SPE4A219R0055 (issued 22Nov19).pdf

SOLICITATION, OFFER AND AWARD 1. THIS CONTRACT IS A RATED ORDER

UNDER DPAS (15 CFR 700)

RATING PAGE OF PAGES

2. CONTRACT NUMBER 3. SOLICITATION NUMBER 4. TYPE OF SOLICITATION 5. DATE ISSUED 6. REQUISITION/PURCHASE NUMBER

CODE7. ISSUED BY 8. ADDRESS OFFER TO (If other than item 7)

NOTE: In sealed bid solicitations "offer" and "offeror" mean "bid" and "bidder".

SOLICITATION

9. Sealed offers in original and copies for furnishings the supplies or services in the Schedule will be received at the place specified in item 8, or if hand carried, in the depository located in until local time

CAUTION - LATE Submissions, Modifications, and Withdrawals: See Section L, Provision No. 52.214-7 or 52.215-1. All offers are subject to all terms and conditions contained in this solicitation.

10. FOR

INFORMATION

CALL:

A. NAME B. TELEPHONE (NO COLLECT CALLS)

AREA CODE NUMBER EXTENSION

C. E-MAIL ADDRESS

11. TABLE OF CONTENTS

(X) SEC. DESCRIPTION PAGE(S) (X) SEC. PAGE(S)DESCRIPTION

A B C D E F G H

I

J

K

L

M EVALUATION FACTORS FOR AWARD

INSTRUCTIONS, CONDITIONS, AND NOTICES TO OFFERORS

REPRESENTATIONS, CERTIFICATIONS AND OTHER

STATEMENTS OF OFFERORS

PART IV - REPRESENTATIONS AND INSTRUCTIONS

LIST OF ATTACHMENTS

PART III - LIST OF DOCUMENTS, EXHIBITS AND OTHER ATTACH.

CONTRACT CLAUSESSOLICITATION/CONTRACT FORM

SUPPLIES OR SERVICES AND PRICES/COSTS

DESCRIPTION/SPECS./WORK STATEMENT

PACKAGING AND MARKING

INSPECTION AND ACCEPTANCE

DELIVERIES OR PERFORMANCE

CONTRACT ADMINISTRATION DATA

SPECIAL CONTRACT REQUIREMENTS

NOTE: Item 12 does not apply if the solicitation includes the provisions at 52.214-16, Minimum Bid Acceptance Period.

OFFER (Must be fully completed by offeror)

12. In compliance with the above, the undersigned agrees, if this offer is accepted within calendar days (60 calendar days unless a different period is inserted by the offeror) from the date for receipt of offers specified above, to furnish any or all items upon which prices are offered at the set opposite each item, delivered at the designated point(s), within the time specified in the schedule.

13. DISCOUNT FOR PROMPT PAYMENT

(See Section I, Clause No. 52.232-8)

14. ACKNOWLEDGMENT OF AMENDMENTS

(The offeror acknowledges receipt of amendments to the SOLICITATION for offerors and related documents numbered and dated):

10 CALENDAR DAYS (%) 20 CALENDAR DAYS (%) 30 CALENDAR DAYS (%) CALENDAR DAYS(%)

DATEAMENDMENT NO.AMENDMENT NO. DATE

15A. NAME AND

ADDRESS

OF OFFEROR

CODE FACILITY 16. NAME AND THE TITLE OF PERSON AUTHORIZED TO SIGN

OFFER(Type or print)

15B. TELEPHONE NUMBER

AREA CODE NUMBER EXTENSION

15C. CHECK IF REMITTANCE ADDRESS IS

DIFFERENT FROM ABOVE - ENTER SUCH

ADDRESS IN SCHEDULE.

17. SIGNATURE 18. OFFER DATE

AWARD (To be completed by Government)

19. ACCEPTED AS TO ITEMS NUMBERED 20. AMOUNT 21. ACCOUNTING AND APPROPRIATION

22. AUTHORITY FOR USING OTHER THAN FULL OPEN COMPETITION:

10 U.S.C. 2304 (c) ( )41 U.S.C. 3304(a)

24. ADMINISTERED BY (If other than Item 7)

26. NAME OF CONTRACTING OFFICER (Type or print)

IMPORTANT - Award will be made on this Form, or on Standard Form 26, or by other authorized official written notice.

AUTHORIZED FOR LOCAL REPRODUCTION

Previous edition is unusable

23. SUBMIT INVOICES TO ADDRESS SHOWN IN

(4 copies unless otherwise specified)

25. PAYMENT WILL BE MADE BY

27. UNITED STATES OF AMERICA

(Signature of Contracting Officer)

28. AWARD DATE

CODE

ITEM

STANDARD FORM 33 (REV. 6/2014)

Prescribed by GSA - FAR (48 CFR) 53.214 (c)

SEALED BID (IFB)

NEGOTIATED (RFP)

(Hour) (Date)

PART I - THE SCHEDULE PART II - CONTRACT CLAUSES

1 62

F108 Workload Augmentation

SPE4A2

SPE4A2-19-R-0055

See Section L See Section L 1500EST

Ingrid Smith ingrid.smith@dla.mil

19 50

2/21/2020

804 279 3148

11/22/2019

DLA Aviation 8000 Jefferson Highway Richmond, VA 23297

CONTINUATION SHEET REFERENCE NO. OF DOCUMENT BEING CONTINUED

SPE4A2-19-R-0055

Page

NAME OF OFFEROR OR CONTRACTOR

50336-101 NSN 7540-01-152-8067

US GOVERNMENT PRINTING OFFICE 1990-262-081

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

GENERAL INFORMATION

A.1 OVERVIEW

A.1.1 The F108 Workload Augmentation acquisition described shall supplement continued organic engine production at United States Air Force (USAF) Oklahoma City Air Logistics Center (OC-ALC). Primarily due to poor material supportability, organic production has not met remanufacture objectives and despite multiple contract efforts to improve support, production continues to lag. As such, the acquisition herein seeks to establish a temporary augmentation to organic support with commercial sources to improve whole engine overhaul output and also, re-energize the industrial base for the remanufacture of this engine. This strategic long-term contract will ensure F108 production supportability is maintained which in-turn will enhance War Readiness Equipment (WRE) availability.

A.1.2 The F108 whole engine remanufacture results in the engine overhaul from an F108-100 to F108-100A in accordance with the technical requirements specified herein.

A.1.3 This solicitation is for a FAR Part 12, Indefinite Delivery, Indefinite Quantity contract and a limited competition acquisition with USAF approved sources CFM International (CFMI) and Lockheed Martin Commercial Engine Services (LMCES).

A.2 Period of Performance

The resulting contract shall establish Firm Fixed Pricing for the one-year base period and four one-year option periods, to be exercised at the discretion of the Government. The total period of performance shall not exceed five years.

A.3 FOB Point

Ready for issue remanufactured engines shall be FOB Destination.

A.4 DCMA Administration

A.4.1 DLA Aviation shall retain administration of the Basic contract. However, the cognizant DCMA office of the awardee(s) shall be delegated the administrative functions listed below for all delivery orders issued for the F108 Workload Augmentation requirement as detailed herein.

A.4.2 Contract administration functions for the F108 Workload Augmentation delivery orders shall reside with the cognizant DCMA office of the awardee. All Government Contract Quality Assurance (GCQA) to include quality surveillance, and inspection & acceptance or remanufactured engines shall reside with the DCMA Quality personnel assigned to the Contractor’s(s’) facility.

A.5 Delivery

The Government’s requested delivery is 90 days from receipt of an F108 engine carcass, however, delivery shall be negotiated.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

A.6 Split Awards

The Government may consider split awards in the event offered pricing is competitive from two acceptable awardees, non-price factors considered. Details are provided at Section M below.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

SECTION B

SUPPLIES OR SERVICES AND PRICES/COSTS

B.1 Offerors shall submit proposed pricing for each year of the proposed contract term that includes all elements of the F108-100 to F108-100A remanufacture requirements as set forth in this solicitation. Prices shall be proposed on a remanufactured F108 engine unit price basis utilizing the quantity price breaks established at the table below for each contract year. If out-year pricing is not proposed, the offeror shall include the applicable proposed escalation, labeled as such in the offeror’s worksheet, along with the basis for such escalation.

CLIN Quantity of

Engines Base Year Unit Price

Option Year 1 Unit Price

Option Year 2 Unit Price

Option Year 3 Unit Price

Option Year 4 Unit Price

20-29

10-19

1-9

0002 Over and Above

B.2 While the Government acknowledges the FAR Part 12 nature of the acquisition, offerors shall provide unit price build up details to ensure a fair and reasonable price determination can be made. This build up may include, but is not limited to: (1) the offeror’s bill of materials for the Quick Engine Change (QEC) kit and all parts identified for replacement within the SOW at Section C and attached technical data (e.g., TC/TOs, Service Bulletins, etc.) and (2) costs for remanufacture labor, testing, etc., or service fee.

B.3 Over and Above (O&A) may apply during contract performance. As described at C.2.2 below, O&A may apply due to unanticipated maintenance costs discovered during the overhaul process of an engine. O&A includes maintenance and/or material replacements not identified within the SOW and associated technical data at time of proposal and contract award.

B.3.1 The Contractor shall advise the DLA POC and USAF Engineering of all unanticipated maintenance costs for disposition and pricing requirements for evaluation against CLIN 0002 under the contract.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

SECTION C

DESCRIPTION / SPECIFICATION / WORK STATEMENT

C.1.0 WORK SCOPE

The purpose of this SOW is to define the major remanufacture requirements for the F108/CFM56-2B TURBOFAN Engine that apply to the following National Stock Numbers (NSN) and Part Numbers (P/N) and limited Quick Engine Change part normally installed on a two-level of maintenance engine.

F108100 ENGINE ASSEMBLY

Input P/N Output P/N Input NSN Output NSN

9995M60G01 9995M60G01 2840F108CF100PN 2840F108CF100PN

Output configuration shall meet all requirements for F108-100A upgrade established in section C.1.2.4.1 build policy table and section C.1.2.5 special work requirements.

The instructions stipulated are brief, concise statements providing general requirements for disassembly, cleaning, inspection, repair and overhaul of the F108/CFM56-2B TURBO FAN Engine. Overhaul will complete upgrade of the engine from the F108-100 to the F108-100A. The contractor shall maintain a Federal Aviation Administration (FAA) Part 145 rated repair facility rated to major overhaul CFM56-2B engines and components; contractor must have the major overhaul capabilities to include appropriate technical data, major overhaul documents, and license agreements, required to accomplish major overhaul of CFM56-2B Engine Assembly and component parts In Accordance With (IAW) the Engine Shop Manual (ESM) and Component Maintenance Manual (CMM). Designated Engineering Representative (DER) repairs may not be used unless previously approved by AFLCMC/LPE Engineering and commercially used parts will not be allowed unless specifically identified in the SOW (see paragraph C.1.2.1.6.).

The contractor is responsible for the production, major overhaul and scheduled delivery of a quality product.

The use of Contractor Furnished Material in support of this engine overhaul program shall not impact existing government parts support contracts.

Contractor employees shall identify themselves as contractor personnel by introducing themselves or being introduced as contractor personnel and displaying distinguishing badges or other visible identification for meetings with Government personnel. In addition, contractor personnel shall appropriately identify themselves as contractor employees in telephone conversations and in formal and informal written correspondence.

C.1.1 Receiving: The contractor shall have physical custody of engines received at their site, and shall maintain constant care over these items while in their possession. Engines should be stored in a covered area to prevent water intrusion and other environmental damage.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

C.1.1.1 The contractor shall perform a receiving visual inspection upon receipt of each F108/CFM56-2B TURBOFAN Engine Assembly. Each engine shall be evaluated for any shipping or packaging damage using ESM.

C.1.1.2 The contractor shall report to the Procurement Contracting Officer (PCO) any received assemblies which are misidentified, misdirected, or incomplete (missing parts); the PCO shall provide disposition instructions. The time between contractor notification and receipt of PCO disposition instructions does not count towards the contractual turnaround time. Discrepant shipments shall be processed IAW the contract’s Appendix B, “End Item and Government Furnished Equipment Management,” Section 7. The contractor shall initiate a Supply Discrepancy Report (SDR) for any assets received in other than authorized packaging.

C.1.2 Major Overhaul: The contractor shall perform a major overhaul of the F108/CFM56-2B TURBOFAN Engine to produce a serviceable engine as follows.

C.1.2.1 Major Overhaul Procedures: The F108/CFM56-2B TURBOFAN Engine Assembly shall be overhauled IAW the procedures outlined in ESM, Workscope Planning Guide (WPG), required Service Bulletins (SB), and Time Compliance Technical Orders (TCTOs) listed in Appendix B. Contractor shall furnish all material, with the exception of C-PUP kits, support equipment, tools, test equipment and services to perform all work for this overhaul effort.

Contractor shall acquire all component parts from Original Equipment Manufacturer approved vendors or commercial inventories approved by the USAF and/or OEM.

C.1.2.1.1 All work shall be documented. Due to the varying degrees of maintenance required on each engine, standard work control documents (WCD) or process control sheets shall be used and maintained for review by Government Representative as necessary.

C.1.2.1.2 All TCTOs and Service Bulletins identified in Appendix B and authorized for depot level accomplishment shall be accomplished on all engines undergoing major overhaul. The PCO and contractor shall negotiate TCTOs released after the contract is awarded on an over and above basis and shall be billed to the Over and Above CLIN (CLIN 0002)

C.1.2.1.3 All installed parts must be capable of meeting the designed functional capabilities as specified in applicable ESM and CMM prior to installation. This includes all engine, accessory, and Quick Engine Change (QEC) kit components.

C.1.2.1.4 Continue in use all Control and Accessory (C&A) and QEC parts and assemblies that are determined serviceable and appropriate as a result of inspection, functional test, or measurement IAW applicable ESM and TO 6J3-4- 113-3-WA-1, unless directed otherwise by the Workscope Planning Group, in which case it is subject to over and above procedures. C&A component items will be evaluated per CMM chapters 73-79.

C.1.2.1.5 Replace unserviceable parts of the end item with serviceable like parts listed in the applicable parts catalog IAW Build Policy Table in C.1.2.4 Maintenance. Documentation of removed part disposition shall be reported to AFLCMC/LPSBA, AFLCMC/ LPSBB and 421 SMCS/GUMBA Technical Services as outlined in section 1.2.16 Reporting.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

C.1.2.1.6 AFLCMC/LPE Cognizant Engineering Authority will be contacted for any questionable component needing disposition. The use of specific commercially used/overhauled parts must be approved prior to use. FAA 8130s (Certificate of Airworthiness) must be provided for all commercially used/overhauled parts installed. The use of commercial used/overhauled life limited parts (LLP) will be evaluated on a case by case basis in coordination with the ACO/PCO.

For consideration of use, the LLPs are limited to one prior ownership and a comprehensive life cycle history must be provided to USAF. This will also include removal history, a list of all repairs accomplished, as well as Eddy Current/Ultrasonic Inspection documentation.

C.1.2.1.7 The Contractor shall ensure the Air Force receives full warranty consideration, if applicable, for engines undergoing major overhaul. Warranty tracking and reporting, if applicable, shall be IAW T.O. 2J-1-F108.

C.1.2.2 Specific Work Requirements

C.1.2.2.1 This work specification covers the On Condition Maintenance concept of the F108- CFM56-2B engine. Work specification and requirements are incorporated in Appendix B and C.

C.1.2.2.2 The Contractor shall review engine records, chip detector information, and Engine Trend Data for performance, and borescope inspection to determine maintenance required to return engine to serviceable status. Engine Trending and performance data (if available) shall be reviewed by SOR prior to workscope meeting. All engines shall be borescoped IAW ESM to the extent necessary to determine the amount of work to be performed to return the engine to a serviceable status.

C.1.2.2.3 After conducting the initial inspection for each engine inducted, the Contractor shall document an initial proposed major overhaul workscope and conduct a workscope meeting with representatives from AFLCMC/LPSBB (as needed), AFLCMC/LPE, AFLCMC/LPSBA, and a MAJCOM representative (as needed). The purpose of the meeting is to determine failure cause, degree of damage, and to develop and implement a plan to restore engine to serviceable status.

The Workscope Planning Group will review and the SOR shall document applicable TCTOs and Service Bulletins that require incorporation. The F108 Workscope Planning Guide (APPENDIX C) shall be used to determine maintenance actions required during workscope meeting. The Workscope Planning Group is fully empowered and authorized to determine the level of maintenance, performance restoration, and any proposed deviations to technical order requirements.

C.1.2.2.4 QEC items shall be inspected, overhauled, and/or replaced IAW T.O. 1C-135(K)R-10.

C.1.2.2.5 All engines produced shall have LCF components/parts with a minimum 3500 cycles of life remaining. Reference Chapter 5 parts list in ESM.

C.1.2.2.6 Line Replaceable Units (LRUs) shall be removed and overhauled as required to return engine to serviceable status. Shop Replaceable Units (SRUs) as shown in Workscope Planning Guide shall be removed and overhauled as required to return engine to serviceable condition.

(List of authorized SRUs is in section C.1.2.4.1).

Page

NAME OF OFFEROR OR CONTRACTOR

50336-101 NSN 7540-01-152-8067

US GOVERNMENT PRINTING OFFICE 1990-262-081

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

C.1.2.2.7 Control and Accessory Time Limits of Workscope Planning Guide, shall be implemented as agreed to by Workscope Planning Group.

C.1.2.3 Disassembly

C.1.2.3.1 The procedures contained in ESM shall be used in disassembling engines input for maintenance; T.O. 1C-135(K)R-10 shall be used for removal and installation of the QEC kit.

C.1.2.3.2 Engines shall be fully disassembled to correct discrepancies noted during evaluation, required scheduled maintenance and performance upgrade modifications. During disassembly, all parts removed shall receive a visual inspection and required maintenance, to restore to a serviceable condition, per applicable technical orders.

C.1.2.4 Maintenance

C.1.2.4.1 Authorized module part numbers, which reflect the latest configuration for installation as listed. The following part numbers are further identified in the attached TCTOs, incorporated herein:

Authorized installation module part numbers for removed modules.

Mod # Module NSN Installation Part Number

1 Fan & Booster 2840-01-139-6655PN 301-285-260-0 2 No.1 & No.2 Bearing Support 2840-01-139-6615PN 305-957-801-0 3 Inlet Gearbox & No. 3 Brg 2840-01-352-8066PN 9995M18G04/G06 4 Fan Frame Assembly 2840-01-262-1952PN 305-957-604-0

Fan Weldment 2840-01-206-9815PN 301-290-896-0 No.3 Brg Aft Air Oil Seal 2840-01-356-3538PN 1663M91G04

5 HP Compressor Rotor (Match Grind) 2840-01-599-6415PN 9995M23G11C 6 HPC Forward Stator (Titanium Case) 2840-01-600-8917PN 9995M12G05C

HPC Forward Stator (Steel Case) 2840-01-598-4723PN 9995M26G05C 7 HPC Rear Stator 2840-01-600-8916PN 9995M25G05C 8 Combustion Case 2840-01-262-0495PN 9529M99G08/G09

9523M17G11 9523M17G13 9523M17G15 9529M99G02 9529M99G06 9529M99G04 1285M90G01 1359M77G05 9529M99G08 9529M99G15 9529M99G09

9 Combustion Chamber 2840-01-242-8336PN 9559M48G08 1493M63G01/G02

10 HPT Nozzle 2840-01-599-4049PN 9995M14G15C 11 HPT Rotor (Match Grind) 2840-01-598-7366PN 9995M22G07C 12 HPT Shroud/Stg 1 LPT Nozzle 2840-01-502-6780PN 9995M27G11/12/20

13/15 LPT Rotor/Stator Assembly 2840-01-229-5786PN 305-482-301-0 305-482-302-0

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

305-482-303-0 14 LPT Shaft 2840-01-189-2941PN 301-316-158-0 16 Transfer Gearbox 2840-01-189-2936PN 305-100-112-0 17 Accessory Gearbox 2840-01-139-4075PN 301-100-208-0

C.1.2.5 Special Work Requirements

C.1.2.5.1 All special inspections required by T.O. 1C-135-6 shall be accomplished and hours shall be zeroed out on all engines while undergoing major overhaul so the engine leaves the SOR with all -6 inspections accomplished regardless of the time remaining when they arrived.

C.1.2.5.2 Starter splines shall be inspected. Replace any defective components.

C.1.2.5.3 All engines will have the starter SEALOL SEAL upgraded to part # 305- 115-707-0.

C.1.2.5.4 QEC components shall be inspected and reworked/replaced as necessary. Engines shall have QEC kit returned to a serviceable condition. QEC material shall be provided by the Contractor (see para 2.1)

C.1.2.5.5 All engines will have EGT margin restored to 30 deg C (54 deg F) or greater from corrected hot day values listed in 72-00-00 Testing 003 Figure 1301.

C.1.2.5.6 All engines undergoing Major overhaul/Rework level maintenance shall be input/output in full QEC configuration as specified in T.O. 1C-135(K)R-10, with the exception of the following items:

(1) Aircraft Hydraulic Pump

(2) Integrated Drive Generator

C.1.2.5.7 All engines inducted for maintenance shall have the Full Set of 44 Fan Blades cleaned, overhauled, balance weight checked, and re-matched assets. Inspect Fan Blades leading and trailing edges to inspection limits in ESM to include moment weight verification and patternization of each set.

C.1.2.5.8 All booster assemblies from Fan and Booster module will be removed and overhauled.

C.1.2.5.9 Fan Frame Abradable Cartridge will be restored to serviceable condition per ESM. If cartridge is beyond reparable limits, it must be replaced.

C.1.2.5.10 All high pressure compressor rotors will be upgraded to the C-PUP configuration and match ground as a set.

C.1.2.5.11 All engines that have thermal spray coated Aft Stator Case shall have the Aft Stator cases replaced with the New Linerless Cases 9995M25G05 and marked with an L after the part number for tracking purposes using a vibropeen etcher. See Build Policy Table for authorized module part numbers for installation. Parts shall be marked IAW the ESM Standard Practice Manual.

C.1.2.5.12 During work on an engine if an obvious defect is discovered in an area that is not related to the problem driving removal of the engine, then the defect shall be brought to the

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

attention of Cognizant Engineering Authority and contracting officer for disposition. The Contractor shall follow CFR 252.217- 7028 if work over and above the work scope of this contract is required.

C.1.2.5.13 The forward and aft sump and Accessory drive module (Accessory and Transfer Gearbox modules) will be flow checked for possible oil flow restrictions on all inducted engines (ref. Appendix D).

1) F108 gearboxes that fail flowcheck but have no other issues, (i.e. contamination, noises, TCTOs and etc.) will be returned to serviceable condition after undergoing a minor overhaul (defined as cleaning and/or replacing nozzles and restrictors as needed to achieve established flow rates IAW ESM).

2) All other gearboxes not meeting these criteria will be fully overhauled IAW ESM.

C.1.2.5.14 All Variable Bleed Valves (slaves and masters) will be removed and overhauled.

Exception: If bleed valves have grease fitting (zerk), properly lubricated VBV and perform manual roll check for smooth operation.

C.1.2.5.15 All Turbine Clearance Control Valves (TCCV) will be removed and overhauled in accordance with applicable CMM.

C.1.2.5.16 All LPT Rotor Modules will have all stages of blades replaced with 100% new or overhauled blades from approved OEM sources. Low Pressure Turbine (LPT) dynamic system balance shall be performed on engines that are “vibration recycles” and those engines requiring a LPT component replacement as required by ESM (ref. Appendix E).

C.1.2.5.17 All engines shall incorporate the 1.3 airflow, Modules 10 and 12.

C.1.2.5.18 All engines will have the high pressure turbine rotor and high pressure turbine shroud assemblies match ground as a set.

C.1.2.5.19 All engines with more than 6000 EOT shall have fuel nozzles cleaned and flow checked.

C.1.2.5.20 All engines received with small tip fuel nozzles installed shall have large tip fuel nozzles installed during overhaul (post 91 configuration). Small tip fuel nozzles removed during overhaul shall be returned to the government supply condition code “F” repairable. The contractor shall be responsible to procure the large tip fuel nozzles required for the upgrade to the post 91 configuration.

Small Tip Standard Flow Small Tip Enriched Flow

P/N NSN P/N NSN

6810184M30 2915-01-190-9242PN 6810184M33 2915-01-219-3163PN

6810184M36 2915-01-219-3163PN

C.1.2.5.21 All engines disassembled to the point that access is gained to and which have aft air/oil seal part numbers 1663M91XXX or 1279M53XXX shall have retention bushings 1960M57P01 installed.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

C.1.2.5.22 Engines with Fan Weldment PN 301-290-885-0, studded aft air/oil seal, shall be reworked to PN 301-290-896-0, IAW ESM, service bulletin 72-213.

C.1.2.5.23 Remove, clean and inspect for re-use all main engine bearings. Exception: If chip detector findings or engine records documentation reveal bearings have been exposed to M50 contamination, replace bearings.

C.1.2.5.24 All engines inducted shall have the #4 bearing updated to the latest configuration.

The new bearing PN shall be one of the following: 335-352-303-0, 340-167-902-0 or 305-355- 718-0.

C.1.2.5.25 Remove and overhaul all main fuel pumps with 6,000 hours or more of service time since original install or last overhaul.

C.1.2.5.26 All components with abradable coating or honeycomb shall have these coatings restored to as-new condition.

C.1.2.5.27 All Main Engine Controls (MEC) will be remanufactured and incorporate Service Bulletins listed in Appendix B.

C.1.2.5.28 Double-walled fuel manifolds will be replaced with single-walled manifolds.

C.1.2.5.29 All VSV Bell Cranks will be overhauled to include the following Service Bulletins: SB 72-0251, SB 72-410, SB 72-0418 and 72-0541

C.1.2.5.30 Clean all oil wetted areas and components per the ESM.

C.1.2.5.31 Remove, clean, flush, inspect, and functionally test all Lube units.

C.1.2.5.32 Clean, inspect and bench check all sensors, controls and valves.

C.1.2.5.33 Parts purchased or replaced will have serviceable parts tags (form 1574) or form 8130-3 or a Certificate of Conformance from the OEM.

C.1.2.5.34 In order to be compliant with UID requirements, the Contractor must comply with service bulletin 72-0772. Process for data plate turn in and receiving to be defined at contract award.

C.1.2.6 Finishing

C.1.2.6.1 Engines, engine parts, QEC components, engine accessories, and accessory parts shall be overhauled or replaced as required by the applicable ESM and CMM unless otherwise specified in this specification. Decals and Data plate entries shall be annotated as required by applicable maintenance manuals.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

C.1.2.6.2 Engine Testing and Government Acceptance

a. Engines shall be tested in the basic configuration IAW ESM testing procedures.

b. Engines undergoing maintenance shall meet all test parameters, and be trimmed to the requirements specified in ESM. If engine fails to meet test parameters per mutually agreed to workscope and must be recycled back to maintenance shop, the Contractor shall reconvene to document trouble shooting and any corrective action. A copy of the final run sheet shall be attached to the engine AFTO Form 95. A data disk will be generated for each engine and shall contain all maintenance actions performed and include engine records action. Any work necessary to correct a failed engine test cell run shall not be the financial responsibility of the Air Force.

c. Run sheets of acceptance runs shall be maintained with the record of maintenance actions accomplished during Contractor overhaul. After completion of engine major overhaul, data/engine records package shall be transferred to AFLCMC/LPSBA within 7 work days.

d. Engine shall be given a full final inspection documented with date, Contractor’s inspector’s name, and phone number. All engines shall be borescoped IAW ESM, recorded and provided on CD media. Once Contractor concludes final inspection, the engine and documentation will be ready for DCMA inspection.

e. Engine shall be wrapped for shipment per T.O. 1C135(K)R-10 section 1 and 2J-1-18 chapter 8 returned to supply QEC configured.

C.1.2.7 Accessory and Component Reuse and Replacement

C.1.2.7.1 Control and Accessories (C&A): Maintenance performed on controls and accessories shall be accomplished IAW specific C&A Manuals listed in the CMM. TCTOs listed in APPENDIX B shall be complied with on all control and accessories.

C.1.2.7.2 Vendor shall comply with 100% of Service Bulletins listed in APPENDIX B. Any additional Service Bulletins not listed in this SOW shall be completed and treated as Over and Above. The Special Inspections under Work Unit Code 27000 as listed in T.O. 1C-135-6 section 2, shall be 100% zeroed out (0) without regard to the time remaining on them. T.O. 1C135(K)R- 10 QEC Kit, 2J-F108 TCTO Series shall require 100% compliance of all TCTOs listed in APPENDIX B. Compliance will be documented on the CEMS report for each engine. In addition, the major overhaul documents shall also include Temporary Revisions that have not been incorporated in the above listed Technical Data.

C.1.2.8 Major Overhaul Deviations: Prior to contractor’s use in remanufacturing of F108/CFM56-2B TURBOFAN Engine and component part, the contractor shall obtain written approval from the PCO for any deviations from the processes, materials, or procedures outlined in ESM. The contractor’s request for deviation must show that the intent of process, materials, or procedures conform to processes required by the ESM and the Statement of Work (SOW).

AFLCMC/LPE and AFLCMC/LPSBA reserve the right to approve or disapprove any deviations

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

when they fail to meet intended configuration requirements of the F108/CFM56-2B TURBOFAN ENGINE, modules and component piece parts.

C.1.2.9 Designated Engineering Representative (DER) Processes and Procedures: Prior to contractor’s use in remanufacturing of F108/CFM56-2B TURBOFAN ENGINE or component parts, the contractor shall obtain written approval from the PCO for all DER processes and procedures.

C.1.2.10 Parts Manufacturing Approval (PMA): PMA will not be considered for use with this contract.

C.1.2.11 Quality System and Quality Assurance: The contractor shall maintain a quality system that addresses the elements of International Standard Organization (ISO) 9001- ANSI/ASQC9001. The Contractor shall deliver all maintained/remanufactured engines in a fully tested, serviceable condition. DCMA will provide contract oversight and monitor contractor quality and performance.

C.1.2.12 Use of Government Property / Material When material is furnished by the government, the supplier’s procedures shall include at least the following:

• Examination upon receipt, consistent with practicality, to detect damage in transit

• Inspection for completeness and proper type

• Periodic inspection and precautions to assure adequate storage conditions to guard against damage from handling and deterioration during storage

• Functional testing, either prior to or after installation, or both, as required by contract determine satisfactory operation

• Verification of quantity

• The supplier will report any Government Furnished Property / Material found damaged, malfunctioning, or otherwise unsuitable for use. In the event of damage or malfunction, during or after installation, the supplier shall determine and record probable cause and necessity for withholding from use.

C.1.2.13 Deficiency Report (DR) Investigation: At the Government’s request, the contractor shall investigate and submit findings to include root causes and a corrective action against all Deficiency Reports submitted to contractor against items manufactured, repaired or overhauled by this contract which are reported to be defective.

The Contractor shall follow its commercial practices for investigating reported deficiencies. A final report including root cause and any correction action plan shall be provided to Air Force within 60 calendar days.

C.1.2.14 Condemned Assets: F108/CFM56-2B MODULE assemblies and components that do not meet present major overhaul and inspection limits, shall be condemned at the contractor’s facility and processed through Plant Clearance Automated Reutilization Screening System (PCARSS) (ref. https://www.dcma.mil/WBT/PCARSS/ ). Condemnations shall be reported to AFLCMC/LPE, and 421 SMCS/GUMBA Technical Services to establish usage rates and cost planning.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

C.1.2.15 Packaging and Handling: The contractor shall utilize its commercial packaging and marking practices in lieu of MIL-STD-2073 or any other standard referenced herein. The contractor shall place a serviceable tag, Department of Defense (DD) Form 1574 inside the package along with the assembly. The contractor shall place another completed DD Form 1574 to the outside of the package.

C.1.2.16 Reporting: The contractor shall provide completed Certificate of Conformance documentation with each F108/CFM56-2B engine assembly and its component parts that have been overhauled with the intent of returning these assemblies or component parts to service.

This documentation shall have part number, serial number, work accomplished, Service Bulletins complied with, on serviceable tag, DD Form 1574. The contractor shall ensure that all reporting as specified under the following Contract Data Requirements is accomplished:

A001: AFMC Form 413 (Depot Maintenance Production Report) A002: Commercial Asset Visibility Air Force (CAVAF) Reporting, formerly CAVII A003:

Comprehensive Engine Management System (CEMS) Reporting

Data in accordance with the AFMC Form 413 report shall not be waived, although contractor’s format with all the same data elements as the AFMC Form 413 report may be accepted, if approved through the PCO. For CAVAF reporting, the contractor shall input the data IAW the Appendix B and CAVAF guide. Each Serial Number Engine and Module Component assembly is loaded into Comprehensive Engine Management System (CEMS) and all part number changes and TCTO accomplishment through major overhaul must be documented. In addition, the contractor shall submit Supply Discrepancy Reports (SDRs) when required IAW the contract’s Appendix B, “End Item and Government Furnished Equipment Management,” Section

7. Contractor shall process Deficiency Reports when required IAW Section C.1.2.12 of this SOW. AFMC Form 413 Depot Maintenance Production Reporting, CAVAF Reporting, Mishap Reporting, and Deficiency Reporting shall be on-time, correct, and complete.

C.1.2.17 Shipping and Transportation: The contractor shall ship or transport applicable assets as appropriate in order to have the assets available to support the customer’s operational requirements and IAW the contract. The contractor shall not destroy reusable shipping containers, and will reuse them for return shipment. Engines must be shipped on a serviceable engine trailer IAW applicable technical data. The Engines shall be properly prepared and shipped IAW T.O. 2J-1-18, and T.O. 00-85-20. Contractor is responsible for remanufacturing/returning damaged engine shipping trailers to serviceable condition IAW applicable technical data. The Contractor shall meet negotiated delivery schedule.

C.1.2.18 Mission Essential Services: The contractor shall prepare for the continuation of essential DoD services during crisis IAW DFARS 252.237-7023.

C.1.2.19 Contractor Performance Objectives: Contractor performance shall be measured and assessed, using Performance Objectives listed in Table 1-1.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

Table 1-1

Performance Objective Reference/ Paragraph (Para)

Performance Threshold and Objective

PO-1 Reporting:

AFMC Form 413 Depot Maintenance Production Reporting; CAVAF Reporting;

Mishap Reporting; and Deficiency Reporting shall be on-time, correct, and complete

SOW

Para C.1.2.16

For each respective reporting period:

• Threshold: no more than

2 errors per report.

• Objective 100% error free

• Upon notice of complaint, the contractor shall submit a corrective action plan.

PO-2 Quality Product:

The Contractor shall deliver all maintained / remanufactured engines in a fully tested, serviceable condition.

SOW

Para C.1.2.11

• Threshold: no more than 2 minor defects per engine

• Objective: 100% defect free

PO-3 Delivery Performance:

The Contractor shall meet the delivery schedule

SOW

Para C.1.2.16 And IAW Contractual Delivery Schedule

F108 engine assemblies shall be delivered IAW the contractual delivery schedule.

• Threshold is 98% on time delivery

• Objective is 100% on time delivery

C.1.2.20 Contractor Performance Evaluation: Evaluation will occur when the F108/CFM56-2B TURBOFAN ENGINE assembly Government PMS or PCO evaluates the performance of the contractor to determine whether or not it meets the performance objectives of the contract. In the event the performance measure is not met, the PCO will issue written notification to the contractor. In cases where the contractor fails to implement corrective action, the PCO will take appropriate measures.

PO - 1: The contractor's failure to meet the requirement for this item shall result in remedies as allowed under Federal Acquisition Regulation (FAR) 52.212-4(a) Inspection/Acceptance. Increased surveillance through Defense Contract Management Agency (DCMA) and AFLCMC can be requested as needed.

PO - 2: The contractor's failure to meet this requirement shall result in remedies as allowed under FAR 52.212-4(a) Inspection/Acceptance subject to the sole remedy of the Government for Single Engine Exhaust Gas Temperature (“EGT”) Margin Guarantee.

Increased surveillance through DCMA and AFLCMC can be requested as needed.

PO - 3: The contractor's failure to meet this requirement shall result in remedies as allowed under FAR 52.212-4(a) Inspection/Acceptance subject to the sole remedy of the

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

Government for Turn Around Time (“TAT”) Guarantee. Increased surveillance through DCMA and AFLCMC can be requested as needed.

C.2.0 MATERIAL

C.2.1 Kits

A complete C-PUP (CFM Propulsion Upgrade) kit will be provided to the Contractor by the USAF for each engine. The kit will be shipped by the USAF to the Contractor’ maintenance facility prior to induction. It is incumbent upon the Contractor to accurately provide kit demand to the USAF in anticipation of maintenance production capability so that kits are in place prior to each engine’s induction. The Contractor shall include the kit ship-to address in their proposal.

Quick Engine Change (QEC) kits will be provide by the Contractor and included in the Contractor’s quoted price for F108 whole engine price. Reference T.O. 1C135(K)R-10 QEC Kit.

C.2.2 Unanticipated Maintenance and Parts Over and Above

Unanticipated maintenance consists of maintenance required for engine issues discovered during the typical overhaul and upgrade of the engine from the F108-100 to the F108-100A.

Over and above does not apply to parts contained in the Government-provided C-PUP kits or identified in this SOW for contractor sourcing and specified at technical data (e.g., TC/TOs, Service Bulletins, etc.) incorporated herein. All unanticipated maintenance and required parts identified for the engine shall be brought to the attention of Cognizant Engineering Authority and contracting officer for disposition. The Contractor shall adhere to clause 252.217-7028 and will bill unanticipated maintenance and parts over and above against CLIN 0002.

All installed parts must be capable of meeting the designed functional capabilities as specified in applicable ESM prior to installation.

During work on an engine if an obvious defect is discovered in an area that is not related to the problem driving removal of the engine, then the defect shall be brought to the attention of Cognizant Engineering Authority and contracting officer for disposition. The Contractor shall follow CFR 252.217-7028 if beyond the work scope of this contract is required.

C.3.0 Seed Engines

The USAF will provide five ‘seed’ engines at the beginning of the period of performance. The Contractor will utilize the seed engines to prime their maintenance production activities. Build-up of the seed engines will be accounted for in the schedule for the first year Period of Performance. At contract award, the Contractor will coordinate the transfer of the five engines from Tinker Air Force Base to the repair location. Seed engines shall be overhauled and delivered to the Air Force at the end of the contract.

C.4.0 Module or Component Support

During the course of this contract the Government may require additional module or component support to supplement organic engine depot production. If a requirement were to develop, the

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

Government will submit a formal request followed by negotiations of cost and schedule. Agreed upon contractual actions will be formalized under contract modification.

C.5.0 CEMS Access and Training

The Contractor is required to have access to CEMS which also requires a government issued Common Access Card (CAC). Additionally, the Contractor is required to provide CAC readers for use with their computers. The Government will coordinate issuance of CAC cards to Contractor personnel.

C.6.0 Program Management Reviews (PMR)

PMRs shall occur at a minimum on an annual basis and may be more frequently during the contract implementation to provide assurance to the USAF of successful execution. The intent of the PMR is to monitor and assess contract performance against contract objectives and defined contract requirements, and to coordinate responses and foster solutions to challenges encountered during and after contract implementation.

If Contractor performance warrants it, the PCO may expand the PMRs to semi-annually and shall provide the Contractor written notification no later than 45 days prior to the next scheduled PMR. If performance warrants it, the PCO or Contractor can reinstate the original PMR requirements at the conclusion of a semi-annual PRB. Less formal in-process meetings, occurring telephonically, are anticipated to occur throughout the contract term, as necessary.

PMRs shall be held in-person, if possible, at predetermined locations. In general, the Contractor shall host the PMR at their remanufacture facility, where contract performance takes places.

The PMRs shall be co-chaired by the USAF and the Contractor, with DLA-A program and PCO participation, as appropriate. The Contractor shall develop an agenda (in accordance with the list of elements below and as approved by the PCO) and distribute the agenda to prospective attendees no later than five (5) days before the PMR.

During the PMR, the Contractor shall provide status of schedules and support goals, any process improvement initiatives, and provide status on the following elements:

1) Support Overview – to include overall schedule status (Delays, Concerns)

2) Impact to USAF War Reserve Engines (WRE) Goals

3) Performance to C.1.2.19 and C.1.2.20

4) Supplier Issues

5) Item Support Issues

6) Quality/Safety Issues

7) Obsolescence / DMSMS Issues

8) Other Issues or Challenges

9) Opportunities to further the partnership and overall repair performance

10) Previous PMR Open Action Items/New Action Item

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

The Contractor shall submit PMR minutes for approval by the PCO within 10 days after each PMR. Other Program Reviews may be conducted as mutually agreed between the Government and the Contractor. The Government and the Contractor are mutually responsible for tracking and resolving, as appropriate, action items identified during the PMR. Action items shall be assigned aggressive due dates and shall be the first agenda item on subsequent PMRs.

Page

NAME OF OFFEROR OR CONTRACTOR

50336-101 NSN 7540-01-152-8067

US GOVERNMENT PRINTING OFFICE 1990-262-081

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

SECTION I

CONTRACT CLAUSES

SECTION D

DFARS 252.211-7006 PASSIVE RADIO FREQUENCY IDENTIFICATION (MAR 2018)

SECTION E

FAR 52.246-11 HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (DEC 2014)

(a) The Contractor shall comply with the higher-level quality standard(s) listed below.

AS 9100 Most Recent Version [Contracting Officer insert the title, number (if any), date, and tailoring (if any) of the higher-level quality standards.]

(b) The Contractor shall include applicable requirements of the higher-level quality standard(s) listed in paragraph (a) of this clause and the requirement to flow down such standards, as applicable, to lower-tier subcontracts, in-

(1) Any subcontract for critical and complex items (see 46.203(b) and (c)); or

(2) When the technical requirements of a subcontract require-

(i) Control of such things as design, work operations, in-process control, testing, and inspection; or

(ii) Attention to such factors as organization, planning, work instructions, documentation control, and advanced metrology.

SECTION F

FAR 52.211-17 DELIVERY OF EXCESS QUANTITIES (SEP 1989)

FAR 52.247-48 FOB DESTINATION – EVIDENCE OF SHIPMENT (FEB 1999)

FAR 52.247-58 LOADING, BLOCKING, AND BRACING OF FREIGHT CAR SHIPMENTS

(APR 1984)

SECTION G

DFARS 252.232.7006 WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)

SECTION H

DFARS 252.223-7001 HAZARD WARNING LABELS (DEC 1991)

(c) The Offeror shall list which hazardous material listed in the Hazardous Material Identification and Material Safety Data clause of this contract will be labelled in accordance with one of the Acts in

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

paragraphs (b)(1) through (5) of this clause instead of the Hazard Communication Standard. Any hazardous material not listed will be interpreted to mean that a label is required in accordance with the Hazard Communication Standard.

MATERIAL (If None, Insert “None.”) ACT

SECTION I

FAR 52.203-19 PROHIBITION ON REQUIRIN CERTAIN INTERNAL CONFIDENTIALITY

AGREEMENTS OR STATEMENTS (JAN 2017)

DFARS 252.203-7000 REQUIREMENTS RELATING TO COMPENSATION OF FORMER DOD

OFFICIALS (SEP 2011)

DFARS 252.203-7002 REQUIREMENT TO INFORM EMPLOYEES OF WHISTLEBLOWER

RIGHTS (SEP 2013)

DFARS 252.203-7003 AGENCY OFFICE OF THE INSPECTOR GENERAL (AUG 2019)

FAR 52.204-4 PRINTED OR COPIED DOUBLE-SIDED ON POSTCONSUMER FIBER

CONTENT PAPER (MAY 2011)

FAR 52.204-9 PERSONAL IDENTITY VERIFICATION ON CONTRACTOR PERSONNEL

(JAN 2011)

FAR 52.204-12 UNIQUE IDENTITY IDENTIFIER MAINTENANCE (OCT 2016)

FAR 52.204-13 SYSTEM FOR AWARD MANAGEMENT MAINTENANCE (OCT 2018)

FAR 52.204-23 PROHIBITION ON CONTRACTING FOR HARDWARE, SOFTWARE, AND

SERVICES DEVELOPED OR PROVIDED BY KASPERSKY LAB AND OTHER COVERED

ENTITIES (JUL 2018)

FAR 52.204-25 PROHIBITION ON CONTRACTING FOR CERTAIN TELECOMMUNICATIONS

AND VIDEO SURVEILLANCE SERVES OR EQUIPMENT (AUG 2019)

DFARS 252.204-7000 DISCLOSURE OF INFORMATION (OCT 2016)

DFARS 252.204-7003 CONTROL OF GOVERNMENT PERSONNEL WORK PRODUCT (APR

1992)

DFARS 252.204-7004 LEVEL I ANTITERRORISM AWARENENSS TRAINING FOR

CONTRACTORS (FEB 2019)

DFARS 252.204-7008 COMPLIANCE WITH SAFEGUARDING COVERED DEFENSE

INFORMATION CONTROLS (OCT 2016)

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

DFARS 252.204-7009 LIMITATIONS ON THE USE OR DISCLOSURE OF THIRD-PART

CONTRACTOR INFORMATION (OCT 2016)

DFARS 252.204-7012 SAFEGUARDING COVERED DEFENSE INFORMATION AND CYBER

INCIDENT REPORTING (OCT 2016)

DFARS 252.205-7000 PROVISION OF INFORMATION TO COOPERATIVE AGREEMENT

HOLDERS (DEC 1991)

FAR 52.209-1 QUALIFICATION REQUIREMENTS (FEB 1995)

DFARS 252.209-7004 SUBCONTRACTING WITH FIRMS THAT ARE OWNED OR

CONTROLLED BY THE GOVERNMENT OF A COUNTRY THAT IS A STATE SPONSOR OF

TERRORISM (MAY 2019)

DFARS 252.211-7003 ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2016)

DFARS 252.211-7005 SUBSTITUTIONS FOR MILITARY OR FEDERAL SPECIFICATIONS

AND STANDARDS (NOV 2005)

SPI Process: ____________________________________________________ (Vendor Fill-in) Facility: _________________________________________________________ (Vendor Fill-in) Military or Federal Specification or Standard: ________________________________________ ________________________________________________________________ (Vendor Fill-in) Affected Contract Line Item Number, Subline Item Number, Component, or Element:

________________________________________________________________ (Vendor Fill-in)

DFARS 252.211-7008 USE OF GOVERNMENT-ASSIGNED SERIAL NUMBERS (SEP 2010)

FAR 52.212-4 CONTRACT TERMS AND CONDITIONS – COMMERCIAL ITEMS (OCT 2018)

FAR 52.212-5 CONTRACT TERMS AND CONDITIONS REQUIRED TO IMPLEMENT

STATUTES OR EXECUTIVE ORDERS – COMMERICAL ITEMS (AUG 2019)

(a) The Contractor shall comply with the following Federal Acquisition Regulation (FAR) clauses, which are incorporated in this contract by reference, to implement provisions of law or Executive orders applicable to acquisitions of commercial items:

(1) 52.203-19, Prohibition on Requiring Certain Internal Confidentiality Agreements or Statements (Jan 2017) (section 743 of Division E, Title VII, of the Consolidated and Further Continuing Appropriations Act, 2015 (Pub. L. 113-235) and its successor provisions in subsequent appropriations acts (and as extended in continuing resolutions)).

(2) 52.204-23, Prohibition on Contracting for Hardware, Software, and Services Developed or Provided by Kaspersky Lab and Other Covered Entities (Jul 2018) (Section 1634 of Pub. L. 115-91).

(3) 52.204-25, Prohibition on Contracting for Certain Telecommunications and Video Surveillance Services or Equipment. (Aug 2019) (Section 889(a)(1)(A) of Pub. L. 115-232).

(4) 52.209-10, Prohibition on Contracting with Inverted Domestic Corporations (Nov 2015).

https://www.acquisition.gov/content/52203-19-prohibition-requ…