Attachment No. 2 entitled Statement of Work.pdf

NASA 801 HSI

Version 1

NASA 865 ACI

Table of Contents

1.0 Background

2.0 Objectives

3.0 Scope

4.0 Requirements

5.0 Deliverables

6.0 Government-Furnished Property (GFP)

7.0 Security Considerations

8.0 Travel

9.0 Special Material Requirements

10.0 Other Unique Requirements and Considerations

11.0 Place of performance

12.0 Period of performance

1. Background

The National Aeronautics and Space Administration (NASA) Armstrong Flight Research Center operates a King Air B200. The aircraft registration number N801NA is currently managed by

NASA Armstrong Flight Research Center (AFRC) and is based at hangar building 4802 located in 4800 Lilly Ave, Edwards, CA 93523. The aircraft will be undergoing phase maintenance at the time the engine HSI is due, making it necessary for servicing personnel to travel to NASA

AFRC to perform the described task.

NASA AFRC requires Hot Section Inspection (HSI) services performed to the aircraft to be suitable for safe flight on NASA missions. This HSI service was previously completed on both engines in accordance with Pratt & Whitney MAINTENANCE MANUAL Model(s) PT6A-52

Manual Part No.3072862. This SOW describes the work to be performed and deliverables to be provided by the contractor capable of these services.

2. Scope and Objectives

To provide scheduled Hot Section Inspection maintenance to two PT6A-52 engines.

2.1 Hot Section Inspection

The Contractor shall perform required inspections and maintenance in accordance with (IAW) the Pratt & Whitney PT6A-52 Maintenance Manual for Turboprop Gas Turbine Engines (Part

Number 3072862) Revision 21.

The Contractor shall use the methods, techniques, and practices prescribed in approved engineering documentation, FAA Advisory Circular 43.13: Acceptable Methods, Techniques, and Practices for Aircraft Inspection and Repair.

The Contractor shall complete all applicable Engine Service Bulletins.

Type Aircraft Beechcraft Beech 200 Super King Air aircraft

Tail Number N801NA

Serial Number BB1164

Total Hours 7325

Total Cycles 6555

Engine Type Pratt & Whitney PT6A-52

Engine Position & Serial Number (Left) PCE-RX0221

Engine Position & Serial Number (Right) PCE-RX0222

Engine Information

Aircraft Information

The Contractor shall provide all personnel, to include supervisory personnel with the required qualifications, experience. Personnel must have FAA part 145 Airframe & Powerplant (A&P) certification for Pratt & Whitney PT6A-52.

The Contractor shall provide all equipment, supplies, tools, materials, documentation, and other items necessary to perform the HSI, except for those items specified as Government furnished data or equipment to be identified after contract award.

Work shall be in accordance with all applicable regulations, publications, manuals, and local policies and procedures to include those provided in Table 1 while conducting all scheduled and unscheduled maintenance on NASA B200 Aircraft.

Table 1: Reference Documents

Document/Part # Title

3072864 Pratt & Whitney Parts Catalog

3072862 Pratt & Whitney Maintenance Manual

SAE AS9100 Quality Management Systems – Requirements for Aviation, Space, and Defense Organizations

NPR 7900.3 NASA Procedural Requirements, Aircraft Operations

Management Manual

2.2 Records

At a minimum, the contractor shall provide the following information for maintenance records:

Maintenance action, Maintenance Reference, Part Number, Serial Number, Installation/Removal date, completion date, manufacturer.

The Contractor shall provide a final Logbook Entry of the aircraft inspection/modification and record completed services for aircraft as instructed by the FAA for accurate tracking of compliance with service schedules.

3. Over & Above Requirements

Over and Above Cost. NASA will authorize what is commonly termed “over and above” inspections as necessary. The NASA Contracting Officer will designate NASA personnel as the

Contracting Officer’s Representative (COR) to determine what “over and above” maintenance is to be performed.

4. Quality Control and Assurance

4.1 The Contractor shall provide and maintain an AS9110 certified Quality

Management System. The Contractor’s inspection program shall ensure compliance with technical guidance, engineering specifications, and

EASA/FAA regulations applicable to CFM56 engine maintenance.

Documentation shall be required for traceability, accountability, and a historical record of design, testing, inspection, qualification, and acceptance of all materials and components.

4.2 Quality System: The Contractor shall possess current EASA/ FAA Repair

Station certification to 14 C.F.R. Part 145 with the following rating:

Powerplant. A certified repair station must establish and maintain a quality control system acceptable to the FAA that ensures the airworthiness of the articles on which the repair station or any of its contractors performs maintenance, preventative maintenance, or alterations.

4.3 The Contractor shall be responsible for Quality Assurance of vendors, suppliers, and subcontractors providing services under this contract to verify compliance with accepted standards. For those vendors who provide EASA/FAA certified parts and services, a copy of the valid certification shall be made available to

NASA.

4.4 Non-conformance: The Contractor shall have in place a procedure for reporting of nonconforming articles, materials, and equipment. (“Non- conformance” is defined as a condition of any article, material, or service in which one or more characteristics do not conform to the specified requirements. This includes failures, discrepancies, deficiencies, defects, anomalies, and malfunctions).

4.5 Inspection: The Contractor shall provide inspectors to verify that work is performed in accordance with technical specifications and the documentation is completed in accordance with the CFM56-2 Maintenance Manual.

4.6 Tool Control: NASA requires the Contractor to utilize a system of positive tool control, including (but not limited to) shadowing of toolboxes. Contractors not in compliance with this requirement shall propose an alternative method of tool control. Toolboxes will be locked when not in use. If unlocked, toolboxes are considered ‘in use’ and will have an inventory completed and documented immediately. Toolboxes will be diligently checked to ensure all contents are accounted for (inventoried) at a minimum of the beginning and end of each shift

(if toolbox is used), and before releasing an aircraft for flight (if flight release occurs before end of shift). All inventories will always check all drawers, pouches, cases, etc., to ensure all items are accounted for at all times

4.7 Government Mandatory Inspection Points:

4.7.1.1 Designated government representative(s) shall be present for engine assessment process.

4.7.1.2 Designated government representative(s) shall inspect all data packages and perform an on-site visual inspection prior to completion.

4.8 The Contractor shall implement and maintain a foreign object debris (FOD) control, Electrostatic Discharge (ESD), and a tool control program while working on NASA aircraft.

4.9 Work areas, engines, and aircraft will be kept clean: Free of FOD, trash, hardware, aircraft parts.

4.10 Government Mandatory Inspection Points (GMIPs)

1) Prior to “Panel Up”

2) Engine Control Operational checks

3) Engine bay cavity inspection: Prior to engine install (as required)

4) Pre-installation engine inspection (engine itself): Immediately prior to install (at aircraft

& as required)

5) Engine installation: Final mount torques, fuel manifold reconnection, and throttle cable reconnection (as required)

6) Throttle quad/connection/rigging: Final rig measurement (as required)

Additional GMIPs may be implemented by NASA QA as required:

1) Critical measurements and key characteristics

2) Mechanical parameters (e.g., function, torque, bonding)

3) Discretionary GMIPs may be applied to activities that have demonstrated a need for increased surveillance (performance history, unexplained hardware or software anomalies, operations with an accelerated schedule, workmanship in critical applications, etc.)

4) Inspection and testing of critical or special testing (e.g., welding, soldering, plating). 5)

Safety precautions to be observed during hazardous operations.

6. Schedule

6.1 Kickoff Teleconference – to be established immediately after contract award; the contractor will provide a task schedule and initial task coordination will occur

6.2 Progress Updates – NASA contacts for regular progress updates will be provided at the kickoff meeting

6.3 Conclusion – coordination between NASA AFRC and the contractor will occur as the task nears completion to ensure preparedness for the final Post Doc Meeting

7. Post Doc Meeting

The Post-Dock meeting is required by NASA maintenance procedures and is intended to identify the maintenance requirements that were accomplished during the major maintenance activities.

The Contractor shall support and present the following topics during the Post-Dock Meeting.

• Maintenance activities accomplished

• Any engineering issues accomplished

• Any items remaining unresolved

8. Deliverables

The Contractor shall provide NASA AFRC with the following documentation:

Upon completion of the HSI, for the aircraft:

• Aircraft Condition Receipt Report

• Over and Above Discrepancies Report

• Parts and Material Certifications

• Logbook Entry

• Completed FAA Form 337’s for all repairs and alterations, where necessary

• All Documentation Required in Maintenance Manual

The Contractor shall provide progress reports (frequency) that include at a minimum:

• Task status

• Percent complete of each sub-task

• Percent complete of overall HSI progress

• Potential schedule changes

• Potential issues and mitigation strategies

• Over and above discrepancies

• Upcoming MIPs

▪ Provide a FAA 8130

▪ Provide a detailed recommendation for assessed engine repairs for continued airworthiness

All deliverables shall be provided in Microsoft Office or Adobe PDF format via email.

10. Other Requirements

The Contractor shall ensure all scheduled and unscheduled maintenance, to include the HSI removal and replacement and/or reinstallation components are documented, and each maintenance action cleared by appropriate signature authorities prior to releasing aircraft “safe for flight”. Additionally, Scheduled Component Removal/Replacement Criteria shall be strictly adhered to while performing the services.

Except for necessary testing, the aircraft shall be kept in a hangar at all times.

Taxiing and engine turn operations shall be performed by NASA operators Flight operations shall be performed by only NASA Code 410 (Aircrew) operators.

11. Pace of Performance

The work must be done at NASA Armstrong Flight Research Center's (AFRC) located in hangar building 4802 located in 4800 Lilly Ave, Edwards, CA 93523

12. Period of Performance

HSI shall be completed 60 days after award.