Attachment 1_ Draft SOW_CF34 Engine.pdf

Federal Aviation Administration

Engine Management Program

For

Challenger CF34‐3A1, CF34‐3B Engine

Statement of Work

DRAFT

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Table of Contents

1.0 INTRODUCTION

2.0 SCOPE

3.0 CONTRACTOR RESPONSIBILITIES

3.1 Contractor Cost Per Engine Operating Hour Coverage

3.2 Contractor Over and Above Support

3.3 Contractor Provided Engine Heavy Maintenance and Parts

3.4 Contractor Personnel

3.5 Contractor Phase‐In

3.6 Contractor Phase‐Out

4.0 FAA RESPONSIBILITIES

4.1 FAA Engine Operating Hour Reporting

4.2 FAA Engine Maintenance Scheduling

4.3 FAA Engine Maintenance Authorizations

4.4 FAA Engine Trend Monitoring Data

4.5 FAA Engine Configuration and Maintenance Data

5.0 PARTS AND MATERIAL REQUIREMENTS

5.1 Time Controlled Parts

5.2 Components/Parts Replacement and Exchange

5.3 Core Part Return

5.4 FAA Owned Parts Used for Maintenance

5.5 Disposition of FAA Owned Parts Removed

6.0 FAA ACCEPTANCE AND INSPECTION

6.1 Engine Inspection and Maintenance Documents

7.0 OVER AND ABOVE (O&A) TASKS AND PROCEDURES

7.1 Over and Above (O&A) Task

7.2 Over and Above (O&A) Procedures

8.0 PROGRAM MANAGEMENT REVIEW (PMR) AND CONFERENCES

8.1 PMR/Conference Agendas

8.2 PMR/Conference Minutes

8.3 Travel for Meetings, Reviews or Conferences

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9.0 INVOICING

10.0 PERIOD OF PERFORMANCE

11.0 PLACE OF PERFORMANCE

12.0 SECURITY REQUIREMENTS

13.0 ACRONYMS AND DEFINITIONS

13.1 ACRONYMS

13.2 DEFINITIONS

APPENDICES

APPENDIX 1 – Engine Status Report

ENGINE MANAGEMENT PROGRAM

CHALLENGER CF34‐3A1, CF34‐3B ENGINE

STATEMENT OF WORK

1.0 INTRODUCTION

The Federal Aviation Administration (FAA) owns and operates three (3) Challenger 601, one (1) Challenger 604, and two (2) Challenger 605 aircraft that are powered by General Electric (GE) CF34‐3A1 and CF34‐3B engines. The FAA Challenger aircraft are typed certificated and modified to a Flight Inspections Aircraft (FIA) to meet special FAA mission requirements. The mission of the FIA is to validate the operating parameters of ground‐based navigation, landing aid facilities, and to validate procedures for both ground based and satellite based facilities. The FAA Challenger aircraft must be airworthy, reliable, and maintained for a high level of availability to perform critical missions and insure the safety of the flying public.

The FAA owned GE CF34‐3A1 and CF34‐3B engines are maintained by the FAA Flight Program Operations Aircraft Maintenance and Engineering Group (AMEG) and FAA AMEG approved maintenance facilities. Maintenance is performed In Accordance With (IAW) Flight Program Operations policies and programs, the Code of Federal Regulations (CFR) Title 14, Aeronautics and Space, Part 135 and GE manuals and specifications. This Statement of Work (SOW) describes the requirements for an Engine Management Program that provides coverage for the cost of scheduled and unscheduled maintenance for six (6) GE CF34‐3A1 and six (6) GE CF34‐3B engines owned by the FAA. The engines must be maintained in airworthy and reliable condition to ensure aircraft availability that supports the FAA missions. Twelve (12) engines are installed on six (6) FAA Challenger aircraft.

2.0 SCOPE

The Contractor must provide an engine management program proposal for six (6) GE CF34‐3A1 and six

(6) GE CF34‐3B engines identified in Appendix 1. The program must provide coverage for the cost of scheduled and unscheduled engine maintenance including parts, labor, engine transportation, engine rentals, and other tasks as described. The cost of the engine maintenance, parts, and support tasks described in Section 3.1 must be provided and billed as a cost per engine operating hour. Other support tasks and services are necessary to maintain the engine in airworthy condition and ensure availability of the FAA Challenger aircraft. The other support tasks and services described in Section 7.0 will be considered as Over & Above (O&A) actions. The Contractor may use a commercially available engine maintenance program as part of the FAA Engine Management Program. The Contractor will be responsible for administration of any commercial programs and payments to the program supplier if a commercial program is used. The Contractor must possess the skills and capabilities necessary to provide an engine management program and the tasks described in this SOW.

In addition, the Contractor must provide Auxiliary Power Unit (APU) drop in maintenance for Repair, Hot Section Inspection, and Overhaul as required based on unit inspection. APU model types are GTCP36‐ 150(RJ) and GTCP36‐150(CL).

3.0 CONTRACTOR RESPONSIBILITIES

3.1 Contractor Cost Per Engine Operating Hour Coverage

The Engine Management Program must provide maintenance and support tasks that include the cost of labor and parts necessary to maintain the GE CF34‐3A1 and CF34‐3B engines in airworthy condition.

Maintenance and support tasks that are provided under the engine management program must include the following:

1. Engine repair due to engine component failure

2. Engine Hot Section Inspection (HSI)

3. Engine overhaul

4. Replacement of engine Life Limited Parts (LLP) and consumable parts, as part of the engine build specification

5. Repair, overhaul, replacement of engine Line Replacement Unit (LRU)

6. Test cell runs

7. Other maintenance or inspections as required by GE specifications, publications, and advisories

8. Compliance of Airworthiness Directives (AD) applicable to the engines. As directed by FAA

9. Mandatory GE Service Bulletins (SB) while in service and SB routinely incorporated during shop visit

10. Labor necessary to perform engine troubleshooting and maintenance/overhaul

11. Labor necessary to perform engine removals and installations when required for scheduled maintenance or unscheduled maintenance due to engine or engine component failure

12. Representatives for technical support to troubleshoot engines problems, arrange contractor maintenance/overhaul activities, and to arrange shipment of engine parts required for FAA line maintenance

13. Mobile Repair Team (MRT) to include travel, to support AOG (Aircraft on Ground) when the DRAFT aircraft is disabled, including engine bearing carbon seal repairs, and which there are no qualified and licensed personnel to perform maintenance (minimum response time of 4 hours)

14. Freight cost for shipment of engines to and from repair/overhaul facilities and freight cost for shipment of engine parts to the FAA maintenance locations

15. Provide GE approved shipping containers for GE CF34‐3A1 and CF34‐3B engines whenneeded

16. Provide engine trend analysis to maintain GE CF34‐3A1 and CF34‐3B engines to predict engine performance problems due to failing components and/or operator error.

17. Scheduled Borescope inspections, including travel, at MMAC and AMEG Line Stations

18. Rental engines when required to keep aircraft available

3.2 Contractor Over and Above Support

The FAA will have a need for the Contractor to provide additional maintenance, parts, and support tasks that are not covered under the cost per engine operating hour task. These tasks are necessary to support maintenance of the FAA GE CF34‐3A1 and CF34‐3B engines and maintain availability of the FAA

Challenger aircraft. Additional maintenance services, parts, and support tasks will be considered as Over and Above (O&A) actions and are described in Section 7.0 Over and Above (O&A) Tasks and Procedures.

O&A actions must be billed on a separate Contract Line Item Number (CLIN). The Contractor must receive prior authorization from the FAA Contracting Officer (CO) or their designated representatives, Contracting Officer Representative (COR), before providing O&A maintenance, parts, or support tasks.

3.3 Contractor Provided Engine Heavy Maintenance and Parts

The Contractor must provide GE CF34‐3A1 and CF34‐3B engine heavy maintenance services under this contract using engine repair or overhaul facilities that are GE approved, FAA approved, and have GE CF34‐ 3A1 and CF34‐3B experience. The facilities must be a FAA approved CFR Part 145 Repair Station Certificate holder. Engine parts and components used in GE CF34‐3A1 and CF34‐3B engine inspections, repairs, and overhauls of the GE CF34‐3A1 and CF34‐3B engines must possess the valid certifications required by CFR, Title 14. All facilities and parts used in support of this contract will be subject to surveillance and acceptance by the FAA AMEG Quality Assurance Section.

3.4 Contractor Personnel

The Contractor must employ personnel who possess the necessary skills to effectively accomplish the requirements of this SOW. The skills must include technical support for engine troubleshooting, engine overhaul, scheduling support for engine heavy maintenance at approved facilities, parts support required for engine maintenance, field support for engine repairs, engine change at worldwide locations, and provides accounting support for invoicing as described in this SOW.

The Contractor must be able to provide technical expertise 24 hours/day, 7 day/week support, and a minimum response time of 4 hours.

3.5 Contractor Phase‐In

The Contractor must provide an implementation plan for the engine management program within thirty

(30) calendar days after contract award. The implementation plan must provide procedures and methods necessary to obtain maintenance services, required authorizations, and parts provided by this SOW. This plan must include Points of Contact (POC) for management support, technical support, logistics support, and invoicing support. The POC information must include the organizational or employee names, business telephone number, business fax number, business cell phone numbers, and business email addresses. The Contractor must provide a copy of any published documents for commercially available engine programs if the programs are used to accomplish the tasks described in this engine management program SOW.

3.6 Contractor Phase‐Out

The Contractor must assist in contract phase‐out activities. This must include a transition plan that outlines the activities that will be necessary to discontinue the engine management program or transfer the engine management program to another Contractor. The Contractor must provide the FAA the dollar amounts reserved in the engine management program that is available to the FAA. All positive reserve balance that is eligible for rebate, credit, or transfer will become the property of the FAA. The FAA will request a proposal for the plan and phase‐out activities at least sixty (60) calendar days prior to the end of the last option year exercised. The FAA will notify the Contractor of how the reserve balances are to be dispersed after the completion of the last option year exercised and within sixty (60) calendar days after the final dollar amount in reserve are identified and available.

4.0 FAA RESPONSIBILITIES

4.1 FAA Engine Operating Hour Reporting

The FAA will report the monthly operating hours of each engine, including engines that did not operate during the month, to the Contractor within 10 days after the end of each month. The report will include the engine serial numbers, aircraft serial numbers and tail numbers, which the engines are currently installed, engine total times and cycles since new, engine total times and cycles since overhaul, and total times and cycles operated during the month reported. The report will be provided by electronic mail in a FAA and Contractor mutually agreed format.

4.2 FAA Engine Maintenance Scheduling

The FAA will schedule GE CF34‐3A1 and CF34‐3B engine maintenance to comply with requirements IAW GE manuals, advisories, and technical specifications. The FAA will notify the Contractor of scheduled engine Overhaul or Hot Sections Inspections requirements at least thirty (30) days prior to them becoming due.

4.3 FAA Engine Maintenance Authorizations

The FAA or their designated repair facility will request maintenance and parts authorizations as described by the Contractor for work to be accomplished IAW this SOW.

4.4 FAA Engine Trend Monitoring Data

The FAA will provide available engine trend data when requested by the Contractor.

4.5 FAA Engine Configuration and Maintenance Data

The FAA will provide engine configuration and maintenance data upon the Contractor’s request. The data provided will be from the FAA tracking systems database and/or from the GE CF34‐3A1 and CF34‐ 3B engine logbooks.

5.0 PARTS AND MATERIAL REQUIREMENTS

5.1 Time Controlled Parts

Time controlled parts are parts where time has expired and must be replaced with new or overhauled parts. When time controlled parts have failed, but time has not expired, they may be repaired and used on the FAA GE CF34‐3A1 and CF34‐3B engines provided the part have sufficient life to achieve its next major scheduled event where access to such part is permitted.

5.2 Components/Parts Replacement and Exchange

Engine components/parts that are removed and exchanged during maintenance of the FAA engines will no longer be the property or responsibility of the FAA. The replacement of newly embodied engine components/parts will become the property of the FAA. All exchange components/parts removed from engines during maintenance by FAA personnel will be returned to the Contractor or their designated supplier in an “as‐is condition”.

5.3 Core Part Return

In those instances when a simultaneous exchange of parts is not feasible, the Contractor must allow the FAA to return the core part within a fourteen (14) day period. If the FAA does not return the part within the fourteen (14) day period the Contractor must provide notification to the FAA of the past due core. If the FAA is unable to return the core part due to the Contractor, the part may be deemed lost. The Contractor will provide the FAA the value of the part. Upon approval of the FAA, the Contractor may invoice the FAA for the value of the part using the O&A procedure.

5.4 FAA Owned Parts Used for Maintenance

The FAA may elect to purchase and maintain spare rotable engine parts in their inventory to have an immediate replacement for engine maintenance performed by the FAA. Should the FAA use a FAA owned spare engine part for maintenance that is covered under the cost per engine operating hour engine management program, the FAA will notify the Contractor of the part used. The Contractor must provide an exchange serviceable replacement part or repair the removed core part to a serviceable condition at no charge.

5.5 Disposition of FAA Owned Parts Removed

Each part removed by the Contractor from a FAA owned engine, not reinstalled therein, or is not replaced or exchanged by the Contractor is the property of the FAA. Such parts must be identified with a tag attached to each part that identifies “FAA Property”, part number, component serial number, cause for removal, and serviceability if known. The parts must be returned to the FAA with a shipping document that lists each part and quantity.

6.0 FAA ACCEPTANCE AND INSPECTION

The FAA will conduct a receiving inspection of all incoming engines and parts IAW TI 4100.24, General Maintenance Manual. Any engines and parts received in a damaged condition or without proper certification documentation will be recorded and identified to the Contractor for resolution. Should the engines or parts require return shipment to the Contractor it will be at the Contractor’s expense.

6.1 Engine Inspection and Maintenance Documents

Upon completion of engine inspections, maintenance, overhaul, etc. the Contractor must provide all certification documents including full copy of work order that describe all details of inspections performed, maintenance performed, components repaired or replaced, problem areas, etc. The Contractor must enter in the historical records (engine logbooks) all FAA airworthiness directives, manufacturers’ service bulletins or other modifications, and all other significant maintenance actions accomplished. In addition, the Contractor must record all previously complied with modifications found to be previously accomplished, but not recorded. The Contractor must indicate in the historical records the nomenclature, part number, location, total time, and total cycles, accumulated for all replacement LLP installed. Any LLP parts that are repaired, reworked, or modified that extend or reduce life will be identified with new limits in the historical records.

7.0 OVER AND ABOVE (O&A) TASKS AND PROCEDURES

The Contractor must provide Over & Above (O&A) support. Additional maintenance, parts, and support task that are not covered under the cost per engine operating hour task will be considered as O&A.

These tasks are necessary to support maintenance availability of the FAA Challenger aircraft.

7.1 Over and Above (O&A) Task

The Contractor must receive prior authorization from the FAA CO and COR before providing O&A maintenance, parts, or support task. The O&A tasks include but are not limited to the following:

1. Foreign Object Damage (FOD) – Repair of damage to the engines resulting from foreign object damage, i.e. hail, bird strikes, rocks, or other debris

2. Damage/Loss –Repair/replacement of parts or components either damaged or lost because of negligence or accident on the part of the FAA.

3. Theft – Replacement of parts because of theft of parts or components from engines other than when in control of the contractor.

4. Acts of GOD – Repairs due to flood, earthquake, volcanic ash, lightning strikes, tornadoes, hurricanes, other local emergencies, etc.

5. Corrosion, Erosion, or Sulphidation – Component repair or replacement costs attributable to damage caused by corrosion, erosion or sulphidation.

6. Service Bulletins – Cost of engine or component Service Bulletins requested and approved by the FAA not covered by the Engine Management Program on a cost per engine operating hour basis.

7. Support Equipment, Materials, Manuals, Technical Support – Cost of support equipment rentals, materials, manuals, technical support, etc. that is not covered by the cost per engine operating hour Engine Management Program.

8. Routine Line Maintenance – Cost for contractor performance of field level routine or periodic maintenance and inspections as specified in the Periodic Inspection table of the GE CF34‐3A1 and GE CF34‐3B engine maintenance manuals or specifications and any parts, fluids, engine washing, desalination, or removal of foreign chemical particles associated with this maintenance.

9. FAA Requested Advance Maintenance – Cost in addition to the cost per engine operating hour rate when the FAA requests scheduled engine maintenance to be performed earlier than standard intervals and allowable limits for scheduling purposes as described in the GE manuals, specifications, and/or contractors cost per engine operating hour program.

10. Spares Parts Purchases – Purchase of spare parts less discount for FAA stock

11. Rental Engine Fees – Rental engines fees if the FAA requests a rental engine and is not included in the cost per engine operating hour program.

7.2 Over and Above (O&A) Procedures

Either the FAA or the Contractor may initiate the O&A action that meets the criteria. If the FAA determines an O&A action is required the FAA CO or COR will request a price quote with supporting pricing documentation for the O&A action. Upon approval of the price quote, the FAA COR will ensure sufficient funding is available on the O&A CLIN. If the Contractor determines an O&A action is required they must submit to the FAA CO and COR a description of the action, an explanation of why it is considered an O&A action, and a Not‐To‐ Exceed (NTE) price, within 3 business days via electronic mail The COR will review the Contractor O&A request with the appropriate FAA personnel and provide approval or disapproval. If approved, the COR will ensure sufficient funding is available on the O&A CLIN. The CO will provide approval to the Contractor by issuing a Call Obligation in FAA format by electronic mail. Upon approval and completion of the O&A task the contractor must submit an invoice within sixty (60) days of receipt of goods or completion of services. At a minimum, O&A actions or proposals must identify the requested maintenance or support action and specify the engine serial number, part number (s), tool, rental fee, etc. with supporting pricing documentation. The contractor must provide a NTE or Firm Fixed Price (FFP).

8.0 PROGRAM MANAGEMENT REVIEW (PMR) AND

CONFERENCES

If determined necessary, the FAA will request, host, and participate in a post award conference and program review meetings with representatives of the Contractor to coordinate the total engine management program effort. If determined necessary, the FAA or Contractor may request formal PMRs. The PMR location will be determined and identified in response to the request. Informal meetings and reviews may be held on an “as needed” basis to resolve problems.

8.1 PMR/Conference Agendas

An agenda, in Contractor format, is required for each PMR and must be transmitted by letter or electronic media (fax, email, etc.). The agenda must include the following:

1. Purpose and objectives of the meeting

2. Date, and time duration

3. Chronological listing of each major topic to be discussed and the time scheduled for each topic.

4. Name of FAA and Contractor Co‐Chairpersons and a list of attendees and their organization.

5. List of all documentation to be available for review

6. Status of action items or problems identified at previous meetings.

8.2 PMR/Conference Minutes

Minutes of each program management review and conference must be prepared in Contractor format and must include, as a minimum, the following:

1. Title page containing the following

a. Contractor name and number

b. Type of meeting and date

c. Name of the Contractor and address to which the CO should send acknowledgements of receipt and comments

2. Purpose and objective of the conference

3. Location of the conference

4. Summary of the discussions, decisions, agreements reached, and directions

5. List of attendees by name, position, organization represented, and phone number

6. Copy of action items. Format of the action items sheets must be as specified by the FAA. The

Contractor must update the status of formal open action items weekly by cc: mail or other means as determined appropriate.

7. Updated conference agenda reflecting the actual agenda as conducted

8. Copy of all briefing/presentation materials

8.3 Travel for Meetings, Reviews or Conferences

Contractor travel costs for meetings, reviews, or conferences, when determined necessary by the FAA will be IAW FAA Acquisition Management System (AMS) policies. Travel is not authorized profit or overhead. Travel expenses shall be subject to the GSA per diem rates. The contractor shall provide supporting pricing documentation to support travel costs.

9.0 INVOICING

The Contractor must submit a monthly invoice for the cost per engine operating hour engine management program and an invoice for approved O&A actions within sixty (60) days after the O&A action is complete. Each invoice must be numbered in Contractor format and include the engine maintenance contract number and delivery order number. The monthly invoices, at minimum, must identify the calendar month for the cost per engine operating hour engine management program, the CLIN, and CLIN description. Each engine serial number and engine monthly operating hours must be identified on the monthly invoice. O&A actions on the invoice must identify the CLIN, and CLIN description, part number, quantity, or task descriptions, unit cost, and extended cost.

10.0 PERIOD OF PERFORMANCE

The period of performance will be a seven (7) year contract, which includes one (1) base year and six

(6) option years.

11.0 PLACE OF PERFORMANCE

The FAA reserves the right to utilize OEM authorized overhaul and repair facilities.

12.0 SECURITY REQUIREMENTS

The Contractor must adhere to all applicable FAA Mike Monroney Aeronautical Center (MMAC) security requirements. Prior to entry onto the MMAC, the Contractor personnel must check‐in at the Main Gate and security checkpoint. The Contractor personnel must wear a “Visitor” badge at all times while on MMAC premises and vehicle registry tag issued by MMAC security must be visible. The Contractor personnel will be escorted on MMAC from an FAA employee.

13.0 ACRONYMS AND DEFINITIONS

13.1 ACRONYMS

AD Airworthiness Directive AMS Acquisition Management System AOG Aircraft on the Ground CFR Code of Federal Regulations CO Contracting Officer

COR Contracting Officer Representative

CLIN Contract Line Item Number

FAA Federal Aviation Administration FAR Federal Aviation Regulations FFP Firm Fixed Price FIA Flight Inspection Aircraft FOD Foreign Object Damage GE General Electric HSI Hot Section Inspection IAW In Accordance With LLP Life Limited Parts LRU Line Replacement Unit MMAC Mike Monroney Aeronautical Center MRT Mobile Repair Team NTE Not to Exceed O&A Over and Above OKC Oklahoma City PM Program Manager PMR Program Management Review SB Service Bulletin SOW Statement of Work

13.2 DEFINITIONS

Aircraft on the Ground:

An aircraft that is non‐operational as a result of a failure of a system, sub‐system, and/or component.

Aircraft Maintenance:

That work which is required to be performed by certificated persons.

Airworthiness Directive:

Bulletin issued by the Federal Aviation Administration in response to a safety‐of‐flight problem occurring in‐service for a specific type of aircraft. It is a mandatory directive for commercial aircraft, which specifies the conditions and limitations, if any, under which the aircraft type may continue to be operated. The AD carries a compliance date and flight hours and/or cycles, that must be complied with to maintain the FAA Airworthiness Certificate.

Component:

Any self‐contained part, combination of parts, subassemblies, or units, which perform a distinctive function necessary to the operation of the airframe, or power plant.

Configuration:

They physical and functional characteristics of systems, equipment and related item(s) of hardware or software, and the relative arrangement and contours of these; the shape of a thing at a given time, or the specific parts used to construct a product, or the functional and/or physical characteristics of hardware/software as set forth in technical documentation and achieved in a product.

Contracting Officer Representative:

An individual designated by the CO to act as their authorized representative for contract administration functions which do not involve changes to the scope, price, schedule, or terms and conditions of the contract. The designation will be in writing, signed by the CO, and will set forth the authorities and limitations of the representatives(s), under the contract. Such designation will not contain authority to sign contractual documents, order contract changes, modify contract terms, or create any commitment or liability on the part of the Government different from the set forth in the contract.

Contractor:

An individual, partnership, company, corporation, or association having a contract with the procuring activity for the design, development, manufacture, maintenance, modification, or supply of item(s) under the terms of a contract. A Government activity performing any or all of the above actions is considered a Contractor.

Cost Per Engine Operating Hour Rate:

Fixed price per hour rate that is applied to engine “operating” hours to determine payment amount.

This rate includes direct and indirect labor, indirect material, direct materials, overheads and profit. It does not include Management fees/cost as it is being paid under a separate contract line item number.

Payment under this applicable rate will be computed by multiplying the total engine operating hours used by the GE CF34‐3A1 and CF34‐3B engine management program hourly rate. The amounts payable for fractional parts of an hour may be prorated by fractions or increments not less than one‐tenth (1/10) of one hour.

Data:

The vehicle for communicating concepts, plans, descriptions, requirements, and instructions relating to technical projects, material, systems and services. Data may include specifications, standards, engineering drawings, associated lists, manuals and reports including scientific and technical reports. It may be in the form of documents, display, sound records, or punched cards.

Equipment:

All item(s) of a durable nature that is capable of continuing or repetitive utilitarian use by an individual or organization.

Heavy Maintenance:

Maintenance actions that are not accomplished at the line maintenance level. Heavy maintenance is the capability to do anything necessary to repair failed system/component/spare(s) to include, fabrication of structural parts(s), replacement of time‐controlled items, major overhauls and refurbishment and complete rebuilding of equipment. Heavy maintenance includes all unscheduled maintenance actions performed, as a result of system/component/spare(s) failure, to restore the system/component/spare(s) to a specified operational condition.

Hot Section Inspection:

The removal and inspection of an engine’s combustion and turbine section components, and the repair or replacement of deteriorated components in compliance with applicable engine maintenance manual.

Inspection:

An examination of an item against a specific standard.

Life Limited Part:

A part or component which has an establish life‐limit, at which time the item(s) must be scrapped and replaced. The life‐limit is established by FAA engineering and the manufacturer.

Line Replaceable Unit:

A component, which may normally be removed and replaced with the engine, installed on the aircraft and as part of normal flight line activities.

Materials:

All other item(s) not directly identified as a spare part, common or bulk items, consumable or other material not specifically identified in this SOW, i.e. corrosion preventive chemicals, etc.

Modification:

A change or series of changes in a completed system to adapt it to another use, correct deficiencies, increase reliability, or improve its effectiveness.

Overhaul:

The disassembly, cleaning, inspection, repair, rework, replacement of parts or components, reassemble and test of any times or accessory IAW applicable tech manuals, directives, or authorized DRAFT manufacturer’s to provide an operationally safe, serviceable, and reliable item.

Repair:

Restoration of an item(s) to a serviceable condition after fault detection.

Service Bulletin:

A document issued to all customers recommending an inspection and possible repair to the engine.

Statement of Work:

That part of the contract that describes the services to be provided.

Standards:

Established or accepted rules, modules, or criteria by which the degree of user satisfaction of a product or service is determined, or against which comparisons are made. A document that establishes such rules for items is called a standard.

Time Controlled Part:

Part or component that has an established service life, at which time certain maintenance must be performed or the item is scrapped. The service life may be based on operating hours, cycles, landing, calendar time, or combinations of these.

APPENDIX 1

DATED 10-24-2018