AG-GPS Draft SOW 5 Feb.pdf

C-130H2

Next Generation (NEXTGEN) Agricultural Global Positioning System (AG-GPS)

STATEMENT OF WORK (SOW)

PR# : TBD

Prepared by

AFLCMC/WLNC

Air Force Life Cycle Management Center

Warner Robins Air Logistics Complex

235 Byron St, Suite 19A

Robins AFB, GA 31098-1670

DISTRIBUTION STATEMENT C. Distribution authorized to U.S. Government

Agencies and their contractors (Critical Technology) (2019-03-06). Other requests for this document shall be referred to (AFLCMC/WLN).

TYPE DESCRIPTION PAGE/PARA DATE

Base Base Document N/A 7 Feb 2020

Contents

1.0 GENERAL

1.1 SCOPE

1.2 BACKGROUND

2.0 GENERAL REQUIREMENTS

2.1 AIRCRAFT SURVEYS

2.2 GENERAL DESIGN

2.3 TRIAL KIT INSTALLATION (TKI) AND VERIFICATION KIT INSTALL (VKI)

2.4 GROUND AND FLIGHT TEST

3.0 INTEGRATION DESIGN AND ANALYSIS REQUIREMENTS

3.1 DESIGN REQUIREMENTS

3.2 ANALYSIS AND DATA REQUIREMENTS

3.2.1 Modification Airworthiness Certification Criteria (MACC) Certification Basis

3.2.2 MACC Compliance Report

3.2.3 Electrical Load Analysis (ELA)

3.2.4 Stress Analysis

3.2.5 Weight and Balance

3.2.6 Safety Assessment Report (SAR)

3.2.7 Interface Control Documents (ICD)

4.0 PROGRAM MANAGEMENT

4.1 MONTHLY STATUS REPORTS

4.2 INTEGRATED MASTER SCHEDULE

4.3 PROGRAM MANAGEMENT REVIEWS AND MEETINGS

4.3.1 Kick Off Meeting

4.3.2 Preliminary Design Review (PDR)

4.3.3 Critical Design Review (CDR)

4.3.4 Test Readiness Review (TRR)

4.3.5 Technical Interchange Meetings (TIM)

5.0 ENGINEERING DATA

5.1 ENGINEERING DATA GUIDANCE CONFERENCE

5.2 IN-PROCESS REVIEW (IPR) OF THE TDP

5.3 RELATIONSHIP OF CONTRACTOR WITH SUBCONTRACTORS/VENDORS

5.4 ENGINEERING DATA UPDATES AND REVISIONS

5.5 ENGINEERING AND DESIGN

5.6 ENGINEERING DESIGN STRIP LIST

6.0 KITS AND SCHEDULE

6.1 KIT COMPOSITION

6.2 KIT DELIVERY SCHEDULE

6.3 KIT INSPECTION/ACCEPTANCE

6.4 KIT INSTALLATIONS

6.5 KIT STORAGE AND TRANSPORTATION

7.0 CONFIGURATION AND DATA MANAGEMENT

8.0 IDENTIFICATION PLATES AND MARKINGS

9.0 TESTING

9.1 TRIAL INSTALLATION KITS TESTS

9.2 ELECTROMAGNETIC TESTS

9.2.1. Electromagnetic Interference

9.3 EXPLOSIVE ATMOSPHERE TEST

9.4 GROUND ACCEPTANCE TEST

9.5 GROUND /FLIGHT TESTING

9.6 TEST PLAN WORKING GROUPS (TPWG)

9.7 TEST AND SUPPORT EQUIPMENT (TE & SE)

9.8 GOVERNMENT SUPPORT FOR TEST

10.0 LOGISTICS

10.1 PROVISIONING TECHNICAL DOCUMENTATION

10.2 SUPPORT EQUIPMENT AND SPECIAL TOOLS

10.3 TECHNICAL PUBLICATIONS

10.4 TO DELIVERY

11.0 QUALITY CONTROL

12.0 DELIVERABLES

13.0 TRAVEL

14.0 AGENCY AFFIRMATIVE PROCUREMENT PROGRAM (AAPP) AND GREEN

PROCUREMENT PROGRAM (GPP)

15.0 CLASSIFICATION AND POSITION SENSITIVITY DESIGNATION

16.0 SYSTEM SECURITY ENGINEERING

16.1 SUPPLY CHAIN RISK MANAGEMENT (SCRM)

16.2 COUNTERFEIT PREVENTION

16.3 COUNTERFEIT PREVENTION ACTIVITIES

17.0 PROCEDURES FOR INVOICING/PAYMENTS/ACCEPTANCE

18.0 APPENDICES

APPENDIX A APPLICABLE DOCUMENTS

APPENDIX B CONTRACTOR DELIVERABLES

APPENDIX D AG-GPS A-KIT PARTS AND MATERIALS

1.0 General

1.1 Scope

The purpose of this SOW is to guide the integration design efforts, technical data development, kit build, qualification testing, and delivery of twenty-five (25) Next

Generation (NEXTGEN) Agricultural Global Positioning System (AG-GPS) kits for C-

130H2 aircraft located at the 910th Airlift Wing (910th AW), Youngstown Air Reserve

Station (ARS), OH. The new system shall replace the existing (legacy) Wingman GPS and utilize a similar interface with the aircraft. The NEXTGEN AG-GPS needs to be procured to ensure the unit can continue its public health pesticide application mission while meeting EPA requirements for ensuring precision targeting of applied chemicals, preventing over-spray and accurately recording and providing a permanent record of where pesticides were applied.

1.2 Background

The legacy Wingman GPS currently in-use on spray-modified C-130H2 aircraft at the

910th Airlift Wing (910 AW) has become obsolete. Therefore, the Government has established the requirement for select C-130H2 aircraft to be modified with the AG-GPS.

The major components for each AG-GPS are listed below:

Nomenclature CAGE Part No NSN

AG NAV GUIA Platinum

Console(Qty 2)

L6463 AAP771-J N/A

(COTS)

AG NAV P887 Internal

Lightbars (Qty 2)

L6463 AAP887-A N/A

(COTS)

P500 GPS Receiver 5HZ

SBAS/Glonasstype 03

L6463 AAP500-

A5-03

N/A

(COTS)

GPS Antenna L6463 MO0602 N/A

(COTS)

Pressurized Hatch (for antenna)

N/A N/A TBD

Harnesses, mounting/installation hardware, cables, documentation, etc

L6463 TBD TBD

2.0 General Requirements

2.1 Aircraft Surveys

The Contractor shall perform an aircraft survey at Youngstown ARS, OH no later than 30 days after contract award. The Contractor shall document all key technical details pertaining to removal of the legacy Wingman GPS and the subsequent integration/installation of the Ag-GPS with an Aircraft Survey Report. [CDRL A001, Technical Report –Study/Services (Aircraft Survey), DI-MISC-80508B/T]

2.2 General Design

The Contractor shall perform non-recurring engineering (NRE) required to remove the existing Wingman GPS and design Group A hardware required to integrate the new AG-

GPS into the C-130H2 aircraft. The Contractor shall develop engineering drawings and technical data required to procure, install, operate, and maintain the AG-GPS. This data shall include the removal of the existing Wingman GPS.

2.3 Trial Kit Installation (TKI) and Verification Kit Install (VKI)

The Contractor shall develop a prototype kit and perform qualification testing required to support United States Air Force (USAF) air worthiness requirements. The Contractor shall provide the kit, draft TCTO, personnel and tools required to perform the prototype

TKI. The contractor shall also provide on-site engineering support for the TKI. For

VKI, the contractor shall provide the kit and TCTO while the 910th Airlift Wing will provide the personnel and tools. The Contractor shall be responsible for producing and documenting a design that shall satisfy all of the SOW requirements. The Contractor shall resolve any deficiencies in the kit, installation, and/or technical data resulting from

TKI, prototype testing, and VKI.

2.4 Ground and Flight Test

The contractor shall develop test procedures required to demonstrate successful integration design, and will also support the USAF test team with development and execution of ground and flight tests. Test support shall include Ground and Flight testing for certification of the AG-GPS to fly on select C-130H2 aircraft. Testing is anticipated to occur immediately following successful TKI. The Contractor shall provide engineering support to the Government for test planning and test data analysis during

Government Test and Evaluation (T&E). Contractor shall support all integration and lab testing, ATPs, etc as defined in para 9.0 below.

2.5 Kit Deliveries

Upon successful prototype kit installation, testing, and Government approval, the contractor shall build and deliver the remaining production kits to the 910th AW at

Youngstown ARS, OH. 910th AW personnel will be responsible for installation and checkout of the remaining production kits.

3.0 Integration Design and Analysis Requirements

3.1 Design Requirements

1. The AG-GPS system integration design shall be in accordance with SAE

ARP1870A. All AG-GPS equipment shall be electrically bonded and grounded to the aircraft ground plane in accordance with SAE ARP1870A, and as indicated in

Sections 5.11 and 5.12 of MILSTD-464C.

2. System displays and light bars shall be NVG compatible and shall not degrade the ability to operate at night with NVGs.

3. The AG-GPS system shall interface with the aircraft “SPRAY ON” indication circuitry in order to provide spray status indication on the AG-GPS displays.

Depending on AG-GPS system attributes, an aircraft modification may be required to enable this functionality. Aircraft system technical data/diagrams will be made available to the contractor.

4. The AG-GPS system shall be compatible with and derive all required power from existing aircraft power busses (115 VAC / 400 Hz and/or 28 VDC).

a. The AG-GPS system shall perform normally, remain safe, and not suffer damage when provided with 28 VDC and/or 115 VAC / 400 Hz power meeting the Normal, Abnormal, and Transfer requirements of MIL-STD-

704F. Note, the performance of equipment is permitted to deviate from normal operation, such as light flicker, during abnormal and transfer power quality scenarios.

b. The AG-GPS system shall not be damaged and will remain safe when exposed to Emergency and Failure power requirements of MIL-STD-

704F.

5. The AG-GPS system design shall provide circuit breaker protection, and breaker(s) shall be located on the aircraft circuit breaker panels on the flight deck.

6. The AG-GPS system shall utilize existing legacy Wingman GPS system component locations to the maximum extent practical, to include (but not limited

to) circuit breakers, light bars, displays, and GPS receiver(s).

7. The new AG-GPS light bars, when mounted, must be the same (or lower) height dimension as legacy light bars. The new AG-GPS light bars shall not impede into pilot vision any more than existing legacy light bars.

a. The new AG-GPS antenna shall be mounted on a qualified C-130H hatch rated for aircraft pressurization.

b. The new AG-GPS displays shall be integrated to utilize existing RAM display mount provisions at copilot and navigator positions.

c. The new AG-GPS displays, lightbars, and hatch-mounted antennas shall be integrated to facilitate easy removal and replacement for maintenance and to enable relocation of components to other aircraft.

d. The design shall not affect egress capability of the aircrew from the aircraft.

8. The design shall permit interfacing with the C-130H aircraft both mechanically and electrically so as not to interfere with or degrade the existing aircraft systems or jeopardize the aircraft’s ability to operate safely within its performance envelope. The system shall consider the design and installation criteria for Human

Engineering requirements of MIL-STD-1472F.

9. All AG-GPS electrical and electronic installations shall conform to MIL-STD-

7080, SAE-AS8700, and applicable Sections 5.2, 5.3, 5.5, 5.7, 5.8, and 5.10 of

MIL-STD-464C.

10. The AG-GPS wiring and installation shall conform to TO 1-1A-14 and SAE-

AS50881. No Polyvinyl Chloride (PVC) jacketed wiring shall be permitted in the design. If PVC wiring, or any unknown wire insulation types, are required to be used, they shall be identified, brought to US Government attention, and reviewed for impact to aircrew safety.

11. The AG-GPS system shall neither be a source nor susceptible to conducted or radiated electromagnetic energy in its intended aircraft electromagnetic environment in accordance with MIL-STD-464C section 5.7.

12. The AG-GPS light bars will be wired in parallel (repeaters) such that the same information is simultaneously displayed for the pilot and copilot positions.

13. The contractor shall remove legacy Wingman GPS system components to include, but not limited to, light bars, displays, processor, receiver, circuit breakers, wiring, hardware/mounts, etc. The legacy system components/information shall also be removed from existing USAF TOs.

14. Parts and Materials:

a. Whenever materials and/or parts are required as a design utilization to satisfy this SOW, military specification parts requirements shall be used unless otherwise explicitly required within. “AN” and “MS” parts shall be used to the maximum extent possible provided they do not compromise design integrity. Electrical parts shall be selected and installed in accordance with MIL-STD-7080.

b. Commercial utility parts, such as nuts, bolts, cotter pins, etc., having suitable properties may be used provided the parts used can be replaced directly with “AN”, “NAS”, “MIL”, or “MS” parts and providing further that the applicable assembly drawings cross-reference the commercial part to the corresponding standard part number.

c. When non-standard parts and/or materials are required, parts and/or materials shall be selected which will not compromise design integrity and that are acceptable for aircraft use. Authority for such non-standard parts and/or material shall be requested through the Procuring Activity with the submittal of such data as fabrication drawings, purchase control specifications, etc., that may be used to evaluate such a request. Upon approval for use, such non-standard parts and/or materials shall be identified on the applicable assembly drawing parts and/or materials lists and shall not be proprietary.

3.2 Analysis and Data Requirements

3.2.1 Modification Airworthiness Certification Criteria (MACC)

Certification Basis

The Contractor shall update the MACC Certification Basis as required. The

MACC Certification Basis shall document which airworthiness criteria are applicable for this modification. For applicable criteria, the MACC Certification

Basis shall document the standard and method of compliance. For non-applicable criteria, the MACC shall document rationale for non-applicability. The MACC

Certification Basis shall be IAW MIL-HDBK-516C and due at PDR. [CDRL

A002, Airworthiness Specification, DI-SESS-81766]

3.2.2 MACC Compliance Report

The Contractor shall generate a MACC compliance report. Delivery of reports and certifications resulting from the airworthiness certifications, ground testing, initial and production installation engineering support, and flight test engineering support shall be IAW MIL-HDBK-516C. The initial submission shall be due 30 days after CDR. The final submission shall be due 45 days after the completion of Flight Tests and include the results from the Flight Tests. [CDRL A003, Airworthiness Certification Criteria Report, DI-SESS-81768]

3.2.3 Electrical Load Analysis (ELA)

The Contractor shall perform and document an ELA of the AG-GPS and its electrical demand on aircraft power in typical modes of operation. Typically, the

ELA shall meet the requirements of MIL-E-7016F. However, in this case the contractor should tailor this requirement and develop a “delta” analysis to identify removed loads of the legacy Wingman GPS, the new loads of the AG-GPS, and the net change in loading. This initial data shall be summarized and presented at the PDR, and subsequently presented at CDR for final Government concurrence.

The ELA shall be submitted to the Government for review 30 days prior to CDR.

[CDRL A004, Scientific and Technical Reports (Electrical Load Analysis), DI-MISC-80711A]

3.2.4 Stress Analysis

The Contractor shall conduct a stress analysis on fixed and removable equipment attachment points and any modified aircraft structure. The modified aircraft structure and system installation shall be analyzed to have a positive margin of safety for an ultimate load that is at a minimum 1.5 times the limit load. If limit load is determined from models or analysis that isn’t validated by test, the margin of safety shall be a minimum of 0.25. The following load factors shall apply in the stress analysis:

Longitudinal - 9.0g's forward, and 1.5g's aft; Lateral - 1.5g's right and left;

Vertical - 4.5g's down and 2.0g's up. [CDRL A005, Scientific and Technical

Reports (Stress Analysis), DI-MISC-80711A]

3.2.5 Weight and Balance

The Contractor shall develop and provide updated weight and balance data for the

AG-GPS system installation. The Weight and Balance analysis shall conform to

TO 1-1B-50. In the event that the Weight and Balance Check reveals that the center of gravity exceeds prescribed limits, action shall be taken by the Contractor to bring the center of gravity within limits for all flight conditions for the baseline

C-130H2 aircraft. Ballast shall not be used to correct out-of-limit center of gravity. [CDRL A006, Sample Chart A and Chart E Report for Aircraft, DI-

MGMT-81502A]

3.2.6 Safety Assessment Report (SAR)

System safety shall be assured by the Contractor. System safety hazards shall be identified and reported to the C-130H System Program Office (SPO) Program

Manager, AFLCMC/WLNCC. Compliance with MIL-STD-882D is required and hazard reporting shall occur at the PDR and CDR. Hazards which may cause adverse effects on aircraft or personnel during system operation, test, maintenance, and training, shall be eliminated or controlled. The Contractor shall generate a SAR for the design effort for integration, installation, and operation of the AG-GPS system on C-130H aircraft. [CDRL A007, Safety Assessment

Report (SAR), DI-SAFT-80102C]

3.2.7 Interface Control Documents (ICD)

The Contractor shall modify, integrate, test, document, deliver and support the

AG-GPS solution on C-130H2 aircraft. The Contractor shall provide the necessary documentation to show the functional and physical characteristics of the system. The Contractor shall provide the required interface control documents

(ICDs) to enable the installation, integration and operation of the modification and installation kit on the aircraft. The Contractor shall produce an aircraft installation ICDs for the final system solution. [CDRL A008, Interface Control

Document, DI-SESS-81248B]

4.0 Program Management

The scope of this effort shall include all requirements necessary for the management of the contract. The Contractor shall maintain an appropriate management team to assure fulfillment of the requirements of the SOW. This team shall be responsible for the overall planning, coordination, execution, monitoring, and reporting of all requirements. A

Program Manager (PM) shall be designated by the Contractor and be responsible for the coordination of all SOW-required activities and will act as the focal point for all coordination with personnel at AFLCMC/WLN. These efforts shall be maintained by the

Contractor in order to assure the managerial performance within the overall effort is clearly identified and understood between the Government and the Contractor. The

Contractor shall be responsible for planning, implementing, monitoring, and reporting the program activities detailed within this SOW. Quarterly Program Management Reviews

(PMRs) shall convene at either Robins AFB, GA, or the Contractor’s facility, as agreed upon by the Government Procurement Contracting Officer (PCO) and Contractor, to discuss program issues. The Contractor shall provide an agenda and develop and distribute minutes from all PMRs. [CDRL A009, Conference Agenda, DI-ADMN-

81249B; CDRL A010, Conference Minutes, DI-ADMN-81250B]

4.1 Monthly Status Reports

The Contractor shall provide a Monthly Status Report (MSR) detailing progress to-date and any obstacles in meeting the delivery schedule. The Contractor shall submit MSRs for the duration of this contract. These reports shall be submitted monthly, with the initial report due after the first full month from the contract award date. The status reports shall include the status of tasks, milestones (achieved and upcoming), man hours and material expenditures during the reporting period, with the overall total to-date. [CDRL A011, Status Report, DI-MGMT-80368A/T]

4.2 Integrated Master Schedule

In addition, the Contractor shall develop and deliver a preliminary Integrated Master

Schedule (IMS) to the Government within 15 days prior to the Kickoff Meeting. A detailed IMS shall be provided in a Microsoft Project 2007 compatible format, unless otherwise directed by the Government in the CDRL. The IMS shall be updated upon mutual agreement between the Contractor and the Government to account for any significant shift in the program delivery schedule. [CDRL A012, Integrated Program

Management Report (IPMR), DI-MGMT-81861A]

4.3 Program Management Reviews and Meetings

Program Management Reviews shall be conducted quarterly after the kick-off meeting in order to inform the Government of current program status. The Contractor shall conduct/support and/or host reviews and audits at major points in the program to ensure program activity is progressing sufficiently. The Contractor shall prepare agenda, presentation materials, and prepare and distribute minutes after each review or meeting described in this section. The reviews or meetings shall be held at Robins AFB, GA, or the Contractor’s facility, as agreed upon by the Government PCO and Contractor. The

Contractor shall be required to conduct reviews on short notice when the Government determines a priority situation requires a program review. Reviews shall be conducted jointly (when feasible) and per the IMS to minimize participant travel events. [CDRL

A009, Conference Agenda, DI-ADMN-81249B; CDRL A010, Conference Minutes, DI-ADMN-81250B, CDRL A013, Presentation Materials, DI-ADMN-81373]

4.3.1 Kick Off Meeting

A kick-off meeting shall be hosted by the Contractor and shall be held at a site and on a date agreed upon by the Government contracting officer and the

Contractor no later than 15 working days after contract award. The purpose of the kick-off meeting is to review the basic contractual requirements and to provide necessary direction and guidance. The Contractor shall develop an agenda and a preliminary IMS with major program milestones for each task and submit it to the

Government no later than 5 days prior to the Kick-off Meeting. [CDRL A009, Conference Agenda, DI-ADMN-81249B; CDRL A010, Conference Minutes, DI-ADMN-81250B, CDRL A013, Presentation Materials, DI-ADMN-81373]

4.3.2 Preliminary Design Review (PDR)

PDR shall be held within three (3) months after contract award. The PDR shall be conducted to help ensure the preliminary design for the AG-GPS is sufficiently mature and ready to proceed into detailed design and can meet the stated performance requirements within program budget, schedule, risk, and other program and system constraints. The Contractor shall host a PDR for the AG-GPS at a site and on a date agreed upon by the USG Contracting officer and the

Contractor. After completing all technical research and developing a preliminary design approach, the Contractor shall present their preliminary design during this review. The PDR shall utilize engineering sketches, block diagrams, design concepts, and other informal documentation as necessary to allow key

Government personnel to examine the Contractor’s design approach for compliance with this specification. The PDR shall be held before the Contractor begins the detailed engineering process and develops the preliminary TDP. The

Contractor shall meet the entry and exit requirement criteria for PDR in accordance with the IEEE 15288.2-2014. The PDR shall be chaired by the USG

Program Manager or Assigned USG representative. The Contractor shall prepare all briefing materials associated with this review and prepare and distribute minutes for this meeting. The PDR shall be considered complete upon USG approval of the minutes and resolution of the action items. Action items may remain open with USG concurrence. [CDRL A009, Conference Agenda, DI-

ADMN-81249B; CDRL A010, Conference Minutes, DI-ADMN-81250B;

CDRL A013, Presentation Materials, DI-ADMN-81373; CDRL A014, Product Engineering Design Data and Associated Lists, DI-SESS-81000F/T]

4.3.3 Critical Design Review (CDR)

The CDR shall be hosted by the Contractor and held at a site on a date agreed upon by the USG Contracting Officer and the Contractor. CDR shall be held no later than six (6) months after contract award. The Contractor shall present their critical design during this review. The CDR shall present detailed design drawings and other documentation as necessary to allow key Government personnel to examine and approve or disapprove the Contractor’s design approach for compliance with this specification. The Contractor shall meet the entry and exit requirement criteria for CDR in accordance with the IEEE 15288.2. The CDR shall be chaired by the USG Representative Chair or USG Program Manager. The

Contractor shall prepare all briefing materials associated with this review and prepare and distribute minutes. CDR shall be considered complete upon USG approval of the minutes and resolution of the action items. Action Items may remain open with USG concurrence. [CDRL A009, Conference Agenda, DI-

ADMN-81249B; CDRL A010, Conference Minutes, DI-ADMN-81250B;

CDRL A013, Presentation Materials, DI-ADMN-81373; CDRL A014, Product Engineering Design Data and Associated Lists, DI-SESS-81000F/T]

4.3.4 Test Readiness Review (TRR)

The TRR shall be conducted 60 days prior Trial Kit Installation (TKI). TRR attendees shall include designated Government personnel, personnel scheduled to conduct the tests, and T&E IPT members. The TRR shall assess the program to ensure it is ready to proceed into formal test. The TRR shall assess test objectives, test methods and procedures, and the tests’ scope, to determine required test resources have been identified and coordinated to support planned tests. The TRR shall verify the traceability of planned tests to program requirements. The TRR shall determine the completeness of test procedures and their compliance with test plans and descriptions. [CDRL A009, Conference Agenda, DI-ADMN-81249B;

CDRL A010, Conference Minutes, DI-ADMN-81250B; CDRL A013, Presentation Materials, DI-ADMN-81373]

4.3.5 Technical Interchange Meetings (TIM)

The Contractor shall conduct TIMs which shall provide the USG with insight into the technical aspects of the program, and to support a forum to resolve technical issues. TIMs shall be held as required, and shall be co-chaired by the Contractor and the USG. The TIMs shall be hosted by the Contractor and shall be held at a site and on a date agreed upon by the USG contracting officer and the Contractor.

The Contractor shall prepare all presentation materials associated with these meetings and prepare and distribute minutes.

[CDRL A009, Conference Agenda, DI-ADMN-81249B; CDRL A010, Conference Minutes, DI-ADMN-81250B; CDRL A013, Presentation

Materials, DI-ADMN-81373]

5.0 Engineering Data

The contractor shall develop/produce/maintain and deliver a Technical Data Package

(TDP) that accurately depicts the final product. TDP data includes, but is not limited to, Computer Aided Design (CAD) data, CAD models, model based definition data sets, Gerber data and Master Bill of Materials (BOM). The TDP shall provide the necessary design, engineering, manufacturing, testing and quality assurance requirements information necessary to enable the procurement or manufacture of an interchangeable item that duplicates the physical and performance characteristics of the original product without additional design engineering effort or recourse to the original design activity or any third party.

The TDP shall represent the approved, tested, and accepted configuration of the defined delivered item(s). This shall include software and all test requirement documentation data required to test systems, subsystems and/or components. Vendor Item Control

Drawings shall be used to specify the requirements for purchased items when such items have been approved for use in the design and are used without alteration, selection or source qualification (testing of an item prior to procurement action to ensure that it satisfies the specified requirements). All engineering product definition data created using Government funding as a result of this contract shall be considered a part of the

TDP and shall be delivered to the Government with unlimited rights. The TDP shall be created IAW the following American Society of Mechanical Engineers (ASME) standards: ASME Y14.100-2017, Appendix B, sections B6 through B9.1 and Appendices

C, D, E, and F in conjunction with ASME Y14.24-2012, ASME Y14.34, ASME Y14.35 and ASME Y14.41 and as defined in the corresponding CDRL for this task to create and deliver Product Drawings Models and Associated Lists (Engineering Data) under this contract. Data set classification code marking IAW Appendix F of ASME Y14.100-2017 is required. CAD model file name and extension identification is required on drawing graphic sheets. TDP data shall specify parts marking requirements for item identification

IAW MIL-STD-130N, other applicable documents referenced therein, and as specified in this contract. Test Criteria for Electrical and Avionics Items shall be IAW document

9579777 Revision B (CAGE 98752) The TDP shall be delivered in accordance with Air

Force Product Data Specification drawing 9579776 Revision N (CAGE 98752), reference attached DD Form 1423 Block 16. [CDRL A014, Product Engineering Design Data and Associated Lists, DI-SESS-81000F/T] The contractor shall submit an engineering drawing tree identifying all system, subsystem and equipment drawings as part of the drawing package prior to CDR. [CDRL A015, Engineering Drawing Tree, DI-DRPR-

81961A]

5.1 Engineering Data Guidance Conference

Concurrent with the Kick-Off meeting, the contractor shall support and co-chair a

Guidance Conference with AFLCMC/LZPEM for engineering data. The contractor shall prepare an agenda and record the minutes of the Guidance Conference. The contractor shall address, discuss, and provide status on the following:

a. Understanding of all CDRL requirements, applicable DIDs, specifications and standards.

b. TDP review requirements and schedules.

c. TDP delivery requirements and schedules.

d. Contractor's drafting practices/procedures/TDP drawing formats/CAD programs.

e. The contractor's quality assurance procedures relating to TDP documents, including quality control of subcontractor and vendor data.

f. The role of subcontractors and vendors who may deliver TDP documents under this contract.

g. The contractor's configuration management system, including methods for releasing documents, approving documents, and incorporating changes into documents.

h. Digital Technical Data Package (TDP) deliverables.

[CDRL A009, Conference Agenda, DI-ADMN-81249B; CDRL A010, Conference Minutes, DI-ADMN-81250B

5.2 In-Process Review (IPR) of the TDP

The contractor shall host, support, and co-chair an IPR of the engineering drawings and associated lists and other documentation to be included in the TDP. The IPR shall be conducted only after the contractor's quality assurance personnel have completely reviewed the data and determined that data are of sufficient quality that Government time will be effectively utilized during the review. IPR may be scheduled when data has reached the 50% completion point and shall be held, when possible, in conjunction with other reviews (i.e., PDR, CDR). Concurrent with the IPR, the contractor shall submit four

(4) representative samples of each digital data format of data for this project in accordance with Air Force drawing 9579776 (CAGE 98752), These shall consist of the

Native, Neutral, Word Searchable PDF, HPGL, Metadata Spreadsheet, BOM, Gerber

Data, and Software/memory Device Data. The contractor shall notify AFLCMC/LZPEM a minimum of 30 days prior to the anticipated date of completion point. The IPR shall focus on the contractor's progress in the preparation of the TDP. The contractor shall support and provide the necessary resources, i.e., meeting agenda, conference room, applicable data, minutes, and appropriate personnel available to answer any questions to perform the IPR effectively. The contractor shall correct all discrepancies identified in the IPR. All subcontractor/vendor data shall be made available for review. If the quantity of subcontractor/vendor data is of sufficient magnitude, the Government may schedule a separate IPR at the subcontractor's/vendor's facility. [CDRL A009, Conference Agenda, DI-ADMN-81249B; CDRL A010, Conference Minutes, DI-

ADMN-81250B; CDRL A013, Presentation Materials, DI-ADMN-81373; CDRL

A014, Product Engineering Design Data and Associated Lists, DI-SESS-81000F/T]

5.3 Relationship of Contractor with Subcontractors/Vendors

The contractor shall levy on sub-contractors and sub-vendors the same requirements for

Technical Data Packages (TDPs) as are levied on them by this contract. This requirement shall apply at all tiers of sub-contractor/vendor levels associated with the program.

5.4 Engineering Data Updates and Revisions

The contractor shall (and shall cause subcontractors and vendors to) update and maintain engineering data for the item(s) designed/ developed/modified/produced and funded by this contract for the life of this contract and shall incorporate all changes in accordance with the following:

a. All engineering changes shall be incorporated into the applicable engineering data within 90 days after engineering release/Air Force concurrence or at intervals of five changes, whichever occurs first, except a change involving safety, which shall be incorporated immediately.

b. All engineering changes shall be incorporated into the applicable engineering data prior to delivery of data for review.

c. All engineering changes shall be incorporated into the applicable engineering data prior to delivery of final media.

d. Revisions to existing engineering drawings/models and associated lists and other documentation to be included in the TDP for which the contractor is the current design activity shall result in the delivery of the entire revised document and associated data file. For example, when a portion of a document is revised the entire document shall be delivered. [CDRL A016, Request for Variance, DI-SESS-80640D]

5.5 Engineering and Design

The TDP shall contain the AG-GPS system components. All drawings, reports, and documentation associated with this program shall be captured and provided to the AFLCMC/WLNEA within a Data Accession List. [CDRL A017, Data

Accession List (DAL), DI-MGMT-81453B]

5.6 Engineering Design Strip List

The Contractor shall deliver a “strip list”, including structural, electrical, and mechanical hardware components associated with the removal of the existing system and integration of the new kits with the existing Group A. This list shall be reviewed during design reviews and verified during TKI. [CDRL A018, Technical Reports – Study/Services (Structural, Electrical, and Mechanical

Component Strip List), DI-MISC-80508B]

6.0 Kits and Schedule

The Contractor shall manufacture twenty-five (25) kits: One (1) kit to support the joint

Government/Contractor-performed TKI/Verification and twenty-four (24) production kits to be installed as required by government personnel.

6.1 Kit Composition

Each kit shall include all parts packaged for shipment and storage. Parts in each kit shall be marked with the noun, part number, and number of items, and then put in boxes and/or crates for shipment. Each kit shall be marked in accordance with MIL-STD-129P (3).

The kit shall be provided by the Contractor and, when combined with the existing on aircraft Group A hardware, shall allow the Government to install an operational AG-GPS system on select C-130H aircraft.

6.2 Kit Delivery Schedule

The TKI kit is required to be delivered no later than 6 months after contract award. Trial kit redlines that affect the production configuration shall be incorporated into the trial kit unit at the expense of the contractor. Initial delivery of 10 production kits shall occur

NLT 60 days after successful flight test with 5 kit deliveries required each 30 days thereafter. Early delivery of kits is encouraged.

[CDRL A012, Integrated Program Management Report (IPMR), DI-MGMT-

81861A]

6.3 Kit Inspection/Acceptance

Inspection will be accomplished by U.S. Government personnel upon delivery, and acceptance of the kits will be done by the owning unit’s Quality Assurance personnel and or WLNC Equipment Specialists at destination. Valid kit deficiencies shall be identified and notification provided to AFLCMC/WLNC within 24 hours. Resolution to kit deficiencies shall be provided within 72 hours of notification.

6.4 Kit Installations

The contractor shall install the prototype kit, and will deliver subsequent production kits for Government installation. The Contractor shall provide a Time Compliance Technical

Order (TCTO) to the Government 60 days prior to TKI detailing specific installation instructions. The TCTO, kits, and tech data shall be delivered in accordance with TM-

86-01Q (reference CDRL A022.) Updates shall be made to the technical manuals identified in the TMCR. [CDRL A019, Technical Manual Contract Requirements

(TMCR), TMCR TM-86-01Q]

910th AW personnel will be responsible for completing pre-and post-modification aircraft systems tests, as well as operationally checking any additional systems that may be disturbed during the installation of the AG-GPS. The contractor shall be responsible for troubleshooting and repair of any systems damaged as a result of the AG-GPS TKI.

The contractor shall demonstrate and utilize a robust tool control program during the installation of the prototype AG-GPS. Tools and materials will be tracked and inventoried daily. In the event of a lost tool, the contractor shall notify 910th AW Quality

Assurance (QA) representatives immediately.

910th AW QA representatives, as well as, 910th AW technicians and Government personnel, will be present during the prototype installation to perform in process inspections and monitor installation progress.

6.5 Kit Storage and Transportation

The Contractor shall package, store, and ship all kits. Using MIL-STD-2073-1E as guidance, the Contractor shall ensure packing and preservation methods are utilized to protect material/items against corrosion, physical and mechanical damage, and other forms of degradation during storage, handling, and shipment and ensure all items arrive at the destination corrosion free in a safe and undamaged condition. Overnight shipping is not required. Packaged kits shall be kept in a dedicated bonded storage area provided by the Contractor in preparation for shipment. All shipments shall be documented on a

DD Form 250 and entered into Wide Area Workflow. Early delivery of production kits is encouraged and can be authorized and approved by the Government PCO at the request of the Contractor.

7.0 Configuration and Data Management

The Contractor shall perform configuration and data management in accordance with the

Contractor’s established configuration and data management processes assuring systematic evaluation, coordination, authorization, change control, and implementation for configuration control for the C-130H AG-GPS system. The Contractor may use EIA-

649 as a guide to perform the following tasks:

a. Update as necessary the functional and physical characteristics of all Group A and

B hardware.

b. Establish and maintain a Configuration/Data Management Plan that employs company standard configuration and data management control processes that are

ISO-9001 compliant.

c. Monitor the subcontractors by conducting audits.

d. Maintain an effective configuration change control system.

e. Report and maintain configuration status accounting and change processing information.

f. Maintain an engineering release system and document release records in accordance with the approved Configuration/Data Management Plan.

8.0 Identification Plates and Markings

The Contractor shall ensure each major component or sub-assembly costing $5,000.00 or more shall have a permanent part number marked in accordance with MIL-STD-130N and comply with Item Unique Identification (IUID) requirements of the contract.

[CDRL A020, Unique Identification (IUID) Marking and Verification Report, DI-

MGMT-81858]

9.0 Testing

The Contractor shall plan, develop, and conduct factory and aircraft ground tests (and support flight tests) for the AG-GPS on the C-130H2. Aircraft level testing shall be accomplished at the aircraft modification location, Youngstown ARS, OH. Laboratory testing will be accomplished at a site designated by the contractor.

9.1 Trial installation Kits Tests

Trial installation tests includes testing which the contractor will conduct to satisfy the elements Safety of flight, functional installation and performance. The contractor shall develop Test Plans, Procedures and Reports, which verifies these elements that include at a minimal:

(a) Electromagnetic Interference (EMI) Test

(b) Explosive Atmosphere Test

(c) Ground Acceptance Test

(d) Aircraft Flight Test

9.2 Electromagnetic Tests

9.2.1. Electromagnetic Interference

The NEXTGEN Ag-GPS shall be neither a source nor susceptible to conducted or radiated electromagnetic energy in its intended aircraft electromagnetic environment in accordance with MIL-STD-464C section 5.7. Electromagnetic

Interference (EMI) testing, or compliance thereof, shall be conducted by the contractor. EMI compliance of the system will be tested in accordance with the following MIL-STD-461 requirements: CE102, CS101, CS114, CS115, CS116, RE102, and RS103.[CDRL A021, EMI Test Plan, DI-NDTI-80566A; CDRL

A022; EMI Test Procedures, DI-NDTI-80603A; CDRL A023, EMI Test

Report, DI-QCIC-81891]

9.2.2 Electromagnetic Compatibility

The Ag-GPS shall not be upset nor interfere with other C-130H electrical and electronic systems, shall be compatible in the intended aircraft electromagnetic environment, and shall comply with MIL-STD- 464C section 5.7.

Electromagnetic Compatibility (EMC) tests will be performed by the Air Force and supported by the contractor. These tests will include ground and flight-testing to ensure the AG-GPS is neither a source nor victim of EMI in the operational environment.

9.3 Explosive Atmosphere Test

The AG Nav system components shall be designed such that no internal or external surface temperature reached shall cause ignition in an explosive atmosphere. This will be verified using MIL-STD-810 Method 511.7 procedure I or commercial equivalent.

[CDRL A024, Explosive Atmosphere Test Plan, DI-NDTI-80566A; CDRL A025;

Explosive Atmosphere Test Procedures, DI-NDTI-80603A; CDRL A026, Explosive

Atmosphere Test Report, DI-QCIC-81891]

9.4 Ground Acceptance Test

The contractor shall develop detailed Acceptance Test Plan (ATP) and Procedures, which shall address the system, design, and test requirements identified in this SOW. The ATP shall exercise the system installed on the aircraft to maximum extent possible on the ground. The acceptance test is conducted to demonstrate that the installation functions as designed and that the specified performance of the AG GPS components are achievable.

The Contractor shall perform acceptance test on the prototype kit at conclusion of the

TKI, with government attendance in providing aircraft operational support. The

Contractor shall request the government perform aircraft leak-down checks on the aircraft in accordance with TO 1C-130H-2-21JG-30-1 and applicable technical orders, prior to modification for baseline leak rate and after the completion of the modification to ensure no degradation. Results of the ground acceptance test shall documented for delivery to the government. [CDRL A027, Acceptance Test Plan (ATP), DI- NDTI-80566A;

CDRL A028, Acceptance Test Procedures, DI-NDTI-80603A; CDRL A029, Acceptance Test Report (ATR), DI-QCIC-81891]

9.5 Ground /Flight Testing

The Contractor shall be responsible for translating AG GPS operational system performance requirements into testable requirements. The contractor shall amend the ground acceptance test procedures with test requirements that requires fight to exercise.

The contractor is responsible for providing the flight test procedures that will be integrated into the government’s flight test plan procedures. The government is responsible for flight test planning, conducting and reporting. Contractor personnel will be physically present for the whole duration of Government flight testing to provide system knowledge, troubleshoot, and repair the system on a timely manner during qualification ground and flight tests.

The Government will accept the system based on test results from contractor-run ground acceptance testing and Government-run qualification ground and flight tests. The contractor is responsible to correct any discrepancies that fail any portion of the acceptance and qualification testing before system acceptance. [CDRL A030, Aircraft

Ground/flight Test Procedures, DI-NDTI-80603A]

9.6 Test Plan Working Groups (TPWG)

The Contractor shall host and co-chair with the Government, Test Plan Working Groups

(TPWGs) to address Contractor Test and Evaluation. The TPWG shall be held in conjunction with the PDR and CDR as a minimum. The TPWG will develop and document the factory, ground, and flight testing processes and procedures required to certify the AG-GPS system flight worthiness. [CDLR A009, Conference Agenda, DI-

ADMN-81249B; CDRL A010, Conference Minutes, DI-ADMN-81250B/T]

The Contractor will support Customer Review Boards (CRB), and government qualification test and evaluation (QT&E) for both ground and flight tests. QT&E of the

AG-GPS will be a tailored type of developmental testing/operational testing that will address applicable aspects of the AG-GPS operational suitability and effectiveness as a functional replacement.

9.7 Test and Support Equipment (TE & SE)

The Contractor’s engineering design and test requirements shall utilize, to the fullest extent practicable, non-peculiar test and support equipment. The Contractor shall design and develop ground checkout procedures that will be documented in the engineering data and technical manuals and verified during TKI. The contractor shall provide required test equipment for contractor led testing, as well as any TE and SE required to operationally check-out and/or maintain the system.

9.8 Government Support for Test

The Government will provide, as required, access to the TKI aircraft, 115 VAC 400/60Hz and 28VDC electrical power, airfield, range, flight crew, and testing permits or approval.

10.0 Logistics

10.1 Provisioning Technical Documentation

An initial provisioning guidance conference shall be held in conjunction with the Kick-Off meeting at a site and on a date agreed upon by the Government contracting officer and the

Contractor. The Contractor shall identify and recommend logical spare/repair parts sufficient to meet system/equipment operation and supportability. SAE GIEA-STD-0007A shall be used as a guide. Format must be consistent with existing Government Provisioning data system (D220). [CDRL A031, Logistics Product Data, DI-SESS-81758; CDRL A032, Logistics Product Data (LPD) Summaries, DI-SESS-81759/T; CDRL A033, Engineering Data for Provisioning (EDFP), DI-SESS-81874; CDRL A009, Conference Agenda, DI-ADMN-81249B; and CDRL A010, Conference Minutes, DI-

ADMN-81250B/T]

10.2 Support Equipment (SE) and Special Tools

As required, the Contractor shall submit Support Equipment Requirements Documents

(SERDs) for all new or modified organizational-level SE requirements. The Contractor shall generate a Logistics Management Information (LMI) Report and submit a separate

SERD for each unique piece of SE, tools, special tools, and all associated technical data.

MIL-HDBK-2097A shall be used as a guide. [CDRL A032, Logistics Product Data

(LPD) Summaries, DI-SESS-81759/T; CDRL A034, Maintenance Test -and Support

Equipment List, DI-SESS-80294B]

10.3 Technical Publications

The Contractor shall develop and deliver a new TCTO to document the configuration of this installation and all supporting technical manuals per the attached TM-86-01Q. The

TCTO and TOs governing the installation, use, and maintenance of the AG-GPS are supplied as required by TMCR TM-86-01Q and Air Force Material Command (AFMC)

Form 873.

The Government will provide the Contractor with certification and verification comments no later than 30 calendar days following TKI completion, in accordance with TM-86-01Q and Contractor/Government agreed upon dates in the IMS and the Technical Manual

Schedule and Status Report.

The Government will retain the right of approval of the final TOs through the in-process publication reviews, certification and verification process and the pre-publication review.

The Contractor shall submit data via hard copies and use of the Interactive Electronic

Technical Manual (IETM) tool. [CDRL A019, Technical Manual Contract

Requirements, TMCR TM-86-01Q; CDRL A012, Integrated Program Management

Report (IPMR), DI-MGMT-81861A]

10.4 TO Delivery

The Contractor shall deliver reproducible and verified Preliminary Technical Orders

(PTOs) for flight and maintenance manuals prior to TKI. The Contractor shall notify the

Government of any additional manuals discovered during the course of this development that require updating. [CDRL A019, Technical Manual Contract Requirements, TMCR TM-86-01Q; CDRL A012, Integrated Program Management Report

(IPMR), DI-MGMT-81861A]

11.0 Quality Control

The Contractor shall permit the Government to periodically access quality-related data and data-related records for the C-130H AG-GPS program. The Government has the right to request corrective action if the Contractor’s quality system fails to meet objectives.

The Contractor shall assure quality through implementation of a quality effort using MIL-

HDBK-896 as a guide. The Contractor is responsible for the performance of all design reviews and inspection requirements as specified herein. The Government reserves the right to perform any informal design review and/or inspection where such reviews and inspections are deemed by the Government as necessary to assure supplies and services conform to all contract specifications.

12.0 Deliverables

Per Department of Defense (DOD) policy, the Contractor shall provide all data deliverables via “paperless” electronic or digital deliveries. Status Reports and Trip

Reports shall be submitted by email. Other documents shall be submitted on disk or as email attachments in a Microsoft Office 2016® compatible format, unless otherwise directed by the Government in the CDRL.

13.0 Travel

The Contractor will be required to travel during the performance of some of the work described within this SOW. The number of trips and personnel traveling shall be limited to the minimum required to accomplish work assignments in accordance with the assigned tasks. Travel will be reimbursed according to the rates outlined in the Federal

Travel Regulations for travel within the CONUS and the Joint Travel Regulations (JTR).

The applicable rates shall be those in effect at the time of travel, and shall be subject to the limitations outlined in FAR Part 31. All Contractor travel, when required, shall require prior written approval of the Government PCO and PM 15 days prior to costs being incurred.