Attachment_2_SOW_Rev1.pdf

Attachment 2 – SOW, Rev 1

FA8106‐23‐R‐0001

United States Air Force

AFLCMC/WLDJ TINKER AFB OK

STATEMENT OF WORK

T-6A Avionics Replacement Program

20 December 2022

FINAL, Revision 1 – 20 Dec 22

Revision Log

Date Revision Number

Reason for Update Paragraph Page

Number Description of Change

5 December

Rev 1

Location of Prototype

Installation and Developmental Test

(DT) update

3.0 - Program Requirements (Aircraft and

ATDs)

Subsection (a), last sentence, added

“Randolph AFB, TX or Naval Air Station (NAS)

Patuxent River, MD”.

5 December

Rev 1 Location Update to

Test Readiness Review (TRR)

Table 3-1 Contractor Conducted Meetings – Technical Reviews

Added “NAS Patuxent

River, MD”

5 December

Rev 1

Location Update to Physical

Configuration Audit

(PCA)

Table 3-1 Contractor Conducted Meetings – Technical Reviews

Added “NAS Patuxent

River, MD”

5 December

Rev 1

Location Update to First Flight

Readiness Review

(FFRR)

Table 3-1 Contractor Conducted Meetings – Technical Reviews

Added “NAS Patuxent

River, MD”

5 December

Rev 1

Location of Prototype

Installation and Developmental Test

(DT) update

5.12.4.1 Developmental

Testing (DT) (Aircraft Only)

Added “or NAS Patuxent

River, MD” to first sentence

Prototype

Installation and Developmental Test

(DT) update

5.12.6 – Physical Prototype

Aircraft (Aircraft Only)

Changed second sentence; replaced

“Randolph AFB, TX or NAS Patuxent River, MD”.

Prototype

Installation and Developmental Test

(DT) update

5.12.6.1 – Aircraft

Installation and Test (Aircraft

Only)

Added language to second sentence, “will be completed at NAS Patuxent River, MD”.

Last sentence re-worded “The T-6A Kit Proof and Val/Ver installations will be completed at Randolph AFB, TX”.

5 December

Rev 1

Location of Prototype

Installation and Developmental Test

(DT) update

11.2 Operator

(Aircraft and

ATDs)

Added “or NAS Patuxent

River, MD” to first sentence

5 December

Rev 1

Location of Prototype

Installation and Developmental Test

(DT) update

11.2 Operator

(Aircraft and

ATDs)

Added “or NAS Patuxent

River, MD” to last sentence

Prototype

Installation and Developmental Test

(DT) update

11.4.1 Operator

(Aircraft Only)

Re-worded to “Randolph AFB, TX or NAS

Patuxent River, MD” in first sentence.

Update to Notional

Event Schedule

Appendix B - Notional

Production Planning Schedule

Added title above schedule “Notional Event Schedule”

Update to Notional

Event Schedule

Appendix B - Notional

Production Planning Schedule

112 Added updated schedule

Rev 1 Events and Milestone update

Appendix E – Prototype Installation

Moved “Prototype Installation” under “ASIL Testing Start”. Updated days to “400”

Appendix E – Test

Readiness Review (TRR)

Moved TRR under

“Prototype Installation”.

Updated days to “450”

Appendix E - Functional

Configuration Audit (FCA)

Moved FCA under “Developmental Testing Start”. Updated days to

“485”

Appendix E - System

Verification Review (SVR)

Moved SVR under “ Functional

Configuration Audit (FCA)”. Updated day to

“485”

CSDR Plan update

Appendix I – CSDR Plan

Addition of approved

CSDR Plan

9 December

EN Review

5.1.2 – Product Life-cycle Management (Aircraft and

ATDs)

Added “Digital Thread(s)” to last sentence of first paragraph

5.10.1 – Aircraft TDP

(Aircraft Only)

Added “documentation, including but not limited to major configuration and modification changes” to second sentence

5.16.1 – Electrical

Wiring Interconnect

System

(EWIS)

Integrity Program

(Aircraft Only)

Deleted first paragraph “The USG expects T-6A ARP STC to comply with

FAA Code of Federal Regulations 14 CFR

25.1701-1733. As part of this effort, the Contractor shall include wiring replacement in harnesses affected by the integration of T-6A

ARP”.

Events and

Milestone update

Appendix E - Prototype Installation

Start

Added “Start” to

“Prototype Installation”

Milestone update

Appendix E - Functional

Configuration Audit (FCA)

Moved “FCA” under “Prototype Installation

Start”. Updated days to “485”

Milestone update

Appendix E - Developmental Testing Start

172 Updated days to “455”

Milestone update

Appendix E - Kit Proof

Installation Start

Added “Start” to “ Kit Proof Installation”.

Updated days to “488”

Milestone update Appendix E -

Kit Buys 172 Updated days to “640”

20 December

GBTS - ATD

Appendix E – Physical

Prototype, Cadre, Spare Kits delivery

Removed Cadre and

Spare

20 December

GBTS - ATD

Appendix E – First

Article/Spare Delivered

Changed to:

Cadre/Spare Kits

Delivered. Updated days to “745”

Table of Contents

1.0 Introduction (Aircraft and ATDs)

1.1 Background (Aircraft and ATDs)

1.1.1 Technology Maturation Risk Reduction (TMRR) (Aircraft and ATDs)

1.1.2 Engineering & Manufacturing Development (EMD) Phase (Aircraft and ATDs)

1.1.3 Production & Deployment (P&D) Phase (Aircraft and ATDs)

1.2 Scope (Aircraft and ATDs)

2.0 Applicable Documentation (Aircraft and ATDs)

2.1 General (Aircraft and ATDs)

2.2 United States Government (USG) Documents (Aircraft and ATDs)

2.2.1 Specifications, Standards, and Handbooks (Aircraft and ATDs)

2.2.2 Other USG Documents, Drawings, and Publications (Aircraft and ATDs)

3.0 Program Requirements (Aircraft and ATDs)

3.1 Program Management (Aircraft and ATDs)

3.1.1 Program Management Plan (Aircraft and ATDs)

3.1.2 Program Management Contingencies (Aircraft and ATDs)

3.1.3 Special Requirements

3.2 Integrated Product Development (Aircraft and ATDs)

3.2.1 Integrated Master Plan (Aircraft and ATDs)

3.2.2 Integrated Master Schedule (Aircraft and ATDs)

3.2.3 Integrated Performance Management (Aircraft Only)

3.2.4 Program Status Report (Aircraft and ATDs)

3.3 Work Breakdown Structure (Aircraft and ATDs)

3.4 Sustaining Engineering (Aircraft and ATDs)

3.5 Contractor Cost and Software Data Reporting (Aircraft and ATDs)

3.6 System Collaboration (Aircraft and ATDs)

3.7 Parts Standardization (Aircraft and ATDs)

3.8 Hazardous Materials (Aircraft and ATDs)

3.9 USG Property Management, Salvage and Disposal (Aircraft and ATDs)

3.10 Intellectual Property (Aircraft and ATDs)

3.11 Data Rights (Aircraft and ATDs)

3.11.1 Technical Data Rights (Aircraft and ATDs)

3.12 Configuration Control and Data Management (Aircraft and ATDs)

3.12.1 Delivery Method for CDRL Deliveries (Aircraft and ATDs)

3.13 Audits (Aircraft and ATDs)

3.13.1 Configuration Audits (Aircraft Only)

3.14 Meeting Support (Aircraft and ATDs)

3.14.1 System Requirements Review (SRR) (Aircraft and ATDs)

3.14.2 System Function Review (SFR) (Aircraft and ATDs)

3.14.3 Preliminary Design Review (PDR) (Aircraft and ATDs)

3.14.4 Critical Design Review (CDR) (Aircraft and ATDs)

3.14.5 Test Readiness Review (TRR) (Aircraft Only)

3.14.6 Functional Configuration Audit (FCA) (Aircraft Only)

3.14.7 Physical Configuration Audit (PCA) (Aircraft Only)

3.14.8 System Verification Review (SVR) (Aircraft Only)

3.14.9 Production Readiness Review (PRR) (Aircraft and ATDs)

3.14.10 Program Management Review (Aircraft and ATDs)

3.14.11 Other Meetings (Aircraft and ATDs)

3.14.12 Post Award Conference (Aircraft and ATDs)

3.14.13 Technical Interchange Meeting (TIM) (Aircraft and ATDs)

3.14.14 System Sustainment Reviews (SSR) (Aircraft Only)

3.14.15 Aircraft Certification Working Group (ACWG) (Aircraft Only)

3.14.16 Crew Station Working Group (CSWG) (Aircraft Only)

3.15 Service Information and FAA Directive Review (Aircraft Only)

3.15.1 Evaluation Content (Aircraft Only)

3.15.2 Urgent FAA Airworthiness Directive (AD) (Aircraft Only)

3.15.3 DoD and USAF Directives

3.15.4 USAF Safety Investigation Board Recommendations

3.16 Quality Assurance Management (Aircraft Only)

3.16.1 Quality Assurance Management (ATD Only)

3.17 Risk Management (Aircraft and ATDs)

3.18 Manpower (Aircraft and ATDs)

3.18.1 Contractor Manpower Reporting (Aircraft and ATDs)

3.18.2 Subcontract Management (Aircraft and ATDs)

3.19 USG Base Access (Aircraft and ATDs)

3.20 Facility/Runway/Security Management (Aircraft Only)

3.21 Program Protection and Cybersecurity (Aircraft and ATDs)

3.21.1 Program Protection Planning (Aircraft and ATDs)

3.21.2 Supply Chain Risk Management and Counterfeit Prevention (Aircraft and ATDs) ... 50

3.21.3 Software Assurance (Aircraft and ATDs)

3.21.4 Cybersecurity (Aircraft and ATDs)

3.21.5 Secure Configuration of Commercial Software (Aircraft and ATDs)

3.22 Heads-Up Display (HUD)

4.0 Logistics Support Requirements (Aircraft and ATDs)

4.1 Integrated Logistics Support (Aircraft and ATDs)

4.2 Diminishing Manufacturing Sources and Material Shortages (Aircraft and ATDs)

4.3 Support Tools, Test Equipment, Tech Data and Hand Tool List (Aircraft and ATDs)

4.4 Supportability (Aircraft and ATDs)

4.5 Support Equipment (SE) (Aircraft and ATDs)

4.6 Facilities Requirement Report (ATD Only)

4.7 Base Site Survey (Aircraft and ATDs)

4.8 Supply (Aircraft and ATDs)

4.8.1 Packing, Packaging Preservation and Transportability (Aircraft and ATDs)

4.9 Supply Chain Risk Management (Aircraft and ATDs)

4.10 Initial Spares Kits (Aircraft and ATDs)

4.11 Key Logistics Criteria (Aircraft and ATDs)

4.11.1 Long-Lead Procurement (Aircraft and ATDs)

4.12 Aircraft Installation Configuration Audit (Aircraft Only)

4.13 Technical Publications (Aircraft Only)

4.13.1 ATD Operator Manuals and Maintenance Manuals Updates (ATD Only)

4.14 Calibration (Aircraft and ATDs)

4.15 Materials Property (Aircraft and ATDs)

4.16 Government Furnished Property (GFP) Resources (Aircraft and ATDs)

5.0 Systems Engineering (Aircraft and ATDs)

5.1 Digital Engineering (Aircraft and ATDs)

5.1.1 Authoritative Source of Truth (ASOT) (Aircraft and ATDs)

5.1.2 Product Life-cycle Management (Aircraft and ATDs)

5.1.3 Model Based Systems Engineering (Aircraft and ATDs)

5.1.4 Model Based Definition (Aircraft and ATDs)

5.1.5 Digital Thread (Aircraft and ATDs)

5.1.6 Aircraft ARP Installed System Program Systems Model (Aircraft Only)

5.1.7 ARP Aircraft Installed System Virtual Prototype (Aircraft Only)

5.1.8 ARP ATD Installed System Virtual Prototype (ATD Only)

5.1.9 ARP ATD Installed System Program Systems Model (ATD Only)

5.1.10 Open System Architecture (Aircraft and ATDs)

5.2 Systems Engineering Management Plan (Aircraft and ATDs)

5.3 Requirements Traceability (Aircraft and ATDs)

5.4 Interface Control Documentation – MBSE (Aircraft and ATDs)

5.5 Reliability and Maintainability Program (Aircraft and ATDs)

5.6 Human Systems Integration (Aircraft and ATDs)

5.7 Frequency Allocation (Aircraft Only)

5.8 Failure Mode, Effects, and Criticality Analysis (FMECA) (Aircraft Only)

5.9 System Safety Program (Aircraft and ATDs)

5.10 Technical Data Packages (TDP) (Aircraft and ATDs)

5.10.1 Aircraft TDP (Aircraft Only)

5.10.2 ATD TDP (ATD Only)

5.10.3 Software (Aircraft and ATDs)

5.10.4 Avionics System Integration Lab (ASIL) TDP (Aircraft Only)

5.10.5 Temporary-2 (T-2) Modification TDP (Aircraft Only)

5.10.6 ASDP Engineering Drawing Tree (Aircraft and ATDs)

5.11 Airworthiness (AW) (Aircraft Only)

5.11.1 Systems Engineering (Aircraft Only)

5.11.2 Airworthiness Process (Aircraft Only)

5.11.3 Support to Obtain Airworthiness Approval (Aircraft Only)

5.11.4 Mishap Incident (Aircraft Only)

5.11.5 Primary Flight Reference (PFR) Endorsement (Aircraft Only)

5.12 Test and Evaluation (Aircraft and ATDs)

5.12.1 Military and Federal Aviation Administration Requirements (Aircraft Only)

5.12.2 Contractor Testing (Aircraft Only)

5.12.3 First Flight Readiness Review (FFRR) (Aircraft Only)

5.12.4 USG Testing (Aircraft Only)

5.12.5 Integration Logbook (Aircraft Only)

5.12.6 Physical Prototype Aircraft (Aircraft Only)

5.12.7 Physical ATD Prototype (ATD Only)

5.13 Avionics System Integration Lab (Aircraft Only)

5.14 PT-406 Fuselage Modification (Aircraft Only)

5.15 Temporary-2 Modification (T-2 Mod) (Aircraft Only)

5.16 Avionics Integrity Program (AVIP) (Aircraft Only)

5.16.1 Electrical Wiring Interconnect System (EWIS) Integrity Program (Aircraft Only)

5.17 Interface Control Documentation (Aircraft and ATDs)

6.0 Aircraft Modification Requirements (Aircraft Only)

6.1 Acceptance of Aircraft (Aircraft Only)

6.2 Aircraft Induction (Aircraft Only)

6.3 Corrosion Control Management (Aircraft Only)

6.4 Aircraft Modification (Production) (Aircraft Only)

6.4.1 Mishap Investigation Support (Aircraft Only)

6.5 Post Installation (Aircraft Only)

6.6 Aircraft Delivery (Aircraft Only)

7.0 Aircrew Training Devices (ATDs Only)

7.1 ATD System Design (ATDs Only)

7.1.1 System/Subsystem Specification (S/SS Specification) (ATDs Only)

7.1.2 Requirements Traceability Verification Matrix (RTVM) (ATDs Only)

7.2 Qualification and Test Activities (ATDs Only)

7.2.1 Test Planning (ATDs Only)

7.2.2 GAT Test Readiness Review (TRR) (ATDs Only)

7.2.3 Government Acceptance Testing (GAT) (ATDs Only)

7.2.4 Deficiency Reports (DRs) (ATDs Only)

7.2.5 Physical Configuration Audits (PCAs) (ATDs Only)

7.3 Installation Program (ATDs Only)

7.3.1 Corrosion Control Management (ATDs Only)

7.3.2 Kitting (ATDs Only)

7.3.3 Installation Tools and Test Equipment (ATDs Only)

7.3.4 Interim Contract Support (ICS) (ATDs Only)

7.4 ATD Software Management and Planning (ATDs Only)

7.4.1 Software Requirements Definition (ATDs Only)

7.4.2 Software Design (ATDs Only)

7.4.3 Software Development (ATDs Only)

7.4.4 Software Testing (ATDs Only)

7.4.5 Software Configuration (ATDs Only)

8.0 Security Management (Aircraft and ATDs)

8.1 Common Access Card (CAC)

8.2 Security Incidents and Violations

8.3 Controlled Unclassified Information (CUI)

8.4 Covered Defense Information

8.5 Operations Security (OPSEC)

9.0 Software Management and Planning (Aircraft and ATDs)

9.1 Software Requirements Definition (Aircraft Only)

9.2 Software Design (Aircraft Only)

9.3 Software Development (Aircraft Only)

9.4 Software Testing (Aircraft Only)

9.5 Software Configuration (Aircraft Only)

10.0 Technical Orders (Aircraft Only)

11.0 Training (Aircraft and ATDs)

11.1 Training Material (Aircraft Only)

11.2 Operator (Aircraft and ATDs)

11.3 Maintenance (Aircraft)

11.4 Instructions (Aircraft and ATDs)

11.4.1 Operator (Aircraft Only)

11.4.2 Civilian Simulator Instructor (CSI) Training (ATDs Only)

11.4.3 Maintenance (Aircraft Only)

11.4.4 Maintenance (ATDs Only)

12.0 Warranties (Aircraft and ATDs)

13.0 Service Summary (Aircraft and ATDs)

14.0 Over and Above (O&A) (Aircraft and ATDs)

15.0 Travel G&A (Aircraft and ATDs)

APPENDIX A

APPENDIX B

APPENDIX C

APPENDIX D

APPENDIX E

APPENDIX F

APPENDIX G

APPENDIX H

APPENDIX I

1.0 Introduction (Aircraft and ATDs)

This Statement of Work (SOW) defines the effort required for the United States Air Force (USAF) T-6A Avionics Replacement Program (ARP). The effort will replace components impacted by Diminishing Manufacturing Sources and Material Shortages (DMSMS) and modify the fleet of an estimated 442 T-6A trainer aircraft, one (1) T-6A Test Aircraft (located at Textron Aviation Defense), one (1) PT-406 fuselage to be referred to as “all T-6A aircraft” for the remainder of this document. Twenty-six (26) T-6A Operational Flight Trainers (OFT), twenty-nine (29) T-6A Instrument Flight Trainers (IFT), nineteen (19) T-6A Unit Training Devices (UTD), six (6) T-6A Egress Procedure Trainers (EPT) and six (6) T-6A Ejection Seat Trainers (EST) to improve reliability and availability while reducing system sustainment and DMSMS costs via a modern, integrated, open-system avionics suite that is better suited to address evolving pilot training strategies.

1.1 Background (Aircraft and ATDs)

The T-6A Texan II is a commercial derivative of the Beechcraft Model 3000 (referred to as the Model 3000 in this document) aircraft with a Federal Aviation Administration (FAA) Type Certificate number A00009WI. The aircraft is a short-range, single-engine turbo-prop aircraft used for basic pilot training and Combat Systems Officer (CSO) training. T-6A Main Operating Bases (MOBs) with aircraft, OFT, IFT, UTD, EPT and EST quantities assigned are identified in Table 1-1.

Table 1-1 (MOBs w/ Aircraft, OFT, IFT, UTD, EPT, EST Quantities)

Base T-6A Test A/C

PT-406

Fuselage

OFT IFT UTD EPT EST

Randolph AFB, TX 45 0 0 3 4 2* 1 1 Laughlin AFB, TX 99 0 0 6 7 5 1 1 Vance AFB, OK 99 0 0 5 7 5 1 1 Columbus AFB, MS 99 0 0 6 6 4 1 1 Sheppard AFB, TX 76 0 0 3 4 3 1 1 CSO Pensacola, FL 24 0 0 3 1 0 1 1 Textron Beech Field, KS 0 1 0 0 0 0 0 0 Tinker AFB, OK 0 0 1 0 0 0 0 0

Totals 442 1 1 26 29 19 6 6 *One (1) UTD located in Original Equipment Manufacturer (OEM) facility (Broken Arrow, Oklahoma)

** The aircraft and ATDs shown are estimates only

1.1.1 Technology Maturation Risk Reduction (TMRR) (Aircraft and ATDs)

1.1.1.1 The role of technical reviews and audits in the USG acquisition life cycle (Aircraft and ATDs) This contract includes technology maturation and risk reduction (TMRR), Engineering and Manufacturing Development (EMD) and Production and Deployment (P&D). Technical reviews and audits are assessment tools that the Department of Defense (DoD) program organization uses to provide decision-makers sufficient information on the program’s technical readiness to proceed to the next phase or to the next decision point within a phase.

1.1.1.2 Technology Maturation & Risk Reduction (TMRR) Phase Purpose (Aircraft and ATDs) The Contractor shall utilize the Technology Maturation & Risk Reduction (TMRR) Phase to reduce technology risk, engineering integration, life-cycle cost risk, and determine the appropriate set of technologies to be integrated into a full system. The Contractor shall deliver virtual prototyping of system elements, refine requirements, and develop the Functional and Allocated Baselines of the end-item system configuration.

1.1.1.3 Technology Maturation & Risk Reduction (TMRR) Phase Objectives (Aircraft and ATDs) The objective of the TMRR phase is the buying down technical risk and developing a sufficient understanding of a solution in order to make sound business decisions on initiating a formal acquisition program in the Engineering, Manufacturing, and Development (EMD) Phase.

1.1.1.4 Technology Maturation & Risk Reduction (TMRR) Phase Process (Aircraft) Technology development is an iterative process of maturing technologies and refining user performance parameters to accommodate those technologies that are not sufficiently mature.

The Contractor shall utilize the Joint Primary Aircraft Training System (JPATS) Operational Requirements Document (ORD) and T-6A ARP System Requirements Document (SRD) to guide the efforts of this phase, leading to an approved System Subsystem Design Document

(SSDD).

1.1.1.5 Technology Maturation & Risk Reduction (TMRR) Phase Reviews (Aircraft and ATDs) The Technical Reviews conducted during the TMRR Phase are:

System Requirements Review (SRR) System Functional Review (SFR) Preliminary Design Review (PDR)

1.1.2 Engineering & Manufacturing Development (EMD) Phase (Aircraft and ATDs) The Engineering & Manufacturing Development (EMD) Phase is where a system is developed and designed before going into production. The EMD Phase starts after a successful Milestone B which is considered the formal start of any program. The Contractor shall complete the development of a system or increment of capability, complete full system integration, develop affordable and executable manufacturing processes, complete system fabrication, and test and evaluate the system before proceeding into the P&D Phase.

1.1.2.1 Engineering & Manufacturing Development (EMD) Phase Reviews (Aircraft and ATDs) Below are the major reviews conducted during the EMD Phase:

Critical Design Review (CDR) (Aircraft and ATDs) Test Readiness Review (TRR) (Aircraft and ATDs) First Flight Readiness Review (FFRR) (Aircraft Only) System Verification Review (SVR) (Aircraft Only) Functional Configuration Audit (FCA) (Aircraft Only) Physical Configuration Audit (PCA) (Aircraft and ATDs) Production Readiness Review (PRR) (Aircraft and ATDs)

1.1.3 Production & Deployment (P&D) Phase (Aircraft and ATDs) The P&D Phase is where a system that satisfies an operational capability is produced and deployed to an end-user. The phase begins after a successful Milestone C review and Engineering, Manufacturing and Development (EMD) Phase. The Contractor shall complete the ARP installation to an estimated 440 T-6A aircraft, not counting the PT-406 Fuselage mock-up and the three (3) T-6A modified during EMD. The Contractor shall also complete the ARP installation of an estimated 84 ATDs, not counting the two (2) ATDs modified during EMD.

1.2 Scope (Aircraft and ATDs)

This is a one-time modification utilizing a single integrator to permanently replace all of the USAF owned and operated T-6A aircraft avionics suites and provide corresponding and equivalent configuration modifications for the new T-6A avionics suites in all USAF owned and operated Aircrew Training Devices (ATDs). ATDs are comprised of two (2) sub-groups; Flight Training Devices (FTDs) and Procedures Training Devices (PTDs). The FTD sub-group is comprised of OFTs, IFTs, and UTDs. The PTD sub-group is comprised of EPTs and ESTs.

Use of the word ‘T-6A’ in this document applies only to USAF T-6A aircraft and ATDs.

The modification solution for this contract utilizes an existing Commercial-off-the-Shelf (COTS) Avionics Suite as a baseline for Virtual and Physical Prototype approval, resulting in a FAA Model 3000 Supplemental Type Certificate (STC) solution for the T-6A aircraft. Solution meets the performance requirements and replaces the components listed in the T-6A ARP SRD.

The modification solution for this contract provides these logistics needs for both the aircraft and ATDs: Supply, Spares, Training Materials, Training, Operations and Maintenance Manuals developed in (or converted to) USAF format, ATD/Trainer manuals, Data Rights, Technical Data Packages (TDP), Frequency Spectrum Data (aircraft only), Cyber Security Analysis, and other data, analysis, and support as described herein.

2.0 Applicable Documentation (Aircraft and ATDs)

2.1 General (Aircraft and ATDs)

The following specifications, standards, and handbooks are a supplement of this SOW to the extent specified herein. Unless otherwise specified, the issues of the documents are those listed in the latest issue of the Department of Defense Index (DoDI) of Specifications and Standards and supplement thereto.

2.2 United States Government (USG) Documents (Aircraft and ATDs)

2.2.1 Specifications, Standards, and Handbooks (Aircraft and ATDs)

Table 2-1 (Specifications, Standards, and Handbooks) Standards Document Number

Document Title Date

MIL-HDBK-61A Configuration Management Guidance 7 Feb 2001 MIL-PRF-32216 Evaluation of Commercial Off-The-Shelf (COTS) Manuals 17 Oct 2006 MIL-HDBK-516C Airworthiness Certification Criteria 12 Dec 2014 MIL-STD-1472G Department of Defense HCI Style Guide 11 Jan 2012 MIL-STD-31000A Technical Data Packages 26 Feb 2013

MIL-STD-38784A

Department of Defense Standard Practice for Manuals, Technical: General Style and Format Requirements

25 Aug 2011

MIL-STD-464C

Electromagnetic Environmental Effects Requirements for Systems

1 Dec 2010

MIL-STD-882E Department of Defense Standard Practice for System Safety 11 May 2012 MIL-STD-130-N Identification Marking of U.S. Military Property 26 Aug 2019 MIL-STD-1472H Human Engineering 17 Jan 2019

MIL-S-8512D

Support Equipment, Aeronautical, Special, General Specs for Design

13 May 2002

MIL-T-28800E Test Equipment for Use with Electrical and Electronic Equipment 4 Jan 1994 TM-86-01R Air Force Technical Manual Contract Requirements (TMCR) 10 Aug 2022

MIL-STD-2073/1E

Change 4

DoD Standards Practice For Military Packaging 22 Apr 2019

MIL-STD-129R

Change 2

DoD Standard Practice Marking for Shipment and Storage 27 Sep 2019

MIL-STD-1366E Interface Standard for Transportability Criteria 31 Oct 2006 MIL-STD-881E Work Breakdown Structures for Defense Material Items Oct 2020

MIL-STD-3022

Documentation of Verification, Validation, and Accreditation (VV&A) for Models and Simulations

Apr 2012

ASTM D3951-10 Standard Practice for Commercial Packaging 18 Feb 2016

BS25301 Rev 3* Flight Training Device (FTD) Program Unique Specification Document (PUSD)

15 Jun 2010

BS25507A

Procedural Training Device (PTD) Program Unique Specification Document (PUSD)

15 Mar 2008

* Note on ATD Document, BS25302 Systems Specification, JPATS GBTS, Revision B dated 22 April 2008, Section J: The following segments are not ARP requirements for the ARP ATD technical solution: Development Courses, Courses Standardized, and Operational Support as depicted in Figure 3.1 GBTS Hierarchy.

Contract Data Requirements List (CDRL)

CDRL # Document Number Document Title Version

A001 DI-MISC-81397D/T

Hazardous Materials Management Program (HMMPP) Report Rev D

A002 DI-MGMT-80368A Status Report, Program Status Report Rev A A003 DI-ADMN-81249C Meeting Agenda, Conference Meeting Agenda Rev C A004 DI-ADMN-81373 Presentation Material A005 DI-ADMN-81250C Meeting Minutes, Conference Meeting Minutes Rev C

A006 DI-MISC-81241/T Airworthiness Directives/Service Bulletins/Advisory Data A007 DI-ADMIN-81401C/T Contract Change Proposals (CCP) Rev C

A008 DI-MGMT-81861C

Integrated Program Management Data and Analysis Report (IPMDAR) Rev C

A009 DI-SESS-80642E Notice of Revision (NOR) Rev E A010 DI-MGMT-81453B/T Data Accession List (DAL) Rev B A011 DI-SESS-80640E/T Request for Variance (RFV), Request for Deviation (RFD) Rev E A012 DI-MISC-80508B/T Technical Report-Study Services, Maintenance Assistance

A013 DI-SESS-82329

Technical Report-Study/Services, Mechanical Equipment and Subsystems Integrity Program (MECSIP) Master Plan

(MP)

A014 DI-QCIC-80126B

Government Industry Data Exchange Program (GIDEP) Alert Response Rev B

A015 DI-MISC-80508B

Technical Report – Study/Services, Aircraft Architecture Analysis Report Rev B

A016 DI-SESS-80294B

Maintenance Test and Support Equipment Requirements List Rev B

A017 DI-SESS-81022E Configuration Audit Summary Report and Certification Rev E A018 DI-SESS-81785A System Engineering Management Plan (SEMP) Rev A A019 DI-IPSC-81431A System/Subsystem Specification (SSS) Rev A A020 DI-IPSC-81433A Software Requirements Specification (SRS) Rev A

A021 CANCELLED

A022 DI-SAFT-81932

Critical Safety Items (CSI)/Critical Application Item (CAI) List

A023 DI-SESS-81766/T Airworthiness Specification, Certification Basis A024 DI-MGMT-82377 Test Plans Rev A

A025 DI-QCIC-81536A Test Information Sheet (TIS) Rev A A026 DI-NDTI-80809B Test/Inspection Report Rev B A027 DI-IPSC-82134 Software Sustainability Package, ATDs A028 DI-NDTI-80603A Test Procedure Rev A A029 DI-SESS-81248B Interface Control Document (ICD) Rev B A030 DI-IPSC-81436A/T Interface Design Description (IDD) Rev A

A031 DI-SESS-81495B

Failure Mode, Effects, and Criticality Analysis, FMECA Report Rev B

A032 DI-SAFT-81626 System Safety Program Plan (SSPP) A033 DI-SAFT-80101C System Safety Hazard Analysis Report (SSHAR) Rev C A034 DI-SAFT-81563 Accident/Incident Report A035 DI-SESS-80776B/T Technical Data Package (TDP) Rev B A036 DI-MGMT-81501A Weight and Balance Report for Aircraft Rev A A037 DI-ILSS-80966A Training Facilities Report A038 DI-IPSC-81432A System/Subsystem Design Description (SSDD) Rev A A039 DI-MGMT-81797 Program Management Plan A040 DI-IPSC-81442A Software Version Description (SVD) Rev A A041 DI-IPSC-81427B Software Development Plan (SDP) Rev B A042 DI-IPSC-81438A Software Test Plan (STP) Rev A A043 DI-IPSC-81435B Software Design Description (SDD) Rev B A044 DI-IPSC-81439A Software Test Description (STD) Rev A A045 DI-IPSC-81440A Software Test Report (STR) Rev A A046 DI-IPSC-81441A Software Product Specification (SPS) Rev A

A047 DI-TMSS-80527D

Commercial Off-The-Shelf (COTS) Manuals and Associated Supplemental Data Rev D

A048 DI-MGMT-81948

Diminishing Manufacturing Sources and Material Shortages (DMSMS) Management Plan

A049 DI-MGMT-80004A/T Management Plan, Airworthiness Rev A A050 DI-SESS-81121A Baseline Description Document Rev A

A051 DI-SESS-81984A

Commercial Derivative Aircraft (CDA) Airworthiness Certification Rev A

A052 DI-SESS-81768/T

Airworthiness Certification Criteria Report, Compliance Report

A053 DI-SAFT-80102C Safety Assessment Report (SAR) Rev C A054 DI-MGMT-82133/T Requirements Traceability Verification Matrix (RTVM) A055 DI-ILSS-80095/T Integrated Logistics Support Plan

A056 DI-MISC-80508B/T

Technical Report – Study/Services, Prime Item Product Functional Specification (PIPFS) Edits/Updates

A057 DI-MISC-80508B/T

Technical Report-Study/Services, Cybersecurity Risk Impact Evaluation Recommendation (CIER) Rev B

A058 DI-MISC-80508B/T Technical Report-Study/Services, Cyber Security Controls Rev B A059 DI-MGMT-80441D Government Property (GP) Inventory Report A060 DI-EMCS-81827 Spectrum Certification Spectral Characteristics Data A061 DI-ILSS-80872 Training Materials, Avionics System Integration Lab (ASIL)

A062 DI-IPSC-81443A

Software User Manual (SUM), Avionics System Integration Lab (ASIL) Rev A

A063 DI-QCIC-80553A

Acceptance Test Plan, Avionics System Integration Lab (ASIL) Rev A

A064 DI-NDTI-80603A Test Procedure, Acceptance Test Procedures Rev A

A065 DI-QCIC-81891

Acceptance Test Report, Avionics System Integration Lab

(ASIL)

A066 DI-MGMT-80004A Management Plan, ASIL Systems Integration Plan Rev A A067 DI-EMCS-81543A Spectrum Supportability Risk Assessment (SSRA) Rev A A068 DI-MISC-81283 Specification Requirement Verification Matrix (SRVM) A069 DI-SES-81646C Configuration Audit Plan Rev C

A070 DI-IPSC-82134

Software Sustainability Package, Ground Support Maintenance Computer

A071 DI-IPSC-82134 Software Sustainability Package, Virtual Crew Station

A072 DI-IPSC-82134

Software Sustainability Package, Software Development Kit (SDK)

A073 DI-MISC-80508B/T

Technical Report – Study/Services, Substantiating Analysis Rev B

A074 DI-IPSC-82134 Software Sustainability Package, ASIL Computer A075 DI-FNCL-82162/T Cost and Hour Report A076 DI-MGMT-82164/T Quantity Data Report A077 DI-FNCL-81765C Contractor Business Data Report Rev C A078 DI-MGMT-82165/T Technical Data Report A079 DI-SESS-80858D Supplier’s Configuration Management Plan Rev D A080 DI-MGMT-81808 Contractor’s Risk Management Plan A081 DI-MGMT-81809 Risk Management Report

A082 DI-MISC-80508B

Technical Report – Study/Services, Advanced Threat Detection, Architecture Analysis Report Rev B

A083 DI-IPSC-82249A Software Assurance Evaluation Report Rev A A084 DI-MGMT-82273 DMSMS Health Assessment Report A085 DI-ILSS-80868 Special Equipment Tools and Test Equipment List A086 DI-MISC-82104/T Site Survey Report (SSR) A087 DI-SESS-82364/T Digital System Model

A088 DI-SESS-82351/T

Acquisition and Sustainment Data Package (ASDP) Product Engineering Design Data and Associated Lists

(EDDAL)

A089 DI-SESS-81496B/T

Reliability and Maintainability (R&M) Block Diagrams and Mathematical Models Report Rev B

A090 DI-SESS-82322 Built-in-Test Fault Tree A091 DI-SESS-81497B/T Reliability and Maintainability (R&M) Predictions Report Rev B

A092 DI-MISC-80652/T

Technical Information Report, DMSMS Impact Assessment

A093 DI-MISC-80508B

Technical Report – Study/Services, Primary Flight Reference (PFR) Endorsement – Display Information Package Rev B

A094 DI-SAFT-81300B Mishap Risk Assessment Report (MRAR) Rev B

A095 DI-DRPR-81961B

Acquisition and Sustainment Data Package (ASDP) Engineering Drawing Tree Rev B

A096 CANCELLED

A097 DI-MGMT-82099A Open Systems Management Plan (OSMP) Rev A A098 DI-MGMT-81468A Contract Funds Status Report (CFSR) Rev A A099 DI-MGMT-81334D Contract Work Breakdown Structure Rev D A100 DI-MISC-81398D Hazardous Materials Management Program (HMMP) Plan Rev D A101 DI-SESS-81903 As-Built Configuration (ABC) Bill of Material (BOM) List

A102 DI-TMSS-81817

Technical Manual Quality Assurance (TMQA) Program Plan

A103 DI-TMSS-81818 TM Validation Plan

A104 DI-FNCL-80449

Design-To-Cost/Life Cycle Cost and Variance Analysis Report

A105 DI-HFAC-81833A Human Systems Integration Report Rev A

A106 DI-MGMT-80258B

Material Improvement Project (MIP) Report, Deficiency Report (DR) Rev B

A107 DI-SESS-80858D

Supplier’s Configuration Management Plan, Software Configuration Management Plans Rev D

A108 DI-ILSS-80872/T Training Materials

A109 DI-MSSM-81751

Department of Defense (DOD) Modeling and Simulation (M&S) Verification and Validation (V&V) Plan

A110 DI-MSSM-81752

Department of Defense (DOD) Modeling and Simulation (M&S) Verification and Validation (V&V) Report

A111 DI-MISC-81562

Temporary Non-Standard Modification Documentation and Marking Requirements for Test Equipment in Aerospace Vehicles and Related Ground Support Equipment, T-2 Modifications for EMD Aircraft

A112 DI-PSSS-80134B Proposed Spare Parts List Rev B

A113 DI-NDTI-80566A Test Plan, ATD System Test Plan Rev A

A114 DI-MGMT-82188 Accident Incident Report

A115 DI-TMSS-81819A TM Validation Certificate

A116 DI-TMSS-80067C

Technical Manual (TM) Contractor Furnished Aeronautical Equipment or Contractor Furnished Equipment

A117 TM-86-01R Technical Manual Contract Requirements (TMCR)

A118 DI-MGMT-80368A Status Report, Frequency Allocation Application Status Rev A

A119 DI-QCIC-81794A Quality Assurance Program Plan (QAPP) Rev A

A120 DI-TMSS-81812 Technical Manual Schedule and Status Report

2.2.2 Other USG Documents, Drawings, and Publications (Aircraft and ATDs)

Table 2-2 (Other USG Documents, Drawings, and Publications) National Institute of Standards and Technology (NIST) Document Number Document Title Version/Date

NIST 800-37

Risk Management Framework for Information Systems and Organizations

23 Apr 2021

Regulations, Instructions, and Technical Orders (TO) Document Number Document Title Version/Date

Department of Defense 5500.7-R

Joint Ethics Regulations (JER) Aug 2013

DoDI 4161.02 Accountability and Management of USG Contract Property

Change 2 31 Aug 2018

DoDI 5000.02 Operation of the Adaptive Acquisition Framework 23 Jan 2020

DoDI 5230.24 Distribution Statements on Technical Documents Change 3 15 Oct 2018

DoDI 8500.01 Cybersecurity Change 1

7 Oct 2019

DoDI 8510.01 Risk Management Framework (RMF) for DoD Information Technology (IT)

Change 3 29 Dec 2020

TO 00-5-3 AF Technical Order Life-Cycle Management 15 Feb 2019

TO 00-35D-54

USAF Deficiency Reporting, Investigation, and Resolution

(DRI&R)

15 May 2015

TO 1-1-689-3 Cleaning and Corrosion Control 16 Apr 2014

TO 1-1B-50

Basic Technical Order for USAF Aircraft Weight and Balance

1 Apr 2008

Forms

DD Form 1149 Requisition and Invoice/Shipping Document 1 Jan 2016 E2ESS Stepstone Application for Equipment Frequency Allocation DD Form 2357 Hazardous Component Safety Data Statement Apr 1999 FAA Form 8130-3 Authorized Release Certificate, Airworthiness Approval Tag 1 Feb 2014 OSHA Form 3514 Material Safety Data Sheet DD Form 1653 Transportation Data for Solicitations 28 Apr 2022 AFMC Form 158 Packaging Requirements 24 Apr 2015

Other Documents

AETCMAN 36-2601 Special Contract Training 3 Mar 2020 AFI 11-2T-6, Volume 3 T-6A Operations Procedures 16 Jul 2015 AFI 17-101 Air Force Risk Management Framework (RMF) Program 6 Feb 2020 AFI 17-220 Spectrum Management 8 Jun 2021 AFI 62-601 Airworthiness 10 Jun 2022 AFI 64-106 Contractor Labor Relations Activities 3 Oct 2019 AFI 63-101/20-101 Integrated Life-Cycle Management 30 Jun 2020 DoDI 5000.89_DAFI99-

Capabilities-Based Test and Evaluation 15 Mar 2022

AFI-91-202 The USAF Mishap Prevention Program 11 Mar 2020 DoDI 5000.83_DAFI63-

Technology and Program Protection to Maintain Technological Advantage

8 Mar 2022

AFPD 17-1 Information Dominance Governance and Management 12 Apr 2016 AIA NAS 411 Hazardous Materials Management Plan 30 Sep 2020

Air Force Life Cycle Management Center Standard Process Cybersecurity Assessment and Authorization

Version: 3.3 (released 21 October 2021).

Committee on National Security Systems Instruction (CNSSI) No.

Security Categorization and Control Selection for National Security Systems

27 Mar 2014

DODI 5000 series Defense Acquisition Guidebook Feb 2014

DoD Integrated Master Plan (IMP) and Integrated Master Schedule (IMS) Preparation and Use Guide

Version 0.9, 21 Oct 2005

DoD Program Protection Plan Outline and Guidance Version 1.0

DoD Risk Management Guide for DoD Acquisition Version 1.0, August 2006

Software Assurance Countermeasures in Program Protection Planning

Mar 2014

Technology Readiness Assessment Guidance Apr 2011

RTCA/DO-160G

Environmental Conditions and Test Procedures for Airborne Equipment

8 Dec 2010

RTCA/DO-178C

Software Considerations in Airborne Systems and Equipment Certification

13 Dec 2011

FAA Order 8110.101A Type Certification Procedures for Military Commercial Derivative Aircraft

25 Feb 2015

AS9100D

Quality Management Systems – Requirements for Aviation

Sep 2016

10 USC § 2320 Rights in Technical Data 31 Dec 2011 Title 44 USC Chapter 35 Coordination of Federal information Policy 14 CFR 21.101 Designation of Applicable Regulations 4 Dec 2012 AWB-130 Certification Basis 2 Jun 2021 AWB-140 Compliance Report 2 Jun 2021 AWB-150 Airworthiness (AW) Risk Assessment and Acceptance 30 Sep 2020 AWB-360 Commercial Derivative Aircraft Airworthiness 1 Sep 2021

IEEE 15288.1-2014

IEEE Standard for Application of Systems Engineering on Defense Programs

15 May 2015

IEEE 15288.2-2014

IEEE Standard for Technical Reviews and Audits on Defense Programs

15 May 2015

DoD 4500.9-R Defense Transportation Regulation 27 Dec 2019

3.0 Program Requirements (Aircraft and ATDs)

The Contractor shall have a proposed avionics suite with a Technical Readiness Level (TRL) 7 IAW Technology Readiness Assessment Guidance, which utilizes standard COTS Line Replaceable Units (LRU) components versus unique to T-6A to facilitate future system growth.

The Contractor shall meet the requirements documented in the T-6A ARP SRD. The Contractor’s proposed avionics suite shall have demonstrated successful operation on Beechcraft Model 3000 or equivalent aircraft. Equivalent aircraft is defined as Title 14 Code of Federal Regulations Part 23 aircraft of similar size and functionality. The Contractor’s proposed solution shall be FAA certified via STC for use in all USAF T-6A aircraft within the contractually designated timeframes outlined in IAW CDRL A052, DI-SESS-81768/T, Airworthiness Certification Criteria Report, Compliance Report.

Issues, anomalies, damage, or problems that arise during any phase after the Contractor’s testing and acceptance of the T-6A with regard to any sensor readings, configurations, installations, fit issues, interfaces, communications with any existing T-6A aircraft systems, avionics, structures, including but not limited to those that arise during design, development, prototyping, testing, kit proof installation, ground test, flight test, and production installations shall have the root cause and corrective actions identified. If the root cause is identified to be caused by the Contractor, then the corrective action implemented will be at the expense of the Contractor.

The Contractor’s solution shall consist of all efforts required to provide an industry standard avionics replacement suite IAW the T-6A ARP SRD. This effort includes, but is not limited to, the following:

a) The Contractor shall perform engineering and design for Physical Prototype efforts required to obtain the FAA STC for the replacement avionics suite on all T-6A aircraft. The

Contractor modified T-6A Physical Prototype shall, at the end of testing, be a fully operational and fully FAA certified aircraft and meet the requirements of the T-6A ARP SRD. The T-6A Prototype installation will be completed at Randolph AFB, TX or Naval Air Station (NAS) Patuxent River, MD.

b) The Contractor shall perform engineering and design for Physical Prototype efforts required to obtain USG approval for a Physical Prototype modification of a T-6A UTD such that it fully represents the replacement avionics suite on T-6A aircraft, including avionics operations and visual representation as described in the T-6A ARP SRD. The Contractor shall accomplish a Physical Prototype on a T-6A UTD. A UTD located at Broken Arrow, OK will be made available to the to the winning contractor for shipment from Flight Safety International in Broken Arrow, OK to the Contractor’s facility after successful completion of the aircraft SFR and will need to be shipped back to the USG (at Randolph AFB, TX) prior to the end of the contract

c) The Contractor modified T-6A Physical Prototype UTD shall, at the end of testing, be a production representative ARP modified UTD, fully operational, and meet the requirements of the T-6A ARP SRD

d) The Contractor shall support all USG operational test and evaluation for aircraft and Government Acceptance Testing (GAT) for ATDs

e) The Contractor shall perform installation and operational checks as part of the installation process as well as the PT-406 fuselage. PT-406 fuselage will be made available to the winning contractor for shipment from Tinker AFB to the Contractor’s facility at the beginning of the contract and will need to be shipped back to the USG (at Tinker AFB, OK) prior the end of the contract

f) The Contractor shall provide Integrated Logistics Support which includes initial spares for the aircraft and ATDs and any additional support/maintenance equipment required for the modification

g) The Contractor shall perform technical data development for aircraft and ATDs

h) The Contractor shall develop and provide training for Test Pilots and 19th AF Studies and

Analysis Squadron (SAS), aircraft maintenance technicians, ATD maintainers and instructors

i) The Contractor shall be the STC holder for the T-6A ARP system

3.1 Program Management (Aircraft and ATDs)

The Contractor shall provide internal management and control on all matters related to this SOW, from conception to final completion. The Contractor shall track program progress, and immediately report (apart from status reports) to the PM and USG Procurement Contracting Officer (PCO) any activity and/or deliverable which will not be achieved as scheduled, citing the cause, contributing factors, impacts, and resolutions to get back on schedule in writing (email acceptable). Failure to do so shall be viewed as an insufficient program management performance, justifying corrective measures to be taken by the USG. The Contractor shall provide programmatic support for the entire acquisition effort. Programmatic support shall include, but not be limited to, development of schedules, evaluation of alternatives, and development of necessary plans and procedures. Program Management Reports will be provided monthly or IAW CDRL A008, DI-MGMT-8186C, Integrated Program Management Data and Analysis Report (IPMDAR).

The Contractor shall establish a T-6A ARP execution organization and shall apply sound management principles to assure success of the program. The Contractor shall provide all manpower, material, equipment, components, skills, expertise, data, and knowledge to fully and successfully complete the contract. This includes, but not limited to all required aircraft and ATD kit deliveries and prototype modifications and all T-6A aircraft and ATD kit deliveries and modifications.

The Contractor shall identify and maintain a single point of contact, PM, for all tasks required for the program. The PM shall be responsible and shall have authority for the control and coordination of all work performed under this contract.

The Contractor shall ensure the USG is provided unlimited access to the Contractor’s T-6A ARP work areas provided by the USG any time work is being performed.

The Contractor shall establish and maintain sufficient resources to support financial control, risk management, aircraft, and training device modification/production throughout the period of performance of the T-6A ARP.

The Contractor shall establish and maintain effective working relationships with the T-6A Program Office (PO), T-6A Ground Based Training Systems (GBTS) PO, and the OEM of the components being installed.

The Contractor shall provide Associate Contractor Agreements (ACA) or subcontracting arrangements for OEMs Textron Aviation Defense and Flight Safety International, and component vendors: Pratt and Whitney, Chelton, Extant Aerospace, Cobham, Honeywell, L3 Harris, General Electric (GE), Scientific Research Corporation (SRC) and ATD CLS contractor:

Delaware Resource Group (DRG) as needed for successful performance through final aircraft and ATD installation, and to meet scheduled contract deliveries/milestones.

The Contractor’s T-6A ARP design solution shall comply with applicable federal, state, local, foreign, and international Environmental and Occupational Safety and Health (EOSH) laws and regulations. Aircraft support requirements will comply with Air Force Occupational, Safety and Health (AFOSH) Standards. The Contractor shall be responsible for the safety and accountability of all its employees. The Contractor shall complete all work tasks IAW contract terms and conditions while complying with the safety program, host base safety requirements, Environmental Protective Agency (EPA) instructions and Occupational Safety and Health Administration (OSHA) Public Law 91-596 and OSHA 29 CFR.

Contractor employees shall identify themselves as Contractor personnel and display distinguishing badges or other visible identification at all times. Contractor personnel shall appropriately identify themselves as Contractor employees in conversations, formal and informal written correspondence, teleconferences, video teleconferences, faxes, and/or other electronic communication whether with Government personnel, other contractor personnel, or with the public when supporting this contract where their status as contractor employees might not otherwise be apparent or where they might be mistaken for civil service employees or military personnel.

The Contractor personnel shall wear distinctive attire which distinguishes the company from the government employees. During winter months when contractors are wearing cold weather gear (if applicable), contractor employees should be easily identifiable for security purposes.

The Contractor shall initiate all contract changes via a contract change proposal IAW CDRL A007, DI-ADMN-81401C/T, Contract Change Proposals and FAR 52.243-1, Changes - Fixed Price.

3.1.1 Program Management Plan (Aircraft and ATDs)

The Contractor shall prepare a Program Management Plan (PMP) that coordinates all activities related to this SOW to ensure successful completion. It is incumbent upon the Contractor to coordinate all internal events and cooperate fully with USG personnel. The PMP shall be presented to the USG for review and approval, and shall illustrate an overall accomplishment plan, allocating responsibilities, and identifying interdependencies and agreements with all parties involved to systematically accomplish the SOW effort. This initial plan will serve as the basis for this work effort, providing a reference to track progress thereby giving the Contractor’s PM a way to measure program accomplishments and delays. The Contractor shall plan, organize, manage, and control configuration management efforts to meet project objectives and document the results. All schedule, management, engineering, configuration, and development issues shall be coordinated and reported to the USG IAW CDRL A039, DI-MGMT-81797, Program Management Plan.

3.1.2 Program Management Contingencies (Aircraft and ATDs)

From time to time, the Government may decide or be forced to close all or part of the Government installation in response to an unforeseen emergency or other occurrence such as a furlough.

Sample emergencies include, but are not limited to, adverse weather such as snow or flood, an act of God such as a tornado or earthquake, or a base disaster such as a natural gas leak or fire.

The Contractor shall be officially dismissed upon notification of closure by the COR or designated USG representative. The Contractor shall promptly secure all GFP appropriately and evacuate in an expedient but safe manner.

3.1.2.1 Emergency Procedures

Contractor employees shall follow the direction of Government employees in regard to emergency procedures, i.e., fire, tornado, active shooter, bomb threats. It shall be the responsibility of the Contractor to provide guidance and establish procedures for responding to emergencies for their employees. The Contractor shall account for their employees following an emergency situation.

Contractor employees shall participate with Government personnel in all fire and tornado drills.

3.1.2.2 Mission Essential Services

The Contractor shall prepare for the continuation of essential DoD services during crisis IAW DFARS Subpart 252.237-7023 “Continuation of Essential Contractor Services.” In a state of emergency, if the Government deems necessary, the Contractor shall continue to provide all services necessary to ensure mission accomplishment. IAW the SOW, the Contractor shall provide a written plan IAW DFARS 252.237-7024, “Notice of Continuation of Essential Contractor Services”. All ARP CFT personnel are considered Mission Essential at all USAF bases.

3.1.3 Special Requirements

3.1.3.1 Safety

The Contractor shall be responsible for the safety and accountability of all its employees. The Contractor shall complete all work tasks IAW contract terms and conditions while complying with the safety program, host base safety requirements, Environmental Protective Agency (EPA) instructions and Occupational Safety and Health Administration (OSHA) Public Law 91-596 and

OSHA 29 CFR 1910.

3.1.3.2 Contractor Tools and Personal Protective Equipment

The Contractor shall ensure each employee assigned to the program has proper tools and Personal Protective Equipment (PPE) common to the specialty of work they are expected to perform (e.g., safety shoes, work boots, safety glasses, ear plugs, goggles, welding gloves, chemical resistant gloves, cut gloves, face shields, hard hats, jackets, booties, coveralls and foul weather gear). All of the items listed above, where applicable, shall be required to be a part of employees required tool list in Contractor’s SOPs. PPE must meet or exceed standards in OSHA

29 CFR 1910.

3.2 Integrated Product Development (Aircraft and ATDs)

To facilitate management of the T-6A ARP, the Contractor’s program team shall be organized into Integrated Product Teams (IPTs), each responsible for specific elements of product development, deployment, and support. The Contractor’s IPTs shall jointly develop, maintain, and use a

Contractor Integrated Master Schedule (IMS) that is completely integrated with the IMP and SOW.

The IMS shall follow the guidance in the DoD IMP and IMS Preparation and Use Guide, Version 0.9, dated 21 October 2005, and Format 6 of DI-MGMT-81861C IAW CDRL A008, DI-MGMT- 81861C, Integrated Program Management Data and Analysis Report.

3.2.1 Integrated Master Plan (Aircraft and ATDs)

The Contractor shall update and maintain the Integrated Master Plan…