RFP_Attachment_11_T38_TRIM_PCIII_SOW_05Nov18.pdf

Solicitation Number: FA8220-19-R-0001

STATEMENT OF WORK

(SOW)

For:

T-38 Fuselage Structural Modification Kit Integration

Pacer Classic III (PCIII) Phase III and Talon Repair Inspection and Maintenance (TRIM)

Structural Modification Programs

5 November 2018

AFLCMC/WLDMA

AIR FORCE LIFE CYCLE MANAGEMENT CENTER

T-38 Program Office

Hill Air Force Base, Utah 84056 i

TABLE OF CONTENTS

RECORD OF REVISIONS ........................................................................................................ III LIST OF TABLES ...................................................................................................................... IV ACRONYMS AND ABBREVIATIONS ..................................................................................... V

1.0 DESCRIPTION

1.1 Scope

2.0 GENERAL INFORMATION

2.1 General Requirements

2.2 Programmatic Objectives and Goals

2.2.1 Management of Functional Expertise

2.3 Period of Performance (PoP)

3.0 SPECIFIC REQUIREMENTS

3.1 Modification Kits

3.2 Supplemental Kits

3.3 Item Unique Identification Requirements

3.4 First Article Test (FAT)

3.4.1 Qualifying Additional Sources

3.5 Packaging/Labeling

3.6 Deficiency Resolution

3.7 Monthly Status and Production Reports

3.8 Meetings

3.8.1 Weekly Technical Interchange Meetings (TIM)

3.8.2 Program Management Reviews (PMR)

3.8.3 Post Award Conference

3.8.4 Final Review

3.9 Integrated Master Plan/Integrated Master Schedule

3.10 Risk Mitigation

3.11 Schedule

3.11.1 Schedule Incentive for Accelerated Delivery

3.12 Operational Safety, Suitability, and Effectiveness

3.12.1 Critical Safety Items

ii

3.13 Travel

3.14 Data Compatibility

4.0 GOVERNMENT FURNISHED PROPERTY (GFP) AND SERVICES

4.1 T-38C Configuration Drawings Technical Data and Material/Equipment Provided

4.1.1 Configuration Drawings

4.1.2 Technical Data

4.1.3 Material/Equipment

4.2 Security and Access to Government Facilities and Equipment

4.2.1 Security Clearance

5.0 QUALITY CONTROL

5.1 Quality Assurance

5.1.1 Subcontractor Management

5.1.2 Quality Assurance Plan

5.1.3 Request for Variance

ATTACHMENT ONE: APPLICABLE CDRL LIST

ATTACHMENT TWO: APPLICABLE DOCUMENTS

ATTACHMENT THREE: BILL OF MATERIALS (BOM)

iii

RECORD OF REVISIONS

REV DATE PAGE(S)

AFFECTED

PARA.

AFFECTED REASON FOR REVISION

N/A N/A Original iv

LIST OF TABLES

Table 1 – PCIII Source Directed Parts Table 2 – TRIM Source Directed Parts v

ACRONYMS AND ABBREVIATIONS

ACC - Air Combat Command AETC - Air Education and Training Command AF - Air Force AFGSC - Air Force Global Strike Command AFMC - Air Force Materiel Command ASIP - Aircraft Structural Integrity Program BOM - Bill of Materials CDRL - Contract Data Requirements List CFS - Canted Fuselage Station CLIN - Contract Line Item Number CSI - Critical Safety Item DCMA - Defense Contracting Management Agency DID - Data Item Description DO - Delivery Order ESA - Engineering Source Authority FAT - First Article Test FS - Fuselage Station GFP - Government Furnished Property IMP - Integrated Master Plan IMS - Integrated Master Schedule IPT - Integrated Product Team IUID - Item Unique Identification MAPA - Mature and Proven Aircraft MAJCOM - Major Command MDS - Mission Design Series NGTS - Northrop Grumman Technical Services NLT - Not Later Than OSS&E - Operational Safety, Suitability, and Effectiveness PCIII - Pacer Classic III POC - Point of Contact PQDR - Product Quality Deficiency Report PN - Part Number PM - Program Manager PMP - Propulsion Modification Program PMR - Program Management Review PO - Program Office PoP - Period of Performance SOW - Statement of Work RFP - Request for Proposal SCC - Stress Corrosion Cracking SQS - Source Qualification Statement TCTO - Time Compliance Technical Order vi

TO - Technical Order TDP - Technical Data Package TIM - Technical Interchange Meeting TRIM - Talon Repair, Inspection, and Maintenance

1.0 DESCRIPTION

This SOW outlines the general requirements to support the T-38A/B/C structural modifications for the Pacer Classic III (PCIII) Phase III and Talon Repair, Inspection, and Maintenance (TRIM) programs.

The PCIII modification will help maintain Operational Safety, Suitability, and Effectiveness (OSS&E) throughout the currently projected lifetime of the T-38 aircraft (only applicable to a subset of the T-38C fleet). The PCIII requirement is the outcome of a T-38 structural sustainment evaluation. Air Education and Training Command (AETC) and the T-38 Program Office (PO) focused on removing and replacing key fuselage structural components on 180 T-38C aircraft which are analytically predicted to have the most fatigue damage. PCIII is the third major structural overhaul on the T-38 fuselage.

The TRIM modification will help maintain OSS&E throughout the currently projected lifetime of the T-38 aircraft. Extended service requirements and continued utilization of T-38A and AT- 38B aircraft have resulted in a need for depot-level maintenance augmentation. This subset of the T-38 fleet did not receive the benefit of repairs made during the Propulsion Modernization Program (PMP). Additionally, the current field-level approach to sustainment of T-38C aircraft not receiving the PCIII modification is insufficient to meet the needs of flying the T-38 to its currently projected retirement. The T-38 Aircraft Structural Integrity Program (ASIP) identified critical areas of these T-38A/B/C aircraft that need depot-level inspections, repairs, or part replacements to sustain them to meet Major Command (MAJCOM) requirements. The T-38 PO is working in conjunction with the AETC, Air Combat Command (ACC), Air Force Global Strike Command (AFGSC) and Air Force Materiel Command (AFMC) to address time-based degradation, specifically stress corrosion cracking (SCC), of critical structural items.

1.1 Scope

PCIII Phase III detailed in this SOW specifies the programmatic and technical activities required to accomplish the PCIII modification parts procurement, kit assembly, and necessary tasks to ensure procurement of the structural modification kits. These tasks are for the manufacturing and kitting of fuselage structural components for PCIII T-38C aircraft. PCIII has three distinct phases described as follows: Phase I – Sole-source to Northrop Grumman Technical Services (NGTS) (phase complete); Phase II – Competitive (small business set-aside) (phase in progress);

Phase III – Competitive (small business set-aside) will provide the remaining kits required to complete the PCIII requirement. The contractor shall provide kit integration, program management, logistics, discrepancy reporting/resolution, and subcontractor management for the life of the contract. Any additional phases would be executed as separate contractual efforts as deemed appropriate by the Government.

This SOW also specifies the programmatic and technical activities required to accomplish the T- 38 TRIM modification parts procurement, kit assembly, and necessary tasks to ensure procurement of the structural modification kits, to include the required fastener kits. These tasks are for the manufacturing and kitting of fuselage structural components and fasteners for TRIM on T-38A/B/C aircraft. TRIM effectivity applies to ACC’s 6 AT-38B aircraft, ACC’s/AFGSC’s

53 T-38A aircraft, 100 of AETC’s/AFMC’s T-38C aircraft and the Navy’s 10 T-38C aircraft.

TRIM kit procurement will include 59 kits specific to T-38A/B models, 110 kits specific to T- 38C models and up to 169 fastener kits necessary to install the above stated modification kits.

The Contractor shall provide the necessary integration of kits, program management, logistics, discrepancy reporting/resolution, and subcontractor management.

2.0 GENERAL INFORMATION

2.1 General Requirements

This SOW is intended to provide the structural modification kits for PCIII Phase III and modification kits for the TRIM effort as well as the program management and reporting necessary for the completion of the PCIII Phase III and TRIM structural modification kit integration.

2.2 Programmatic Objectives and Goals

PCIII Phase III will replace vital, fatigue-sensitive structural items including the following: steel dorsal longerons, upper cockpit longerons, and the upper/lower center longerons. In addition, associated bulkheads/formers, skins, floors, and fasteners will be included in this remove and replace effort.

TRIM is the solution for ensuring the structural service life of the T-38 fleet up to and beyond 2030. TRIM will replace vital, fatigue sensitive structural items with high susceptibility to SCC including the following: the upper/lower center longerons at FS 284 production break, wing attach bulkhead at FS 362, and the CFS 487 former. In addition, associated bulkheads, formers, attach angles, skins and support structure will be included in this remove and replace effort.

Furthermore, a variety of inspections and repairs will be made such as the bulkhead web repair at FS 388, former repairs at FS 394 and FS 400, and splice repairs to the lower cockpit longeron.

The Contractor shall perform the following integration functions: material procurement, manufacturing, kit assembly, delivery of kits, and deficiency reporting/remediation.

2.2.1 Management of Functional Expertise

Contractor shall retain a similar level of expertise and qualifications from positions involved with proposal submission through end of contract period of performance. For example, the engineering and programmatic functional expertise that provided interpretations of drawings and evaluation factors listed within the proposal shall be retained or replaced in a timely manner.

2.3 Period of Performance (PoP)

The basic Indefinite Delivery Indefinite Quantity (IDIQ) contract structure will consist of a five-year basic ordering period with an optional five-year ordering period, and will allow up to one year for deliveries after an order is placed. The total PoP for this contract shall not exceed 11 years total.

For the PCIII Phase III requirement, the PoP will be from contract award through the acceptance of the final modification kit. The PoP is anticipated as a three-year ordering period, with an additional one year for delivery after an order is placed. The total PoP for Phase III will span four years.

For the TRIM requirement, the PoP will be from contract award through the acceptance of the final modification kit. For TRIM, the PoP is anticipated as a 10-year ordering period, with an additional one year for delivery after an order is placed. The total PoP for TRIM will span 11 years.

3.0 SPECIFIC REQUIREMENTS

The Contractor shall be required to perform the requirements outlined in this SOW, subparagraphs 3.1 through 3.14, and the applicable Contract Data Requirements List (CDRL).

Contractor shall provide all deliverables listed in Attachment One. Delivery requirements can be found in DD Forms 1423-1.

3.1 Modification Kits

For PCIII Phase III: The Contractor shall provide complete parts and hardware kits as specified in the Bill of Materials (BOM), located in Attachment Three, and Technical Data Package (TDP), to include the Engineering Data List, attachments of the Request for Proposal (RFP). Parts and hardware shall comply with the specifications identified in the TDP. Nine part numbers, listed below in Table 1, are classified as Source Directed Parts and must be manufactured by a qualified/directed source. Source Qualification Statements (SQS) can be found in Attachment A of the TDPs. Defense Contract Management Agency (DCMA) inspection of these characteristics will be communicated upon award and the Contractor shall facilitate these inspections.

Table 1 – PCIII Source Directed Parts Part Number Part Name 110-1101-13* Upper (Cockpit) Longeron FS 144-284 LH 110-1101-14* Upper (Cockpit) Longeron FS 144-284 RH 3-11413-3* Steel Dorsal Longeron, FS 284-445, LH 3-11413-4* Steel Dorsal Longeron, FS 284-445, RH 2-11412-13 Upper (Center) Longeron, FS 284-325, LH 2-11412-14 Upper (Center) Longeron, FS 284-325, RH 2-11308-13 Lower (Center) Longeron, FS 284-325, LH 2-11308-14 Lower (Center) Longeron, FS 284-325, RH 3-11608-503 Former, CFS 487.223

*Northrop Grumman Source Directed Parts

For TRIM: The Contractor shall provide complete parts and hardware kits as specified in the BOM, located in Attachment Three and TDP. Parts and hardware shall comply with the specifications identified in the TDP. Six part numbers, listed below in Table 2, are classified as Source Directed Parts and must be manufactured by a qualified/directed source. Source Qualification Statements can be found in Attachment A of the TDPs. DCMA inspection of these characteristics will be communicated upon award and the Contractor shall facilitate these inspections.

Table 2 – TRIM Source Directed Parts Part Number Part Name

2-11412-13 Upper (Center) Longeron, FS 284-325, LH 2-11412-14 Upper (Center) Longeron, FS 284-325, RH 2-11308-13 Lower (Center) Longeron, FS 284-325, LH 2-11308-14 Lower (Center) Longeron, FS 284-325, RH

3-11322-502* Skin, Side, FS 284-325 3-11608-503 Former, CFS 487.223

*Northrop Grumman Source Directed Parts

3.2 Supplemental Kits

The Contractor shall provide supplemental kits that may result from validation/verification activities. Supplemental kits will be an un-priced Contract Line Item Number (CLIN); however, this CLIN will have supplemental kit pricing matrix at the time of contract award. If/when supplemental kits are required; the Air Force will require a fixed price proposal to award a Delivery Order (DO) to produce any additional parts or supplemental kits. A Request for Proposal (RFP) will call for submittal as soon as possible, but no later than 30 calendar days after notification.

3.3 Item Unique Identification Requirements

The Contractor shall mark Item Unique Identification (IUID) relevant parts in accordance with MIL-STD-130N1 and DFARS 252.211-7003.

3.4 First Article Test (FAT)

The Contractor shall coordinate and comply with Government FAT requirements. The First Article Inspection (FAI) requirements for the parts shall be AS 9102 compliant.

All kit contents for PCIII Phase III except the Northrop Grumman directed parts, RH/LH Upper Cockpit Longerons (Part Number (PN) 110-1101-13, 110-1101-14) and the RH/LH Steel Dorsal Longerons (PN 3-11413-3, 3-11413-4), will require FAT or a waiver approved by the Government.

All kit contents for TRIM except the Northrop Grumman directed part, Side Skin, (P/N 3-11322- 502), will require FAT or a waiver approved by the Government.

The Contractor shall account for Government FATs in detail within the provided Integrated Master Schedule (IMS). First Article partial waivers can be granted for existing parts suppliers for the specific item(s) being produced under existing contracts. These shall be submitted specifically stating the sub-kit, part number, nomenclature, the existing supplier (name and cage code) and existing prime supplier (name and cage code). Upon waiver approval, these items will not require shipment to the FAT Lab.

3.4.1 Qualifying Additional Sources

Source qualification is an option and requirements are specified in FAR 9.202, section (a). See standard SQS in Attachment A of the TDPs for a description of requirements that must be satisfied to become a qualified source.

3.5 Packaging/Labeling

The Contractor shall clearly mark packages in accordance with contract requirements and include a kit contents list with each kit. All kits shall be packaged and marked for domestic shipments in accordance with delivery order requirements or as identified in Section D of the contract, and in MIL-STD-2073-1E2, MIL-STD-130N1, and MIL-STD-129R1.

3.6 Deficiency Resolution

The Contractor shall provide direct engineering and programmatic support to the Government regarding any modification kit deficiency issues, technical or otherwise. Responses to deficiency reports shall be provided within five calendar days of discovery. If more than five calendar days will be required to respond then the Contractor shall propose an approach and expected schedule to resolution. Discrepancies/deficiencies will be reported and tracked through the Product Quality Deficiency Report (PQDR) system. The plan for correction of deficiencies shall be provided within 10 calendar days of disposition. Corrective and preventive action shall be implemented on future DOs to eliminate repeat discrepancies. (CDRL A001, B001)

3.7 Monthly Status and Production Reports

The Contractor shall submit status and production reports by the 15th of the month following the period being reported to the Government. Monthly status and production reports shall contain the following information (list is not all-inclusive; Contractor and the Government can add additional categories as appropriate throughout the period of performance): 1) production milestones, 2) manufacturing status and schedule, 3) kitting status and schedule, 4) subtotal travel, 5) deficiency reporting and remedial planning, and 6) summary of requests for variance and associated corrective action plans. Additional details regarding the content of these reports are found in Data Item Description DI-MGMT-81867, DI-MGMT-80227 and the applicable CDRLs (CDRL A002, B002; CDRL A006, B006).

3.8 Meetings

3.8.1 Weekly Technical Interchange Meetings (TIM)

The Contractor shall conduct weekly TIMs between the Government and the Contractor.

Information exchanges via teleconferencing are acceptable. Support for this meeting will include preparation of briefing materials as appropriate and meeting minutes. Meeting minutes are to be submitted no later than two days after weekly meetings. (CDRL A003, B003)

3.8.2 Program Management Reviews (PMR)

The Contractor shall conduct quarterly PMRs. Support for these meetings will include preparation of briefing materials as appropriate to be submitted no later than seven calendar days prior to the scheduled conference date and preparation/distribution of meeting minutes no later than 10 calendar days following. (CDRL A003, B003)

3.8.3 Post Award Conference

The Contractor shall conduct a post award conference to review the Government requirements and the Contractor activities that must be accomplished before a comprehensive IMS has been fully developed. Support for this meeting will include preparation of briefing materials as appropriate to be submitted no later than 7 calendar days prior to the scheduled conference date and preparation/ distribution of meeting minutes no later than 10 calendar days following.

(CDRL A003, B003)

3.8.4 Final Review

The Contractor shall plan and prepare a final review conference to present the results and discuss the outcomes of this effort. This review shall be held at the conclusion of each fiscal year.

Support for this meeting will include preparation of briefing materials as appropriate and a final report to be submitted no later than 7 calendar days prior to the scheduled conference date and preparation/distribution of meeting minutes no later than 10 calendar days following. (CDRL A003, B003)

3.9 Integrated Master Plan/Integrated Master Schedule

The Prime Contractor shall produce a comprehensive Integrated Master Plan (IMP). The IMP shall include a detailed, fully integrated management approach that identifies how the contractor will accomplish an effort of this size. The IMP shall include an IMS for the processes and milestones involved in: kit development, FAT, procurement, production, assembly, and delivery.

The IMS shall include a detailed timeline of the following: tooling production, First Article manufacture and inspection, material purchase to include long lead items, necessary subcontractor actions and milestones, production rate for each fiscal year, scheduled audits and acceptance checks. The file must be unlocked and format must be Microsoft Project 2016 or a compatible earlier version. First submittal shall be within 30 days of contract award. The IMS will be reviewed monthly at the corresponding TIM. (CDRL A004, B004)

3.10 Risk Mitigation

The Contractor shall provide a thorough risk analysis and mitigation plan from the date of contract award through the end of the PoP. The risk mitigation plan shall be reviewed semiannually at the corresponding PMR. First submittal shall be within 45 days post contract award. (CDRL A005, B005)

3.11 Schedule

The Contractor shall perform according to the Contractor developed IMS and maintain on-schedule delivery dates for all kits in accordance with the issued DO. The Government will issue DOs lead-time away. When applicable, Liquidated Damages per day will be assessed in accordance with FAR 52.211-11 in Section F if late delivery results from a Contractor caused delay. The Schedule, Section B will specify delivery dates in each DO. The Government requires the Contractor to make advance notification as specified in the CDRLs.

3.11.1 Schedule Incentive for Accelerated Delivery

The Government intends to provide an incentive to the Contractor to accelerate the schedule for the production and delivery of the initial delivery order of TRIM aircraft parts kits, which would be preceded by compliance with and passage of FAT requirements. Please refer to separate document titled, Delivery Incentive Agreement for Accelerated Delivery of TRIM Aircraft Structural Parts Kits and designated fastener kits.

3.12 Operational Safety, Suitability, and Effectiveness

The Contractor shall ensure kits and parts meet OSS&E requirement as defined in AFI 63-1201 and AFMCI 63-1201 as well as any Critical Safety Item (CSI) characteristics defined in the provided TDPs.

3.12.1 Critical Safety Items

The Contractor shall manage CSIs in accordance with the Aviation Critical Safety Item Management Handbook, and AFI 20-106 dated 25 January 2006, Management of Aviation Critical Safety Items, and as defined below.

3.13 Travel

The Contractor shall propose necessary travel requirements with each DO proposal. Travel will be issued on a Cost Reimbursable No Fee CLIN. The Contractor must attain approval from the Government Program Office NLT seven calendar days prior to each trip.

3.14 Data Compatibility

The Contractor shall provide Government compatible and unlocked documents for all Contractor work. The Government uses a Microsoft Windows 10 based operating system, 2013 MS Office, and current versions of Adobe products.

4.0 GOVERNMENT FURNISHED PROPERTY (GFP) AND SERVICES

4.1 T-38C Configuration Drawings Technical Data and Material/Equipment Provided

4.1.1 Configuration Drawings

The Government will provide the Contractor with Government owned Technical Orders (TO), Time Compliant Technical Orders (TCTO), drawings, specifications, and Contractor reports as they are identified and requested by the Contractor and as they pertain to the SOW.

4.1.2 Technical Data

The Government will provide the Contractor with all necessary Government TCTOs, Air Force Form 761 packages, and Attachment A data to accomplish the tasks detailed in this SOW.

4.1.3 Material/Equipment

All required tooling to include but not limited to reference tools, shop aids, templates, fabrication tools, machine tools, bonding tools, assembly and installation tools, IUID materials/tools, inspection tools, extrusion dies and castings shall be identified and produced by the contractor as Contractor-Acquired Property. Upon payment through Wide Area Workflow and at contract conclusion, all tooling produced and funded under this effort will become property of the Government through passage of title. Disposition instructions for all tooling produced and GFP will be given at a later date. Contractor-acquired property items shall be marked as required by DFARS clause 252.245-7001.

4.2 Security and Access to Government Facilities and Equipment The Contractor shall be responsible for safeguarding all Government property provided for the Contractor’s use. Contractors are prohibited from Government facilities without the presence of Government personnel. The Contractor shall coordinate the need, time, and personnel requiring access to Government facilities with the Government Program Manager (PM), at least one week prior to the requested need date. The Government PM, or designated representative, will coordinate between the Contractor and base personnel as needed.

4.2.1 Security Clearance

The efforts required for this task are UNCLASSIFIED and will not require Contractor personnel to obtain a security clearance. Contractor personnel shall abide by all Government rules, procedures, and standards of conduct. If Contractors require access to Government Automated Information Systems they shall have background investigations and security awareness training completed prior to the start of contract performance. When the PoP is complete and/or the Contractor personnel leave work on this project, they shall return all access cards and base identification badges prior to departure.

5.0 QUALITY CONTROL

The Contractor shall abide by quality control programs defined below. All tasks outlined in this SOW will be conducted in a professional manner and in accordance with the CDRLs and official Government guidance in order to provide products that are accurate, free of error, and complete.

5.1 Quality Assurance

Quality control processes are critical to meeting delivery schedule requirements. The Prime Contractor shall be AS 9100 compliant or equivalent. Subcontractors supporting production of the PCIII Phase III and TRIM kits shall also be AS 9100 compliant or equivalent.

5.1.1 Subcontractor Management

The Prime Contractor is responsible for all subcontractors to meet the Prime Contractor’s quality system requirements. The Prime Contractor shall show subcontractor compliance with the Prime Contractor’s quality system requirements to the Government. The means of verification shall include audits of the quality system compliance as well as physical on-site audits of the subcontractor processes, procedures, records, facilities, etc. (CDRL A006, B006)

5.1.2 Quality Assurance Plan

The Prime Contractor shall provide the Government a Quality Assurance Plan. (CDRL A007, B006) The Quality Assurance Plan shall define the quality control processes used by the Prime Contractor to ensure dimensional accuracy, material selection, and assembly of the PCIII Phase III/TRIM kits meet specifications and matches the configuration baseline. The Quality

Assurance Plan shall address how non-conformances and Product Quality Deficiency Reports (PQDRs) are to be handled.

5.1.3 Request for Variance

The Prime Contractor shall submit a DD Form 1694 for any request for variance or deviation on any part found to be non-conforming with all requirements per the technical data package provided. The Prime Contractor shall present this form and supporting documentation (per the instructions on the form) for Government Engineering review and disposition. All planned corrective actions will then become action items to be discussed during subsequent technical interchange meetings (between the Government and contractor) until corrective action has been successfully implemented and the need for future requests for variance is resolved. Requests for variance and associated corrective actions will also be summarized in the monthly status reports.

Additional information to support the request for variance may be required and should be provided to the Government within 5 business days.

The Mature and Proven Aircraft (MAPA) Engineering Branch, AFLCMC/WLDE, is the ESA for disposition of all non-conforming products under this effort.

A complete set of each DD Form 1694 applicable to parts within a kit shall be electronically provided to the Contracting Officer and enclosed with each kit shipment. (CDRL A007, B007)

ATTACHMENT ONE: APPLICABLE CDRL LIST

Applicable CDRLs SOW Paragraph CDRL CDRL Description DID

3.6 A001, B001 Discrepancy Reports/Get-well Plans FAA-ILS-014

3.7 A002, B002 Monthly Status Reports DI-MGMT-80227

3.8.1, 3.8.2, 3.8.3, 3.8.4

A003, B003 Briefing Material DI-MGMT-81605

3.9 A004, B004 Integrated Master Schedule DI–MGMT-81861

3.10 A005, B005 Risk Mitigation Plan DI-MGMT-81808

3.7, 5.1.1 A006, B006 Production Report DI-MGMT-81867 5.1.2, 5.1.3 A007, B007 Quality Assurance Plan DI-QCIC-81794/T

ATTACHMENT TWO: Applicable Documents

MIL-STD-129R Change 1 –“Military Marking for Shipment and Storage,” 28 May 2018

MIL-STD-130N Change 1 – “Identification Marking of U.S. Military Property,” 16 Nov 2012

AFI 30-1201 Change 1 – “Life Cycle Systems Engineering,” 12 Sep 2011

AFMCI 63-1201 – “Implementing Operational Safety, Suitability, and Effectiveness (OSS&E) and Life Cycle Systems Engineering (LCSE),” 28 Mar 2017

MIL-STD-2073-1E Change 2 –“Standard Practice for Military Packaging,” 09 Jul 2018

DFARS 252.211-7003 – “Item Unique Identification and Valuation,” Mar 2016

ATTACHMENT THREE: BILL OF MATERIALS (BOM)

The Technical Data Package is available upon request after submittal of signed Non-Disclosure Agreement.

2.3 Period of Performance (PoP)