DRAFT SOW MDR Power Supply.pdf

U.S. Department of Transportation Federal Aviation Administration

Logistics Center

MDR Power Supply

Statement of Work

Prepared by FAA Logistics Center Automation Communications Product Group (AJW-L800)

Date 5/7/24

MDR Power Supply Contract

Table of Contents

1.0 INTRODUCTION

1.1 FAA LOGISTICS CENTER

1.2 PRODUCT GROUP

1.3 ACQUISITION BACKGROUND

2.0 SCOPE OF WORK

2.1 OVERVIEW

2.2 OBJECTIVES

3.0 APPLICABLE DOCUMENTS

3.1 OVERVIEW

3.2 DOCUMENT LIST

4.0 DESCRIPTION OF TASKS

4.1 MANUFACTURE PARTS

4.2 TEST PARTS

4.3 DELIVER PARTS

4.4 PROVIDE DOCUMENTATION

4.5 PROVIDE QUALITY CONTROL

5.0 OTHER REQUIREMENTS

5.1 PLACE OF PERFORMANCE

5.2 PERIOD OF PERFORMANCE

5.3 ADDITIONAL REQUIREMENTS ............................................. ERROR! BOOKMARK NOT DEFINED.

6.0 PARTS

6.1 PARTS TABLE

6.2 PART SPECIFICATIONS

7.0 DOCUMENTATION DELIVERABLES

7.1 DOCUMENTATION TABLE

7.2 DOCUMENTATION REQUIREMENTS

APPENDIX A - ACRONYMS

APPENDIX B - PARTS TABLE

APPENDIX C - PRODUCT SPECIFICATIONS AND REQUIREMENTS

1.0 Introduction

1.1 FAA Logistics Center

The Federal Aviation Administration Logistics Center (FAALC) is located at the Mike Monroney Aeronautical Center (MMAC) in Oklahoma City, Oklahoma. The FAALC is responsible for providing the critical functional discipline that establishes and maintains supply support for the National Airspace System (NAS) systems while cost effectively providing core logistics activities.

The FAALC:

a. Performs centralized maintenance, repair and overhaul of NAS equipment and test equipment, including engineering, and configuration management at the line replaceable unit (LRU).

b. Operates the FAA’s only centralized distribution center, which houses the FAA NAS inventory valued at over $825 million dollars using a state-of-the-art warehouse management system.

c. Provides 24/7/365 supply chain management and logistics support services for the NAS for over 62,000 national stock numbers (NSNs).

d. Works in conjunction with FAA’s Air Traffic Organization in providing support to the NAS through each phase of the product lifecycle for all the elements of integrated logistics support planning.

e. Provides core logistics capabilities to the FAA (such as rapid response to contingencies, quick reaction to technical surprises, last source for systems no longer supported by contractors, etc.).

f. Provides on-site maintenance and installation teams and project management field support.

g. Manages NAS parts and operates the FAA’s centralized logistics ordering system.

h. Provides traffic management and transportation services in support of FAALC program and

MMAC requirements.

i. Provides engineering capability and operates a central shop for fabrication, modification, overhaul, repair, test, and calibration of NAS systems equipment and components.

j. Manages and controls FAA supply support activities conducted with other Government entities and friendly foreign Governments.

k. Develops and recommends supply chain management procedures and standards for the

FAA.

1.2 Product Group

AJW-L800 Automation/Communication Product Group:

The FAALC AJW-L800 Automation/Communication Product Group is responsible for the repair and distribution of FAA Automation and Communication equipment used within the NAS. This includes flight controller automation systems such as information and aircraft control displays, aircraft position computers and displays, automated weather and facilities information broadcast equipment. Communications equipment for ground facilities, both inter facility and long distance intra facility communications. AJW-L800 also supports the radio communication systems used for emergency response and air to ground communication.

The AJW-L800 Automation/Communication Product Group provides logistics support to the field sites within the FAA and DoD in the form of supply support provided by the LCSS ordering system and monitored by the Item Managers (IM). These individuals monitor and ensure adequate stock levels through purchase and repair of assets. The IMs provide direct communication to the field sites with regard to questions and warranty issues as they arise. The IMs are directly supported by the Provisioners (PV), Logistics Management Specialists (LMS) and Engineers (ENG) who research and support the sustainment activities and coordinate with the National Program Offices and necessary. AJW-L800 also provides repair support by highly trained Electronics Technicians (ET) using the manufacturer’s documentation to the same standards as are expected from the field or higher.

1.3 Acquisition Background

This acquisition is needed to support CAVU-2100 Multimode Digital Radios (MDR) to provide long term sustainment in support of the FAA En-Route Communication facilities.

This statement of work (SOW) describes the requirements for the production of CAVU-2100 Power Supply Assemblies Rev 1 (MDR PS). These power supplies were developed by the FAA Oklahoma Communication Engineering Team AJW-153 (OKCET) in response to the high failure rate of the original power supply used in the MDR.

SOW acronyms are defined in Appendix A.

2.0 Scope of Work

2.1 Overview

Contractor must provide all required labor, plant facilities, tools, equipment, test equipment, fixtures, parts, supplies, materials, appropriate technical data/expertise, transportation, preservation, packaging, packing and marking, and all other items required to complete SOW tasks and provide SOW deliverables.

• Contractor must manufacture the CAVU-2100 Power Supply PCB to the specifications provided in SOW Attachment 8 thru 17. Complete Gerber and manufacturing files will be provided to the award contractor.

• Components used must correspond to Attachment 9 20230502_CAVU2100PWRSUP_BOM_Baseline_PWB8199132-FAA-2A.xlsx Any deviations or planned substitutions must be approved by AJW-L800 and the Bill Of Materials revised to reflect the change.

• The contractor must manufacture the Heat Sink, pn 110405b, to the specifications described in Attachment 7.

• The Heat Sink must be attached to the CAVU-2100 Power Supply PCB and power regulators using the hardware listed in the BOM lines 93-96.

• The PCB/Heatsink assembly must be tested in accordance with Attachment 1 CAVU-2100 SOW Test Procedures.

• The assembled and tested PCB/Heat Sink Assembly must be placed in a static resistant bag meeting the specifications listed in Attachment 26 TDR for 100027530

CAVU2100 PSU and Attachment 27 PHS&T for MDR Power Supply 100027530.

This bag will have a metallized internal coating and static resistant external bag of sufficient strength and protective qualities to provide both Electro-Statis Discharge protection and physical support to prevent incidental damage to the PCB/Heat Sink assembly.

• The contractor must complete a test report, Attachment 3 CAVU_2100_TEST, and provide this form with the complete assembly.

• The contractor must manufacture the AC Monitor Cable in accordance with Attachment 18 thru 25. Complete Gerber and manufacturing files will be provided to the award contractor.

• The contractor must test each cable assembly in accordance with the procedures in Attachment 1 CAVU2100 SOW Test Procedures.

• The contractor must provide a Front Panel Label in a separate static resistant bag for each assembled assembly.

• The contractor must place one (1) each PCB/Heat Sink Assembly in the protective bag, the test document, one (1) each AC Monitor Cable and one (1) each Front Panel Label in a box meeting the requirements of Attachment 26 TDR and Attachment 27 PHS&T with sufficient padding to prevent damage. A label must be affixed to the box with the following information:

LCSS Part Number 100025730 Cage Code and Manufacturer’s Part Number Part Description CAVU2100 Power Supply Assy Quantity and Unit of Issue one (1) each Delivery Order# and Contract # ESD Label and precautionary markings

• FAA Power Supply Board; update BOM to add second sourcing and also update obsolete components. Create the Altium libraries that were not included in the design package. Modify the schematic and PCB with the updated and new components.

Generate all necessary manufacturing files. Deliver any updated or modified files to the FAALC as updates to the product documentation. include Altum package:

Schematic, PCB, Libraries, Gerber Files, Pick & Place Files, Drill Files, Panel Files, BOM, Component Datasheets.

• Deliver completed assemblies to the FAALC at this address:

6973FF OPS Stock, 6500 S. MacArthur Blvd, Oklahoma City, Oklahoma, 73169

2.2 Objectives

The objective of this acquisition is:

a. Provide AJW-L800 with QTY 600 MDR PS assemblies per year to facilitate the repair of the MDR transmitter.

3.0 Applicable Documents

a. Attachment 1 CAVU 2100 SOW Test Procedures.pdf

b. Attachment 2 TemperatureChamberTesting.pdf

c. Attachment 3 CAVU_2100_TEST.pdf

d. Attachment 4_Cover_TestingAll_MDR_TX_RX_ITTvsRev1_PS_w_BackPage26.pdf

e. Attachment 5 CAVU-2100 NOT USED Label Description.pdf

f. Attachment 6 CAVU-2100 Panel Label.jpg

g. Attachment 7 Heat Sink 8199217b.pdf

h. Attachment 8 CAVU2100_PWRSUPPLY_Rev2_20190425.pdf

i. Attachment 9 20190708_CAVU2100PWRSUP_BOM_Baseline_PWB8199132-FAA-

2A.xlsx

j. Attachment 10 CAVU-2100 Power Supply Assembly Drawings – Bottom.pdf

k. Attachment 11 CAVU-2100 Power Supply Assembly Drawings – Top.pdf

l. Attachment 12 CAVU-2100 Power Supply Composite Drill Drawing.pdf

m. Attachment 13 CAVU-2100 Power Supply PCB 3D Prints - Bottom.pdf

n. Attachment 14 CAVU-2100 Power Supply PCB 3D Prints – Top.pdf

o. Attachment 15 CAVU-2100 Power Supply PCB PCB Prints – Bottom.pdf

p. Attachment 16 CAVU-2100 Power Supply PCB PCB Prints – Top.pdf

q. Attachment 17 CAVU-2100 Power Supply Schematic Prints.pdf

r. Attachment 18 CAVU2100_AC_Monitor_CableAssembly_Rev1a_8220004_01092018.pdf

s. Attachment 19 8220005 Assembly Drawing – Top.pdf

t. Attachment 20 8220005 Composite Drill Drawing.pdf

u. Attachment 21 8220005 PCB 3D Prints - Bottom.pdf

v. Attachment 22 8220005 PCB 3D Prints - Top.pdf

w. Attachment 23 8220005 PCB Prints - Bottom.pdf

x. Attachment 24 8220005 PCB Prints - Top.pdf

y. Attachment 25 8220005 Schematic Prints - Top.pdf

z. Attachment 26 TDR for 100027530 CAVU2100 PSU.pdf

aa. Attachment 27 PHS&T for MDR Power Supply 10 yr 100027530.pdf

bb. Attachment 28 Drawings combined.pdf

3.1 Overview

Contractor must comply with the applicable documents specified in this SOW. Contractor must perform in accordance with (IAW) the version of these documents in effect at the time of contract award, unless newer versions are incorporated through contract modifications. Contractor must advise FAA in the event of discovering a conflict between this SOW and any of the applicable documents. The Contracting Officer (CO) or Contracting Officer’s Representative (COR) will work with the Contractor to resolve the discrepancy.

4.0 Description of Tasks

Contractor must complete the following tasks.

4.1 Manufacture Parts

• Procure all items listed on the Bill of Materials (BoM) (See Attachment 9 20230502_CAVU2100PWRSUP_BOM_Baseline_PWB8199132-FAA-2A.pdf, Attachment 7 Heat Sink 8199217b.pdf, Attachment 5 CAVU-2100 NOT USED

Label Description.pdf and Attachment 18_OKCET_CAVU2100_AC_Monitor_CableAssembly_Rev1a_8220004_0101201 8.pdf).

• Manufacture of MDR PS PCB (Attachment 8 CAVU2100_PWRSUPPLY_Rev2_20190425.pdf and Attachments 10 thru 17 Assembly Drawings)

• Manufacture the MDR PS Heat Sink (See Attachment 7 Heat Sink 8199217b.pdf).

• Produce the MDR PS Front Panel Label (See Attachment 5 CAVU-2100 NOT

USED Label Description.docx and Attachment 6 CAVU-2100 Panel Label.jpg).

• Manufacture the MDR PS Transformer Cable (See Attachment 18

CAVU2100_AC_LineVoltageMonitorCableAssembly_Rev1a_8220004_ 01092018.pdf and Attachment 19 thru 25 8220005 Assembly Drawings).

• Attach MDR PS Heat Sink to MDR PS PCB (Hardware described in BOM lines 93- 95).

• Initial Set-Up and Test Evaluation (See Attachment 1 CAVU 2100 SOW Test Procedures.pdf).

• Transformer Cable test validation (See Attachment 1 CAVU 2100 SOW Test Procedures.pdf).

• Packaging of the assembly and components to prevent damage during shipping (See Attachment 26 TDR for 100025730 CAVU2100 PSU.pdf and Attachment 27 PHS&T for MDR Power Supply 100025730.pdf).

• Delivery of assemblies to the FAA Logistics Center (see section 4.3.4).

4.2 Test Parts

Contractor must provide CAVU 2100 Power Supply assemblies for First Article Testing and establish Production Testing procedures as per this section.

4.2.1 First Article Testing

Contractor must submit to FAA a quantity of ten (10) first article assemblies for FAA’s testing unless a first article inspection has previously been performed on the manufacturer’s product. This is in addition to the production quantity. FAA must receive first articles within 60 calendar days after date of contract award. FAA has 120 calendar days after receipt of first articles to issue written notice to the Contractor of approval or disapproval. First articles must be shipped to the following address:

FAA Logistics Center, AJW-L830 Technical Support Facility - Building 215 WC810 7100 South MacArthur Blvd.

Oklahoma City, OK 73169 Mark For: Paul Hornbeck

First articles must meet or exceed the following requirements in order to be approved before production can commence:

a. Physical Conformity analysis meeting the specifications given in the design documentation.

b. Transformer Cable testing as per Attachment 1 CAVU 2100 SOW Test Procedures.pdf.

c. Power Relay testing as per Attachment 1 CAVU 2100 SOW Test Procedures.pdf.

d. Temperature Chamber Testing: Performance evaluation from -10° C to 50° C patterned after

Attachment 2 TemperatureChamberTesting.pdf.

e. Field performance testing as directed by AJW-173 OKCET. This will be performed in a similar fashion to Attachment 4_Cover_TestingAll_MDR_TX_RXITTvsRev1_PS_w_ BackPage.pdf.

4.2.2 Production Testing

Contractor must perform parts production testing. Contractor must:

a. Perform the transformer cable and initial set-up and test evaluation per Attachment 1 CAVU 2100 SOW Test Procedures.pdf.

b. Perform the CAVU-2100 Trip set points initial setup.

c. Perform CAVU-2100 Output verification.

d. Perform CAVU-2100 Relay Burn-In Testing.

e. Fill out and complete the Test Report summary for each board (Attachment 3

CAVU_2100_Test.pdf.

4.3 Deliver Parts

4.3.1 Preservation, Packaging, Packing and Marking

a) All components and equipment with a consignee other than the FAALC must be preserved, packaged, and packed to American Society for Testing and Materials ASTM D-3951, “Standard Practices for Commercial Packaging”.

b) All components and equipment consigned to the FAALC must be individually packaged to American Society and Testing and Materials ASTM D-3951 (packaging).

Performance testing of packaging will be in accordance with ASTM D-4169 assurance level II distribution cycle 18.

c) All components, equipment and spares with a consignee other than FAALC must be marked in accordance with the marking requirements of ASTM-D-3951. In addition, each unit, intermediate, and exterior shipping container must be marked with the following information:

1) National Stock Number 5998-01-685-1441

2) Part Number 100025730

d) All components, equipment and spares consigned to the FAALC must be marked in accordance with MIL-STD-129R. In addition to MIL-STD-129R, each unit, intermediate, and exterior shipping container must be marked with the following information:

1) National Stock Number 5998-01-685-1441

2) Part Number 100025730

3) Warranty Expiration Date

4) Contract Number

Contractor must meet the following preservation, packaging, packing and marking (PPP&M) requirements.

Wrapping Material: MIL-PRF-81705 Type III, Class I, Transparent, Electrostatic-Protective, Static Shielding Barrier Material (This material must have a metallized interior surface and a static dissipative outer surface)

Cushioning Thickness: 2 inch Minimum on All Surfaces

Marking: Each container must be clearly marked with the following information:

(1) LCSS Part Number 5998-01-685-1441

(2) Cage Code and Manufacturer’s Part Number

(3) Part Description CAVU2100 MDR Power Supply Assy

(4) Quantity and Unit of Issue

(5) PO# and Contract #

(6) ESD Label and precautionary markings

Copies of the ASTMs can be attained from:

ASTM

100 Barr Harbor Dr.

West Conshohocken, PA 19428

(610) 832-9500

Copies of the MIL-STD can be attained from:

DODSSP

Customer Service Standardization Documents Order Desk 700 Robbins Avenue Building 4D Philadelphia, PA 19111-5094

4.3.2 Storage and Handling

The contractor must handle and store the parts in such a manner as to preclude damage due to handling and the elements.

4.3.3 Transportation

Contractor must provide shipping to the FAALC, Oklahoma City, OK.

4.3.4 Delivery Destination

Contractor must ship all production assemblies FOB destination to the following address.

SSC 697349, M-F Operational Stock 6500 S. MacArthur Blvd.

Oklahoma City, OK 73169

4.3.5 Delivery Schedule

Contractor must meet the following parts delivery schedule.

First delivery of production units will be within 90 calendar days of issuance of delivery order following First Article Acceptance. Subsequent orders must be delivered within 90 calendar days of issuance of delivery order(s).

4.4 Provide Documentation

Contractor must provide the following documentation:

4.4.1 Parts Testing Documentation

Contractor must provide parts testing documentation. Contractor must provide test procedures, test data forms and test results. Contractor must enclose a copy or close facsimile of Attachment 3 CAVU_2100_TEST.pdf. with each assembly.

4.4.2 Quality Control Documentation

Contractor must provide quality control documentation. Contractor must provide a copy of Attachment 3 CAVU_2100_TEST.doc with each assembly, or a close facsimile thereof.

4.4.3 Parts Technical Documentation

Contractor must maintain component technical documentation. Contractor must adhere to the component specifications as described in the technical documentation. Before any changes can be attempted the Contractor must contact the COR to confirm product compatibility requirements. Any updated files must be provided to the Federal Aviation Administration for configuration control purposes. Any updated documentation becomes the property of the FAA.

4.5 Quality Control

4.5.1 Quality Management System

Contractor must maintain quality control for all tasks, parts and documentation deliverables the Contractor provides under this SOW. FAA will monitor the Contractor’s performance. Contractor must work with FAA to resolve performance issues. Contractor must provide:

An auditable Quality Management System containing all Elements of the ANSI/ASQC/ISO 9000 Standard exist. Applicable IPC workmanship standards must be followed. Product will be inspected and accepted/ rejected at destination by the FAA for Technical Specifications and Packaging Specifications, as stated in the Contract. Certificates of Compliance must be supplied where applicable.

The following specifications are applicable to this acquisition:

a) Manufacturer’s specification must be within those specifications given in Section 4.1 of this document.

b) ANSI/ASQC Q9001 Quality Assurance in Design, Development, Production, Installation and Servicing

c) ANSI/ASQC Q9002 Quality Assurance in Production, Installation and Servicing

d) ANSI/ASQZ1.4-1993 Sampling Procedures and Tables for Inspection by Attributes

e) The calibration of measuring and testing equipment must adhere to the requirements of one of the following:

a. ANSI/NCSL Z540-1-1994; ISO/IEC 17025:2005; or other calibration standards or systems that are equivalent to, or better than, the ANSI/NCSL/ISO standards

4.5.2 Inspection and Acceptance

FAA has the right to inspect and determine acceptance to the extent specified in the SOW and the other contract documents such as inspection/acceptance clauses. Contractor must meet the following inspection and acceptance requirements.

Product will be inspected and accepted/rejected at destination by the FAA for Technical Specifications and Packaging Specifications, as stated in the Contract.

4.5.3 Warranty

Contractor must meet the following warranty requirements:

A one-year warranty will be provided for the assemblies.

5.0 Other Requirements

Contractor must meet the following requirements.

5.1 Place of Performance

FAA expects the primary work location will be at the Contractor’s facility.

5.2 Period of Performance

The contract period of performance is a one (1)-year base period and four (4) 1-year option periods to be exercised at the sole discretion of the government.

6.0 Parts

6.1 Parts Table

Contractor must deliver in new condition the parts shown in the Parts Table in Appendix B.

Contractor must supply these parts in the quantities ordered and meet the delivery schedule specified in the contract and delivery orders.

6.2 Part Specifications

Contractor must deliver parts that meet the provided manufacturing specifications. Any substitutions or deviations must be pre-approved by AJW-L800 and documented in the appropriate specifications.

7.0 Documentation Deliverables

7.1 Documentation Table

Contractor must provide the documentation deliverables shown in the following Documentation Table. Contractor must submit each deliverable on or before the due date given in this table. The COR under special circumstances may extend a due date.

Documentation Table

SOW # Deliverable Deliverable Description Due Date

4.2, 4.4.1 Parts Testing Documentation

Test Procedures, Test Data Forms and Test Results

Within 90 calendar days of contract start

4.4.2, 4.5 Quality Control Documentation CAVU_2100_TEST.pdf To be delivered with each assembly

4.4.3, 6.2 Parts Technical Documentation

As Required by changes in design or construction As required

7.2 Documentation Requirements

FAA has the right to inspect, determine acceptance and require changes prior to final acceptance for all documentation deliverables developed under this contract. FAA actions in this regard will be consistent with SOW requirements, the contract and industry best practice. All documentation deliverables provided by the Contractor become the exclusive property of the FAA and for FAA to use without limits, unless existing intellectual property rights or other parts of this contract supersede that.

Contractor must submit documentation deliverables to the COR. Contractor must use Microsoft Office 2010 applications for documentation deliverables developed under this contract, unless FAA authorizes otherwise. Documentation must be submitted by email in editable formats, unless FAA authorizes otherwise. For example, portable document format (PDF) files are not editable, but may sometimes be necessary.

Appendix A - Acronyms

AJW-L Federal Aviation Administration Logistics Center BOM Bill of Materials CO Contracting Officer (refers only to a FAA position) COR Contracting Officer’s Representative (refers only to a FAA position) ENG Engineer FAA Federal Aviation Administration FAALC Federal Aviation Administration Logistics Center FOB Freight on Board IAW In Accordance With IM Item Manager LMS Logistics Management Specialist MDR Multi-Mode Digital Radio (CAVU-2100) MDR PS CAVU-2100 Power Supplies Rev 1 MMAC Mike Monroney Aeronautical Center NAS National Airspace System NSN National Stock Number OKCET Oklahoma Communications Engineering Team AJW-173 PDF Portable Document Format PHS&T Packaging, Handling, Shipping and Transportation PN Part Number PPP&M Preservation, Packaging, Packing and Marking PV Provisioner QTY Quantity SOW Statement of Work TDR Technical Data for Requirements US United States

Appendix B - Parts Table

Parts Table

Part Number Item Description Qty

100027530 CAVU 2100 Power Supply Assembly (Consists of the 110405b Heat Sink and

PWB8199132-FAA-2A CAVU 2100 Power Supply Rev 1 assembly, the 8220004 CAVU 2100 Cable Assembly and the CAVU 2100 Panel Label)

Note: Quantities in above table are an estimate for each contract year.

Appendix C - Product Specifications and Requirements

Attachment 1 CAVU 2100 SOW Test Procedures Attachment 2 TemperatureChamberTesting Attachment 3 CAVU_2100_Test.pdf Attachment 4 Cover_TestingAll_MDR_TX_RX_ITTvsREV1_PS_w_BackPage26.pdf Attachment 5 CAVU-2100 NOT USED Label Description.pdf Attachment 6 CAVU-2100 Panel Label.pdf Attachment 7 Heat Sink 110405b.PDF Attachment 8 CAVU2100_PWRSUPPLY_Rev2_20190425.pdf Attachment 9 20230502_CAVU2100PWRSUP_BOM_Baseline_PWB8199132-FAA-2A.xlsx Attachment 10 CAVU-2100 Power Supply Assembly Drawings-Bottom.pdf Attachment 11 CAVU-2100 Power Supply Assembly Drawings-Top.pdf Attachment 12 CAVU-2100 Power Supply Composite Drill Drawings.pdf Attachment 13 CAVU-2100 Power Supply PCB 3D Prints-Bottom.pdf Attachment 14 CAVU-2100 Power Supply PCB 3D Prints-Top.pdf Attachment 15 CAVU-2100 Power Supply PCB Prints-Bottom.pdf Attachment 16 CAVU-2100 Power Supply PCB Prints-Top.pdf Attachment 17 CAVU-2100 Power Supply Insulator Notes.pdf Attachment 18 OKCET_CAVU_2100_AC_Monitor_CableAssembly_Rev1a_8220004_01092018.pdf Attachment 19 822005 Assembly Drawing-Top.pdf Attachment 20 822005 Composite Drill Drawing.pdf Attachment 21 822005 PCB 3D Prints-Bottom.pdf Attachment 22 822005 PCB 3D Prints-Top.pdf Attachment 23 822005 PCB Prints-Bottom.pdf Attachment 24 822005 PCB Prints-Top.pdf Attachment 25 822005 Schematic Prints.pdf Attachment 26 TDR for 100027350 CAVU2100 PSU.pdf Attachment 27 PHS&T for MDR Power Supply 100027530.pdf Attachment 28 Drawings combined.pdf