Attachment J.1 SOW MDR Power 06-20.pdf

U.S. Department of Transportation Federal Aviation Administration

Logistics Center

MDR Power Supply

Statement of Work

Prepared by FAA Logistics Center Organization Name (AML-8000)

Date 7/10/2019

MDR Power Supply Contract

Table of Contents

1.0 INTRODUCTION

1.1 FAA LOGISTICS CENTER

1.2 PRODUCT DIVISION

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 ................................................................. ERROR! BOOKMARK NOT DEFINED.

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 - PART SPECIFICATIONS

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.

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 Division

AML-8000 Automation/Communication Product Division

The FAALC AML-8000 Automation/Communication Product Division 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. AML-8000 also supports the radio communication systems used for emergency response and air to ground communication.

The AML-8000 Automation/Communication Product Division 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. AML-8000 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 Supplies Rev 1 (MDR PS). These power supplies were developed by the FAA Oklahoma Communication Engineering Team AJW-173 (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:

• Procure all items listed on the Bill of Materials (BoM) (See Attachment 9 20190708_CAVU2100PWRSUP_BOM_Rev_2_Baseline.pdf, Attachment 7 Heat Sink 8199217_A.pdf, Attachment 5 CAVU-2100 NOT USED Label Description.pdf and Attachment 18 OKCET_CAVU2100_AC_Monitor_CableAssembly_Rev1a_8220004_01012018.pd f).

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

• Manufacture 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)

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

• Assembly of components

• 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 100021888 CAVU2100 PSU.pdf and Attachment 27 PHS&T for MDR Power Supply 100021888.pdf)

• Delivery of kits to the FAA Logistics Center

2.2 Objectives

The objective of this acquisition is:

a. Provide AML-8000 with 1200 MDR PS kits per year to facilitate the repair of the MDR

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 8199217_A.pdf

h. Attachment 8 CAVU2100_PWRSUPPLY_Rev2_20190425.pdf

i. Attachment 9 20190708_CAVU2100PWRSUP_BOM_Rev2_Baseline.pdf

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 Insulator Notes.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 100021888 CAVU2100 PSU.pdf

aa. Attachment 27 PHS&T for MDR Power Supply 10 yr 100021888.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

Contractor must manufacture the parts listed in Appendix B. Contractor must use the components as listed in the BoM and inform OKCET and AML-8000 of any issues with parts availability or planned substitutions. All substitutions must be approved by AJW-1731 OKCET.

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 10 first articles for FAA’s testing unless a first article inspection has previously been performed on the manufacturer’s product (i.e. Maverick Technologies, Inc.). This is in addition to the production quantity. FAA must receive first articles within 60 calendar days after date of contract award. FAA has 30 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, AML-8050 Technical Support Facility - Building 215 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 and for production to 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

4.3 Deliver Parts

4.3.1 Preservation, Packaging, Packing and Marking

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

Cushioning Thickness: 2 inch Minimum on All Surfaces

Unit Container: PPP-B-1672E, Type II, Style D Folding Convoluted Cushioning in Re-Usable Box (Slide Pack), NSN 8115-01-019-4084

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

(1) LCSS Part Number

(2) Cage Code and Manufacturer’s Part Number

(3) Part Description

(4) Quantity and Unit of Issue

(5) PO# and Contract #

(6) ESD Label and precautionary markings

Contractor must meet the following barcoding requirements.

None

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

4.3.4 Delivery Destination

Contractor must ship all parts 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 products will be within 30 days of First Article Acceptance. Subsequent orders shall be delivered within 30 days of issuance of delivery order.

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.

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 provide parts 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 Paul Hornbeck, AML-8050 and Bill Fields AJW-173 to confirm product compatibility requirements.

4.4.4 Other Documentation

Contractor must provide other documentation for SOW tasks. Contractor must ensure billing documents (i.e. invoices) must reach the designated FAA accounting department within 30 days of product delivery

4.5 Provide 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 …

An auditable Quality Management System containing all Elements of the ANSI/ASQC/ISO 9000 Standard exist. Applicable IPC workmanship standards shall 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 shall be supplied where applicable.

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

Contractor must perform work at the locations necessary to complete SOW tasks. FAA expects the primarily work location will be at the Contractor’s facility. FAA will not fund Contractor travel, unless authorized in advance by the CO or COR under special circumstances.

5.2 Period of Performance

The contract period of performance is a 1-year base period and 4 1-year option periods.

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 as per Appendix C.

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 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

4.4.4 Other Documentation None (To Be Specified by

FAALC Engineer)

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

AML Federal Aviation Administration Logistics Center 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 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

100021888 CAVU 2100 Power Supply Assembly (Consists of one 100020551 CAVU 2100 Power Supply Rev 1 assembly, one 100020552 CAVU 2100 Cable Assembly and one 100020553 CAVU 2100 Panel Label)

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

Appendix C - Part Specifications

Bill of Material found in:

Attachment 7 Heat Sink 8199217_A.PDF Attachment 9 20190708_CAVU-2100PWRSUP_BOM_Rev2_20190425.pdf Attachment 18 OKCET_CAVU_2100_AC_Monitor_CableAssembly_Rev1a_8220004_01092018.pdf