Section J_Attach 1_SOW_Final RFP 5 Feb 21.pdf

FA8626-21-R-0002

Section J, Attachment 1

Statement of Work

For

Lots 2+

F-15EX Propulsion System

1 February 2021

Table of Contents

1 OVERVIEW

1.1 SCOPE

2 APPLICABLE DOCUMENTS & DEFINITIONS

2.1 DEFINITIONS

3 REQUIREMENTS

3.1 PROPULSION SYSTEM

3.1.1 Engineering

3.1.2 Engine Configuration Management

3.1.3 Logistics

3.1.4 Systems Engineering Management

3.1.5 Manufacturing Management Program

3.1.6 Quality

3.1.7 Data

3.1.8 Contractor Furnished Fuel

3.2 PROGRAM MANAGEMENT

3.2.1 Work Scope

3.2.2 Program Meetings, Reviews, and Events

3.2.3 Contract Work Breakdown Structure (CWBS)

3.2.4 Cost and Software Data Reporting (CSDR)

3.2.5 Integrated Master Plan (IMP) / Integrated Master Schedule (IMS)

3.2.6 Reserved

3.2.7 Reserved

3.2.8 Reserved

3.2.9 Risk Management

3.2.10 Contractor Facilities

3.2.11 Government Furnished Property (GFP)/Government Furnished Equipment (GFE)

3.2.12 Information Security

3.2.13 Environmental, Safety, and Occupational Health (ESOH) Program

3.3 (OPTION) F-15EX PROPULSION SYSTEM INTEGRATION INTO THE F-15EX SYSTEM

3.3.1 F-15EX Aircraft Flight Control Computer

3.3.2 Air Vehicle

3.3.3 Systems Engineering

3.3.4 F-15EX Aircraft Configuration Management

3.3.5 System Requirements

3.3.6 Air Vehicle Certifications/Accreditation/Approval Processes

3.3.7 System-Level Electromagnetic Environmental Effects (E3) Integration Program

3.3.8 Air Vehicle Noise and Vibration Impact Analysis

3.3.9 Mission Planning/Mission Support

3.3.10 System Security Engineering

3.3.11 System Safety Program

3.3.12 Air Vehicle Reliability and Maintainability Program

3.3.13 Product Support

3.3.14 Test and Evaluation

3.3.15 Production and Manufacturing

3.3.16 Program Security

APPENDIX A | REFERENCES

APPENDIX B | MEETINGS

APPENDIX C | CERTIFICATIONS

APPENDIX D | ACRONYMS

1 OVERVIEW

1.1 SCOPE

This Statement of Work (SOW) includes integration, test, certification, verification, manufacturing, and delivery of an F-15EX Propulsion System, as documented in Section C, as well as spare engines, training materials, technical data, and technical support. The scope also includes necessary efforts to integrate the F-15EX Propulsion System into the F-15EX System as detailed in paragraph 3.3. The only modifications anticipated are those required to integrate the

F-15EX Propulsion System into the F-15EX System.

Systems engineering, program management, configuration management, data management, and other support tasks are identified where applicable.

2 APPLICABLE DOCUMENTS & DEFINITIONS

The documents listed in Appendix A form a part of this SOW to the extent specified herein. The revision letters, notices, and document dates identified in the Appendix A are the applicable versions of these documents referenced in subsequent SOW paragraphs. Any documents referenced within these applicable documents are equally applicable to this SOW. The

Contractor shall bring any such discovered conflicts to the attention of the Government

Contracting Officer.

2.1 DEFINITIONS

F-15EX Aircraft. The F-15EX physical air vehicle, which meets the requirements of the F-15EX

System Requirement Document (SRD).

F-15EX Baseline. The F-15EX Lot 1 System, which meets the requirements of the F-15EX SRD.

F-15EX Propulsion System. Two 29,000 pound thrust class engines, engine Computer

Software, and any required on aircraft components, including Computer Software, previously integrated on the F-15E, F-15SA, F-15QA, or F-15EX aircraft, which meets the requirements of the Contract Section C engine specification.

F-15EX System. The F-15EX System consists of the F-15EX Aircraft, support equipment, alternate mission equipment, and technical data.

Integrate. All activities that encompass the work necessary to incorporate the F-15EX

Propulsion System into the F-15EX System, including design, development, modification, documentation, testing, and airworthiness certification that complies with paragraph 3.3.

Lot 1A Aircraft. F-15EX Production Lot consisting of contract-compliant F-15EX Baseline

Aircraft under Indefinite Delivery/Indefinite Quantity (ID/IQ) contract FA8634-20-D-2704, Delivery Order FA8634-20-F-0022.

Modified for the F-15EX. Item was present on prior F-15 variants (United States Air Force

(USAF) or Foreign Military Sales (FMS)) but has been modified for the F-15EX System.

Newly Developed. Item developed for use on the F-15EX only.

Unique to the F-15EX. Item is only incorporated in the F-15EX System and is not present in the legacy USAF F-15 Fleet or the FMS fleet.

3 REQUIREMENTS

3.1 PROPULSION SYSTEM

The Contractor shall fabricate and/or procure parts, assemble, test, and deliver complete engines that meet the requirements of the Contract Section C Engine Specification. The Contractor shall deliver all production engines to the configuration approved by the Government at time of contract award.

CDRL A010, DI-MISC-80508B/T, Technical Report - Study/Services, Engine Specification

3.1.1 Engineering

3.1.1.1 Engine Cycle Model

The Contractor shall deliver an engine cycle model and user’s guide for the engine, including updated installation effects for the F-15EX application. The engine cycle model shall be delivered with both steady state and transient models.

CDRL A025, DI-MSSM-81966A/T, Gas Turbine Engine Steady State and Transient Performance Presentation for Computer Programs

3.1.1.2 Propulsion System Integrity Program (PSIP) Master Plan

The Contractor shall develop, implement, and deliver a tailored PSIP Master Plan, applying the guidance of Military-Standard (MIL-STD) 3024, Propulsion System Integrity Program

(PSIP), and tailoring appropriate to include relevant updates due to integration of the

F-15EX Propulsion System into the F-15EX Baseline. The Contractor shall provide support for Government to execute PSIP reviews in accordance with MIL-STD-3024 guidance.

CDRL A012, DI-MISC-80508B/T, Technical Report – Study/Services, PSIP Master Plan

3.1.1.3 Verification

The Contractor shall develop and deliver a Verification Matrix Report, documenting the verification of the requirements specified in the Contract Section C F-15EX Propulsion

System Specification and the Contract Section C Engine Specification. This report shall include substantiating data and reports on the analysis, test, or other activities that verify achievement of these requirements.

CDRL A032, DI-MISC-80508B/T, Technical Report – Study/Services, Verification Matrix Report

3.1.1.4 Airworthiness Certification

The Contractor shall provide support for the USG to obtain a Propulsion-Military Type

Certificate (P-MTC) of the F-15EX Propulsion System using the guidance in USAF

Airworthiness Bulletin (AWB) 330A, Propulsion System Type Certification.

3.1.1.4.1 Airworthiness Certification Plan

The Contractor shall develop, implement, deliver and maintain an Airworthiness

Certification Plan that documents its airworthiness program, processes and procedures, organization, interfaces, and Government certification tasks, products, and schedule. Within the Airworthiness Certification Plan, the Contractor shall include certification test planning and scheduling and test facility identification as required in pursuit of P-MTC. The

Contractor shall address airworthiness requirements in the Airworthiness Certification Plan as detailed in AWB-002A, Airworthiness Planning.

CDRL A034, DI-MGMT-80004A/T, Management Plan, Engine Airworthiness Certification Plan

3.1.1.4.2 Airworthiness Certification Criteria Report

The Contractor shall deliver an Airworthiness Certification Criteria Report that documents and demonstrates compliance of all certification criteria using the guidance in AWB-003A, Tailored Airworthiness Certification Criteria/Modification Airworthiness Certification

Criteria (TACC/MACC) Document Approval Process and AWB-005, Tailored Airworthiness

Certification Criteria/Modification Airworthiness Certification Criteria (TACC/MACC)

Document Construction and Format, and consistent with the approved Type Model Series

Certification Basis. The Contractor shall provide all compliance data to the Government for review. The Government is the final authority of the applicability and appropriateness of all

Contractor compliance data.

CDRL A035, DI-SESS-81768, Airworthiness Certification Criteria Report

3.1.1.5 Product Acceptance

3.1.1.5.1 Acceptance Test Plans (ATP)

The Contractor shall update, deliver, and maintain the F-15EX Propulsion System ATP. The test plan defines the acceptance test, performance objectives, criteria and detailed procedures for the acceptance of the engines supporting the F-15EX Aircraft and associated components and articles that will be accepted and delivered to the Government.

CDRL A009, DI-QCIC-80553A/T, Acceptance Test Plan

3.1.1.5.2 Acceptance Test Records

The Contractor shall provide all acceptance test records to Defense Contract Management

Agency prior to Department of Defense (DD) Form 250, Material Inspection and Receiving

Report, signature and engine acceptance.

3.1.1.6 Critical Safety Items (CSI)

The Contractor shall update, deliver, and maintain an F-15EX Propulsion System CSI list using the Joint Aeronautical Commanders’ Group (JACG) Aviation Critical Safety Item

Management Handbook as a guide. The Contractor shall comply with the Government’s heightened risk-based surveillance requirements and flow these requirements to subcontractors.

CDRL A008, DI-SAFT-80970A/T, Critical Safety Item (CSI) Characteristic and Critical Defect Report, Critical Safety Item List

3.1.2 Engine Configuration Management

The Contractor shall support configuration management at Propulsion Sustainment Division

(AFLCMC/LPS) using existing Government processes.

3.1.2.1 Contract Change Proposal (CCP)

The Contractor shall propose non-technical contract changes using existing Government

CCP processes.

CDRL A015, DI-ADMN-81401C/T, Contract Change Proposals (CCPs)

3.1.2.2 Specification Change Notice (SCN)

All specification changes generated under this contract shall be subject to Government approval and submitted as SCN.

CDRL A011, DI-SESS-80643E/T, Specification Change Notice (SCN)

3.1.2.3 Deviations and Waivers

The Contractor shall prepare requests for deviation and waivers using existing Government processes.

CDRL A003, DI-SESS-80640E/T, Request for Variance (RFV) CDRL A004, DI-SESS-81732/T, Request for Waiver (RFW)

3.1.3 Logistics

3.1.3.1 Comprehensive Engine Management System (CEMS)

The Contractor reporting responsibilities are described in Technical Order (TO) 00-25-254-1, Comprehensive Engine Management System (CEMS) Engine Configuration. The Contractor shall:

Accomplish CEMS reporting on engine status changes no later than close of business of the next business day following the date/time of the occurrence.

Obtain AF Portal and CEMS access. AF Portal access instructions can be found at https://www.my.af.mil/gcss-af/USAF/ep/home.do. The Contractor can obtain the necessary forms and instructions for obtaining CEMS access by sending an email request to the CEMS Program Management Office (PMO) Security Office at cems.pmo.security@us.af.mil.

Update all serially tracked assets whether repaired or new production into CEMS, once access is granted.

The prime Contractor is responsible for processing security investigation packages for subcontractor personnel.

3.1.3.2 Engine Item Unique Identification (IUID) Markings

The Contractor shall mark the engine data plate with IUID in accordance with

MIL-STD-130N, Identification Marking of U.S. Military Property, or equivalent standard. Any currently IUID marked engine components shall be maintained for this program. The Contractor shall upload the IUID assigned numbers and information into the https://www.my.af.mil/gcss-af/USAF/ep/home.do mailto:cems.pmo.security@us.af.mil

Government IUID Registry following the Using Service‘s guidance and procedures. The

IUID shall contain, at a minimum: applicable Enterprise Identifier (EID), Serial Number, and

Part or Identifying Number (PIN).

IUID markings shall be visible during normal handling, be readable, withstand the specified environment and cleaning processes, and be as permanent as the service life of the unit or at least to the unit’s point of rebuild.

3.1.3.3 Diminishing Manufacturing Sources & Material Shortages (DMSMS) Production

Planning

The Contractor shall develop and deliver a plan to address and manage all DMSMS for the life of the contract using existing Propulsion Directorate (AFLCMC/LP) DMSMS, Component Improvement Program and Engineering Change Proposal processes. The

Contractor shall include the impact of recurring and nonrecurring DMSMS costs and schedule in all production pricing options and schedule awarded via this contract.

CDRL A044, DI MGMT 81948, Diminishing Manufacturing Sources & Material Shortages (DMSMS) Management Plan

3.1.3.4 Packaging, Handling, Storage, and Transportation (PHS&T)

The Contractor shall be responsible for the preservation and packaging of all necessary components and engines for shipment IAW the Packaging Instructions specified on Air

Force Materiel Command (AFMC) Form 158, Packaging Requirements. The Contractor shall follow packaging, handling, storage, transportation practices in accordance with applicable TOs. The Contractor shall place a special tag, DD Form 1574, inside the package along with the assembly as well as outside the package. In addition, all marking and labeling of unit and shipping containers shall be in accordance with MIL-STD-129R, Military Marking for Shipment and Storage.

3.1.3.4.1 Shipping Install Engines

The Contractor shall prepare engines for shipment to the Aircraft manufacturer using the engine transportation unit or 3000 series trailer with suitable adapters as necessary.

3.1.3.4.2 Shipping Spare Engines

The Contractor shall prepare spare engines within reusable protection bags for shipping.

Spare engines will be shipped using the contractor provided 3000 series trailers with suitable transportation mounts.

3.1.3.5 Special Tooling/Special Test Equipment

The Contractor shall provide a list of all special tooling, special test equipment, and new support equipment unique to the F-15EX Propulsion System and required in the F-15EX

System.

CDRL A022, DI-SESS-80294B/T, Maintenance Test and Support Equipment Requirements List

3.1.4 Systems Engineering Management

The Contractor shall perform the systems engineering management efforts applicable to the production phase.

3.1.4.1 Reserved

3.1.4.2 Government Industry Data Exchange Program (GIDEP)

The Contractor shall participate in the GIDEP. The Contractor shall generate “alerts” when applicable, acquire “alerts” from GIDEP Operating Center (Naval Surface Warfare Center, Corona, CA 92878), and take corrective action when “alerts” impact the production program.

CDRL A005, DI-QCIC-80125B/T, Government Industry Data Exchange Program (GIDEP) Alert/State - Alert Report

CDRL A006, DI-QCIC-80126B/T, Government Industry Data Exchange Program (GIDEP) Alert Response

CDRL A007, DI-QCIC-80127A/T, Government Industry Data Exchange Program (GIDEP) Annual Progress Report

3.1.4.3 Cybersecurity

The Contractor shall support the Government in identifying and assessing cybersecurity vulnerabilities, threats, and associated risks, by providing technical support including, but not limited to, technical information and source code, to aid the Government’s efforts to obtain an Interim Authority to Test (IATT) and Authority to Operate (ATO).

3.1.5 Manufacturing Management Program

The Contractor shall maintain manufacturing management in accordance with Society of

Automotive Engineers (SAE) Aerospace Standard (AS) 6500, Manufacturing Management

Program, or equivalent internal procedures. Notification and explanation of any changes to these procedures shall be provided to the Administrative Contracting Officer and Procuring

Contracting Officer.

3.1.5.1 Bill of Material (BOM)

The Contractor shall maintain the BOM for the F-15EX Propulsion System.

3.1.6 Quality

3.1.6.1 Quality Management System (QMS)

The Contractor shall provide and maintain a quality system compliant with either the

International Organization for Standardization (ISO) 9001:2015(E), Quality Management

Systems - Requirements – Fifth Edition or the SAE AS9100D, Quality Management System

– Requirements for Aviation, Space and Defense Organizations.

3.1.6.2 QMS Reporting

The Contractor shall report and address quality issues to include narrative of issue, date and location of occurrence, root cause, corrective action, safety risk assessment, and estimated completion date of corrective action. The Contractor shall provide a Quality Assessment

Report consisting of a description and summary of actions taken by the Contractor’s (and suppliers', when applicable) quality system(s) to identify, categorize, report, and correct issues relating to production and repair quality.

CDRL A014, DI-QCIC-81187, Quality Assessment Report

3.1.6.3 Foreign Object Damage (FOD) Prevention Program

The Contractor shall maintain a FOD Prevention Program. The Contractor shall assure FOD

Prevention is accomplished and the work area maintained in a manner to prevent foreign objects from entering and remaining in the structure.

3.1.7 Data

3.1.7.1 Data Management

The Contractor shall submit all Contract Data Requirement List (CDRL) documentation through electronic media. The Contractor shall ensure adequate numbers of personnel possess and utilize the Government’s propulsion security data delivery tool (i.e., PCOL+) as authorized by the Government Contracting Officer to ensure task traceability and facilitate team awareness of activity. The Contractor shall ensure the requirements and restrictions of the SOW are flowed down to vendors and subcontractors.

3.1.7.1.1 Data Accession List

The Contractor shall maintain and deliver a list of all data to be generated during the performance of the contract.

CDRL A065, DI-MGMT-81453B/T, Data Accession List (DAL)

3.1.7.2 Technical Orders (TOs)

The Contractor shall deliver source data for incorporating F-15EX Propulsion System unique technical data contents into existing Government organizational, intermediate and depot level TOs to include the illustrated parts breakdown.

CDRL A050, DI-SESS-81359B/T, Parts List CDRL A016, TM-86-01Q/T, Technical Manual Contract Requirements, TMCR

3.1.7.3 (Option) Digital Enterprise

The Contractor shall deliver data and information that will enable and enhance the

Government’s continued organic sustainment activities for the F-15EX Propulsion System throughout the engine lifecycle, to include digital thread and digital twin technology areas.

The Contractor shall deliver previously-developed, existing models, drawings, and data, excluding Contractor proprietary data (e.g. special manufacturing processes, process controls) that will be utilized by the Government and the Contractor in fulfillment of the

Department of Defense (DoD) Digital Engineering Strategy goals.

3.1.7.3.1 Existing Engineering Drawings/Models

For items developed under previous Government-funded activities and not delivered to the

Government, the Contractor shall deliver any and all existing 3-D digital drawings (i.e. no conversion to digital format) and geometric, functional, and analytical models for the

F-15EX Propulsion System.

CDRL A021, DI-SESS-81000F/T, Product Engineering Design Data and Associated List – Existing Data Items

3.1.7.3.2 Reserved

3.1.7.3.3 Reserved

3.1.7.3.4 Digital Inspection Records

For engines procured under this contract, the Contractor shall deliver any and all digital inspection records (i.e. no conversion to digital format) for time tracked and/or fracture-critical and/or rotating components (e.g. eddy current, vibration survey, Material Review

Board).

CDRL A047, DI-NDTI-80809B/T, Test/Inspection Report, Digital Inspection Records

3.1.7.4 Software Requirements

The following sub-paragraphs apply to any newly developed or modified Computer

Software required for the F-15EX Propulsion System.

3.1.7.4.1 Software Development Requirements

The Contractor shall update and implement, as necessary, Computer Software in accordance with the Software Development Plan (SDP) to verify requirements set forth in the Contract

Section C Engine Specification and the Interface Control Document (ICD) are achieved. The

Government will assist in setting the content priority prior to each Computer Software release, as well as version control.

CDRL A045, DI-MISC-81454C/T, Automated Computer Program ID Number (ACPIN) Data & Control Record, Air Force Resource Inventory Data

CDRL A052, DI-IPSC-81427B/T, Software Development Plan (SDP) CDRL A054, DI-IPSC-81439A/T, Software Test Description (STD) CDRL A055, DI-IPSC-81438A/T, Software Test Plan (STP) CDRL A056, DI-IPSC-81440A/T, Software Test Report (STR) CDRL A063, DI-IPSC-81442A/T, Software Version Description (SVD) CDRL A064, DI-AVCS-80700A/T, Computer Software Product End Item

3.1.7.4.2 Software Development Plan (SDP)

The Contractor shall update and maintain an SDP that satisfies the Contract Section C

Engine Specification and is coordinated, as necessary with the Weapon System Contractor.

CDRL A052, DI-IPSC-81427B/T, Software Development Plan (SDP)

3.1.7.4.3 Software Requirement Specification (SRS)

The Contractor shall update a SRS for each Computer Software product. Each SRS shall include an Interface Requirement Specification or data required to facilitate interfaces with other systems and applications and identify the appropriate document(s) further defining those interfaces.

CDRL A049, DI-IPSC-81434A/T, Interface Requirements Specification (IRS) CDRL A053, DI-IPSC-81433A/T, Software Requirements Specification (SRS)

3.1.7.4.4 Software Design Description (SDD)

The Contractor shall update a SDD for each Computer Software application.

CDRL A051, DI-IPSC-81435A/T, Software Design Description (SDD)

3.1.7.4.5 Software Product Delivery

The Contractor shall deliver all Computer Software products to the Government on digital media. The Computer Software products shall be delivered to the Government Software

Control Center for storage and configuration control.

CDRL A049, DI-IPSC-81434A/T, Interface Requirements Specification (IRS) CDRL A053, DI-IPSC-81433A/T, Software Requirements Specification (SRS)

3.1.7.4.6 Data Definitions and Decoder

The Contractor shall deliver a specification that describes the recorded daily flight data (e.g.

data dictionary, file structure, and element names). The Contractor shall deliver a data decoder that parses raw recorded data into data engineering units that is suitable for applying analytics. The Contractor shall deliver a document that provides information to build a data decoder in lieu of a standalone application that is integrated into a larger Information

Technology (IT) system.

CDRL A046, DI-IPSC-81434A/T, Interface Requirements Specification, Data Definition Report CDRL A058, DI-IPSC-81442A/T, Software Requirement Specification (SRS), Data Decoder CDRL A060, DI-AVCS-80700A/T, Computer Software Product End Items, Data Decoder Software

3.1.7.4.7 Engine Trending & Diagnostics (ET&D) and Condition-Based Maintenance+ (CBM+)

The Contractor shall update and deliver data to support USAF ET&D and CBM+ activities for the F-15EX Propulsion System.

For any changes to the existing capability of the legacy USAF fleet for the F-15EX application, the Contractor shall deliver a description of on-aircraft faults and alerts, the algorithms describing how on-aircraft faults and alerts are set, a description of on-ground faults and alerts, and the algorithms for how on-ground faults and alerts are set.

CDRL A057, DI-IPSC-81442A/T Software Version Description (SVD), CBM+ Fault Algorithms CDRL A059, DI-AVCS-80700A/T, Computer Software Product End Item, CBM+ Fault Algorithms

Software CDRL A061, DI-MISC-80508B/T, Technical Report – Study/Services, Engine Trending & Diagnostics

3.1.7.4.8 Commercial Computer Software

Under this contract, the Government may become the Licensee in certain Commercial

Computer Software licenses, which software is specifically defined at DFARS 252.227-

7014(a)(1).

In Section J, Attachment 7, the Contractor shall provide a listing and copies of all commercial Computer Software licenses to be obtained on behalf of or provided to the US

Government under this contract.

In order to permit the Government to become a Licensee in the commercial Computer

Software licenses, the Contractor shall first review the Commercial Computer Software licenses intended for transfer to the Government and ensure compliance with the procurement law and the government’s requirements.

Licenses shall be approved by the Contracting Officer before Government acceptance and issuance of DD250. Computer Software incorporated into another deliverable must be approved before incorporation.

The terms and conditions required to permit any commercial Computer Software licenses to be transferred to the Government (e.g., Government to become a Licensee) include the following:

Any license shall be perpetual in nature and may not be unilaterally terminated by the Licensor. All remedies available shall be consistent with the Disputes Clause in the underlying contract

The Licensor shall not use the fact that the Licensee is using the Licensor's products in any notification to the public (e.g., no publicity rights permitted).

The Licensee is a Federal entity governed by Federal Statutes, Caselaw. and

Federal Regulations. Therefore, the Licensor shall remove any references to binding the Licensee through any laws of any municipality, state, or foreign country.

The Licensor shall not include any clauses indicating a right to enter the premises of Licensee for the purpose of auditing the use of any license, as the Licensee cannot allow an auditor access to the Licensee's facility or systems due to security concerns. The Licensor may submit to the Licensee written notice indicating a substantiated belief that the Licensee is not using the software within the terms described in the license and the Licensee may consider conducting its own internal audit and providing a statement of its findings to the Licensor.

The Licensor shall not use any integration clauses.

The Licensor shall not use any injunctive relief clauses.

The Contractor shall clearly correlate or map commercial software license(s)to:

o Contract Line Item Numbers;

o CDRLs;

o Paragraphs in the SOW; and/or o Portions of any functional block diagrams and/or system architecture diagrams, so that it can be readily determined where certain commercial

Computer Software corresponding to certain software license agreement(s) are physically located on the system to be delivered under the contract.

The Licensor shall not include any clause in the license agreement that in any way restricts assignment to the Government and/or restricts the Contractor from continuing as a licensee in said license agreement for the beneficial use of said license agreement for the Government

The license shall not subject the Government to payment of attorney fees in the event of a dispute.

The license shall not disclaim all warranties through use of an "as is" provision.

The license shall not restrict the Government from using the product at various sites

(i.e. applicable to a product-type license for a movable product, as opposed to a site-specific license for a non-movable product) nor restrict use of the product by various Government agencies or third parties performing work on behalf of the

Government personnel as well as Government contractors may use the software.

Additionally, the software may be used at Government sites and Government contractor sites and the sites may change over time.

The license shall not include non-substitution language that would preclude or limit the Government from switching to another vendor/reseller and/or another product to fulfill Government requirements.

The Licensor shall include the following clause (and no other) for disputes: "Since the Licensee is a Government entity, any dispute arising from or in connection with this agreement shall be subject to resolution in accordance with the Disputes Clause included ln the contract and/or the Government may decide to resolve any disputes using an appropriate Alternate Dispute Resolution remedy.”

3.1.7.5 Engineering Drawings/Models

The Contractor shall deliver any and all drawings and geometric, functional, and analytical models for the F-15EX Propulsion System developed under this contract.

CDRL A023, DI-SESS-81000F/T, Product Engineering Design Data and Associated Lists – Newly Developed Data Items

3.1.8 Contractor Furnished Fuel

The Contractor shall furnish petroleum and fuel necessary for use in the performance of this contract for engine assembly and acceptance testing. The Contractor shall comply with American

Society for Testing and Materials (ASTM) D1655-20d, Standard Specification for Aviation

Turbine Fuels, with the following additives: Inhibitor, Corrosion/Lubricity Improver

(MIL-PRF-25017), Inhibitor, Icing, Fuel System, High Flash NATO Code Number S-1745 (MIL-DTL-85470B), an approved antioxidant material listed in MIL-DTL-5624 or

MIL-DTL-83133, an approved static dissipater additive listed in MIL-DTL-5624 or

MIL-DTL-83133, a thermal stability improver additive as described in MIL-DTL-83133.

3.2 PROGRAM MANAGEMENT

3.2.1 Work Scope

The Contractor shall plan, schedule, execute, and manage the authorized contract work scope to ensure timely, on-cost delivery of required products to the quality and performance standards/specifications cited herein. The Contractor shall avoid duplication of tasks resulting from related contract overlaps. The Contractor shall provide the Government with insight into subcontractor management and performance.

3.2.2 Program Meetings, Reviews, and Events

The Contractor shall host and conduct a Post Contract Award Conference as specified in

Appendix B. The Contractor shall host and conduct quarterly Program Management Reviews

(PMR) as specified in Appendix B.

CDRL A001, DI-ADMN-81250B/T, Conference Minutes CDRL A002, DI-ADMN-81373, Presentation Materials

3.2.3 Contract Work Breakdown Structure (CWBS)

The Contractor shall develop, deliver, and maintain a CWBS and a CWBS Dictionary in accordance with MIL-STD-881E, Work Breakdown Structures for Defense Material Items, except where the Government has tailored via the Cost and Software Data Reporting (CSDR)

Plans and this SOW. The Contractor shall request and receive Government approval before making any changes to the CWBS and/or associated definitions impacting reporting level Work

Breakdown Structure elements.

CDRL A013, DI-MGMT-81334D/T, Contractor Work Breakdown Structure

3.2.4 Cost and Software Data Reporting (CSDR)

The Contractor shall systematically collect and electronically report to the Cost Assessment Data

Enterprise the actual contract costs and technical information based on the Office of the

Secretary of Defense (OSD) Deputy Director Cost Assessment (DDCA) approved CSDR Plans in accordance with the Department of Defense Manual (DoDM) 5000.04, Cost and Software

Data Reporting (CSDR) Manual.

The Contractor shall conduct a post-award review of CSDR requirements as specified in

Appendix B. The Contractor shall present its approach to satisfy the CSDR guidelines contained in DoDM 5000.04, Cost and Software Data Reporting (CSDR) Manual, and the requirements in the OSD DDCA-approved CSDR Plan for the contract, DD Form 2794, Cost and Software Data

Reporting Plan, and the related Resource Distribution Table.

CDRL A038, DI-FNCL-81765B/T, Contractor Business Data Report (DD Form 1921-3), Contractor Cost Data Reporting (CCDR)

CDRL A039, DI-FNCL-82162, Cost and Hour Report (Flex File), Contractor Cost Data Reporting (CCDR) CDRL A040, DI-MGMT-82165, Technical Data Report CDRL A041, DI-MGMT-82164, Quantity Data Report, Contractor Cost Data Reporting (CCDR)

3.2.5 Integrated Master Plan (IMP) / Integrated Master Schedule (IMS)

The Contractor shall develop, deliver, implement, and maintain an IMP that includes a list of program events as well as entry and exit criteria for each event.

The Contractor shall develop, deliver, implement, and maintain an IMS that identifies the contracted F-15EX Propulsion System scope and external critical dependencies, such as integration and test schedules. The Contractor shall map the IMS to the IMP and CWBS.

CDRL A033, DI-MGMT-81861B/T, Integrated Program Management Data & Analysis Report (IPMDAR) CDRL A036, DI-MGMT-81797/T, Program Management Plan, Integrated Master Plan

3.2.6 Reserved

3.2.7 Reserved

3.2.8 Reserved

3.2.9 Risk Management

The Contractor shall develop, deliver, implement, and maintain an F-15EX Propulsion System

Risk Management Plan using Air Force Instruction (AFI) 63-101/20-101, Integrated Life Cycle

Management, AFPAM 63-128, Integrated Life Cycle Management, and the AFLCMC Standard

Process to Execute Risk and Issue Management in Acquisition Programs as guides. The

Contractor shall present risk status at PMRs as specified in Appendix B.

CDRL A042, DI-MGMT-81808, Contractor’s Risk Management Plan

3.2.10 Contractor Facilities

The Contractor shall provide Government access to facilities and office/administrative resources, including phone and internet access. The Contractor shall provide unescorted badge access to facilities, when possible.

3.2.11 Government Furnished Property (GFP)/Government Furnished Equipment (GFE)

The Contractor shall manage and maintain all GFP and GFE.

3.2.12 Information Security

The Contractor shall comply with the security requirements identified in the following:

DoDM 5200.01, Volume 4, DoD Information Security Program: Controlled

Unclassified Information (CUI)

Defense Counterintelligence and Security Agency (DCSA) Assessment and

Authorization Process Manual DAAPM v2.2

DoD 5220.22-M, National Industrial Security Program Operating Manual

(NISPOM)

The Contractor shall notify the Government Contracting Activity (GCA), including Government

Contracting Officer and Security Manager, within 48 hours after the discovery of a Security

Incident involving the loss, compromise, or suspected compromise of classified information.

The Contractor shall incorporate this reporting requirement into all subcontracts; the subcontractor shall report the security incident to the Contractor within 24 hours; the Contractor shall notify the GCA within 24 hours after notification from the subcontractor.

3.2.12.1 Protections of Controlled Unclassified Information (CUI)

The Contractor shall comply with DoDM 5200.01, Volume 4, DoD Information Security

Program: Controlled Unclassified Information (CUI), Enclosures 3 and 4, for identification, protection, and training requirements of CUI. The Contractor shall protect unclassified DoD information not approved for public release on non-DoD Information Systems in accordance with Department of Defense Instruction (DoDI) 8582.01, Security of Non-DoD Information

Systems Processing Unclassified Nonpublic DoD Information, Enclosure 3, and the F-15

Eagle/Strike Eagle Security Classification Guide.

3.2.12.2 Identification of Covered Defense Information (CDI)

The Contractor shall identify and affirm marking requirements with the Government for

CDI, as prescribed by DoDI 5230.24, Distribution Statements on Technical Documents. The

Contractor shall implement and flow these CDI marking requirements to its subcontractors.

3.2.12.3 CDI/CUI System Security Plan

The Contractor shall develop, and make available to the Government for review at the

Contractor’s facility, a DFARS 252.204-7012-compliant CDI/CUI System Security Plan

(SSP) and enterprise-level plans of action in accordance with National Institute of Standards and Technology (NIST) Special Publication (SP) 800-171 Rev. 2, Protecting Controlled

Unclassified Information in Nonfederal Systems and Organizations. In the CUI/CDI SSP, the Contractor shall describe the Contractor’s unclassified information system(s)/network(s) where CDI associated with the execution and performance of this contract is processed, stored, and/or transmitted.

3.2.13 Environmental, Safety, and Occupational Health (ESOH) Program

The Contractor shall maintain an ESOH program to integrate ESOH efforts into the systems engineering and program management processes. This process will help support the ESOH program at a system level. The ESOH program references MIL-STD-882E, System Safety, as a guide. The Contractor shall conduct a System Safety Program in accordance with applicable paragraphs of MIL-STD-882E, System Safety, (excluding paragraph 4.4 and sub-paragraphs).

3.3 (OPTION) F-15EX PROPULSION SYSTEM INTEGRATION INTO THE F-15EX

SYSTEM

In order to meet fielding date of the F-15EX Lot 2, the Contractor shall complete aircraft integration efforts no later than 31 March 2023 to allow the Government time required to finalize airworthiness certifications.

The Contractor shall fabricate and/or procure parts, assemble, test, and deliver complete F-15EX

Propulsion Systems and modify one F-15EX Baseline Aircraft.

3.3.1 F-15EX Aircraft Flight Control Computer

The Contractor shall integrate, verify, and test the F-15EX Propulsion System with the F-15EX

Baseline, to include, but not limited to fly-by-wire flight control laws, to support the Government certifications.

The Contractor shall recommend Problem Report (PR)/Deficiency Report (DR) dispositions for

Government approval. As a minimum, the Contractor shall resolve Priority 1 and 2 PRs/DRs associated with systems and capabilities unique to the F-15EX Propulsion System integration.

The Contractor shall evaluate and recommend a set of hardware and software metrics.

CDRL B005, DI-IPSC-81442A/T, Software Version Description (SVD) CDRL B011, DI-AVCS-80700A/T Computer Software Product End Items CDRL B069, DI-MGMT-80368A/T, Status Report, Hardware and Software Metrics

CDRL B075, DI-MISC-80508B/T, Technical Report – Study/Services, Flight Control Modification Description and Analysis Report

CDRL B076, DI-MISC-80508B/T, Technical Report – Study/Services, Auto Pilot Control Authority Assessment Report

CDRL B077, DI-MISC-80508B/T, Technical Report – Study/Services, Substantiation Data Report for Flying/Handling Qualities

CDRL B078, DI-NDTI-80603A/T, Test Procedure, F-15EX ADCP II Manned Flight Hardware Simulation (MFHS) Regression Test Procedures

CDRL B079, DI-NDTI-80809B/T, Test/Inspection Report, F-15EX ADCP II MFHS Regression Test Report CDRL B080, DI-MISC-80508B/T, Technical Report – Study/Services, Flight Control System, Control Power

Assessment Analysis Report

3.3.2 Air Vehicle

3.3.2.1 Strength

The Contractor shall conduct analyses to ensure any structural changes to the F-15EX

Baseline do not adversely affect the structural integrity of the F-15EX Aircraft. The

Contractor shall design any new equipment installations to meet F-15EX Aircraft structural integrity and proper operation for the required service life. The Contractor shall develop and deliver Structural Analysis Summary Reports for any structures that are unique to or modified due to the F-15EX Propulsion System. The Contractor shall update and deliver a

Strength Summary and Operating Restrictions Report.

CDRL B031, DI-SESS-82123/T, Strength Summary and Operating Restrictions (SSOR) Report CDRL B053, DI-SESS-80198B/T, Internal Loads and Static Strength Analysis Report

3.3.2.2 Structural Dynamics and Loads

For any primary structural modifications from the F-15EX Baseline that impact loads, the

Contractor shall perform and deliver a loads analysis report, or deliver a report documenting why loads analysis is not required.

CDRL B029, DI-MISC-81390A/T, Flutter Analysis Report CDRL B056, DI-SESS-82271, Aircraft External Loads Analysis Report

3.3.2.3 Mass Properties

The Contractor shall weigh the test F-15EX Aircraft modified to support the F-15EX

Propulsion System integration. The Contractor shall update and deliver actual weight reports for the weighed aircraft. The Contractor shall update and deliver a Weight and Balance

Handbook, including Automated Weight and Balance System files, for the modified F-15EX

Aircraft.

CDRL B032, DI-MGMT-81501A/T, Weight and Balance Report for Aircraft CDRL B052, DI-MISC-80508B/T, Technical Report-Study/Services, Weight and Balance Handbook

3.3.2.4 Fatigue and Fracture

The Contractor shall perform a Durability and Damage Tolerance Analysis (DADTA) and if necessary, update the F-15EX DADTA Report and F-15EX Force Structural Maintenance

Plan. In the DADTA, the Contractor shall include damage tolerance analysis of safety of flight parts that are unique to or modified from the F-15EX Baseline. The Contractor shall document the resultant structural inspection requirements in Publication Change Requests to be used for Technical Publication updates.

CDRL B054, DI-SESS-81983/T, Durability and Damage Tolerance (DADT) Analysis Report CDRL B055, DI-SESS-82039/T, Force Structural Maintenance Plan (FSMP)

3.3.2.5 Size, Weight, and Power-Cooling

The Contractor shall conduct an analysis and update the F-15EX Baseline report on the instrumented aircraft and the non-instrumented aircraft configurations to determine:

The aircraft-level cooling capacity and margin

The aircraft-level electrical power/loads and margin

Primary locations available for future Line Replaceable Unit (LRU) installations

CDRL B034, DI-MISC-80508B/T, Technical Report-Study/Services, Size, Weight, and Power-Cooling

3.3.3 Systems Engineering

3.3.3.1 Technical Reviews

3.3.3.1.1 Integrated Design Review (IDR)

The Contractor shall host and conduct an IDR, as specified in Appendix B, which covers the content normally included in the System Requirement Review, Preliminary Design Review, and Critical Design Review to establish the functional, allocated, and product baselines for

F-15EX Propulsion System Integration to document changes since the F-15EX Baseline

Delta-IDR. The Contractor shall meet the entry and exit criteria defined in the IMP.

3.3.3.1.2 System Verification Review (SVR)

The Contractor shall conduct an SVR for the F-15EX Propulsion System Integration as specified in Appendix B to verify the performance and maturity against the F-15EX Baseline configuration.

The Contractor shall meet the entry and exit criteria for each SVR event as defined in the IMP.

3.3.3.1.3 Technical Interchange Meetings (TIMs)

The Contractor shall support, host, and/or conduct TIMs to resolve engineering issues as specified in Appendix B.

3.3.4 F-15EX Aircraft Configuration Management

3.3.4.1 Configuration Baseline Management

The Contractor shall update the F-15EX Baseline functional, allocated, and product baselines in accordance with the F-15EX Addendum to the Eagle TALON Configuration

Management Plan (CMP). The product baseline will be verified during SVR.

The Contractor shall host and participate in Functional Configuration Audits and Physical

Configuration Audits, as specified in Appendix B, for Configuration Items (CI) and

Computer Software Configuration Items (CSCI) that are unique to or modified from the

F-15EX Baseline, as documented in the F-15EX Audit Plan. The Contractor shall make data, including subcontractor data, available for review during audits to verify compliance with the functional and physical configuration baselines.

3.3.4.2 Configuration Status Accounting (CSA)

The Contractor shall update and deliver CSA information capturing the F-15EX System change history for the as-designed, as-built, and as-delivered hardware CI. The Contractor shall also update and deliver CSA information capturing the F-15EX System change history for the as-delivered, as-modified, and as-tested CSCIs.

CDRL B073, DI-SESS-81253D/T, Configuration Status Accounting (CSA) Information, CSA Information

3.3.4.3 Nomenclature and Computer Program Identification Numbers (CPIN)

The Contractor shall develop, document, and process requests for nomenclature in accordance with MIL-STD-196G, Joint Electronics Type Designation Automated System, for all CIs developed specifically for the integration of the F-15EX Propulsion System.

The Contractor shall develop and deliver a recommended listing of system hardware CI, CSCIs, and interfaces for Government review and approval. For production software intended to be fielded, the Contractor shall submit CPIN requests within the Enhanced Technical

Information Management System (ETIMS), for Government review and approval. The

Contractor shall independently label and thoroughly describe CPIN requests in ETIMS in accordance with TO 00-5-16, Computer Program Identification Number (CPIN) Management, guidelines. The Contractor shall ensure a USAF CPIN is assigned for each CSCI.

CDRL B008, DI-MISC-81454D/T, Computer Program Identification Number (CPIN) Catalog Information CDRL B009, DI-SESS-81254C/T, Request for Nomenclature (DD Form 61) CDRL B030, DI-SESS-82007A/T, Configuration Item (CI) Documentation Recommendation

3.3.4.4 F-15EX Aircraft Item Unique Identification (IUID)

In accordance with MIL-STD-130N, Identification Marking of U.S. Military Property, the

Contractor shall follow standard IUID processes for all new items developed for the integration of the F-15EX Propulsion System. For items developed under legacy F-15 USAF or FMS Programs, the Contractor shall maintain the same IUID marking requirements as specified in the applicable DoD contracts.

The Contractor shall enter the data for IUID-marked items into the Procurement Integrated

Enterprise Environment and submit the IUID information before completion of the associated electronic DD Form 250, Material Inspection and Receiving Report. The

Contractor shall update and deliver an IUID Marking Activity Validation and Verification

Report.

CDRL B023, DI-MGMT-81804A/T, Item Unique Identification (IUID) Marking Activity, Validation and Verification Report

3.3.5 System Requirements

3.3.5.1 Systems Engineering Management Plan (SEMP)

The Contractor shall update and deliver an F-15EX addendum to the Government-approved

F-15 Eagle TALON SEMP (Boeing STL2002F0032) to guide technical management of the

F-15EX Program.

CDRL B010, DI-SESS-81785A/T, System Engineering Management Plan (SEMP)

3.3.5.2 Requirements Management

The Contractor shall manage F-15EX Propulsion System requirements supporting the

F-15EX System requirements using the Requirements Management Process in the F-15

Eagle TALON SEMP (Boeing STL2002F0032), as a guide.

3.3.5.3 Specification

In accordance with the F-15EX Addendum to the Eagle TALON CMP, the Contractor shall update and deliver the F-15EX System Specification to define the functional baseline (Tier 1 and 2), which is approved by the Government, that captures the full content of the F-15EX

SRD requirements and verifications. In accordance with the F-15EX Addendum to the Eagle

TALON CMP, the Contractor shall update and deliver the F-15EX subsystem specifications to define the allocated (Tier 3 and 4) and product baselines. In accordance with the F-15EX

Addendum to the Eagle TALON CMP, the Contractor shall update and deliver a

Specification Requirement Verification Matrix.

CDRL B071, DI-IPSC-81431A/T, System/Subsystem Specification (SSS) CDRL B072, DI-MISC-81283/T, Specification Requirement Verification Matrix

3.3.5.4 Interface Control Documents (ICD)

In accordance with the F-15EX Addendum to the Eagle TALON CMP, the Contractor shall update and deliver the F-15EX interface system, subsystem, and CI/CSCI ICD as impacted by this effort.

CDRL B001, DI-SESS-81248B/T, Interface Control Document (ICD)

3.3.5.5 Specification Tree

In accordance with the F-15EX Addendum to the Eagle TALON CMP, the Contractor shall update, and deliver an F-15EX Specification Tree showing the relationship and hierarchy of the complete F-15EX System (Tier 1-4) to include hardware/software, system/subsystem, ICDs, and CI/CSCI as impacted by this effort.

CDRL B033, DISESS82177/T, Specification Tree

3.3.5.6 Specification Verification

The Contractor shall verify the F-15EX System Specification (Tier 1-4). In accordance with the F-15EX Addendum to the Eagle TALON CMP, the Contractor shall update and deliver verification reports for all activity contained in the F-15EX System Specification

Requirements Verification Matrix.

CDRL B048, DI-NDTI-80809B/T, Test/Inspection Report, Specification Requirements Verification Matrix Verification Report

3.3.6 Air Vehicle Certifications/Accreditation/Approval Processes

Appendix C includes a comprehensive list of certifications, accreditations, approvals, waivers, and endorsements required throughout this SOW.

3.3.6.1 Airworthiness Program

The Contractor shall update, and deliver the F-15EX Airworthiness Plan, which successfully achieves airworthiness certification for the F-15EX with no serious or high airworthiness risks. The Contractor shall use Air Force Life Cycle Management Center (AFLCMC)

OI 62-601, Airworthiness Circulars, and Military-Handbook (MIL-HDBK)-516C, Airworthiness Certification Criteria, as guides.

The Contractor shall update and deliver a TACC document and an Airworthiness

Specification. The TACC document defines the F-15EX Program Airworthiness

Certification Basis and, when populated with compliance artifacts (Compliance Report), documents compliance to the defined certification basis using MIL-HDBK-516C, Airworthiness Certification Criteria, and the Airworthiness Certification Tool. The

Contractor shall update and deliver a comprehensive list of all airworthiness verification artifacts per each compliance report criteria that apply to the F-15EX Aircraft configuration, as modified from the F-15EX Military Flight Release baseline. The Contractor shall develop and deliver airworthiness verification artifacts new to or modified for the F-15EX Aircraft, and provide legacy verification artifacts upon request. The Contractor shall ensure the

Government can obtain a Military Type Certificate for the F-15EX Aircraft.

CDRL B016, DI-SESS-81768, Airworthiness Certification Criteria Report, TACC Compliance Report

(CR)

CDRL B051, DI-MGMT-80004A/T, Management Plan, Contractor Airworthiness Plan

3.3.7 System-Level Electromagnetic Environmental Effects (E3) Integration Program

The Contractor shall update and deliver the F-15EX System E3 Integration and Analysis Report

(E3IAR). The Contractor shall support E3 Working Group Meetings and teleconferences, as specified in Appendix B.

CDRL B021, DI-EMCS-81540B/T, Electromagnetic Environmental Effects (E3) Integration and Analysis Report (E3IAR)

3.3.7.1 Equipment-Level E3

The Contractor shall conduct Electromagnetic Interference (EMI) tests for any equipment or subsystems that are new…