.4.2.2 Surface Preparation (i.e., NSI 009-32 FY22 CH1, Table 2, Line 1, Column A):
3.2.2.4.2.2.1 Remove all surface imperfections such as sharp fins, sharp edges, weld splatter, etc.
3.2.2.4.2.2.2 Solvent clean all surfaces to be coated prior to surface preparation to a SSPC-SP 1 cleanliness level.
3.2.2.4.2.2.3 QC/QA CHECKPOINT: Inspect cleanliness IAW 4.5.2 and TABLE XIV, Section II, Line 2A.
3.2.2.4.2.2.4 Abrasive blast non-critically machined steel surfaces to a SSPC-SP 10 cleanliness level with a surface profile of 2-4 mils. Abrasive blasting over intact sealants around fasteners and joints is authorized. SSPC-SP 10 cleanliness shall only be validated on steel surfaces.
For critically machined steel surfaces, power tool clean to a SSPC-SP 11 cleanliness level. The minimum profile requirement of 2 mils for SSPC-SP 11 on critically coated areas in NSI 009-32 FY22 CH1 is waived.
3.2.2.4.2.2.4.1 Water jetting or pressure wash is not allowed.
3.2.2.4.2.2.5 After abrasive blasting/power tool cleaning, use a vacuum and a small hand tool or the corner or edge of a putty knife to remove abrasive media entrapped in sealant used in joints in the work zones.
3.2.2.4.2.2.6 Verify that entrapped grit is removed via visual inspection without magnification. Grit that cannot be removed with a small hand tool/putty knife and vacuum cleaning may be retained.
3.2.2.4.2.2.7 Solvent clean all surfaces to be coated immediately prior to coating application to a SSPC-SP 1 cleanliness level.
3.2.2.4.2.2.8 QC/QA CHECKPOINT: Inspect surface preparation IAW 4.5.3, 4.5.4, and 4.5.5 and TABLE XIV, Section II.
3.2.2.4.2.2.9 Pretreat bare substrate surfaces with zinc phosphate per TT-C-490 Methods 1 and 3, Type
5. The applicable quality control and quality assurance requirements of TT-P-490 still apply.
3.2.2.4.2.2.10 Correct surface imperfections resulting from corrosion, mechanical damage, etc. after abrasive blasting, solvent cleaning, and surface treatment using Devcon steel putty IAW product manufacturer directions. If depth of damage exceeds 1/16” in any area, contact NSWC Crane Requiring Technical Activity (RTA) for proper corrective action before proceeding with the remainder of applicable steps.
3.2.2.4.2.3 Primer Application (i.e., NSI 009-32 FY22 CH1, Table 2, Line 1, Column B):
3.2.2.4.2.3.1 Masking of the retained sealant is not required, and the coating system shall be applied uniformly over any flush-mounted fasteners. Allow primer application over sealant around fasteners and joints.
3.2.2.4.2.3.2 Critically machined metal surfaces shall remain bare unless otherwise specified by the part spec control drawing. If the spec control drawing calls for a protective coating, DFT shall be as specified in the spec control drawing.
3.2.2.4.2.3.3 Primer color shall be of a contrasting color to 26270 (Color #26270) or the specified topcoat color.
3.2.2.4.2.3.4 QC/QA CHECKPOINT: Inspect primer coat IAW 4.5.7 and TABLE XIV, Section II, Line 2A.
3.2.2.4.2.3.5 Topcoat Application (i.e., NSI 009-32 FY22 CH1, Table 2, Line 1, Column G):
3.2.2.4.2.3.6 Topcoat shall be 26270 in color (Color #26270) unless otherwise specified herein.
3.2.2.4.2.3.7 Critically machined surfaces shall not be top coated.
3.2.2.4.2.3.8 Topcoat shall be applied within the dry-to-recoat/overcoat window of any applied primer and/or stripe coat. If primer overcoat window has been exceeded, reactivate the surface IAW NAVSEA-reviewed ASTM F718 for critical applications before proceeding with topcoat application.
3.2.2.4.2.3.9 The primer and topcoat shall be from the same manufacturer.
3.2.2.4.2.3.10 QC/QA CHECKPOINT: Inspect topcoat IAW 4.5.7 and TABLE XIV, Section II, Line
2A.
3.2.2.4.2.3.11 Stenciling shall be applied within the dry-to-recoat/overcoat window of the applied topcoat and IAW the spec control drawing requirements for the part being painted. If the topcoat overcoat window has been exceeded, reactivate the surface IAW NAVSEA-reviewed ASTM F718 for critical applications before proceeding with stenciling. Use mild detergent solution cleaning followed by recommended cleaning solvent in coating mixing procedures.
3.2.2.4.3 Nonferrous Surfaces (Aluminum and Copper Alloys)
3.2.2.4.3.1 Prepare and coat nonferrous (i.e., aluminum and copper alloy) surfaces IAW NSI 009-32
FY22 CH1, Table 2, Line 54, Columns A, B, and G amended as follows.
3.2.2.4.3.2 Surface Preparation (i.e., NSI 009-32 FY22 CH1, Table 2, Line 54, Column A):
3.2.2.4.3.2.1 Remove all surface imperfections such as sharp fins, sharp edges, weld splatter, etc.
3.2.2.4.3.2.2 Solvent clean all surfaces to be coated prior to surface preparation to a SSPC-SP 1 cleanliness level.
3.2.2.4.3.2.3 QC/QA CHECKPOINT: Inspect cleanliness IAW 4.5.2 and TABLE XIV, Section II, Line 2A.
3.2.2.4.3.2.4 Abrasive blast non-critically machined aluminum or copper alloy surfaces to a SSPC-SP
17 cleanliness level with a surface profile of 2-4 mils. Abrasive blasting over intact sealants around fasteners and joints is authorized. SSPC-SP 17 cleanliness shall only be validated on metallic surfaces. For critically machined surfaces, power tool clean to a SSPC-SP 11 equivalent cleanliness level. The profile requirement of 2 mils for SSPC-SP 11 on critically coated areas in NSI 009-32 FY22 CH1 is waived.
3.2.2.4.3.2.5 Water jetting or pressure wash is not allowed.
3.2.2.4.3.2.6 After abrasive blasting/power tool cleaning, use a vacuum and a small hand tool or the corner or edge of a putty knife to remove abrasive media entrapped in sealant used in joints in the work zones.
3.2.2.4.3.2.7 Verify that entrapped grit is removed via visual inspection without magnification. Grit that cannot be removed with a small hand tool/putty knife and vacuum cleaning may be retained.
3.2.2.4.3.2.8 Solvent clean all surfaces to be coated immediately prior to coating application to a SSPC-SP 1 cleanliness level.
3.2.2.4.3.2.9 QC/QA CHECKPOINT: Inspect surface preparation IAW 4.5.3, 4.5.4, and 4.5.5 and TABLE XIV, Section II.
3.2.2.4.3.2.10 Pretreat bare substrate surfaces with conversion coating per MIL-DTL-5541 Type I or II Class 1A, MIL-PRF-8625 Type I Class 1, or alternatively with SurTec 650 ChromitAL TCP (preferred choice), Safeguard CC-6100, or Alodine 5700. If using a MIL-DTL-5541 alternative, the applicable quality control and quality assurance requirements of MIL- DTL-5541 still apply.
3.2.2.4.3.2.11 Correct surface imperfections resulting from corrosion, mechanical damage, etc. after abrasive blasting, solvent cleaning, and surface treatment using Devcon aluminum putty for aluminum alloy substrates or bronze putty for copper alloy substrates IAW product manufacturer directions. If depth of damage exceeds 1/16” in any area, contact NSWC Crane Requiring Technical Activity (RTA) for proper corrective action before proceeding with the rest of this document.
3.2.2.4.3.2.12 Primer Application (i.e., NSI 009-32 FY22 CH1, Table 2, Line 54, Column B):
3.2.2.4.3.2.13 Masking of the retained sealant is not required, and the coating system shall be applied uniformly over any flush-mounted fasteners. Allow primer application over sealant around fasteners and joints.
3.2.2.4.3.2.14 Critically machined metal surfaces shall remain bare unless otherwise specified by the part spec control drawing. If the spec control drawing calls for a protective coating, DFT shall be as specified in the spec control drawing.
3.2.2.4.3.2.15 Primer color shall be of a contrasting color to 26270 (Color #26270) or the specified topcoat color.
3.2.2.4.3.2.16 QC/QA CHECKPOINT: Inspect primer coat IAW 4.5.7 and TABLE XIV, Section II, Line 2A.
3.2.2.4.3.2.17 Topcoat Application (i.e., NSI 009-32 FY22 CH1, Table 2, Line 54, Column G):
3.2.2.4.3.2.18 Topcoat shall be 26270 in color (Color #26270) unless otherwise specified herein.
3.2.2.4.3.2.19 Critically machined surfaces shall not be top coated.
3.2.2.4.3.2.20 Topcoat shall be applied within the dry-to-recoat/overcoat window of any applied primer and/or stripe coat. If primer overcoat window has been exceeded, reactivate the surface IAW NAVSEA-reviewed ASTM F718 for critical applications before proceeding with topcoat application.
3.2.2.4.3.2.21 The primer and topcoat shall be from the same manufacturer.
3.2.2.4.3.2.22 QC/QA CHECKPOINT: Inspect topcoat IAW 4.5.7 and TABLE XIV, Section II, Line
2A.
3.2.2.4.3.2.23 Stenciling shall be applied within the dry-to-recoat/overcoat window of the applied topcoat and IAW the spec control drawing requirements for the part being painted. If the topcoat overcoat window has been exceeded, reactivate the surface IAW NAVSEA-reviewed ASTM F718 for critical applications before proceeding with stenciling. Use mild detergent solution cleaning followed by recommended cleaning solvent in coating mixing procedures.
3.2.2.5 The Contractor shall provide and install new identification plates and warning labels with the same stamped information as the original plates/labels removed during motor evaluation. The Contractor shall use rivets to install new identification plates and warning labels.
3.2.2.6 The contractor shall perform a standard overhaul on SPS-49 Elevation Drive DC Motors as directed by orders and in accordance with paragraph 3.2. The contractor shall test the subassembly upon completion of the standard overhaul and/or supplemental repair (if required and approved) in accordance with paragraph 3.3 of this SOW.
3.2.3 Extensive & Supplemental Overhaul
3.2.3.1 AN/SPS-49 Pedestal DC Motor Level II Overhaul – DC Motor Brush Holder Assembly. The Contractor shall replace the DC elevation drive motor brush holder assembly and associated hardware parts that are identified as non-mandatory in Table 9-4, 9- 6, and Figure 9-3 (item number 35) of Specification SE110-A2-MMD-010; and IAW Drawing 914104 and Specification 914321.
3.2.3.2 AN/SPS-49 Pedestal DC Motor Level III Overhaul – Rotor/Stator Repairs. The Contractor shall complete partial magnet replacement, field coil repairs, partial armature winding repairs, and yoke repairs.
3.2.3.3 AN/SPS-49 Pedestal DC Motor Level IV Overhaul – Armature Assembly. The Contractor shall replace the armature assembly and associated hardware parts that are identified as non-mandatory in Table 9-4, 9-5, 9-6, and Figure 9-3 (item number 27) of Specification SE110-A2-MMD-010;
and IAW Drawing 914104; and Specification 914321.
3.2.3.4 AN/SPS-49 Pedestal DC Motor Level V Overhaul – Frame Assembly. The Contractor shall replace the frame assembly and associated hardware parts that are identified as non-mandatory in Table 9-4, 9-5, 9-6, and Figure 9-3 (item number 55) of Specification SE110-A2-MMD-010; and IAW Drawing 914104 and Specification 914321.
3.2.3.5 AN/SPS-49 Pedestal DC Motor Level VI Overhaul – Back End Bracket. The Contractor shall replace the back end bracket and associated hardware parts that are identified as non-mandatory in Table 9-4, 9-5, 9-6, and Figure 9-3 (item number 44) of Specification SE110-A2-MMD-010;
and IAW Drawing 914104 and Specification 914321.
3.3 Testing Requirements - 914104 – Direct Current Motor (CDRL A003)
3.3.1 Vendor shall test all assets IAW SE110-A2-MMD-010 Section 6 para 9-6 Post Reassembly
Testing
3.3.2 Vendor shall provide all reports/data per specification number SE110-A2-MMD-010 Section 6
Para 9-6.1
3.3.2.1 Exception to locked motor shaft during test: Test will be conducted using a dynamometer, and motor loaded between 30.5-31.5 amps. This requirement is in lieu of the 100amp locked rotor requirement.
3.3.3 Vendor shall provide all reports/data per specification number SE110-A2-MMD-010 Section 6 Para 9-6.2.
3.3.4 Vendor shall provide all reports/data per specification number SE110-A2-MMD-010 Section 6 Para 9-6.3
3.3.5 Vendor shall provide all reports/data per specification number SE110-A2-MMD-010 Section 6 Para 9-6.4
3.3.6 Vendor shall provide all reports/data per specification number SE110-A2-MMD-010 Section 6 Para 9-6.5
3.3.7 Vendor shall provide all reports/data per specification number SE110-A2-MMD-010 Section 6 Para 9-6.6
3.3.8 Vendor shall provide all reports/data per specification number SE110-A2-MMD-010 Section 6 Para 9-6.7
3.3.9 Vendor shall provide all reports/data per specification number SE110-A2-MMD-010 Section 6 Para 9-6.8
3.3.10 The aforementioned requirements apply and shall be performed for every delivery item, and overhaul, as stated.
3.3.11 Test report for each overhauled asset shall show all test results in table type format comparing test values with corresponding performance requirements, difference (in percentage), allowed tolerance, and pass or fail rating. The Contractor’s test report shall identify the serial number of the refurbished motor and a hard copy of the test report shall accompany the DC Elevation Drive Motor when returned to the Government.
3.4 Component Certifications
3.4.1 As specified in the drawing specifications of each assemblies’ components, a Certificate of
Conformance shall be delivered to the Government with each order with the exception of overhauled assets. Replaced components must be accompanied with a Certificate of Conformance. (CDRL A004)
3.4.2 The Contractor shall inspect each manufactured item and/or purchased item against drawings/specifications, and shall provide a Certificate of Compliance to document conformance of each hardware item/component with item drawings/specifications. The Contractor shall provide a hard copy of the Certificate of Compliance with each item produced IAW with this SOW to be shipped with the asset. Contractor shall make electronic copies of the Certificate of Compliance available to the Government upon request. (CDRL A005)
4. GOVERNMENT FURNISHED PROPERTY (CDRL A006)
4.1. GOVERNMENT FURNISHED INFORMATION (GFI): The documents/drawings listed in section 2 of this SOW will be provided along with associated part lists and subassembly drawings owned by the government. Military and Commercial Specifications will not be provided.
4.2. GOVERNMENT FURNISHED MATERIAL (GFM): The Government will provide AN/SPS-49 Elevation Drive DC Motors as required for evaluation, overhaul, and supplemental repair.
4.2. GOVERNMENT FURNISHED EQUIPMENT (GFE): The Government will not provide equipment for execution of requirements.
5. Data Deliverables
5.1. The Contractor shall submit the following data deliverables in accordance with the requirements listed in the Contractor Data Requirements Lists (CDRL’s).
CDRL: A001
DID Number: DI-MISC-80508B DID Title: Technical Report-Study/Services DID Sub-Title: Engineering Change Proposal SOW Paragraph: 3.1.7
CDRL: A002
DID Number: DI-NDTI-80809B DID Title: Test/Inspection Report DID Sub-Title: Evaluation Report SOW Paragraph: 3.2.1
CDRL: A003
DID Number: DI-NDTI-80809B DID Title: Test/Inspection Report DID Sub-Title: Unit Test/Inspection Report SOW Paragraph: 3.3; 3.2.2.4
CDRL: A004
DID Number: DI-MISC-80809B DID Title: Certificate of Conformance SOW Paragraph: 3.4.1
CDRL: A005
DID Number: DI-MISC-81356A DID Title: Certificate of Compliance SOW Paragraph: 3.4.2
CDRL: A006
DID Number: DI-MGMT-80441D DID Title: GFP SOW Paragraph: 4.0
6. Special Conditions
6.1 Quality
6.1.1 Quality Program: The contractor shall have a quality program that is ISO 9001-2008 compliant or meets the following requirements: monitor and control critical processes; continuously improve processes; establish mechanisms for performance feedback; and maintain an effective root cause analysis and corrective action system.
6.1.2 Quality Assurance. The contractor shall ensure each final machined and/or repaired subassembly meets all specifications IAW the applicable drawings and subsequent referenced documents.
The contractor shall ensure that only approved parts and processes were used to fulfill requirements of this SOW. All assets shall be government inspected and accepted at destination.
6.2 Counterfeit Parts and Material
6.2.1 Counterfeit materiel is a serious threat to the safety and operational effectiveness of DoD systems. The contractor (and subcontractors at all levels) shall implement a risk mitigation process when obtaining critically or high risk materiel in accordance with Paragraphs (6.2.1 and 6.2.2) below:
6.2.2 If the materiel is currently in production or currently available, the materiel shall be obtained only from authorized sources. Authorized sources are the original manufacturer, a source with the express written authority of the original manufacturer or current design activity, or an authorized aftermarket manufacturer.
6.2.3 If the materiel is not in production or currently available from authorized sources, the materiel shall be obtained from suppliers that meet appropriate counterfeit avoidance criteria. Counterfeit avoidance criteria can be found in the following Industry Standards – SAE AS5553A; SAE AS5452; SAE AS6081; SAE ARP617; SAE AS6174; and SAE AS6301.
6.2.4 Contractors shall notify the KO when critical or high risk materiel cannot be obtained from an authorized source. The contractor shall take mitigating actions to authenticate the materiel if purchased from another source. The contractor shall report instances of counterfeit and suspect counterfeit materiel to the Contracting Officer and the Government Industry Data Exchange Program (GIDEP) as soon as the contractor becomes aware of the issue.
7 Point of Contacts
7.1 Brian Brinegar
Crane Division, Naval Surface Warfare Center (NSWC Crane) Harnessing the Power of Technology of the Warfighter, Building 3168 300 Highway 361 Crane, IN 47522-5001 Phone: 812-854-5106 Cell: 812-381-7529 Email: brian.w.brinegar.civ@us.navy.mil mailto:brian.w.brinegar.civ@us.navy.mil
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