FA855226RB001 RFP Attachment 16 PWS (CUI).pdf

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Performance Work Statement for the

HH-60W Combat Rescue Helicopter “Jolly Green II”

Degraded Visual Environment System (DVES)

Solicitation: FA8552-26-R-B001

18 June 2026

DISTRIBUTION STATEMENT C: Distribution authorized to U.S. Government Agencies and their Contractors (Critical Technology, Procurement, OPSEC; 1 Oct 2025). Other requests for this document shall be referred to AFLCMC/WIH, Robins AFB, GA 31098.

DESTRUCTION NOTICE: Destroy by any method that will prevent disclosure of contents or reconstruction of the document.

Controlled by: AFLCMC/WIH CUI Categories: CTI, PROCURE, OPSEC

LDC: FEDCON

Distribution Statement C POC: David Jones, david.jones.189@us.af.mil, DSN 497-4312 mailto:david.jones.189@us.af.mil

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Table of Contents

1.0 Description Of Services

1.1 Objective

1.2 Benefit to the USAF

1.3 Background

1.3.1 HH-60W Jolly Green II

1.3.2 HH-60W Program Status

1.3.3 HH-60W DVES Program

1.4 Definitions and Order of Precedence

2.0 Services Summary

2.1 Contract Performance Objectives

2.2 PWS Scope

2.3 Major Tasks and Program Objectives

2.4 DVES Integrated Product Team (IPT)

3.0 Government Property

3.1 Contractor Responsibility

3.1.1 Responsibilities

3.1.2 Contractor Acquired Property (CAP)

3.1.3 Shipping

3.2 Government Property to be Provided

3.2.1 Government Furnished Equipment/Property (GFE/GFP)

3.2.2 Government Furnished Information (GFI)

3.2.3 Reporting of Government Property

3.2.4 Loss of Government Property

3.3 Base Support

3.3.1 Holidays and Facility Closings

4.0 Technical Task Statements And Deliverables

4.1 Period and Place of Performance

4.1.1 Period of Performance (PoP)

4.1.2 Place of Performance

4.2 Contract Data Requirements List(s) (CDRL)

4.2.1 Quality of CDRL Deliverable

4.2.2 Receipt of CDRL Deliverable

4.3 DVES Key Performance Parameters (KPP) and Key System Attributes (KSA)

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4.3.1 KPPs

4.3.2 KSAs

4.4 Systems Engineering

4.4.1 System Maturity Requirements

4.4.2 Configuration Management

4.4.3 Diminishing Manufacturing Sources and Material Shortages (DMSMS)

4.4.4 Maintenance Support

4.4.5 Support Equipment (SE)

4.5 Orientation and Familiarization

4.6 Software

4.6.1 Software Transition and Use

4.6.2 Software Development Plan (SDP)

4.6.3 Computer Programming Manual (CPM)

4.6.4 Software Requirements Specification (SRS)

4.6.5 Software Transition Plan (STrP)

4.6.6 Software Design Description (SDD)

4.6.7 Software Product Specification (SPS)

4.6.8 Software Version Description (SVD)

4.6.9 Firmware Support Manual (FSM)

4.6.10 Software Test Plan (STP)

4.6.11 Software Test Description (STD)

4.6.12 Software Test Report (STR)

4.6.13 Software User Manual (SUM)

4.6.14 Software Architecture Document (SAD)

4.6.15 Integrated Development Environment (IDE)

4.6.16 Computer Software End Products

4.6.17 Software Field Loading

4.7 Engineering Analysis

4.7.1 System Engineering Master Plan (SEMP)

4.7.2 Materials and Processes

4.7.3 Crash Load Factors

4.7.4 Factor of Safety

4.7.5 Strength and Deformation

4.7.6 Human Factors

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4.7.7 Weight and Balance

4.7.8 Electrical Power Distribution

4.7.9 Technical Report-Studies/Services

4.7.10 Airworthiness

4.7.11 System Architecture Analysis Report (AAR)

4.7.12 Safety

4.7.13 Aircraft Structural Integrity

4.7.14 Reliability and Maintainability (R&M)

4.7.15 Electromagnetic Interference/Compliance (EMI/EMC)

4.7.16 Failure Mode Analysis

4.7.17 System/Subsystem Specification (SSS)

4.7.18 System/Subsystem Design Description (SSDD)

4.7.19 Interface Design Description (IDD)

4.7.20 Interface Control Document (ICD)

4.7.21 Interface Requirements Specification (IRS)

4.7.22 Acceptance Test Plan (ATP)

4.7.23 Aerodynamics

4.7.24 Thermal and Infrared (IR) Signature

4.7.25 Functional Thread Analysis

4.7.26 Aircraft External Equipment and Outer Mold Line

4.8 System Testing and Evaluation

4.8.1 Test and Evaluation Master Plan (TEMP)

4.8.2 Site Survey

4.8.3 Government Test Support

4.8.4 Environmental Testing

4.8.5 Bench Testing

4.8.6 Aircraft Testing

4.9 Technical Documentation

4.9.1 Engineering Data

4.9.2 Technical Orders (TOs)

4.9.3 Provisioning

4.9.4 Program Protection Implementation Plan (PPIP)

4.10 Prototype and Verification Installations

4.10.1 Prototype Installation (PI)

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4.10.2 Prototype Installation Test

4.10.3 Verification Installation (VI)

4.10.4 Verification Installation Test

4.10.5 Certification/Verification

4.10.6 Design and Deficiencies

4.11 Program Management

4.11.1 Performance Management

4.11.2 Risk Management

4.11.3 Quality Assurance Management

4.11.4 Integrated Program Management Report (IPMR)

4.11.5 Monthly Status Report/Performance Reporting

4.11.6 Travel

4.11.7 Cost and Software Data Reporting (CSDR)

4.12 Program Meetings and Technical Reviews

4.12.1 Kickoff Meeting

4.12.2 Engineering Data Guidance Conference

4.12.3 Provisioning Guidance Conference

4.12.4 Technical Order Guidance Conference

4.12.5 System Requirements Review (SRR)

4.12.6 Preliminary Design Review (PDR)

4.12.7 Critical Design Review (CDR)

4.12.8 Test Readiness Review (TRR)

4.12.9 In Process Review (IPR) of Technical Data Package (TDP)

4.12.10 Program Management Reviews (PMR)

4.12.11 Test Plan Working Group (TPWG)

4.12.12 Technical Interchange Meeting (TIM)

4.12.13 Crew Station Working Group (CSWG)

4.13 Logistics

4.13.1 Item Unique Identification

4.13.2 Packaging

4.13.3 Storage

4.13.4 Shipping and Transportation

4.13.5 Counterfeit Electronic Parts

4.13.6 Supply Chain Risk Management (SCRM) Process

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4.13.7 Integrated Logistics Support Plan (ILSP)

4.13.8 Obsolescence

4.13.9 RDT&E Aircraft Kits

4.13.10 Laboratory and Simulator Kits

4.13.11 Production Kits

4.13.12 Combined System Warranty and Period Clause

4.14 Cybersecurity

4.14.1 Cybersecurity Requirements

4.14.2 Cybersecurity Controls

4.14.3 Cybersecurity Risk Management

4.14.4 Cybersecurity and Information Assurance (IA)

4.14.5 Cybersecurity in Technical Data

4.14.6 Cybersecurity Schedule

4.14.7 Cybersecurity Workforce

4.14.8 Cybersecurity Regulations

5.0 General Information

5.1 Continuation of Mission-Essential Services During a Crisis

5.2 Security Requirements

5.2.1 Safeguarding and Overall Security

5.2.2 Operations Security (OPSEC)

5.2.3 Controlled Unclassified Information (CUI)

5.2.4 Communications Security (COMSEC)

5.2.5 Export-Controlled Information

5.2.6 Example CUI and Export Markings

5.2.7 Security Clearance

5.2.8 Security Incident or Violation

5.2.9 Access to Government System(s)

5.2.10 Access to Government Facility or Military Installation

5.2.11 Identification (ID) Card/Badge

5.2.12 Common Access Card (CAC)

5.3 Environmental Management System (EMS)

5.4 Agency Affirmative Procurement Programs

5.5 Safety Requirements

5.5.1 Contractor Environmental, Safety, and Occupational Health Compliance

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5.5.2 Mishap Notification/Investigation

5.6 Service Contracting Reporting (SCR)

5.7 Invoicing/Payment and Receipt/Acceptance

5.8 Quality Control Plan/Quality Management System (QMS)

5.9 Trafficking in Persons

5.10 Conflicting Requirements

5.11 Administration

5.12 Inspection of Services Clause

5.13 Restrictions on the use of Proprietary Material

5.14 Prohibitions against Unauthorized Disclosures

5.15 Relationship of Contractor with Sub-Contractors/Vendors

6.0 Appendices

6.1 Appendix A: Statement of Objectives (SOO)

6.1.1 DVES Program Phases

6.1.2 DVES Program Schedule

6.1.3 Integration

6.1.4 Training and Training Devices

6.1.5 Production and Fielding

6.1.6 Sustainment and Maintenance

6.1.7 Retirement and Disposal

6.2 Appendix B: TRL/MRL and Definitions

6.2.1 TRL Criteria Definitions

6.2.2 MRL Levels and Definitions

6.3 Appendix C: References

6.4 Appendix D: Acronyms and Definitions

Table of Tables Table 1: DVES Contractor Performance Objectives Table 2: DVES IPT Table 3: HH-60W DVES CDRLs Table 4: DVES KPPs Table 5: DVES KSAs Table 6: Notional DVES Schedule and Kit Production

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1.0 Description Of Services

1.1 Objective

This Performance Work Statement (PWS) defines contractual work requirements to be performed by the contract awardee (hereinafter referred to as "the Contractor") in support of the HH-60W Degraded Visual Environment System (DVES) Program (hereinafter referred to as "the DVES Program", or "the Program"), which is managed by the U.S. Air Force (USAF) Life Cycle Management Center (AFLCMC) Intelligence, Surveillance, Reconnaissance & Special Operations Forces (ISR-SOF) Directorate, AFLCMC/WIH Helicopter Division (hereinafter referred to as "the Government") located at Wright Patterson Air Force Base (WPAFB) in Dayton, OH and Robins Air Force Base (RAFB) in Warner Robins, GA. The DVES Program specifically is managed by the Helicopter Sustainment Branch (AFLCMC/WIHBB) located at RAFB, which is organized within AFLCMC/WIH.

1.2 Benefit to the USAF

This acquisition will benefit the USAF by providing aircrews with enhanced situational awareness (SA) during all flight operations in all conditions, resulting in improved safety-of-flight which will significantly reduce the risk of aircraft losses, encompassing both equipment and personnel.

Furthermore, the DVES will provide the USAF with improved capabilities, ensuring maximum mission effectiveness during Combat Search and Rescue (CSAR) operations. The purpose of the DVES Program is to design, develop, integrate, test, produce, install, and deploy a system that mitigates risks associated with operation of the HH-60W in degraded visual environments (DVEs).

A DVE occurs when aircraft-induced or ambient environmental conditions result in a loss of visual flight references (VFR) among pilots and aircrew. Causes of and contributors to DVE conditions include aircraft-induced brownout and whiteout, as well as ambient environmental conditions such as smoke, rain, fog, smog, clouds, darkness, flat light, and blowing sand, dust, and snow. These conditions significantly impair visibility, increasing the risk of Controlled Flight Into Terrain (CFIT), collisions with obstacles, dynamic rollover, and hard landings (brownout/whiteout).

DVES will contribute to safer flight operations during critical phases of flight in both DVE and visual meteorological conditions (VMC) by providing real-time or near real-time obstacle and terrain imagery, intuitive visual displays and symbology, and clear visual and aural warnings, cautions, and advisories. DVES will detect landing zone hazards, such as poles, vehicles, fence posts, wires, ditches, berms, holes, and large rocks, and en route hazards such as terrain, antennas, wires, and poles. DVES will thereby provide enhanced SA to HH-60W pilots and aircrew, enabling them to accomplish their mission more safely and effectively.

1.3 Background

1.3.1 HH-60W Jolly Green II

The HH-60W is a dual-piloted, multi-engine, rotary wing aircraft based on the Army fielded UH- 60M platform. The primary mission capability of the helicopter is to conduct CSAR and Personnel Recovery (PR) worldwide, from isolated, hostile, or denied territory. Secondary missions include collateral missions inherent to the capabilities required to conduct PR, such as combatant insertion/extraction missions, non-conventional assisted recovery, civil Search and Rescue (SAR), noncombatant evacuation operations, emergency aero-medical evacuation, international disaster relief and humanitarian aid, homeland security, and National Aeronautics and Space Administration (NASA) mission support. The HH-60W is employable in all environmental regions

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of the globe, day or night, in adverse weather, and under a variety of threat conditions including the presence of chemical, biological, radiological, and nuclear (CBRN) hazards. The HH-60W is capable of rapid deployment from main operating bases (MOB), forward operating bases (FOB), and austere or unprepared sites. The aircraft can also deploy from near or aboard United States Navy (USN) surface ships, or to conduct PR from commercial vessels. The HH-60W also features an in-flight refueling capability to enable airborne alert and extended range missions.

While most of the airframe structural components and all the dynamic system structures, including the blades, rotors, and transmissions, remain unchanged from the UH-60M, the HH-60W does feature some modifications, some non-developmental items (NDI) incorporated from other programs, and some newly developed elements. Structural modifications provide support to the two expanded main fuel tanks, modified aerial refueling system, and modified countermeasure dispensing system. The cockpit and cabin are outfitted with a new armor system, armored seats, and a new cabin floor featuring seat pans, pallet interfaces, and litter interfaces.

The HH-60W instrument panel maintains the UH-60M configuration with cockpit multi-function display (MFD), magnetic compass, master warning panel, digital clock, Integrated Vehicle Health Management System (IVHMS) event switch, and Electronic Standby Instrument System (ESIS) display. The HH-60W has upgraded ethernet, circuit breaker panels, data concentrator units, air data system, and a modified IVHMS. The aircraft also features an embedded Cross Domain Solution (CDS), which is used to ensure separation of Red (classified) mission data from Black (unclassified) maintenance data. The CDS receives data from the IVHMS, Advanced Mission Computer (AMC), and Flight Management System (FMS).

The HH-60W features two AMCs that integrate the mission processing, data links, sensors, defensive avionics, and controls and displays subsystems. The AMCs manage aircraft subsystems by performing control and status operations, and they provide tactical video to the MFDs (2 per pilot station, 4 total) and cabin displays (1 per gunner station, 1 center, 3 total). The AMC is connected to avionics equipment via ethernet, a dual MIL-STD-1553 mission bus, ARINC 708, ARINC 429, and RS-422 along with SMPTE-292 video to displays.

The AMC provides the following capabilities: onboard mission planning including Automated Route Replanner (ARR), Electro-Optical/Infrared (EO/IR) display, weather radar display, data link track management, GEOSIT display, image display, checklist display, and equipment status display. The onboard mission planning capability with ARR service provides onboard mission management capabilities, including automated mission planning based on operator-provided constraints. The data on the Data Transfer Device (DTD) is used by the AMC for display of mission data on the MFDs. The data link track management capability provides device and link management for the Common Interactive Broadcast (CIB), Situational Awareness Data Link (SADL), and Link-16 data links. The digital map service customizes digital maps from the Mass Memory Unit (MMU) and Data Transfer System (DTS). The EO/IR display provides video from the EO/IR sensor, as well as full sensor control and tactical overlays. The weather radar display provides sensor data and control. The image display provides a means to view images that were transferred from offboard sources. The checklist display provides a means to view electronic aircraft procedures. The system status display provides rolled-up status information for all avionics subsystems.

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The following is a non-exhaustive list of mission equipment highlighting key subsystems of the HH-60W platform:

• Aircraft Survivability Equipment (ASE) o AN/ALE-47 Countermeasures Dispensing System (CMDS) o AN/AAR-57 Common Missile Warning System (CMWS) o AN/AVR-2B Laser Detecting Set (LDS) o AN/APR-52 Radar Warning Receiver (RWR)

• Communications o AN/ARC-210 Receiver/Transmitter (R/T) radio sets (5x) o AN/ARS-6(V) Personnel Locator System (PLS) o AN/DPX-7 Reduces Size Transponder (RST) Identification Friend or Foe (IFF) o Cabin Wireless Intercommunication System o ASQ-177D R/T-1995(C)/G Series R/T Enhanced Position Location Reporting

System (EPLRS) o Embedded National Tactical Receiver (ENTR) V4 / TacNet Tactical Radio (TTR)

• Data Links o Situational Awareness Data Link (SADL) using EPLRS o Common Interactive Broadcast (CIB) using ENTR V4 o Link-16 using TTR o Blue Force Tracker (BFT)

• Data Transfer System (DTS) o Data Transfer Unit (DTU) o 3x 256 Gigabyte (GB) Data Transfer Device (DTD) o Crash-Survivable Memory Unit (CSMU)/Flight Data Recorder (FDR) o Cryptographic Ignition Key (CIK)

• Interference Blanker Unit

• Navigation o Embedded Global Positioning System (GPS)/Inertial Navigation System (INS) (EGI) Including future upgrade/modification planned from the FOCUS program, regarding the Honeywell EAGLE-M EGI o AN/ARN-147(V) Very-High Frequency (VHF) Omnidirectional Range (VOR) /

Instrument Landing System (ILS) o AN/ARN-149 Low Frequency (LF) Automatic Direction Finder (ADF) o AN/ARN-153(V) Tactical Airborne Navigation (TACAN) System o APN-209 Radar Altimeter (RADALT)

• Sensors o MX-10 Turret

EO High Definition (HD) Dual-Camera, Daylight (Color) and Low Light (Monochrome) Sensor

Mid-Wave IR (MWIR) Sensor (Monochrome) Laser Range Finder (LRF) and Laser Illuminator o P-701A Weather Radar (tail numbers prior to 14522) o RDR-7000 Weather Radar (tail numbers 14522 and subsequent)

• Weapons o GAU-2 Minigun (7.62x51 NATO) and/or GAU-18/21 Machine Gun (.50 cal)

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1.3.2 HH-60W Program Status

The HH-60W Jolly Green II Program is an Acquisition Category (ACAT) 1C program managed by the AFLCMC/WIH Helicopter Program Office (HPO) (now Helicopter Division) headquartered at WPAFB. The original contract award for the development of the HH-60W and its associated training systems, support equipment, and technical data to Sikorsky Aircraft Corporation (SAC) on 26 Jun 2014. Initial Operational Capability (IOC) was declared on 4 Oct 2022, and the decision to proceed to Full Rate Production (FRP) was made on 27 Apr 2023. The HH-60W is currently in production with deliveries expected to continue alongside the early stages of the DVES program. Modification programs impacting both aircraft hardware and software are also expected to run concurrently with the DVES program. The DVES program will implement technical and schedule deconfliction strategies to minimize adverse impacts both to DVES and other modification programs.

At the outset of the HH-60W acquisition program, the HPO tasked SAC with management of the engineering baselines and technical data product (TDP) for the aircraft. The program is currently in the process of transitioning management of the aircraft baseline and technical data to AFLCMC/WIH. In parallel, software sustainment for the AMC and FMS is being transitioned to the 580th Software Engineering Squadron (SWES) under the overall direction of AFLCMC/WIH.

Since these transitions are still in progress, the Original Equipment Manufacturer (OEM) continues to support software sustainment, and many of the technical documents delivered by the OEM continue to form the basis of AFLCMC/WIH systems engineering processes. The AFLCMC/WIH is in the process of refining these processes and updating the program engineering documentation to reflect the transition of systems engineering and integration responsibilities fully from the OEM to the USAF. As a result, documentation on engineering processes delivered to prospective proposers at the time of the DVES solicitation may be superseded prior to contract award or early in the DVES program.

1.3.3 HH-60W DVES Program

As stated in the introduction, the purpose of the DVES Program is to design, develop, integrate, test, produce, install, and deploy a system that mitigates risks associated with operation of the HH- 60W in degraded visual environments (DVE). The Helicopter Sustainment Branch is pursuing a DVES materiel solution that satisfies the system requirements documented in the Systems Requirements Document (SRD) for the HH-60W Jolly Green II DVES. The combined PWS, SRD, and concept of operations (CONOPS) have been developed together to ensure that DVES Program requirements are clear to all Government stakeholders and the Contractor. The DVES modification was validated via USAF review/coordination as a Safety modification and is intended to be a permanent aircraft modification.

1.4 Definitions and Order of Precedence

In the event of a conflict between the PWS and the SRD, the requirements of the PWS shall take precedence. In the event of a conflict between the PWS and the DD1423 Contract Data Requirements List (CDRL), the DD1423 takes precedence.

Statements within this document containing the verb “shall” or “must” are explicit work requirements that are mandatory.

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Statements within this document containing the verb “will” are statements of fact. A “will” statement may declare the purpose of, or clarify expectations with respect to, a given task requirement.

Statements within this document containing the verb “should” articulate goals of the program that should be assessed by the Contractor; however, fulfilment of these goals is not formally required.

Statements within this document containing the verb “may” are intended to provide a possible course of action (COA) that the Contractor may consider in determining how to perform a given task.

The term "Logical Interface" refers to the set of non-physical interface characteristics (e.g., data content, format, timing, protocol, and behavior) for DVES to exchange specific information with another HH-60W subsystem, network, or LRU, independent of how the physical connectivity is implemented. A logical interface requirement does not imply:

• a specific physical connection between DVES and the other system or LRU, nor

• a direct logical coupling between their implementations

The task/requirement is satisfied if DVES can obtain or provide the required data in the specified format with the specified characteristics via any available physical path (e.g., shared data bus, intermediary LRU, or network).

The term "Physical Interface" refers to the set of hardware and low-level electrical/optical characteristics that enable the transfer of signals or data between DVES and another HH-60W subsystem, network, or LRU. A physical interface includes, as applicable:

• connectors and pin assignments

• wiring/cabling and topology

• electrical/optical characteristics (i.e., voltage levels, signal types, termination, impedance, power levels, etc.)

• physical layer protocols (e.g., line coding, bit rates, MIL-STD-1553/ARINC 429/Ethernet physical layer, etc.)

A physical interface task/requirement specifies how DVES is physically connected and how signals are physically conveyed, independent of the higher-level data content, format, or behavior carried over that connection.

The generic term "Interface" refers to the combination of a Logical Interface and Physical Interface.

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2.0 Services Summary

2.1 Contract Performance Objectives

The following table identifies the Contract Performance Objectives and pertinent criteria/ thresholds essential for ensuring HH-60W DVES contract success. These items will serve as criteria for evaluating Contractor performance specified in this PWS during the PoP.

Table 1: DVES Contractor Performance Objectives

Performance Objective

PWS Ref. Performance Criteria / Threshold

Quality of CDRL deliverable 4.2.1

There shall be no more than one (1) rejection of any single deliverable.

There shall be no more than a total of five (5) rejections of deliverables per contract quarter.

Receipt of CDRL deliverable 4.2.2

There shall be no more than three (3) late receipt(s) of deliverables per quarter.

Develop, adhere, and maintain an Integrated Master Schedule (IMS)

4.11.4

The Contractor is required to adhere to the critical path schedule outlined in the IMS, maintaining a timeframe of no more than ten

(10) business days, unless a re-baseline occurs.

Provide Monthly Status Reports (MSRs), hold Program Management Reviews (PMRs), and provide timely Cost data

4.12.5

The MSR report must be submitted by the 15th of each month. In the event that the 15th coincides with a holiday or weekend, the report will be required on the following business day. The first MSR report is due on the 15th of the second month following the award of the contract.

Develop and provide agenda, presentation materials, and minutes for program meetings

4.4.2, 4.9.2.2,

4.12 (all)

The Contractor shall submit draft agendas and draft presentation materials ten (10) business days before the scheduled event. The Contractor shall provide minutes from any event within five (5) business days following the event

Adherence to Contractor Quality Management System (QMS)

5.8

Provide support to USAF inquiries and DCMA surveillance;

including process audits, corrective actions, and internal Contractor adherence to QMS compliance is 100%.

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2.2 PWS Scope

The Contractor shall design, develop, test, integrate, validate/verify, and deliver a functional system that mitigates risks associated with HH-60W operation in DVE. The DVES system shall be integrated and installed onboard the USAF HH-60W platform; including all DVES kit production, technical data (including Technical Orders (TOs)), spares, support equipment, training materials and modifications to training/simulator devices, and sustainment deliverables, in accordance with the task and deliverable requirements specified in this PWS and the technical requirements listed in the HH-60W DVES SRD.

The Contractor shall execute the tasks described in this PWS under the direction and supervision of AFLCMC/WIH, and in coordination and collaboration with the DVES IPT detailed below in Section 2.4. The PWS covers work requirements extending across the Engineering & Manufacturing Development (EMD), Production & Deployment (P&D), and the Operations & Support (O&S) phases that are typical of Department of Defense (DoD) acquisition Programs of Record (PoR). Successful completion of Prototype and Verification kits during the EMD phase (Non-Recurring Engineering - NRE) may result in DVES Full Rate Production (FRP) and retrofit installation across the USAF HH-60W fleet, as well as concurrent modification to Trainer devices and Simulators (contingent upon successful contract execution to that point, enabling FRP approval). The period of performance for the contract consists of one (1) base period of two (2) years, with six (6) options of one (1) year each, as further detailed in Section 4.1.

2.3 Major Tasks and Program Objectives

Refer to Appendix A for the program Statement of Objectives (SOO), which further details the envisioned program phases and schedule for DVES development, integration, testing, and fielding.

The Government desires a mature, readily available solution based on technologies with a Technology Readiness Level (TRL) of 8-9 and a Manufacturing Readiness Level (MRL) of 9 or above. The TRL levels are crucial to swift execution of the DVES Program and have different criteria between Hardware and Software, as detailed in Appendix B. The Contractor shall perform the following major, over-arching tasks to accomplish the DVES program objectives, as further detailed in this PWS:

1. Integrated Master Schedule (IMS): Develop, maintain, and adhere to an IMS for timely execution of all project tasks and milestones. The IMS shall comprehensively capture all project schedule items, deliverables, milestones, and interdependencies defined in this

PWS.

2. Monthly Status Reports (MSR): Provide prompt and comprehensive MSRs to the Government, detailing project and deliverables progress/status, completed tasks, challenges, and upcoming activities.

3. Software Integration Lab (SIL) Testing: Conduct thorough SIL testing prior to ground and flight testing to identify and mitigate potential functional, integration, and human factors issues.

4. Technical Data Package (TDP): Develop and maintain a comprehensive and up-to-date TDP accurately depicting the DVES architecture, components, functionalities, and interfaces.

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5. Technical Orders (TOs): Generate and deliver complete, clear, concise, and technically accurate DVES TOs in accordance with the CDRLs, facilitating proper system installation, operation, maintenance, and troubleshooting.

6. DVES Development: Develop and integrate a DVES for the HH-60W helicopter to improve crew coordination and situational awareness during Restricted Visibility Approaches (RVAs) and en route flight operations in relevant operational conditions – including limited visibility or challenging terrain. The DVES shall include a capability to build a geo-referenced mapping of obstacles and hazards from collected data to implement a “see-and-remember technique” so that the crew can maintain awareness of obstacles that do not remain within a sensor Field of View (FOV) for as long as the obstacle or hazard remains operationally relevant. Sensor video with symbology overlay shall be recordable and available for playback during aircrew debriefing.

7. Real-Time Visual Displays: The DVES system shall provide near real-time visual displays of en route and terminal area hazards (including, but not limited to, terrain features, antennas, wires, poles, vehicles, fence posts, ditches, berms, holes, and large rocks) integrated with existing cockpit and cabin Multifunction Displays (MFDs).

8. System Performance, Cybersecurity, and Airworthiness: Ensure and verify system performance, cybersecurity, and airworthiness requirements are met for the DVES modification, resulting in a fully operational, airworthy, and cyber-secure system.

9. DVES System/Kit Installation: Install and integrate the DVES on a minimum of two test aircraft, documenting the process and demonstrating acceptable system integration and functionality.

10. Leveraging Existing Systems and Data Fusion: The DVES shall leverage existing HH-60W sensor systems, display infrastructure, navigation, avionics, and flight management systems to the maximum extent possible. It shall utilize data from digital geospatial sources (e.g., Digital Terrain Elevation Data (DTED), Digital Obstacle File (DOF), Digital Vertical Obstruction File (DVOF), Electro-Optical/Infrared (EO/IR) sensors, and other relevant data sources), and tactical symbology (e.g., Integrated Cueing Environment (ICE)) using TRL 8-9 technology. The use of existing Commercial Off-The-Shelf (COTS) components, software, and other items is highly encouraged. The solution should model the US Army DVE solution, where or if possible, to produce efficiencies in research, development, procurement and sustainment.

11. Minimally Invasive Installation: The DVES system installation will be as minimally invasive as possible and shall not compromise the structural integrity, aerodynamic performance, or operational capabilities of the HH-60W. Specifically, it shall not cause damage to the aircraft when full weight is on the ground, create significant drag during flight, or restrict landing attitude, airspeed, bank angles, or weapons employment.

2.4 DVES Integrated Product Team (IPT)

The success of the DVES Program depends upon the coordinated efforts of the entire DVES Integrated Product Team (IPT). The Contractor shall execute the tasks described in this PWS under the direction and supervision of the Acquisition Program Office, and in coordination and collaboration with the DVES IPT. The DVES IPT includes Government and non-Government

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personnel spanning multiple organizations and geographic locations. Key organizations within the DVES IPT are listed in Table 2 below.

Table 2: DVES IPT

Organization Location Role

AFLCMC/WIH Helicopter Division

Wright-Patterson AFB, Dayton, OH

HH-60W Acquisition Program Office, Senior Materiel Leader

AFLCMC/WIHBB Helicopter Sustainment Branch

Robins AFB, Warner Robins, GA

DVES Acquisition Program Office, HH-60W Sustainment

ACC/A589 Personnel Recovery Requirements Division

Joint Base Langley-Eustis (JBLE), Hampton, VA MAJCOM, Requirements Owner

AFSC 402d Software Engineering Group, 580th Software Engineering Squadron (SWES)

Robins AFB, Warner Robins, GA

HH-60W System Integration Laboratory (SIL), Software Sustainment

ACC 53rd Wing, 53rd Test and Evaluation Group, 88th Test & Evaluation Squadron (TES)

Nellis AFB, Las Vegas, NV*

CSAR Combined Test Force:

Lead Developmental Test & Evaluation Organization (LDTO) and Operational Test Organization (OTO)

Georgia Tech Research Institute (GTRI) Atlanta, GA Technical and Program Support

*-The CSAR CTF may be re-assigned to Davis-Monthan AFB in Tucson, AZ. The move/transfer of the unit is still TBD however, albeit may occur in 2029.

3.0 Government Property

3.1 Contractor Responsibility

3.1.1 Responsibilities

The Contractor shall be responsible for all government property provided under this contract in accordance with the Revolutionary Federal Acquisition Regulation Overhaul ((RFO), such as RFO 52-245.1), Revolutionary Defense Federal Acquisition Regulation Supplement (R-DFARS, such as R-DFARS Part 245), and all other applicable government regulations and contract/order clauses. The Government will provide the contractor with access to facilities on an as-needed basis to complete the Program; such as lab, office, and conference room space, access to HH-60W aircraft and SIL, Government computers and network access, and other government furnished items as necessary to complete this tasking under this contract.

3.1.2 Contractor Acquired Property (CAP)

The Contractor shall furnish all consumables, material, support equipment, and supplies required for performing the work of this PWS. An active inventory of all CAP shall be maintained for tracking and accountability purposes. Upon completion of the contract, all CAP materials procured with program funding shall be made available to the Government, who will coordinate transfer to a follow-on contract or back to the government for inventory.

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3.1.3 Shipping

All costs associated with shipping, handling, packaging, and delivery of any CAP, materials, equipment, or deliverables required for the performance of this PWS are the sole responsibility of the Contractor, exclusive of any Government Furnished Equipment/Property (GFE/GFP) assets provided by the government. The Government will not be responsible for any shipping or delivery charges associated with contractor performance of PWS tasks or deliverables. Refer to Section

4.13 for more detailed information regarding packaging, shipping, transportation, and handling.

3.2 Government Property to be Provided

3.2.1 Government Furnished Equipment/Property (GFE/GFP)

If required, GFE/GFP shall be provided in accordance with a request from the contractor, along with a requisite contract/order GFE/GFP attachment. The GFE/GFP shall be returned to the program office within 30 calendar days after the period of performance.

3.2.2 Government Furnished Information (GFI)

The Government shall provide the Contractor with access to USAF engineering and technical information, including Technical Orders (TOs) and engineering drawings, during the term of this contract. Specifically, the Government will provide to the maximum extent possible:

• TOs: Access to TOs via Technical Order Distribution Office (TODO) registration and TO requests.

• Time Compliance Technical Order (TCTO) Template: A TCTO template/module, including installation instructions, illustrated parts, operations, and maintenance instructions.

• Operator and Maintainer Manual Templates: Templates and/or Modules for Operator and Maintainer Manuals, including instructions for the DVES modification installation on the

HH-60W.

• Engineering Data/Drawing Templates and/or Modules: Any software/tools necessary to develop the DVES TDP and all data/drawing deliverables, such as Air Force Product Data Specification drawing 9579776 Revision N (CAGE 98752).

• References: Access to all references documented in this PWS as requested.

• HH-60W Electrical Loads Analysis: The latest version of the HH-60W Electrical Loads.

• HH-60W Weight and Balance: The latest version of HH-60W weight and balance documentation and calculations.

• Integrated Cueing Environment (ICE) Design Documentation (when/if available and applicable): ICE visual and aural cueing set design documentation, software, and functionality descriptions.

• Digital Ground Elevation Data (DGED) Design Documentation (when/if available and applicable): Design package documentation for DGED formatting (slated to replace Digital Terrain Elevation Data (DTED) for precision position and elevation data used by ICE and symbology). DTED will also be supplied by the Government as needed. Existing or future

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digital terrain data sets are in research and may be made available if necessary (such as TanDEM-X, ArcticDEM, Reference Elevation Model of Antarctica (REMA), and GeoData Cooperative data sets).

• Digital Vertical Obstruction File (DVOF): Vertical object files, produced by the DoD National Geospatial-Intelligence Agency (NGA).

• Digital Obstacle File (DOF): Vertical object files, produced by the Federal Aviation Administration (FAA).

• SCG: The latest USAF HH-60W and Army BlackHawk Security Classification Guide, and any other pertinent SCGs as required during contract execution.

• Systems Engineering Plan (SEP) and Test and Evaluation Master Plan (TEMP): The SEP, which will serve as the basis for the Contractor's Systems Engineering Management Plan (SEMP), Risk Management Plan (RMP), and Integrated Program Management Report

(IPMR).

• HH-60W Technical Data Package: Access to drawings, wiring diagrams, existing subsystem design or interface documentation, and other artifacts necessary for DVES development and integration.

3.2.3 Reporting of Government Property

The Contractor shall have a system of internal controls to manage (control, use, protect, repair, maintain, and preserve) Government property in its possession in accordance with RFOR 52.245- 1, Government Property, and its property management system shall be adequate to satisfy the requirements of this clause. The contractor shall record receipt and return of all GFE/GFP, as well as the reporting of shipment, consumption, disposal, or transfer to another contract, in the GFP Module in Procurement Integrated Enterprise Environment (PIEE), https://piee.eb.mil, as stipulated by R-DFARS 252.245-7005, Management and Reporting of Government Property. This reporting requirement does not change any liability provisions or other reporting requirements that may exist under the contract. GFP training and guidance is located at the Department of Defense (DoD) Procurement Toolbox at https://dodprocurementtoolbox.com/. Any/all GFE/GFP, Government Furnished Material (GFM), and/or Contractor Acquired Property (CAP) records shall be updated monthly and submitted as an attachment to the MSR.

(CDRL A01E/B01E/C01E/D01E/E01E/F01E/G01E,

DI-MGMT-80269, Status of GFE Report)

(CDRL A00Y/B00Y/C00Y/D00Y/E00Y/F00Y/G00Y, DI-MGMT-80368A, Status Report)

3.2.4 Loss of Government Property

3.2.4.1 Definition of Loss of Government Property

“Loss of Government property” means unintended loss of or damage to Government property including property that cannot be found after a reasonable search, loss due to inadequate storage, loss due to lack of security, theft, damage requiring repair to restore the item to usable condition, or damage that renders the property useless for its intended purpose or Beyond Economical Repair (BER). Loss of Government property does not include manufacturing defects, obsolescence, normal wear and tear, or purposeful destructive testing. Unless otherwise stated in the https://piee.eb.mil/ https://dodprocurementtoolbox.com/

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contract/order, loss of Government property does not include normal and reasonable inventory adjustments, i.e., losses of low priority consumable material, such as common hardware, as agreed to by the Contractor and the Government Property Administrator.

3.2.4.2 Reporting Loss of Government Property

The Contractor shall report loss of Government property in the GFP Module located in PIEE (https://piee.eb.mil).

3.2.4.3 Return or Retention of Government Property

All property provided by the Government remains the property of the Government and shall be returned to the Government as directed, but no later than completion of the contract/order, unless the Procuring Contracting Officer (PCO) directs the Contractor to retain the property for continued use under a successor contract. All Government property shall be returned to the Government in the condition provided unless approved in advance by the PCO. All material generated under the contract/order becomes the property of the Government and shall be returned to the Government as directed, but no later than completion of the contract/order, unless the PCO directs the Contractor to retain the material for continued use under a successor contract.

3.3 Base Support

If necessary, the Government shall provide facilities and incidental resources at the place of performance. The Government, in coordination with the contractor, shall arrange for the contractor to have access to all necessary military installations including test ranges, facilities, aircraft, and requisite support necessary to complete all aspects of the tasks. This access is not to be considered a primary duty location.

3.3.1 Holidays and Facility Closings

Contractor/subcontractor personnel shall observe holidays and facility closings as directed by the Government, regarding Government facilities. Contractor/subcontractor personnel shall only be permitted access to Government facilities when Government personnel are present.

4.0 Technical Task Statements And Deliverables

4.1 Period and Place of Performance

4.1.1 Period of Performance (PoP)

The period of performance for the contract consists of One (1) base period of two (2) years with One

(1) Ordering Period and One (1) Option to turn on Ordering Periods 2-6. A total period of performance of eight (8) years. The Government intends to include RFO 52.217-8, Option to Extend Services and RFO 52.17-9 Option to Extend the Term of the Contract.

4.1.2 Place of Performance

The Contractor shall primarily perform services at its facility. Periodic travel to the HH-60W 580th SIL at Robins Air Force Base (AFB), designated HH-60W Combined Test Force (CTF), or other military facilities (HH-60W operational bases, such as may be required for aircraft familiarization and surveys) will be required. The Government may also require additional testing at other locations offering suitable testing environments, infrastructure, and logistical advantages.

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Furthermore, the Contractor shall be prepared to travel to various CONUS locations as needed to support program activities throughout the PoP.

4.2 Contract Data Requirements List(s) (CDRL)

The below Table 3 lists each CDRL, each appropriate contract year applicable, the applicable Data Item Description (DID, available from https://quicksearch.dla.mil), CDRL Title/Name, and referenced PWS sections/paragraphs herein. The remainder of this PWS Section 4 entails the technical tasks, intent statements, declarations of specific Contractor activities, and reference back to each relevant CDRL, per topic/task. Overall, CDRLs may be written to be delivered as dictated by the program phase, or task function – in any event of conflict between this PWS and the actual CDRL DD1423, the DD1423 shall take precedence.

In the event of the exercise of RFO 52.217-8 (Option to Extend Services), the numeration of CDRLs will remain the same as the preceding option period.

https://quicksearch.dla.mil/

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Table 3: HH-60W DVES CDRLs

CDRL Data Item Number DID Title PWS Reference(s)

Base Ordering Period 1

Ordering Period 2

Ordering Period 3

Ordering Period 4

Ordering Period 5

Ordering Period 6

A001 B001 C001 D001 E001 F001 G001 DI-ADMN-

81249C Meeting Agenda

4.4.2, 4.9.2.2, 4.12, 4.12.1 4.12.2, 4.12.3, 4.12.4, 4.12.5 4.12.6.2, 4.12.7.2, 4.12.8.2, 4.12.9, 4.12.10, 4.12.11, 4.12.12, 4.12.13

A002 B002 C002 D002 E002 F002 G002 DI-ADMN-

81250C Meeting Minutes

4.4.2, 4.9.2.2, 4.12, 4.12.1 4.12.2, 4.12.3, 4.12.4, 4.12.5 4.12.6.2, 4.12.7.2, 4.12.8.2, 4.12.9, 4.12.10, 4.12.11, 4.12.12, 4.12.13

A003 B003 C003 D003 E003 F003 G003 DI-ADMN-

81373 Presentation Materials

4.4.2, 4.9.2.2, 4.12, 4.12.1 4.12.2, 4.12.3, 4.12.4, 4.12.5 4.12.6.2, 4.12.7.2, 4.12.8.2, 4.12.9, 4.12.10, 4.12.11, 4.12.12, 4.12.13

A004 B004 C004 D004 E004 F004 G004 DI-PSSS-

81656B

Bill of Material (BOM) for DMSMS Management Plan 4.4.3

A005 B005 C005 D005 E005 F005 G005 DI-MGMT-

81948 DMSMS Management Plan 4.13.8

A006 B006 DI-ILSS-

80872 Training Materials 4.5

A007 B007 DI-IPSC-

81427B

Software Development Plan

(SDP) 4.6.2

A008 B008 DI-IPSC-

81431A

System/Subsystem Specification (SSS) 4.7.17

A009 B009 DI-IPSC-

81447A

Computer Programming Manual (CPM) 4.6.3

A00A B00A DI-IPSC-

81433A

Software Requirements Specification (SRS) 4.6.4

A00B B00B DI-IPSC-

81429A

Software Transition Plan (STrP) 4.6.5

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CDRL Data Item Number DID Title PWS Reference(s)

Base Ordering Period 1

Ordering Period 2

Ordering Period 3

Ordering Period 4

Ordering Period 5

Ordering Period 6

A00C B00C DI-IPSC-

81432A

System/Subsystem Design Description (SSDD) 4.7.18

A00D B00D DI-IPSC-

81436A

Interface Design Description

(IDD) 4.7.19

A00E B00E DI-SESS-

81248B

Interface Control Document

(ICD) 4.7.20

A00F B00F DI-IPSC-

81441A

Software Product Specification (SPS)

4.6.7 4.6.15.1

A00G B00G DI-IPSC-

81442A

Software Version Description

(SVD) 4.6.8

A00H B00H DI-IPSC-

81448B

Firmware Support Manual

(FSM) 4.6.9

A00J B00J DI-IPSC-

81438A Software Test Plan (STP) 4.6.10

A00K B00K DI-IPSC-

81439A

Software Test Description

(STD) 4.6.11

A00L B00L DI-IPSC-

81440A Software Test Report (STR) 4.6.12

A00M B00M DI-IPSC-

81443A Software User Manual (SUM) 4.6.13

A00N B00N DI-SESS-

82043A

Software Architecture Document (SAD) 4.6.14

A00P B00P DI-IPSC-

81434A

Interface Requirements Specification (IRS) 4.7.21

A00Q B00Q DI-HFAC-

80745C

Human Engineering Systems Analysis Report (HESAR) 4.7.6.2

A00R B00R DI-QCIC-

80553A Acceptance Test Plan (ATP) 4.6.15.1

4.7.22

A00S B00S DI-SESS-

81785B

Systems Engineering Management Plan (SEMP) 4.7.1

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CDRL Data Item Number DID Title PWS Reference(s)

Base Ordering Period 1

Ordering Period 2

Ordering Period 3

Ordering Period 4

Ordering Period 5

Ordering Period 6

A00T B00T DI-MGMT-

81501A

Weight and Balance Report for Aircraft 4.7.7

A00U B00U DI-SAFT-

80101D

System Safety Hazard Analysis Report (SSHAR) 4.7.12.2

A00V B00V DI-ENVR-

81840

Programmatic Environmental Safety and Health Evaluation

(PESHE) Plan 4.7.12.3

A00W B00W DI-SESS-

81497B

Reliability and Maintainability Predictions

Report 4.7.14

A00X B00X DI-SESS-

81495C

Failure Modes, Effects, and Criticality Analysis Report 4.7.16

A00Y B00Y C00Y D00Y E00Y F00Y G00Y DI-MGMT-

80368A Status Report

3.2.3, 4.8.2, 4.11.1, 4.11.2 4.11.5, 4.11.6

A00Z B00Z DI-HFAC-

80747C

Human Engineering Design Approach Document –

Maintainer (HEDAD-M) 4.7.6.3

A010 B010 C010 D010 E010 F010 G010 DI-MGMT-

82001

DoD RMF Package Deliverables

4.7.11 4.7.11.1 4.7.11.5

A011 B011 DI-NDTI-

80809B Test/Inspection Report 4.8.4, 4.8.5, 4.8.6

4.10.2, 4.10.4

A012 B012 DI-SESS-

81000F

Product Drawings/Models and Associated Lists 4.9.1, 4.9.1.1, 4.9.1.2

A013 B013 TM-86-01 Technical Manuals Contract Requirements (TMCR)

4.9.2 4.9.2.1

A014 B014 DI-SESS-

81758A/T Logistics Product Data 4.9.3

A015 B015 DI-SESS-

81874

Engineering Data for Provisioning 4.9.3

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CDRL Data Item Number DID Title PWS Reference(s)

Base Ordering Period 1

Ordering Period 2

Ordering Period 3

Ordering Period 4

Ordering Period 5

Ordering Period 6

A016 B016 DI-ADMN-

81306

Program Protection Implementation Plan (PPIP) 4.9.4

A017 B017 C017 D017 E017 F017 G017 DI-MGMT-

81808

Contractor's Risk Management Plan 4.11.2

A018 B018 C018 D018 E018 F018 G018 DI-MGMT-

81861C

Integrated Program Management Report (IPMR)

4.11.4 4.14.6

A019 B019 DI-MGMT-

82135

Cybersecurity Risk Management Framework (RMF) Assessment and Authorization Products

4.7.11.1, 4.7.11.3 4.7.11.4, 4.7.11.6 4.7.11.7, 4.7.11.8

A01A B01A DI-ILSS-

80095

Integrated Logistics Support Plan 4.13.7

A01B B01B DI-MGMT-

81804A

Item Unique Identification (IUID) Marking Activity, Validation and Verification Report

4.13.1.1

A01C B01C DI-MGMT-

81803A

Item Unique Identification (IUID) Marking Plan 4.13.1.1

A01D B01D DI-MISC-

81832 Counterfeit Prevention Plan 4.13.5

4.13.6

A01E B01E C01E D01E E01E F01E G01E DI-MGMT-

80269 Status of GFE Report 3.2.3

A01F B01F DI-MISC-

80711A

Scientific and Technical Reports

4.4.4, 4.4.5, 4.7.8, 4.7.9, 4.7.11.2, 4.7.12.1, 4.7.13

4.7.15, 4.7.23, 4.7.24, 4.7.26, 4.8.5, 4.8.6, 4.10.1, 4.10.2, 4.10.3, 4.10.4

A01G B01G C01G D01G E01G F01G G01G DI-SAFT-

81563 Accident/Incident Report 5.5.2

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CDRL Data Item Number DID Title PWS Reference(s)

Base Ordering Period 1

Ordering Period 2

Ordering Period 3

Ordering Period 4

Ordering Period 5

Ordering Period 6

A01H B01H DI-IPSC-

81435B

Software Design Description

(SDD) 4.6.6

A01J B01J DI-MGMT-

81453C Data Accession List (DAL) 4.6, 4.6.15, 4.6.16, 4.6.17, 4.9.1.1, 4.9.1.2

A01K B01K C01K D01K E01K F01K G01K DI-QCIC-

81722 Quality Program Plan 5.8

A01L B01L DI-MGMT-

82133A

Requirements Traceability Verification Matrix (RTVM) 4.7.17

A01M B01M DI-MGMT-

82404

Acquisition and Sustainment Data Package (ASDP) -

Functional Thread Analysis (FTA) Report

4.7.25

A01N B01N DI-SESS-

82351A

Acquisition and Sustainment Data Package (ASDP)

Engineering Design data and Associated Lists (EDDAL))

4.9.1

A01P B01P DI-SESS-

82397 Airworthiness Plan 4.7.10

A01Q B01Q DI-SESS-

81766

Airworthiness Certification Basis 4.7.10

A01R B01R DI-SESS-

81768

Airworthiness Compliance Report 4.7.10

A01S B01S DI-AVCS-

80700A

Computer Software Product End Items 4.6, 4.6.15, 4.6.16, 4.6.17

A01T B01T C01T D01T E01T F01T G01T DI-FNCL-

82162

Cost and Hour Report (FlexFile) 4.11.7

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4.2.1 Quality of CDRL Deliverable

There shall be no more…