Multi-Engine Repair Services FINAL DRAFT SOW PWC and GE Engines 20240123 1114.docx

STATEMENT OF WORK (SOW)

ATTACHMENT 1

REPAIR/OVERHAUL/MODIFICATION OF

PRATT & WHITNEY CANADA (PWC) TURBINE AIRCRAFT ENGINES

and GENERAL ELECTRIC (GE) T700 (series) TURBINE AIRCRAFT ENGINES (Insert Contract or IDIQ Number, and/or Task Number) 23 January 2024

Table of Contents

BACKGROUND

1.1. The United States Department of State (DoS), Bureau for International Narcotics and Law Enforcement Affairs, Office of Aviation (INL/A) provides aviation support for the eradication and interdiction of illicit drugs, training of contractor and host nation personnel, embassy transport support, movement of personnel and equipment, reconnaissance, personnel recovery (PR), medical evacuation, security of personnel and equipment, and ferrying of aircraft. In support of the above referenced missions, INL/A presently maintains a fleet of fixed and rotary wing aircraft (various types) utilizing Pratt & Whitney Canada (PWC) turbine engines (various models) and General Electric (GE) T700 (series) engines.

The engine type, manufacturer (OEM), and model is based upon the DoS present aircraft fleet type, model, and quantities. The DoS has and is likely to add to and delete from its present aircraft fleet over the period of performance of this contract. The contractor may be required to provide support for engines not presently listed in Table 2.1 below based on aircraft fleet changes over time.

SCOPE

1.2. INL/A requires, on an as needed basis, for a period of five (5) years an Original Equipment Manufacturer (OEM) approved source/s to provide limited life cycle support (overhaul, repair, conversion, and/or modification) of DoS aircraft turbine engines listed on but not limited to Table 2.1 below. The OEM approved source/s must have the capability to overhaul, repair, convert and modify engines to the most current OEM specifications to include but not limited to the following:

· all applicable OEM production, repair and overhaul specifications

· all OEM Service Bulletins (SBs)

· all Federal Aviation Administration (FAA) and Transport Canada Airworthiness Directives (ADs)

· Department of the Army standards including Safety of Flight (SOF) messages, Aviation Safety Action Messages (ASAM), Aviation Maintenance Action Messages (AMAM), Maintenance Information Messages (MIM), Technical Bulletins (TB), Modification Work Orders (MWO), etc.

Table 2.1

Engine Model / Aircraft

On AC

ASL

Stock

Total Projected OH/ Repairs (5yrs)

REQUIREMENTS

1.3. Certification

1.3.1. The Contractor/Repair facility used shall be a Pratt & Whitney Canada (PWC) and General Electric (GE) approved facility as applicable specializing in the inspection, testing, troubleshooting, cleaning, overhauling, repairing, conversion, modification and preservation of turbine aircraft engine power units, modules, and components of the engines identified in Table 2.1 as a minimum requirement.

1.3.2. The Contractor/Repair facility shall be a FAA Part 145 authorized repair station, maintain current ISO 9001: 2015 and AS 9110 certification and be certified by the OEM to perform engine overhaul/repair/modification and maintain current licensure and certifications throughout the contract period of performance. The prime contractor shall ensure all subcontractors and other vendors are properly certified to perform the component work or service required.

1.3.3. Should it become necessary for the contractor/vendor to have repairs or overhauls performed at one of their Repair Stations located Outside the United States and its Territories; the Repair Station(s) shall be in compliance with FAA Order 8900.1 for Certifying/Renewing/Amending 14 CFR Part 145 Certification and not Under a Maintenance Implementation Procedure (FAA Order 8900.1, VOL 2, CHAP 11, SECT 3) and be EASA Part-145 Certified (FAA Order 8900.1, VOL 2, CHAP 11, SECT 7).

1.3.4. If the Contractor’s facility, for any reason, loses its Federal Aviation Administration (FAA) certification, ISO 9001: 2015 and AS9110 certification, or PWC/GE OEM certification or any combination thereof for any engine type or model identified in this SOW during the period of performance, this will constitute a material breach of contract, which may, at the discretion of the Contracting Officer (CO), result in contract termination. The Contractor shall notify the CO verbally and in writing, not later than five (5) calendar days after any certification loss, forfeiture, revocation, suspension for any reason and disclose all facts relevant to the certification loss. (CDRL A001)

1.3.5. Technician qualifications. All Pratt & Whitney Canada (PWC) and General Electric (GE) turbine aircraft engine technicians working on DoS assets shall be qualified, trained, and certified for FAA Part 145 turbine aircraft engine maintenance, quality systems and engineering services.

1.4. Capabilities

1.4.1. The Contractor shall be responsible for all necessary resources required to perform the services required and comply with all OEM and regulatory certification requirements. This includes, but is not limited to, technically qualified, trained, and certified personnel, quality systems, required tooling, manuals, test equipment, parts, material, engineering services, management, maintenance, documentation, preservation, and shipping of engine power units, modules, and components. All special tooling, test equipment, and engine test cells shall be FAA or OEM approved. Engine test cells must be correlated to the engine type under test using FAA-approved correlation procedures or be an OEM correlated test cell. Engines must be tested and certified by the repair station in accordance with current OEM procedures for the engine type under test.

1.4.2. Utilizing the support items from the previous section (3.2.1 of this SOW), the Contractor shall maintain the expertise necessary to satisfactorily inspect, test, troubleshoot, clean, overhaul, repair, modify, and preserve PWC and GE engine power units, modules, and components IAW OEM specifications, to include the most current revisions of PWC and GE applicable Technical Data and Drawings, Maintenance, Repair and Overhaul (MRO) manuals, Service Bulletins (SB), Alert Service Bulletins (ASB), Service Instruction Letters (SIL), and/or other PWC and GE Airworthiness Directives (AD) to include all FAA and Transport Canada directives as applicable.

1.4.3. When modifying GE engine series T700-GE-700/701 to OEM T700-GE-701/C/D specifications, the Contractor shall be familiar with and comply with the General Services Administration (GSA), Federal Management Regulation (FMR), Subchapter B, Part 102-33.115, Acquiring Government Aircraft and Aircraft Parts, rules pertaining to Flight Safety Critical Aircraft Parts (FSCAP) and FAA Advisory Circular 20-142.

1.4.4. All GE T700 Series engines must be maintained to Department of the Army standards, i.e., Safety of Flight (SOF) messages, Aviation Safety Action Messages (ASAM), Maintenance Advisory Messages (MAM), Maintenance Information Messages (MIM), Technical Bulletins (TB), Modification Work Orders (MWO), etc.

1.5. Warranty

1.5.1. The Contractor shall establish, provide, and deliver a warranty plan (CDRL A001) to ensure that all replacement parts and workmanship are covered by warranty. The warranty plan shall provide a warranty repair process to include, but not limited to, procedures for notification, processing, validation, length of warranty from time of return shipment from vendor facility, shipping instructions and a point of contact (POC) between the Contractor and INL/A. At a minimum, the warranty plan shall ensure each engine, component or accessory overhauled, reworked, repaired or supplied is free of defects in performance, material condition, and workmanship under normal use and service.

1.5.2. Engine Overhaul. All DoS overhauled engines shall be warranted to be free of defects in workmanship for a period of 2 years/1,000 operational hours from date of return shipment, whichever comes first. All overhauled engines shall be received in a Ready For Issue condition and ready for installation in an aircraft with no defects in performance or material condition.

1.5.3. Engine Repair. All DoS engine repairs shall be warranted to be free of defects in workmanship for 1 year/1000 operational hours from date of return shipment, whichever comes first. All repaired engines shall be received in a Ready For Issue condition and ready for installation in an aircraft with no defects in performance or material condition.

1.5.4. New Engine Parts. Warranty on new parts installed during engine overhaul or repairs shall meet or exceed a minimum warranty period of 2 years/1,000 operational hours from date of return shipment of engine to DoS or as supported by the engine/parts manufacturer’s warranty. The Contractor shall act on behalf of the United States Government (USG) in the processing of claims or adjustments arising out of, and because of, defective parts, materials, and workmanship as applicable. The contractor shall provide new parts warranty documentation at the request of the USG.

1.5.5. Repaired/Overhauled Engine Parts. Warranty on repaired/overhauled parts, components and accessories installed during engine overhaul or repairs shall meet or exceed a minimum warranty period of 1 year/1,000 operational hours or 1 year from date of return shipment of engine to DoS or as supported by the repaired/overhauled parts vendor’s warranty. The Contractor shall act on behalf of the USG in the processing of claims or adjustments arising out of, and because of, defective parts, materials, and workmanship as applicable. The contractor shall provide repaired/overhauled parts warranty documentation at the request of the USG.

1.5.6. All warranty discrepancies shall be validated, corrected, return shipped and accepted by INL/A in a timeframe not to exceed 210 calendar days from initial notification. The Contractor shall expedite the repair or replacement of validated and warranted defective components at the Contractor’s expense.

1.5.6.1. The Contractor shall expedite the repair or replacement of validated and warranted defective components at the Contractor’s expense.

1.5.6.2. Non-validated warranty repairs shall be quoted and expensed to INL/A utilizing the Procedures established in section 3.8 of this SOW.

1.6. Documentation

1.6.1. The Contractor shall provide the following documentation for each PWC and GE engine contracted repair/overhaul/modification event:

1.6.1.1. Vendor specific repair/overhaul documentation to include but not be limited to Teardown Inspection Report (TIR), photos, engine log, engine history record, engine operating record, engine maintenance record, maintenance release record, and all engine test cell run/s data and findings record.

1.6.2. Department of the Army (DA) specific forms In Accordance With (IAW) Department of the Army Pamphlet (PAM) 738-751. Specific forms include but are not limited to DA Form 2408-5-1 (Equipment Modification Record (Component)), Form 2408-16 (Aircraft Component Historical Record), DA Form 2419 (Aircraft Engine Turbine Wheel Historical Record) DA Form 2408-20 (Oil Analysis Log)

1.6.3. FAA airworthiness Form 8130-3, Certificate of Conformance (CoC) and other FAA authorized airworthiness forms as required or requested by INL/A. The Certificate of Conformance (CoC) shall contain detail of work performed with emphasis on all life limited tracked parts replaced to include at a minimum the Part Number, Serial Number with identification of “New”, “Overhauled” or “Serviceable”; List of compliance with all applicable Airworthiness Directives, Service Bulletins and/or other required instructions.

1.7. Test Cell Certification

1.7.1. The Contractor shall only utilize an FAA or OEM correlated and certified engine performance run test cell/s for all DoS engines to determine acceptable engine performance to include placing a load on the engine to simulate flight conditions on each post repair test cell full performance run.

1.7.2. The contractor shall provide all test cell performance run documentation for government approved induction test cell run/s as part of an engine evaluation. The contractor shall maintain and provide to INL/A all post repair and ad-hoc engine performance test cell run/s documentation and records.

1.7.3. The contractor shall maintain, and make available to the USG documentation during the period of performance of this contract that states the contractor maintains or has access for use, a currently certified Pratt & Whitney Canada (PWC) and General Electric (GE) turbine aircraft engine performance run test cell/s to determine acceptable engine performance for DoS turbine aircraft engines in accordance with the requirements in this SOW.

1.8. Shipping

1.8.1. All engines requiring service will be shipped from/to the INL/A Logistics Center in Melbourne, Florida unless otherwise directed by the government. Upon notification from the CO, or his/her designated INL/A representative, DoS engines or components that require service the Contractor shall coordinate shipping schedules and verify assets are ready for shipment. Within seven (7) days after consensus between the two organizations has been reached, the Contractor shall take all the necessary actions required to take possession and ship engines from the INL/A Logistics Center at

US Department of State, Logistics Division 2765 Business Center Blvd Melbourne, FL 32940 to the Contractor’s repair facility and return the asset to same location. The contractor shall provide to the government a Bill of Lading (BOL) in advance of scheduled pickup and delivery dates. Scheduled pickup and delivery dates shall be coordinated during normal INL/A workdays and working hours. The Contractor shall utilize only transportation carriers that are certified (both drivers and equipment) to transport engines and components. The Contractor shall be responsible for any International Traffic in Arms Regulation (ITARs) and all required customs clearances and documentation.

1.8.2. The Contractor shall notify, in writing, the CO or his/her representative confirming receipt of all engines and components. Notification of item receipts shall include, but are not limited to, the following information: Nomenclature, Part Numbers (P/N), Serial Numbers (S/N), Contract Number, Contract Line Item Numbers (CLIN), and dates of receipt. Notifications of item receipts via email are acceptable and may contain single or multiple notification entries. (CDRL A003)

1.9. Inventory Upon Arrival

1.9.1. Upon arrival at the Contractor facilities, an incoming inventory shall be performed on all engines, power units, modules, components, and shipping containers. If inventory irregularities are identified upon receipt of an engine or components, the Contractor shall notify the CO, or his/her representative, within ten (10) calendar days of receipt of shipment. The CO, or his/her representative will provide guidance for inventory shortages within ten (10) calendar days of receipt of notification by the Contractor. If no guidance is received from the CO, or his/her representative after 10 calendar days, the Contractor shall quote and highlight the costs associated for replacement and/or repair of missing inventory within the quote for repair/overhaul of the engine assembly (section 3.8 of this statement of work (SOW)) under a sub-heading labeled “Shortage upon Arrival”. Notifications of missing inventory discrepancies via facsimile/email are acceptable and may contain single or multiple notification entries. (CDRL A004).

1.9.1.1. Missing Components: Within ten (10) calendar days after the receipt and inspection of the components, the Contractor shall notify the CO, or his/her representative in writing of any missing parts or sub-assemblies required for final inspection and acceptance. (CDRL A004)

1.9.1.2. Counterfeit or Suspect Components: Upon receiving components exhibiting evidence of being counterfeit, the Contractor shall notify the CO, or his/her representative in writing (CDRL A004) and in detail, within ten (10) calendar days and discontinue all actions until receipt of written authorization to proceed from the CO. The CO reserves the right to appoint a technical representative who shall witness the remaining teardown and inspection of the component.

1.9.1.3. INL/A reserves the right to provide OEM approved, documented, and traceable Government Furnished Property (GFP) to replace parts or hardware identified as missing or determined to be unserviceable.

1.10. Incoming Inspections

1.10.1. Incoming inspections shall be performed on all engines, power units, modules, components and shipping containers. Once assets are received at the Contractor’s facility, the Contractor has 45 calendar days to inspect and evaluate the engine for all necessary repairs. The engine inspection and evaluation report shall reflect all costs associated to repair or overhaul engine power units, modules, and components to current OEM and FAA specification standards. All applicable Service Bulletins (Category 1 through 6) for the specific engine model will be incorporated during repair or overhaul. Once the inspection has been accomplished, the Contractor shall submit to the CO, or his/her designated representative a teardown, inspection, and analysis report (TIR) (CDRL A002) for the affected engine along with a written quotation (CDRL A005) for all actions necessary (repair, overhaul, or modification) and projected time to bring the affected engine up to current OEM standards. Notifications via email are acceptable and may contain single or multiple notification entries. No further expenses shall be incurred against the affected engines without direction from the CO, or his/her representative. Any additional (Over and Above (O&A)) work identified during the engine repair process shall be communicated to the DoS at earliest and followed by a written quote to include any pertinent documentation and pictures for review and written approval to proceed with the additional repair and costs. The CO, or his/her designated representative will review all repair quotes and will direct the Contractor to execute one of the following actions:

1.10.1.1. Quotation is acceptable: Contractor shall execute all actions as stated in the quotation after receipt of the corresponding Task Order.

1.10.1.2. Partial Approval: Contractor shall execute only quoted items specified by the CO, or his/her designated representative.

1.10.1.3. Beyond Economical Repair (BER): When the cost of returning the engine to a serviceable condition exceeds the replacement cost of that asset or when the engine or component cannot be restored due to damage or wear beyond the material properties, characteristics, or specifications of the item being repaired, the Contractor upon direction from the CO, or his/her designated representative shall take the necessary actions to demilitarize and dispose of the non-serviceable components/equipment per the DoS Property Administer approved property disposal plan addressed in section 3.9 of this SOW. All remaining serviceable engine parts, components, assemblies, etc. shall be returned to the DOS or may be retained by the contractor at the discretion of the government for future use, whichever course of action may be applicable.

1.10.1.4. Core Exchange: Core exchanges for engines, assemblies, components, equipment. When in the process of evaluation or repair it becomes evident the engine will exceed economical repair cost/Beyond Economical Repair (BER) the contractor shall notify the government prior to submitting a repair quote. The government may at that time elect to inquire about and execute an engine “core exchange” if the contractor has a serviceable engine to replace the BER engine via “Purchase of Engine” CLIN. The contractor shall prepare and provide a proposal for a replacement engine with the “core exchange” credit amount and the catalog price of a new/repaired/overhauled engine included and highlighted in the proposal.

1.10.1.5. Engine Purchase. The Contractor shall submit a proposal for each engine purchase request to the Contracting Officer or the Contracting Officer's Representative (COR) for approval in advance. New/Repaired/Overhauled engines must meet the most recent Original Equipment Manufacturer (OEM) et al criteria as described in Section 2 - Scope of the Statement of Work. Also, to be included with the engine shall be a serviceable condition metal engine shipping and storage container designed to be used for the specific engine type. All engines purchased shall be covered under the warranty plan as described under Section 3.3 – Warranty of the Statement of Work. The Contractor shall provide all relevant documentation and historical logs for each engine.

1.11. Property Disposal Plan

1.11.1. The Contractor shall develop a USG approved property disposal plan based on Federal Acquisition Regulations (FAR) Part 52.245, and Subpart 45 and approved by the DoS Government Property Administrator. (CDRL A006)

1.12. Turn Around Time

1.12.1. Once authorization to proceed has been given to execute the actions specified by the CO, or his/her designated representative in section 3.8 (item #3.8.1.1 and item #3.8.1.2 only) of this SOW, the Contractor, upon given the notice to proceed, shall have a maximum of 180 calendar days from the time of notification to accomplish the tasks necessary to repair, overhaul, modify, and deliver the affected engine and or components to the INL/A Logistics Center in Melbourne, Florida. Unless otherwise specified by the CO, early completion of repair/overhaul/modification of USG assets is authorized and encouraged. The time to accomplish item #3.8.1.3 of this SOW shall be IAW the approved Contractor developed USG approved property disposal plan from section 3.9 of this SOW.

1.13. Environmental Requirements

1.13.1. All engine parts must be thoroughly cleaned IAW applicable OEM repair/overhaul manuals. In lieu of specific Pratt & Whitney cleaning procedures, the repair facility must utilize FAA Advisory Circular 43-205, Guidance for Selecting Chemical Agents and Processes for Depainting and General Cleaning of Aircraft and Aviation Products, to ensure they are as free as practicable of all hazardous dust to include hexavalent chromium, cadmium, lead, etc., prior to being returned to DoS. DoS may take random samples of parts to ensure they are free as practicable of all hazards. Information on these hazards can be found in Occupational Safety and Health Standards 1910.1025 (lead), 1910.1026 (Hexavalent Chromium) and 1910.1027 (Cadmium).

1.14. Replacement Parts Used During Overhaul or Repair

1.14.1. All replacement parts utilized in the overhaul or repair of DoS engines shall be traceable new OEM parts or parts and materials that are OEM authorized, traceable, and overhauled IAW applicable specifications. FAA certified Parts Manufacturer Approval (PMA) replacement parts are not acceptable for use on INL/A engines.

1.14.2. Component parts determined to be in serviceable condition IAW OEM specifications and functional testing can be reused.

1.14.3. All life limited parts that are reused shall have sufficient time and/or cycles remaining to reach the next scheduled heavy maintenance action or next scheduled hot end inspection.

1.15. Maintenance and Repair

1.15.1. All internal and external engine components and accessories shall be repaired or overhauled by an approved PWC or GE facility using approved technical data as applicable.

1.15.2. All Fuel Regulators, Fuel Controls and Governors shall be overhauled in accordance with PWC and GE data by an approved vendor/facility as applicable.

1.16. Work In Progress Discrepancies or Safety of Flight (SOF) identified discrepancies.

1.16.1. If additional in-work or in-progress discrepancies are identified after the initial Teardown Inspection Report (TIR) (CDRL A002) and quote (CDRL A005) has been submitted, funded and approved, the Contractor shall submit a revised quote to the USG for review, funding and approval of the increased repair effort and costs. All quote approvals must be in writing from CO or his/her designated representative.

1.16.2. In conjunction with section 3.14.1 of this SOW, if unforeseen SOF items are directed from the OEM, FAA, Transport Canada, or the CO, the Contractor shall submit a revised quote to the USG for review, funding and approval of the increased repair effort and costs. All quote approvals must be in writing from an authorized USG representative.

1.16.3. Under no circumstances is the Contractor authorized to exceed, without CO or his/her designated representative’s authorization, the previously agreed upon cost to repair quote (CDRL A005).

1.17. Test Cell Engine Performance Runs

1.17.1. Test cell engine performance runs (full performance run) shall be performed for all post manufacture, maintenance, repair, overhaul, or modification events. The contractor shall request and obtain government approval to prior to performing an induction test cell run/s as part of an engine evaluation. Additionally, the Contractor shall confirm all test cell engine run and performance documentation is included with the documentation package returned to INL/A (IAW with this SOW, section 3.5). Additionally, the Contractor shall perform and document all post engine run Foreign Object Damage (FOD) inspections, leak checks, filter changes, cleaning, oil analysis, and preservation have been accomplished IAW OEM specifications prior to shipment.

1.18. Return Shipping

1.18.1. The Contractor shall not ship any DoS assets utilizing unserviceable shipping materials. Engines shall be preserved, packaged, and marked (IAW section 9 of this SOW), and secured IAW OEM instructions prior to shipment. Prior to shipment, the USG reserves the right to inspect the engine, shipping container, and all technical documentation and paperwork.

1.18.2. The Contractor shall return ship (FOB destination) engines to the INL Logistics Center in Melbourne, Florida, utilizing procedures from section 3.6 and section 4.0 of this SOW.

1.19. Technical Field Service Support

1.19.1. On-Site Technical Assistance. On an as needed basis, DoS may require technical assistance which may require Contractor personnel to travel to/from locations away from the Contractor’s facility. Examples include but are not limited to minor repairs, warranty repairs, performance evaluations, accident investigations, engineering assistance, training, etc. When requested by the CO, or his/her designated representative, the Contractor shall send personnel to the required location to support DoS requirements. DoS expects no more than 200 man-hours/year will be required for technical assistance away from the Contractor’s facility.

1.20. Status Reporting

1.20.1. The Contractor shall submit a formal status report for each engine in the repair cycle. The report shall be submitted to the CO, and his/her designated representative, on the first and third Monday of each month. (CDRL A007)

DELIVERY

1.21. All completed engines, modules, and components shall be delivered (FOB Destination) to the following address:

US Department of State, Logistics Division 2765 Business Center Blvd Melbourne, FL 32940

1.22. Engines shall be delivered to the address in section 4.1 of this SOW no later than 187 calendar days after initial receipt at the Contractor’s repair facility unless a different date has been negotiated with the CO. Early delivery is encouraged.

GOVERNMENT FURNISHED PROPERTY

1.23. Aircraft Engines (various models) listed in Table 1

PLACE OF PERFORMANCE

1.24. Engine maintenance, repair, overhaul, and/or modification shall be accomplished at OEM approved facilities described in section 3.1 of this SOW.

PERIOD OF PERFORMANCE

1.25. The Contractor shall provide the services required in this SOW for a period of five (5) years from Contract award.

APPLICABLE DOCUMENTS

1.26. All OEM technical drawings, shop, inspection, repair and overhaul, or other OEM Component Maintenance Manuals (CMMs) and revisions as applicable to specific engine power units, modules, and components.

1.27. All OEM SBs, ASBs, SILs, ADs, amendments, modifications, and specifications as applicable to the specific engine power units, modules, and components.

1.28. All FAA and Transport Canada ADs as applicable to the specific engine.

1.29. All OEM applicable documentation or specifications revealed, published, or updated during the contract period, shall be considered as being within the scope of this SOW and may be added to the contract as agreed upon by both parties. If the Contractor receives information more current than that previously provided to DoS, the Contractor must identify the OEM Manuals, CMMs, revisions, and specifications, including service bulletins, amendments, and modifications and provide a brief synopsis of the revisions and dates to DoS/INLA designated representatives.

MARKING, PACKAGING, AND PRESERVATION

1.30. All DoS engines shall be preserved IAW OEM specifications prior to return shipment to INL.

1.31. Packaging shall be in accordance with ASTM D3951-10 and OEM best commercial practices. Packaging shall provide protection from normal climatic / weather conditions and incidental mishandling during shipping.

1.32. All engines shall be shipped to the following address:

US Department of State, INL/A Logistics Division 2765 Business Center Blvd Melbourne, FL 32940 Tel. 321-783-9865 x33216

1.33. Markings shall include the following information:

Location: Longitudinally on either side of packaging in one (1) inch block letters stencil the following:

1. Nomenclature: Engine Model

2. Mfr. Part Number: As Applicable

3. Engine Serial Number: As Applicable

4. Manufacturer: Pratt & Whitney Canada

5. Contract #: TBD

Location: Longitudinally across both sides of the packaging in two (2)-inch block letters stencil the following:

Property of the Department of State Office of Aviation

INSPECTION AND ACCEPTANCE

1.34. Inspection and acceptance of material under this contract, to ensure that equipment is in accordance with manufacturer's specifications, shall be performed at destination by a designated INL/A Quality Assurance (QA) specialist.

1.35. A FAA Form 8130-3 or other FAA authorized airworthiness form shall be required for all items provided on this contract. The certificate must be signed by an authorized official of the approved source and must specify the nomenclature, manufacturer's part number and date of manufacture.

DEFINITIONS & ACRONYMS

1.36. Definitions:

CONTRACTOR. A supplier or vendor awarded a contract to provide specific supplies or service to the government. The term used in this contract refers to the prime.

CONTRACTING OFFICER. A person with authority to enter into, administer, and or terminate contracts, and make related determinations and findings on behalf of the government. Note: The only individual who can legally bind the government.

CONTRACTING OFFICER'S REPRESENTATIVE (COR). An employee of the U.S. Government appointed by the contracting officer to administer the contract. Such appointment shall be in writing and shall state the scope of authority and limitations. This individual has authority to provide technical direction to the Contractor as long as that direction is within the scope of the contract, does not constitute a change, and has no funding implications. This individual does NOT have authority to change the terms and conditions of the contract.

DEFECTIVE SERVICE. A service output that does not meet the standard of performance associated with the Performance Work Statement.

DELIVERABLE. Anything that can be physically delivered, but may include non-manufactured things such as meeting minutes or reports.

KEY PERSONNEL. Contractor personnel that are evaluated in a source selection process and that may be required to be used in the performance of a contract by the Key Personnel listed in the PWS. When key personnel are used as an evaluation factor in best value procurement, an offer can be rejected if it does not have a firm commitment from the persons that are listed in the proposal.

PHYSICAL SECURITY. Actions that prevent the loss or damage of Government property.

QUALITY ASSURANCE. The government procedures to verify that services being performed by the Contractor are performed according to acceptable standards.

QUALITY ASSURANCE Surveillance Plan (QASP). An organized written document specifying the surveillance methodology to be used for surveillance of contractor performance.

QUALITY CONTROL. All necessary measures taken by the Contractor to assure that the quality of an end product or service shall meet contract requirements.

SUBCONTRACTOR. One that enters into a contract with a prime contractor. The Government does not have privity of contract with the subcontractor.

WORK DAY. The number of hours per day the Contractor provides services in accordance with the contract.

WORK WEEK. Monday through Friday, unless specified otherwise.

ACRONYMS

LIST OF CDRLs:

A001 Warranty Plan A002 Teardown Inspection Report (TIR) A003 Confirmation of receipt after shipping A004 Notification of Missing Inventory A005 Quotation for Repair/Overhaul Services A006 Property Disposal Plan A007 Status Reporting (Info for CDRL)

· Type Engine: Self Explanatory (SE)

· Engine Serial Number: SE

· Status – State at what major step in the repair cycle the item is currently at. For instance, In

· Transit (repair station or Melbourne Fl), Inventory, TIR, Repairs in-work, Test Cell, etc.

· Date Received: SE

· Missing Inventory: Y/N (If Yes, identify items)

· Approved Quote: Y/N

· Type of Repair: State the repair expected to receive.

· Estimated Completion/Delivery Date:

· On Schedule: Y/N (If No, explain)

· Within Authorized Approved Funding: Y/N (If No, explain)

(End of SOW)