Tab 16 Attachment 6_SOW_Min Order.pdf

Federal Aviation Administration

Engine Maintenance Overhaul

Program For

PW Beechcraft 300 PT6A‐60A Engine S/N: PCE‐95354

Statement of Work

1.0 INTRODUCTION

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. 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.

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 The contactor must have the approved tooling and equipment, along with parts and material to adequately maintain all PW Beechcraft 300 PT6A‐60A engines. 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 the overhaul, and perform an airworthiness release in accordance with Flight Program Operations’ FAA-approved CAMP.

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 Overhaul Program

When using engine overhaul facilities that are PW approved, FAA approved, must 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.

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 conditions new, overhaul, repaired or serviceable.

Current cycles, landing and restoration date must be listed on the certification and service maintenance documents. Restored parts must have traceability back to a FAA-Approved 14 CFR Part 145 repair station starting the part was restored in accordance with the OEM manual.

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.

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 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

5.0 Over and Above (O&A) Tasks and Procedures.

4.0 Engine Inspection and Maintenance Documents

Upon completion of engine overhaul 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.

5.0 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.

5.1 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.

6.0 PERIOD OF PERFORMANCE / DELIVERY TIMES

Period of performance: The contractor has sixty (60) days to complete the overhaul once the engine arrives at the authorize PW repair facility.

7.0 PLACE OF PERFORMANCE

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.