Attachment 1_KC-46 Initial Spares SOW.pdf

FA8609-22-R-0001

Section J, Attachment 1

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DEPARTMENT OF THE AIR FORCE

MOBILITY AND TRAINING AIRCRAFT DIRECTORATE KC-46 DIVISION

WRIGHT PATTERSON AIR FORCE BASE, OHIO 45433

STATEMENT OF WORK (SOW)

FOR

KC-46 INITIAL SPARES

SOLICITATION/CONTRACT NO. : FA8609-22-R-0001

CONTENT OWNER:

KC-46 Sustainment Integrated Program Team (IPT)

Program Manager (PM) Signature

Lt. Col. Dibya Das PM Name Printed

10-19-2021

Date

Controlled by: AFLCMC Controlled by: KC-46 Sustainment IPT CUI Category: Defense Distribution/Dissemination Controls: N/A POC: Lt Col Dibya Das, DSN 986-5702

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Table of Contents

1.0 Background………………………………………………………………………..……..3

2.0 Objectives…………………………………………………………………………..…….3

3.0 Tasks……………………………………………………………………………………...4

3.1 Initial Reparable Spares……………………………………………………...…4

3.2 Certificate of Conformity…………………………………………………..…...4

3.3 Item Unique Identification…………………………………………………..….4

3.4 Package, Handle, Store, & Transport……………………………………..…...4

3.5 USG Acceptance & Product Delivery…………………………………….……4

3.6 Product Warranty…………………………………………………………..…...5

4.0 Reviews.,………………………………………………………………………………….5

4.1 Post Award Conference…………………………………………………………5

Appendix A – Applicable Documents for Reference……………..……………………… 6

Appendix B – Definition of United States Air Force Specific Terms

Appendix C – Program Performance Summary ………………………………………… 8

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1.0 Background

1.1 KC-46 Aircraft provides worldwide, day and night, and adverse weather aerial refueling to receiver-capable US, allied, and coalition military aircraft, including unoccupied aircraft. The KC-46 Tanker is based on commercial, Federal Aviation Administration (FAA) or equivalent, certified 767-2C aircraft, which is finished to meet the unique KC-46 Tanker requirements. To uphold this certification for an accepted KC-46, the sustainment requirements will ensure compliance with Amended, Supplemental, and Military Type Certifications (ATC/STC/MTC).

1.2 Per the October 2016 KC-46 Life Cycle Sustainment Plan (LCSP) (Appendix A, Reference 1), The

United States Government (USG) will use an organic two-level maintenance (2LM) posture for sustainment of the KC-46 Tanker: Organizational Level (O-Level) and Depot Level (D-Level). The 2LM will best ensure compliance with certification requirements.

1.3 In order to mechanize this 2LM sustainment posture, the KC-46 Tanker Program will require initial spares for the reparable line replaceable units (LRUs). The KC-46 Tanker Program will outfit each main operating base (MOB) and Air Logistics Complex (ALC) located worldwide with an initial quantity of reparable spare LRUs using the parts listed in the Capability Statement (FA8609-22-R- 0001, Section J, Attachment 3). This list is subject to a possible increase of 10% parts over the baseline within the duration of this acquisition.

1.4 USG will annually conduct Spares Modeling to determine the initial quantities from the baselined end item list required for MOB(s) projected for stand up and ALC capability initialization.

1.5 The initial outfitting of reparable spare LRUs will optimize 2LM and enable mission responsiveness for the newly stood-up MOB(s) and ALC capabilities.

2.0 Objectives

2.1 The Contractor shall provide reparable LRUs to worldwide locations to include but not limited to USG and Foreign Partner Military locations.

2.2 The Contractor shall ensure that all reparable LRUs complies with FAA-defined processes and procedures defined in the May 2017 FAA and Industry Guide to Product Certification (Appendix A, Reference 2).

USG will accept new, new surplus, overhauled, serviceable, or parts manufactured approval (PMA)/ aftermarket parts as required and per the following definitions:

2.2.1 New: The part is brand new from the factory Original Equipment Manufacturer (OEM) and has its appropriate OEM trace and certification (8130-3 if applicable).

2.2.2 New Surplus: Part is brand new and never been used but was not obtained from the OEM, rather a third party (DAR 8130 if required)

2.2.3 Overhauled: Part was disassembled, cleaned, inspected, repaired as necessary to finally get reassembled, and it has been tested in according to approved manual standards of that specific part that includes technical data and current standards (FAA 8130-3)

2.2.4 Serviceable: processed through bench test by a FAA Authorized 145 repair station to determine if the LRU is functional, if not then appropriately fix only what caused non-functionality (FAA 8130-3)

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2.2.5 PMA: Manufactured in accordance with OEM specification and certifiable through the FAA.

2.2.6 Service Life Cycles: The number of times a LRU has undergone an overhaul. An LRU can be overhauled a predetermined number of times before it is deemed unserviceable.

2.3 The Contractor shall ensure that all reparable LRUs with Foreign Partner MOB delivery destinations comply with International Traffic in Arms Regulations (ITAR) (Appendix A, Reference 3).

3.0 Tasks

3.1 Initial Reparable Spares: The Contractor shall deliver reparable LRUs and notify the USG of the destination and respective locations in the quantities identified in each DO. The Contractor shall at a minimum provide the following for any deviations from the RFP:

3.1.1 Immediate notification after receipt of RFP DO for each reparable LRU that encountered part number roll, excluding substitutions and interchangeable parts. Notification shall include but not limited to impact to price, effectivity data for current and new parts, and delivery.

3.2 Certificate of Conformity (CoC): The Contractor shall ensure that all reparable LRUs receive an 8130-3 or CoC pursuant to a quality system as required by the appropriate design approval authority.

3.3 Item Unique Identification (IUID): The Contractor shall mark applicable reparable LRUs with an

IUID in accordance with the December 2007 MIL-STD-130N (Appendix A, Reference 4). Radio frequency identification (RFID) is not applicable to KC-46 Reparable LRUs and is not considered an equivalent replacement for IUID.

3.4 Package, Handle, Store, & Transport (PHS&T): The Contractor shall conduct PHS&T of reparable LRUs in accordance with latest Air Force Materiel Command (AFMC) Form 158.

3.5 USG Acceptance & Product Delivery: The Contractor shall support USG acceptance and product delivery of each reparable LRU, and at a minimum:

3.5.1 Notify USG of destination, location, and quantities of items delivered no less than 15 days prior to item delivery.

3.5.2 Include a packing slip and 8130-3/CoC for each reparable LRU to the appropriate USG acceptance organization to include, but not limited to, the cognizant Defense Contract Management Agency (DCMA) Contract Management Office (CMO).

3.5.3 Provide an Engineering or Technical Support Single Point of Contact (SPOC) to provide at a minimum the following:

3.5.3.1 Responses to USG inquiries

3.5.3.2 Responses to USG clarification requests

3.5.3.3 Assistance with Grief Activities at delivery destination

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3.5.4 The Contractor shall meet the minimum level of metrics maintained at the delivery order (DO) level including on-time fill percentage and delinquency rate. An item delivered more than 48 hours after the date stated in the DO shall be delinquent.

3.5.5 Acceptable Quality Levels (AQLs) on these metrics are set forth in Appendix C. The Contractor shall not be liable for not meeting an AQL in any of the areas if default is caused by any items identified in 52.212-4(f) or 52.249-8 (c). The Contractor shall notify the Contracting Officer in writing as soon as it is reasonably possible after the commencement of any excusable delay, setting forth the full particulars in connection therewith, shall remedy such occurrence with all reasonable dispatch, and shall promptly give written notice to the Contracting Officer of the cessation of such occurrence.

3.6 Product Warranty: Contractor shall provide at least the same warranty terms, including offers of extended warranties, offered to the public in customary commercial practice for the items acquired under the contract. Also reference FAR 52.212-4. The Contractor will accept returns, and if the authorized customer still requires the product(s), replace the product(s) under the following conditions:

3.6.1 Incorrect products were shipped;

3.6.2 Products were damaged in shipment;

3.6.3 Products arrived with concealed shipping damages;

3.6.4 Other returns consistent with the Contractor’s normal return policy to include return of excess material ordered by the customer based on a project estimate.

4.0 Reviews: The Contractor shall at a minimum support and attend the following reviews per USG request as applicable:

4.1 Post Award Conference (PAC):

4.1.1 Scheduling: No later than 30 calendar days after contract award.

4.1.2 Focus: Review the contract terms and conditions, and discuss the actions and activities necessary to successfully complete the program.

4.1.3 Additional Details: Held virtually using an electronic communication venue mutually agreeable by both the Procuring Contracting Officer (PCO) and the Contractors. The number of Contractor attendees shall be limited to a maximum of four persons and the PAC duration shall not exceed four hours. The PCO will coordinate the actual date and time of the PAC with the Contractor after contract award.

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APPENDIX A

APPLICABLE DOCUMENTS FOR REFERENCE

Ref # Document Name Date Section 1 KC-46 Life Cycle Support Plan Oct 2016 11.4

2 Federal Aviation Administration and Industry Guide to Product Certification May 2017 1.3.1

3 International Traffic in Arms Regulations Jan 2020 CFR Title 22 Vol. 1 Ch. 1 Sub-Ch. M

4 MIL-STD-130N Identification Marking of US Military Property, w/ CHANGE 1 Nov 2012 5.2.1.4

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APPENDIX B

DEFINITION OF UNITED STATES AIR FORCE SPECIFIC TERMS

FAA Form 8130-3: Is the Statement of Compliance with Federal Aviation Regulation. Also known as the airworthiness approval tag or authorized release certificate. It is used to certify compliance with applicable requirements of 14 CFR Part 21 and certifies if a new part, engine, or entire plane is airworthy but can also be used to return a part, engine, or plane back to service after repair.

Certificate of Conformity (CoC): The actual FAA Aircraft Certification Form 8130-3 that is used to document maintenance performed on an aviation article (e.g., inspection, repair, or overhaul).

Routine Use: Commonplace tasks, activity or duties that must be accomplished on a regular basis or at specific intervals.