Statement of Work.pdf

U.S. DOT Federal Aviation Administration

Federal Aviation Administration

Hawker Beechcraft C90 GTi

PT6A-135A Engine Power By Hour

Maintenance and Overhaul Program

Statement of Work

August 16, 2017

SIR Attachment A, SOW – eFAST Procurement Action 16-038 i

[Date]

Table of Contents

1 Introduction

2 Scope

3 Contractor Responsibilities

3.1 Contractor Cost Per Engine Operating Hour Coverage

3.2 Contractor Cost Per Engine Operating Hour Fees and Account Reserves . 3

3.3 Contractor Over & Above Support

3.4 Contractor Provided Maintenance and Parts

3.5 Contractor Personnel

3.6 Contractor Phase-In

3.7 Contractor Phase-Out

4 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 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 FAA Acceptance and Inspection

6.1 Engine Inspection and Maintenance Documents

7 Over and Above (O&A) Tasks and Procedures

7.1 Over and Above (O&A) Tasks

7.1.1 Foreign Object Damage (FOD)

7.1.2 Damage/Loss

7.1.3 Theft

7.1.4 Acts of God

7.1.5 Corrosion, Erosion, or Sulphidation

7.1.6 Service Bulletins

7.1.7 Support Equipment, Materials, Manuals, Technical Support

7.1.8 Routine Line Maintenance

7.1.9 FAA Requested Advanced Maintenance

7.1.10 Spares Parts Purchases

7.1.11 Rental Engine Fees

7.2 Over and Above (O&A) Procedures

8 Engine Maintenance and Overhaul Program Fees and Costs

9 Applicable Documents

9.1 Code of Federal Regulations (CFR)

SIR Attachment A, SOW – eFAST Procurement Action 16-038 ii

9.2 Other Publications

10 Program Management Requirements

10.1 Program Management Reviews (PMR) and Conferences

10.1.1 PMR/Conference Agendas

10.1.2 PMR/Conference Minutes

10.1.3 Travel for Meetings, Reviews or Conferences

11 Invoicing

12 Acronyms and Definitions

12.1 Acronyms

12.2 Definitions

13 Required Contractor Property

Appendix A – Sample Monthly Status Report

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-1

May 19, 2017

1 Introduction

The Federal Aviation Administration (FAA) Flight Standard Services (AFS) Flight

Program Office (FPO) provides Aviation Operations Safety Inspectors (ASI) with multi-turbine engine currency based training, initial multi-turbine engine training and standardization training. This ensures that ASI’s conduct inspections and surveillance of people, equipment, and organizations in a standardized format for commercial operations. Flight training is conducted using FAA AFS owned aircraft.

AFS owns and operates nine (9) Hawker Beechcraft (HBC) C90GTi aircraft. The AFS aircraft fleet have critical missions for training and certification of FAA ASI pilots. Each

AFS C90GTi aircraft is powered by two (2) Pratt & Whitney Canada (PWC) model PT6A-

135A engines. PWC is the engine Original Equipment Manufacturer (OEM) of the PT6A-

135A engines.

The AFS C90GTi aircraft fleet will have a total of eighteen (18) PT6A-135A engines. All in-service aircraft had the Digital Aircraft Acquisition System (ADASd) installed, within the first 100 hours of engine operation, and have been on ECTM since the first 10 hours of engine operation.

All engines have initial warranty coverage by PWC’s Enhanced Warranty for New Engines and Service Policies for PT6A Engines in Hawker Beechcraft Aircraft. The engine warranty period is 5-years or 2500 hours, whichever occurs first.

The PT6A-135A engines are maintained by the FAA Aircraft Maintenance and Engineering

Group (AMEG) and FAA AMEG approved maintenance facilities. Engines must be maintained as airworthy, safe, and reliable for a high level of C90GTi aircraft availability necessary to perform AFS training flights. Maintenance is performed In Accordance With

(IAW) and AFS FPO Approved Aircraft Inspection Program (AAIP), Manufacturers

Programs, AMEG procedures and policies, and the Code of Federal Regulations (CFR)

Title 14, Aeronautics and Space, Part 135 and PW manuals and specifications.

This Statement of Work (SOW) describes the requirements for an engine Maintenance and Overhaul program for eighteen (18) PWC PT6A-135A engines operated on the FAA

AFS C90GTi aircraft. The PT6A-135A engine Maintenance and Overhaul program must provide management of timely maintenance at a predictable cost.

2 Scope

The Contractor shall provide a Power By Hour (PBH) Engine Maintenance and Overhaul program for eighteen (18) PT6A-135A engines identified in APPENDIX 1. The program must include scheduled and unscheduled maintenance, engine line replacement parts, engine hot section inspections, engine overhauls, technical support, and other engine support tasks necessary to maintain the engine in serviceable and airworthy condition.

The cost of the engine maintenance, parts, and support tasks described in SOW paragraph

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-2

3.1 must be provided and billed as a cost per engine operating hour. Other support tasks and services that are necessary to maintain the engines in airworthy condition and ensure availability of the AFS C90GTi aircraft are described in SOW paragraph 7.0 will be considered as Over and Above (O&A) actions.

The Contractor may provide a commercially available PT6A-135A engine support program as part of the PBH Maintenance and Overhaul program. The Contractor will be responsible for administration of any commercial programs and payments to the program supplier if a commercially available program is used.

The period of performance for this contract will be five (5) years which includes one (1) base year and four (4) one (1) year options.

3 Contractor Responsibilities

3.1 Contractor Cost Per Engine Operating Hour Coverage

The PBH Maintenance and Overhaul program must provide coverage for maintenance and support tasks that includes labor and parts necessary to maintain the PT6A-135A engines in serviceable and airworthy condition at a cost per engine operating hour. Maintenance and support tasks covered under the cost per engine operating hour must include but are not limited to the following.

1. Engine Repair due to engine component failure,

2. Engine Overhauls,

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

4. Repair, Overhaul, or Replacement of an engine Line Replacement Unit (LRU),

5. Test cell runs when required,

6. Other maintenance or inspections as required by PWC specifications, publications, and advisories,

7. Compliance of Airworthiness Directives (AD) applicable to the engine(s),

8. PWC Service Bulletins that are required,

9. Labor necessary to perform engine troubleshooting and maintenance,

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

11. Representatives for technical support to troubleshoot engines problems, arrange contractor Maintenance and Overhaul activities, and to arrange shipment of engine parts required for FAA line maintenance,

12. Mobile Repair Team (MRT) for AOG aircraft when the aircraft cannot fly from a location, where there are no qualified and licensed personnel to perform maintenance,

13. 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,

14. Provide PWC approved shipping containers for PT6A-135A engines when needed, Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-3

15. Provide an Engine Condition Trend Monitoring (ECTM) program for the PT6A-135A engines which includes engine operating recommendations and provides trend reports when requested,

16. Provide 24/7/365 AOG technical and parts support,

17. Provide Rental/Loaner engines during events requiring FAA engine removal for maintenance covered by PBH Maintenance and Overhaul Program.

3.2 Contractor Cost Per Engine Operating Hour Fees and Account Reserves

Cost per hour fees must be billed monthly based on the operating hours of each engine during the reported month. Cost per hour payments made by the FAA must be used for maintenance of the PT6A-135A engines IAW SOW paragraph 3.1. FAA payments that are not used for maintenance IAW SOW paragraph 3.1 must be held in reserve. Positive reserve amounts at contract expiration or contract termination, less Contractor fees and profit, will become the property of the FAA and must be available as a rebate, credit, or for transfer to a follow-on contract.

3.3 Contractor Over & 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 tasks.

These additional tasks are necessary to support maintenance of the FAA PT6A-135A engines and maintain availability of the AFS C90GTi aircraft. Additional maintenance services, parts, and support tasks will be considered as 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 or their designated representatives, Contracting Officer Representative (COR), before providing O&A maintenance, parts, or support tasks.

3.4 Contractor Provided Maintenance and Parts

The Contractor must provide parts and maintenance of the PT6A-135A engines under this contract using engine repair or overhaul facilities and that are PWC approved, FAA approved, and that have experience with PT6A-135A engines. The facilities must be a

FAA 145 repair station certificate holder. Personnel performing engine maintenance must be trained and experienced on PT6A-135A engines. Parts and components used in

PT6A-135A engine inspections, repairs, and overhauls must possess the valid certification required by CFR, Title 14. All facilities, parts and maintenance personnel used in support of this contract will be subject to surveillance and acceptance by the FAA

AMEG Quality Assurance. Maintenance performed during the engine warranty period must be in compliance with PWC document “Enhanced Warranty for New Engines and

Service Policies for PT6A Engines in Hawker Beechcraft Aircraft”.

3.5 Contractor Personnel

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-4

The Contractor must employ personnel who possess the necessary skills to effectively accomplish the requirements of the SOW. The skills must include program management, technical support for engine troubleshooting, scheduling support for engine maintenance at approved facilities, parts support required for engine maintenance, and accounting support for invoicing as described in this SOW.

3.6 Contractor Phase-In

The Contractor must provide an implementation plan for the engine Maintenance and

Overhaul program within thirty (30) calendar days after contract award. Engine hour reporting requirements and invoicing procedures must be described in the implementation plan. The implementation plan must provide procedures and methods necessary to obtain maintenance services, required authorizations, and parts provided by this SOW. The implementation 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 name, business telephone numbers, business fax numbers, business cell phone numbers, and business email addresses. The Contractor must provide a copy of any published documents of commercial engine programs if the programs are used to accomplish the tasks described in this Maintenance and Overhaul program SOW.

3.7 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

Maintenance and Overhaul program or transfer the engine Maintenance and Overhaul program to another Contractor. The Contractor must provide the FAA the dollar amounts in reserve in the Maintenance and Overhaul program that are available to the

FAA. All positive reserve balances that are 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 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 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 being reported. 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

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-5 mail or entered in an electronic data base in a FAA and Contractor mutually agreed format or procedure.

4.2 FAA Engine Maintenance Scheduling

The FAA will schedule PT6A-135A engine maintenance to comply with requirements

IAW PWC manuals, advisories, and technical specifications. The FAA will notify the

Contractor of scheduled engine Overhaul requirements at least thirty (30) days prior to the estimated date of maintenance.

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

Engine Condition Trend Monitoring (ECTM) data is available almost instantly for monitoring from the system on each engine via ADASd. Data will be provided electronically to the Contractors designated ECTM provider in a format as agreed upon by the FAA and 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 system data base and/or from the PT6A-135A engine log books.

5 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 PT6A-135A engines provided the part has 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 or 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”.

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-6

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 part for maintenance that is covered under the cost per engine operating hour Maintenance and Overhaul 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 from and 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 shipping document that lists each part and quantity.

6 FAA Acceptance and Inspection

The FAA will conduct a receiving inspection of all incoming engines and parts IAW the

FPO maintenance program and AMEG Repair Station procedures. 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, overhauls, etc. the Contractor must provide all certification documents that describe details of inspections performed, maintenance performed, components repaired or replaced, problem areas, etc.

7 Over and Above (O&A) Tasks and Procedures

The tasks defined in this section are considered to be O&A actions and are not covered by the specified support and maintenance actions provided in the cost per engine operating hour engine Maintenance and Overhaul program.

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-7

7.1 Over and Above (O&A) Tasks

7.1.1 Foreign Object Damage (FOD)

Repair of damage to the engines resulting from foreign object damage, i.e. hail, bird strikes, rocks, or other debris.

7.1.2 Damage/Loss

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

7.1.3 Theft

Replacement of parts because of theft of parts or components from engines other than when in control of the Contractor.

7.1.4 Acts of God

Repairs due to flood, earthquake, lightning strikes, tornadoes, hurricanes, other local emergencies, etc.

7.1.5 Corrosion, Erosion, or Sulphidation

Component repair or replacement costs attributable to damage caused by corrosion, erosion or sulphidation.

7.1.6 Service Bulletins

Cost of engine or component Service Bulletins requested and approved by the FAA not covered by the engine Maintenance and Overhaul program on a cost per engine operating hour basis.

7.1.7 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 Maintenance and Overhaul program.

7.1.8 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 PWC PT6A-135A engine maintenance manuals or specifications and any parts, fluids, engine washing, desalination, or removal of foreign chemical particles associated with this maintenance.

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-8

7.1.9 FAA Requested Advanced Maintenance

Cost in addition to the cost per engine operating our 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 PWC manuals, specifications, or Contractors cost per engine operating hour program.

7.1.10 Spares Parts Purchases

Purchase of Spare Parts for FAA stock.

7.1.11 Rental Engine Fees

Rental engines fees if the FAA requests a rental engine that is not covered under the

Maintenance and Overhaul program on a cost per engine operating hour basis.

7.2 Over and Above (O&A) Procedures

Funding for “routine” O&A actions will be provided by a separate CLIN in the contract and must be processed as follows:

1. Either the FAA or the Contractor may initiate the O&A action that meets the criteria in paragraph 7.1.

2. If the FAA determines an O&A action is required the FAA Contracting Officer 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 Contracting Officer will provide approval to the Contractor by issuing a Purchase Approval in FAA format or written notification by electronic mail.

3. 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 may be done either by letter or 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 Contracting Officer will provide approval to the Contractor by issuing a Purchase Approval in FAA format or notification by electronic mail.

4. 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. The contractor must provide a NTE or Firm-Fixed-Price (FFP) for all O&A actions.

Failure to agree on a reasonable price must be considered a question of fact, subject to the DISPUTES clause of the contract.

8 Engine Maintenance and Overhaul Program Fees and Costs

Eighteen (18) FAA PWC PT6A-135A engines that are currently “in-service” were in new condition at time of delivery to the FAA.

To enter the engines in a new Maintenance and Overhaul program the Contractor must identify the following;

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-9

1. Engine Buy-In Costs, if Applicable.

a. Engine buy-in cost, if proposed, must be identified as one-time flat rate cost per engine or as a one-time cost based on engine hours accrued from inception through the effective date of the contract.

2. Engine Enrollment Cost, if Applicable

a. Engine enrollment cost, if proposed, must be identified as a one-time flat rate cost per engine.

3. Engine Cost Per Hour (CPH) rate.

a. The engine CPH rate must be a fixed rate for each 12-month period of performance of the contract duration.

b. CPH rate may be proposed as two different rates for two different engines groups.

1. Group One; “In-Service” engines which delivered to the FAA from November 2009 through October 2010 and consist of eighteen (18) engines as shown in APPENDIX 1.

2. Group Two; “New-Engines” delivered in August 2013 and consist of two (2) engines as shown in APPENDIX 1.

9 Applicable Documents

9.1 Code of Federal Regulations (CFR)

CFR Title 14 Aeronautics and Space, as applicable

CFR Title 49 Transportation, as applicable

9.2 Other Publications

Work accomplished on this contract may require the following FAA manuals and PWC warranty publication. The FAA manuals or applicable section(s) of the manual and PWC warranty publication are available to the Contractor in electronic format or printed format, if electronic is not available.

AFS Flight Program Office General Maintenance Procedures Manual (GMPM), Approved

Aircraft Inspection Program (AAIP), AMEG Repair Station Policies and procedures as amended.

Pratt & Whitney Canada document “Enhanced Warranty for New Engines and Service

Policies for PT6A Engines in Hawker Beechcraft Aircraft” which describes the engine warranty coverage and requirements.

10 Program Management Requirements

10.1 Program Management Reviews (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 PT6A-135A engine Maintenance and Overhaul program effort. If determined necessary, the FAA or Contractor may request formal PMR’s. The PMR

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-10 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.

10.1.1 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.

10.1.2 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. Contract name and number

b. Type of meeting and date

c. Name of the Contractor and address to which the Contracting Officer should send acknowledgments of receipt and comments

2. Purpose and objectives 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 item 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

10.1.3 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.

11 Invoicing

The Contractor must submit a monthly invoice for the cost per engine hour Maintenance and Overhaul program and an invoice for approved O&A actions within sixty (60) days after the O&A action is completed. Each invoice must be numbered in Contractor format and include the engine maintenance contract number and deliver order number. The monthly invoices, at minimum, must identify the calendar month for the cost per hour engine Maintenance and Overhaul program, the CLIN, and CLIN description. Each engine serial number and engine monthly time in service hours must be identified on the

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-11 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.

12 Acronyms and Definitions

12.1 Acronyms

AAIP Approved Aircraft Inspection Program

ADAS Aircraft Data Acquisition System

AD Airworthiness Directive

AFS Flight Standard Services

AFIS Automated Flight Inspection System

AOG aircraft on the Ground

AMEG Aircraft Maintenance and Engineering Group

AMS Acquisition Management System

ASI Aviation Safety Inspector

AVN Aviation System Standards Program

CAGE Commercial and Government Entity Code

CAS Cost Accounting Standards

CDRL Contractor Data Requirements List

CFR Code of Federal Regulations

CO Contracting Officer

COR Contracting Officer’s Representative

CLIN Contract Line Item Number

CPH Cost Per Hour

CSN Cycles Since New

CSO Cycles Since Overhaul

E&R Exchange & Repair

ECTM Engine Condition Trend Monitoring

FAA Federal Aviation Administration

FAR Federal Aviation Regulations

FFP Firm Fixed Price

FIA Flight Inspection Aircraft

FOD Foreign Object Damage

FPO Flight Program Office

FY Fiscal Year

GAO General Accounting Office

GFP Government Furnished Property

HBC Hawker Beechcraft

HIS Hot Section Inspection

IAW In Accordance With

ID Item(s) Delivered

IPT Integrated Product Team

IR Item(s) Received

LLP Life Limited Parts

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-12

LRU Line Replaceable Unit

MMAC Mike Monroney Aeronautical Center

MRT Mobile Repair Team

NAS National Aerospace System

NLT No Later Than

NTE Not to Exceed

O&A Over and Above

OEM Original Equipment Manufacturer

OKC Oklahoma City, Oklahoma

PBH Power By Hour

PHS&T Packaging, Handling, Storage and Transportation

PM Program Management

PMR Program Management Review

POC Point of Contact

PWC Pratt & Whitney Canada

SB Service Bulletin

SF Standard Form

SIC Standard Industrial Classification Code

TBD To Be Determined

TDR Teardown Report

TI Technical Issuance

TIN Taxpayer Identification Number

TSO Time Since Overhaul

UCA Undefinitized Contractual Actions

12.2 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 specified the conditions and limitations, if any, under which the aircraft type may continue to be operated. The AD carries a compliance date plus flight hours and/or cycles that must be complied with to maintain the FAA Airworthiness Certificate.

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-13

Component: Any self-contained part, combination of parts, subassemblies or units, which performs distinctive function necessary to the operation of the airframe, or power plant.

Configuration: The 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’s Representative: An individual designated by the Contracting

Officer to act as their authorized representative for contact 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 Contracting Officer, and will set forth the authorities and limitations of the representatives, 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 to be 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.

Cost Per Engine 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 hours used by the PT6A-135A Maintenance and Overhaul 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

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-14 reports including scientific and technical reports. It may be in the form of documents, displays, 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 indirect work of overhead and supervisory employees such as officers, engineers, supervisors, foremen, quality control inspector, 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 Cycle: 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 in accordance with the applicable regulatory requirements.

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

Exchange and Repair: Repairable item(s) which, when unserviceable, is returned in exchange for a serviceable replacement.

Flight Inspection Aircraft Maintenance and Engineering Group: An Aviation Systems

Standards activity providing line maintenance, major inspection and overhaul services to the FAA aircraft fleet and equipment.

Flight Time: Refer to Time In Service.

Government Furnished Property (GFP): 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 re 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 part(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.

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-15

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 the 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.

Life Limited Part: A part or component which has an established 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 Maintenance: Includes routine and non-routine maintenance, bench checks, calibration, repairs accomplished in support of day-to-day aircraft operations, and engine removal and replacement.

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, consumables or other material not specifically identified in this SOW, i.e.

corrosion preventive chemicals.

Modification: A change or series of changes in a completed system to adapt it to another system 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 item or accessory in accordance with 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.

Repaired Parts: Parts that have been restored to a serviceable condition and are 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 (SOW): That part of the contract that describes the services to be provided.

Hawker Beechcraft C90GTi PT6A-135A Engine Power By Hour Maintenance & Overhaul Program A-16

Standards: Established or accepted rules, models, or criteria by which the degree of user satisfaction of a product or service is determine, 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, landings, calendar time, or combinations of these.

Time In Service: With respect to flight log documents, FAA computer tracking system, ADASd 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.

13 Required Contractor Property

SIR Attachment A, SOW – eFAST Procurement Action PA-16-038 A-17

Appendix A – Sample Monthly Status Report

SAMPLE MONTHLY STATUS REPORT

REGULATION AND CERTIFICATION INFRASTRUCTURE FOR ABC

PROGRAM

CONTRACT NO. DTFAWA-XXXXX

TASK ORDER NO. DTFAWA-XXXXXX

- Monthly Status Report -

Period: mm/dd/yy-mm/dd/yy

I CONTRACT SUMMARY

Contract Name: ABC, Program Office: Code, Section

Contracting Officer: Name

TOR: name, code, tel#

Alternate TOR: name, code, tel#

Contractor Project Manager: name, code, tel#

Contract Period of Performance: mm/dd/yy –mm/dd/yy

II CONTRACT PROFILE

The contractor is providing technical and implementation support to for the abc program.

III WORK PROGRESS SUMMARY

1. Milestones

DELIVERABLES DUE DATE

Monthly Status Report NLT the xth day of each month zyx required documents As Directed

SIR Attachment A, SOW – eFAST Procurement Action PA-16-038 A-18

2. Work/Travel Completed This Reporting Period (Month):

Participated in formal telecoms and team meetings

̶ Meeting XYZ, Participants – Joe (16 hrs) , Bob (8 hrs) , John (4 hrs)

Continued refinement of the document (attached document ver x.y)

3. Work/ Travel planned for the Forthcoming Period (November):

Continue to draft the document (to include sections worked on), including risk and other sections

Attend and participate at the xyz meetings

Continue to participate in xyz program related meetings and planning for travel

(define each meeting).

IV PROBLEM AREAS

Problems Encountered/Resolved: N/A

Problems Anticipated/Possible Solutions:

V FINANCIAL SUMMARY

Contract Value

Contract Funding

Reporting Period Expenditures Cumulative Expenditures

Funds Remaining Percent of Funds Expended Projected Date for 75% Expenditure of Funds Estimated Funds Expiration Date