Tab 16 Attachment 2_Statement of Work.pdf

Federal Aviation Administration

Engine Maintenance Overhaul

Program For

PW Beechcraft 300 PT6A‐60A Engine

Statement of Work i

Table of Contents

1.0 INTRODUCTION

2.0 SCOPE

3.0 CONTRACTOR RESPONSIBILITIES

3.1 Contractor Scheduled Maintenance Program/Overhaul and Trend Monitoring Support

3.2 Replacement Asset/Equipment Condition and Documentation

3.3 Contractor Over and Above (O&A) Support

3.4 Component Warranty

3.5 Contractor Personnel

3.6 Work Force Drug Free Program………………………………………………………………………………………………6

3.7 Government Property

4.0 FAA RESPONSIBILITIES

4.1 FAA Engine Overhaul Maintenance Scheduling

4.2 FAA Engine Maintenance Scheduling

4.3 FAA Engine Maintenance Authorizations

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

9.0 Travel for Meetings, Reviews or Conferences

10.0 PERIOD OF PERFORMANCE

11.0 INVOICING

12.0 PLACE OF PERFORMANCE

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13.0 SECURITY REQUIREMENTS

14.0 ACRONYMS AND DEFINITIONS

14.1 ACRONYMS

Appendix 1………………………………………………………………………………………………………………………………….17

1.0 INTRODUCTION

The Federal Aviation Administration (FAA) owns and operates seventeen (17) Beechcraft 300 aircraft that are powered by Pratt & Whitney (PW) Beechcraft 300 PT6A‐60A engines. The FAA Beechcraft 300 aircraft are type certificated and modified to a Flight Inspections Aircraft to meet special FAA mission requirements. The mission of the Flight Inspection Aircraft 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 Beechcraft 300 aircrafts must be airworthy, reliable, and maintained for a high level of availability to perform critical missions and ensure the safety of the flying public.

The FAA owned the FAA Flight Program Operations Aircraft Maintenance maintains PW Beechcraft 300 PT6A‐60A engines and FAA 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 PW manuals and specifications.

2.0 SCOPE

The contractor must perform work at an authorized PW service center with a 14 CFR Part 145 Repair Station Certificate and associated Operations Specifications listing the appropriate ratings and limitations, have access to the original equipment manufacturer (OEM) engineering support, and have the ability to provide Aircraft on Ground (AOG),Overhaul Maintenance, Hot Section Inspections and Trend Monitoring support.

Approved tooling and equipment, along with parts and material to adequately maintain all PW Beechcraft 300 PT6A‐60A engines, are required. The contractor when outsourcing repairs that repair station must be a PW approved repair station. The contractor must also correct all non-routine discrepancies discovered during these overhaul, and perform an airworthiness release in accordance with Flight Program Operations’ FAA-approved CAMP.

The program must provide coverage for the cost of all overhaul, parts, support, unscheduled maintenance tasks described in Section 3.1. The contractor must provide other support tasks and services that are necessary to maintain the engine in airworthy condition and ensure availability of the FAA Beechcraft 300 aircraft.

The contractor must ensure that engine logbooks are properly completed in accordance with Flight Program Operations’ FAA-approved CAMP and FAA-accepted GMM, as applicable, following any maintenance completed by the contractor/subcontractor.

3.0 CONTRACTOR RESPONSIBILITIES

3.1 Contractor Scheduled Maintenance Program/Overhaul and Trend

Monitoring Support The Contractor must provide PW Beechcraft 300 PT6A‐60A engine overhaul services, hot section inspections and a trend monitoring program under this contract using engine repair or overhaul facilities that are PW approved, FAA approved, and have PW Beechcraft 300 PT6A‐60A experience. The facilities must be a PW approved facility as well as a FAA approved CFR Part 145 Repair Station Certificate holder. Engine parts and components used in PW Beechcraft 300 PT6A‐60A engine inspections, repairs, and overhauls of the PW Beechcraft 300 PT6A‐60A 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 Flight Program Operations Quality Assurance Section.

The contractor must provide Mobile Repair Team (MRT) for AOG aircraft when the aircraft cannot fly from a location, which there are no qualified and licensed personnel to perform maintenance. The MRT request has to be acknowledged within four (4) hours and are dispatched in an expedite manner. The contractor must provide technical experience and troubleshooting support 24 hours/day, 7 days/week for PW Beech 300 PT6A-60A engines experiencing operating discrepancies and abnormalities.

Provide an Engine Condition trend Monitoring (ECTM) program for PW Beechcraft PT6A-60A engines Representatives for technical support to troubleshoot engine problems. Arrange contractor maintenance/overhaul activities and arrange shipment of engine parts required for FAA line maintenance. Provide PW approved shipping containers for PW Beechcraft PT6A-60A engines as required.

3.2 Replacement Asset/Equipment Condition and Documentation

Any part required to accomplish overhaul or to correct discrepancies discovered during the performance of overhaul may be procured or purchased by the contractor with prior authorization from the FAA CO or COR.

Any asset(s) required to replace existing component(s) necessary for the accomplishment of the contracted work must meet the following requirements:

Reasonable Parts Handling markup/surcharge fees will be negotiated by Federal Aviation Administration and Contractor prior to contract being awarded and must not exceed 10%. All shop fees must be included in the overhaul/unscheduled maintenance price and not separately priced.

Any asset(s) required to replace existing component(s) necessary for the accomplishment of the contracted work must meet the following requirements:

Components offered as “New” must:

• Have zero (0) hours and zero (0) cycles in service since time of manufacture, and the internal components must have (0) hours and zero (0) cycles in service since time of manufacture.

• Have documentation that provides full traceability of parts and assemblies, if applicable, and a copy of the original shipping invoice from the Production Approval Holder (PAH) to the supplier providing evidence that the origin of the part is from a FAA PAH or that the original acquisition was from a FAA-approved source.

• Have documentation that identifies assembly internal components that are required to be tracked for traceability in accordance with the OEM manuals.

Documents must identify part number and serial number.

Components offered as “Overhauled/Repaired/Serviceable” must:

• Be restored by an FAA-approved 14 CFR Part 145 Repair Station in accordance with the OEM manual requirements.

• Be restored after January 1, 2011, and have zero (0) time and zero (0) cycles in service since time of restoration.

• Have documentation that identifies all assemblies and assembly components meet the OEM 120-month restoration requirement.

• Have documentation that identifies assembly internal components that are required to be tracked for traceability in accordance with the OEM manuals.

Documents must identify part number, serial number, and times/cycles/landings since new or overhaul.

All components must:

• Be properly identified as an approved aeronautical part in accordance with 14 CFR Part 21 and 14 CFR Part 45.

• Have a shipping invoice from the contractor to the FAA identifying part numbers and serial numbers.

3.3 Contractor Over and Above (O&A) Support

The Contractor must provide PW Beechcraft 300 PT6A‐60A engine heavy maintenance services under this contract using engine repair or overhaul facilities that are PW approved, FAA approved, and have PW Beechcraft 300 PT6A‐60A experience.

• The facilities must be a FAA approved CFR Part 145 Repair Station Certificate holder. Engine parts and components used in PW Beechcraft 300 PT6A‐60A engine inspections, repairs, and overhauls of the PW Beechcraft 300 PT6A‐60A 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 Flight Program Operations Quality Assurance Section.

• The FAA has a need for the Contractor to provide maintenance, parts, and support tasks. These tasks are necessary to support maintenance of the FAA PW Beechcraft 300 PT6A‐60A engines and maintain availability of the FAA Beechcraft 300 aircraft. Additional maintenance services, parts, and support tasks will be considered as Over and Above (O&A) actions and are described in

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.

3.4 Component Warranty

The contractor shall provide a written statement of warranty for the work performed for the FAA. The warranty statement must identify what is covered under warranty and the warranty duration.

3.5 Contractor Personnel

The Contractor must employ personnel who possess the necessary skills to effectively accomplish the requirements of this Statement of Work (SOW). The skills must include technical support for engine troubleshooting, engine hot section inspections, 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.

3.6 Work Place Drug Free Program

The contractor must maintain a drug-free facilities and maintain a drug-testing program of all new employees and ongoing random testing of all employees that will be providing maintenance under this contract.

3.7 Government Property

An inventory of loose equipment will be performed and the property will be stored as Government Property (GP) and returned with the aircraft upon completion of the maintenance. GP will be stored in a secure location.

4.0 FAA RESPONSIBILITIES

4.1 FAA Engine Overhaul Maintenance Scheduling

The FAA shall ferry the aircraft at the Government’s expense, to and from any location, for all scheduled and unscheduled maintenance operations. The Government will assume all costs (including pilots, fuel, and travel expenses) for ferrying the aircraft to and from a place of disablement, to a service center for repairs.

The FAA may elect to perform any repair or inspection to the aircraft at home base or grounded location site using FAA maintenance personnel and equipment.

4.2 FAA Engine Maintenance Scheduling

The FAA will schedule PW Beechcraft 300 PT6A‐60A engine scheduled overhaul maintenance to comply with requirements IAW PW manuals, advisories, and technical specifications. The FAA will notify the Contractor of scheduled engine Overhaul maintenance 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 Engine Condition Tend Monitoring (ECTM) data monthly or when necessary due to engine performance problems or for engine troubleshooting purposes. Data will be provided electronically to the Contractors designated ECTM provider in a format as agreed upon by the FAA and the Contractor.

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 PW Beechcraft 300 PT6A‐60A 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 must 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 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 will be considered as O&A. These tasks are necessary to support maintenance availability of the FAA PW Beechcraft 300 PT6A-60A engine.

7.1 Over and Above (O&A) Task

The Contractor must receive prior authorization from the FAA CO or 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.

7. Support Equipment, Materials, Manuals, Technical Support – Cost of support equipment rentals, materials, manuals, technical support, etc.

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

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 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.

• The CO will provide approval to the Contractor by issuing a Call Obligation in FAA format by electronic mail. If the Contractor determines an O&A action is required they must submit to the FAA COR a description of the action, an explanation of why it is considered an O&A action, and a Not‐To‐ Exceed (NTE) price, as soon as practical. This must be done by 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 thirty (30) 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 information (Parts, Labor, other fees). The contractor must provide a NTE or Firm Fixed Price (FFP). Failure to agree on a reasonable price must be considered a question of fact subject to the DISPUTES clause of the contract.

• Reasonable O&A Parts Handling markup/surcharge fees will be negotiated by Federal Aviation Administration and Contractor prior to contract being awarded and must not exceed 10%. Shop fees are not authorized against O&A labor or parts. These fees are to be included in scheduled maintenance/inspection price.

9.0 Travel for Meetings, Reviews or Conferences

Contractor travel costs for AOGs, meetings, reviews, or conferences, when determined necessary by the FAA will be IAW FAA Acquisition Management System (AMS) policies. All travel shall be authorized by the CO or COR prior to making travel arrangements. 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.

10.0 PERIOD OF PERFORMANCE

The period of performance will be a five (5) year contract, which includes one (1) base year and four (4) option years.

11.0 Invoicing

The Contractor must submit an invoice for the engine overhaul services, MRT/AOG services and approved O&A actions within thirty (30) days of any of these maintenance activities being completed. Each invoice must be numbered in Contractor format and include the engine maintenance program contract number and deliver order number. The invoice, at minimum, must identify the engine hours/cycles, and engine serial number. The

O&A actions on the invoice must identify the CLIN, and CLIN description, part number, quantity, or task descriptions, unit cost, and extended cost.

12.0 PLACE OF PERFORMANCE

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

13.0 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.

14.0 ACRONYMS AND DEFINITIONS

14.1 ACRONYMS

AD Airworthiness Directive AMS Acquisition Management System AOG Aircraft on the Ground CDRL Contract Data Requirements List CFR Code of Federal Regulations CO Contracting Officer COR Contracting Officer Representative CLIN Contract Line Item Number CSN Cycle Since New CSO Cycle Since Overhaul E&R Exchange and Repair FAA Federal Aviation Administration FAR Federal Aviation Regulations FFP Firm Fixed Price FIA Flight Inspection Aircraft FOD Foreign Object Damage FY Fiscal Year GFP Government Furnished Property HSI Hot Section Inspection IAW In Accordance With ID Item(s) Delivered IR Items(s) Received LLP Life Limited Parts

LRU Line Replacement Unit MMAC Mike Monroney Aeronautical Center

MRT Mobile Repair Team NLT No Later Than NTE Not to Exceed OEM Original Equipment Manufacturer O&A Over and Above OKC Oklahoma City PHS&T Packaging, Handling, Storage and Transportation PM Program Manager PMR Program Management Review PPH Power Per Hour PW Pratt & Whitney SB Service Bulletin SF Standard Form SOW Statement of Work TBD To be Determined TDR Teardown Report TI Technical Issuance TSN Time Since New TSO Time Since Overhaul

14.2 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.

Airframe:

The fuselage, booms, nacelles, cowlings, fairings, airfoil surfaces (including rotors but excluding propellers and rotating airfoils of engines), and landing gear of an aircraft and their accessories and controls.

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.

Contract Data Requirements List (CDRL):

A contract form (DD Form 1423) listing all data and information which the Contractor will be required to deliver under contract.

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.

Contractor’s Cost:

Means the net cost to the contractor (after deducting cash or trade discounts, rebates, commissions and any other allowances and credits available to the contractor, regardless of date purchased, plus properly identified and supported freight or transportation costs) for parts acquired by the contractor for performance under this contract.

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.

Direct Labor Hours:

Means those hours of labor which are identifiable as being performed directly on an item/task of the contract and which serve as the basis for payment of the Hourly Composite Rate set forth in Section B. The method of charging direct labor hours to this contract must conform to the Contractor’s accepted normal accounting practices and procedures, and allow for verification to the sources of the costs incurred. The term Direct Labor Hours does NOT include time for the indirect work of overhead and supervisory employees such as officers, engineers, supervisors, foremen, quality control inspectors, material handlers, clerks, typists, timekeepers, watchmen, and truck drivers.

Direct Material: Materials, if required, which are not encompassed by the definition of “Indirect Materials”.

Engine Cycles:

Any engine operational sequence involving an engine start, aircraft take‐off, flight and landing, and culminating in an engine shutdown.

Engine Hours:

Engine operating time in hours accrued by an engine as recorded in a logbook and tracking database IAW the applicable regulatory requirements.

Equipment:

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

Exchange and Repair:

Reparable item(s) which, when unserviceable, is returned in exchange for a serviceable replacement. Flight Inspection Aircraft Maintenance and Engineering Group: Flight Inspection Services activity providing line maintenance, major inspections and overhaul services to the FAA aircraft fleet and equipment.

Flight Time:

Refer to Time In Service.

Government Furnished Property:

Property in the possession of, or acquired by the Government, and subsequently delivered or otherwise made available to the Contractor.

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.

Indirect Material:

All supplies and materials, if required, which do not become an integrated part of the assembly, accessory, or component. Price of indirect material must be included in the Hourly Composite Rate. Inspection:

An examination of an item against a specific standard.

Inventoried Spare Engines:

FAA owned repairable/serviceable engines.

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.

New Parts:

Parts or material produced in conformity with approved data that is accompanied by a manufacturer’s material certification at the time of sale and has no operating time or cycles.

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 manufacturer’s to provide an operationally safe, serviceable, and reliable item.

Repair:

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

Repair Parts:

Parts that have been restored to a serviceable condition and in compliance with approved data.

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.

Subcontractor:

Any supplier, distributor, vendor or firm, which enters into a formal contract to furnish items, services, parts, or supplies to a prime Contractor.

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.

Time In Service:

With respect to flight log documents and/or FAA computer tracking system and cost per hour rate, the time from the moment an aircraft leaves the surface of the earth until it touches down at the next point of landing.

APPENDIX 1

DATED 2/26/2020