Attachment_1__P-8A_SOW_Amendment_0007.pdf

N00019-15-R-2004 Attachment (1), Part A

Statement of Work for

The

P-8A Poseidon Multi-mission Maritime Aircraft Airframe and Engine Maintenance and Repair DEPOT

ATTACHMENT 1

17 May 2016

Distribution Statement A. Approved for Public Release

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Part “A”

Statement of Work (SOW)

For

P-8A Poseidon Airframe Depot

17 May 2016

Table of Contents

SCOPE - AIRCRAFT DEPOT ............................................................................................... 7 1.0

Background ................................................................................................................................................ 7 1.1

System Description .................................................................................................................................... 8 1.2

Depot Maintenance Concept ..................................................................................................................... 8 1.3

REFERENCES AND GOVERNMENT FURNISHED INFORMATION.......................... 9 2.0

INTEGRATED MAINTENANCE AGE EXPLORATION PLAN DEPOT 3.0

SPECIFICATION

AEPD Induction....................................................................................................................................... 11 3.1

Equipment Removal ................................................................................................................................ 11 3.2

Initial Assessment Report Estimate to Completion .............................................................................. 11 3.3

Age Exploration Plan Depot Discrepancies ........................................................................................... 12 3.4

Delay Notifications ................................................................................................................................... 12 3.5

Records and Documentation ................................................................................................................... 12 3.6

AEPD Completion ................................................................................................................................... 12 3.7

Acceptance ............................................................................................................................................... 13 3.8

UNSCHEDULED MAINTENANCE .................................................................................... 13 4.0

Unscheduled Drop-in Depot Maintenance ............................................................................................ 13 4.1

Unscheduled In-Field Maintenance ....................................................................................................... 15 4.2

Flap Track Attach Fitting Concurrent with AEPD .............................................................................. 16 4.3

Stand-alone Flap Track Attach Fitting .................................................................................................. 16 4.4

TECHNICAL DIRECTIVE (TD) INCORPORATION ..................................................... 17 5.0

Requirements ........................................................................................................................................... 17 5.1

TD Incorporation Concurrent with AEPD ........................................................................................... 17 5.2

TD Incorporation Non-Concurrent with AEPD (Drop-In DEPOT) ................................................... 17 5.3

In-Field TD Incorporation ...................................................................................................................... 19 5.4

CONTRACTOR AIRCRAFT ON GROUND (AOG) DEPOT FIELD TEAM ............... 20 6.0

Assessment ............................................................................................................................................... 20 6.1

Discrepancies ........................................................................................................................................... 21 6.2

Critical Safety Items ................................................................................................................................ 21 6.3

Completion ............................................................................................................................................... 21 6.4

PROGRAM MANAGEMENT .............................................................................................. 21 7.0

Program Management Reviews ............................................................................................................. 21 7.1

Meeting Agenda ....................................................................................................................................... 22 7.2

Meeting Minutes ...................................................................................................................................... 22 7.3

Post-Award Conference .......................................................................................................................... 22 7.4

Induction Readiness Review Meetings ................................................................................................... 22 7.5

Technical Interchange Meeting .............................................................................................................. 23 7.6

IMC/P Site Coordinator Office .............................................................................................................. 23 7.7

Program Planning and Control .............................................................................................................. 23 7.8

Sub-Contracts Management ................................................................................................................... 23 7.9

Configuration Management (CM) Plan ................................................................................................. 24 7.10

Risk Mitigation Plans .............................................................................................................................. 24 7.11

RESERVED ............................................................................................................................................. 24 7.12

Financial and Manpower Reporting ...................................................................................................... 24 7.13

GENERAL REQUIREMENTS ............................................................................................ 26 8.0

Title 14 Code of Federal Regulations Part 145 Certifications ............................................................. 26 8.1

Quality Assurance Program ................................................................................................................... 26 8.2

Tool Control and Foreign Object Damage Prevention ........................................................................ 27 8.3

Systems Safety Plan ................................................................................................................................. 27 8.4

Electrostatic Discharge Control Program ............................................................................................. 27 8.5

Hazardous Material and Waste .............................................................................................................. 27 8.6

Classified Material ................................................................................................................................... 28 8.7

Technical Data Deficiencies .................................................................................................................... 28 8.8

Government Furnished Property ........................................................................................................... 28 8.9

Aircraft Fuel ............................................................................................................................................ 29 8.10

Material and Parts ................................................................................................................................... 29 8.11

Critical Safety Items ................................................................................................................................ 31 8.12

Flight Operations Plan ............................................................................................................................ 32 8.13

Deficiency Reporting ............................................................................................................................... 32 8.14

Mishap Reporting .................................................................................................................................... 32 8.15

Security ..................................................................................................................................................... 33 8.16

Engineering Investigations...................................................................................................................... 35 8.17

Disturbed Systems ................................................................................................................................... 35 8.18

Parts Utilization ....................................................................................................................................... 35 8.19

Weight and Balance ................................................................................................................................. 36 8.20

Aircraft Strip and Painting ..................................................................................................................... 36 8.21

Depot Engineering Support .................................................................................................................... 36 8.22

Liaison Engineering ................................................................................................................................. 37 8.23

DEPOT STAND-UP/STAND-DOWN .................................................................................. 38 9.0

Definition .................................................................................................................................................. 38 9.1

RESERVED ............................................................................................................................................. 38 9.2

Transition Plan ........................................................................................................................................ 38 9.3

Government Furnished Equipment Inventory ..................................................................................... 39 9.4

Government Furnished Delivery ............................................................................................................ 39 9.5

ACCESS TO FEDERALLY CONTROLLED FACILITIES, UNCLASSIFIED 10.0

SENSITIVE OR NON-SENSITIVE INFORMATION, AND UNCLASSIFIED

INFORMATION TECHNOLOGY SYSTEMS

Navy Commercial Access Control System............................................................................................. 39 10.1

Identification ............................................................................................................................................ 39 10.2

Control of Common Access Card ........................................................................................................... 40 10.3

SECURITY REQUIREMENT .............................................................................................. 40 11.0

JOINT PERSONNEL ADJUDICATION SYSTEM RECORD MAINTENANCE ......... 40 12.0

BASE INSTALLATION SECURITY REQUIREMENTS ................................................ 41 13.0

INFORMATION ASSURANCE ........................................................................................... 41 14.0

Information Assurance Certification ..................................................................................................... 41 14.1

ACRONYMS .......................................................................................................................... 42 15.0

DEFINITIONS ........................................................................................................................ 44 16.0

SCOPE - AIRCRAFT DEPOT 1.0

This Statement of Work (SOW) is for P-8A Aircraft Depot scheduled and unscheduled maintenance, Depot In-Service Repair (ISR)/Planner & Estimator (P&E) requirements, Technical Directive incorporation , Airframe modifications and Aircraft on Ground (AOG) support. Technical Directive incorporation will be at the System level.The depot work tasks may change due to changes to the maintenance concept or additional requirements at the depot level. This contract supplies all P-8A

Depot level Airframe and Engine maintenance but does not include Depot maintenance requirements for aircraft systems or mission systems components unless specified in the in the Depot Specification

Attachment 5

The Navy is completing the Full Scale Fatigue Testing (FSFT) and Damage Tolerance Analysis

(DTA) for P-8A. Completion of these efforts may result in additional fatigue inspections, and possible pre-emptive repair actions to address structural issues.

Sustainment strategies include the best use of public and private sector capabilities through

Government and industry partnering initiatives. The contractor must provide facilities, labor, services, travel, equipment, tools, parts, materials, and consumables to perform the work requirements; Aircraft Depot Maintenance identified in this SOW, the P-8A Age Exploration Plan

Depot (AEPD), Scheduled Maintenance Plan (SMP) and other references listed below in Section 2

Applicable Documents. The Contractor must remove and replace engines if airframe related work requires it.

Additionally, the Royal Australian Air Force (RAAF) P-8A aircraft will utilize this contract as an option for scheduled and unscheduled depot maintenance, field team assessments, in service repairs, modifications, airframe retrofit installations and AOG services for Continental United States

(CONUS) and Outside Continental United States (OCONUS).

Additionally the P-8A has been offered for Foreign Military Sales (FMS) to other nations. Those nations who sign a Letter of Acceptance from the USG may elect to utilize this contract via the FMS

CLIN’s: X043, X044, X045, X046 for unscheduled depot maintenance, field team assessments, in service repairs, and AOG services both CONUS and OCONUS.

Background 1.1

The Navy is currently transitioning from the P-3C to the new P-8A Poseidon. The P-8A fleet plans to conduct operations out of two Main Operating Bases (MOBs) – Naval Air Station

(NAS) Jacksonville, FL, and NAS Whidbey Island, WA and three overseas Primary

Deployment Sites (PDSs). Squadrons deploy from MOBs to PDSs in order to meet their operational commitments. Under the proposed basing plan, a Permanent Detachment Site will also be established in Kaneohe Bay, HI. RAAF / Australian Defense Force (ADF) P-8A aircraft will be conducting operations out of one MOB; RAAF Edinburgh and three Forward Operating

Base’s (FOBs), RAAF Darwin, RAAF Pearce and RAAF Townsville. To date there is a single

FMS Case established for the P-8A with the United Kingdom Royal Air Force (RAF), with the potential of additional cases established prior to the end of production.

P-8A is an International Program comprised of a Joint Project Office (JPO) and FMS

Customers(s). The JPO participants include the United States Department of Defense (US

DoD) and the Australian Department of Defense (Australian DoD). The Contractor is responsible for full compliance with all USG export control laws and regulations and for obtaining the appropriate export approvals. The Contractor shall ensure deliverable data, developed for the International Cooperative Program, is exportable, in accordance with the existing Technical Assistance Agreements or subsequent export authorizations, all other

International Traffic in Arms Regulations (ITAR), and Export Administration Regulations

(EAR) requirements. The Contractor shall implement protections and risk mitigation procedures to allow access and participation, by Australian Nationals and FMS customers holding appropriate clearances, in exportable and releasable program meetings, working groups, and developmental milestone events. It is the Contractors responsibility to comply with export license requirements, to include cost of the license. The Contractor shall ensure that all necessary International Traffic in Arms Regulations (ITAR) compliance measures and proprietary and data rights requirements are in place to allow for information exchange between the Contractor , US DoD, the Australian DOD, and FMS customers. Contractor export requirements for deliverables will be specified via a Contract Data Requirements List (CDRL).

System Description 1.2

The P-8A is a militarized version of the Boeing 737-800. The P-8A has the fuselage of a 737-

800 and the wings of a 737-900ER. Specific dimensions of the P-8A are contained in the

Aircraft Maintenance Manual (AMM) and are different than a 737-800. The P-8A Poseidon is a long-range Anti-Submarine Warfare (ASW), Anti-Surface Warfare (ASuW), Intelligence

Surveillance and Reconnaissance (ISR) aircraft capable of broad-area, maritime, and littoral operations. It is supported by Navy organic Organizational Level (O-Level) maintenance with limited Intermediate Level (I-Level) maintenance capability.

Depot Maintenance Concept 1.3

The P-8A Airframe utilizes a calendar based maintenance program. The maintenance plan for the P-8A is broken into two Maintenance levels. Organizational Level (“A” Check) maintenance occurs every 90 calendar days and Depot (“D” Check) maintenance intervals are based on a Fixed Induction Date (FID). The first FID is scheduled for 72 months after aircraft delivery with subsequent FID intervals of 48 months. Specific depot requirements are contained in the AEPD Specification (Attachment (5)). Scheduled P-8A Depot Maintenance includes; visual inspection, servicing, Non-Destructive Inspection (NDI), and functional checks of the airframe, engines, flight systems, and sub-systems. The aircraft paint interval begins with the first depot event and re-occurs on every other depot interval. Mission avionics system component maintenance is not a requirement. The P-8A Periodic Maintenance Information

Card (PMIC) A1-P8AAA-PMIC-000 provides the aircraft “A” and “D” check schedule for the duration of this SOW. During performance of an AEPD event incorporation of modifications and age exploration tasks may be required.

REFERENCES AND GOVERNMENT FURNISHED INFORMATION 2.0

The latest specifications, standards, and document Series shall be used during contract performance.

Reference changes/additions after contract award will be directed by contract modification.

Publication Title

14 CFR PART-145 14 CFR Part 145 Repair Station

A1-P8AAA-AMM-100 Aircraft Maintenance Manual Part I - System Description Section

A1-P8AAA-AMM-200 Aircraft Maintenance Manual Part II - Practices and Procedures

A1-P8AAA-MTC-000 P-8A Maintenance Task Cards and Index

A1-P8AAA-NFM-000 P-8A NATOPS

A1-P8AAA-PMIC-000 P-8A Poseidon Periodic Maintenance Information Card (PMIC)

A1-P8AAA-SRM-000 P-8A Structural Repair Manual

A1-P8AAA-NFM-010 Supplemental NATOPS Functional Checkflight Checklist

ANSI/EIA-649 National Consensus Standard for CM

ANSI/ESD S20.20-2007 Electrostatic Discharge Control Program Standard

AS9110 Aerospace Standard - Maintenance Organizations

CNAFINST 4790.2 Series Naval Aviation Maintenance Program https://logistics.navair.navy.mil/

CNAFINST 4790.2B P-8A Mission Essential Subsystem Matrix (MESM)

CPRGINST 4790.12 P-8A Minimum Equipment List (MEL)

DoD Manual 4140.01 DoD Supply Chain Materiel Management Procedures

DoDD 5220.22 Series

Department of Defense Directive (DoDD) Industrial Security Program http://www.dtic.mil/whs/directives/corres/html/522022m.htm dated 18

Mar 2016

DWG 403A3014 Exterior Markings and Finish Schemes for P-8A https://logistics.navair.navy.mil/ http://www.dtic.mil/whs/directives/corres/html/522022m.htm

TBD Exterior Markings and finish Schemes for U.K. P-8A

ESD ADV 53.1-1995 ESD Protective Workstations

ESD TR20.20-2000 Electrostatic Discharge Handbook

MIL-HDBK-61A(SE) Configuration Management Handbook

MIL-STD-882E DoD Standard Practice for System Safety

NA-01-1B-40 Weight and Balance Handbook

NA 15-01-500 Preservation of Naval Aircraft

NAS 412

National Aerospace Standard 412 Tool Control and Foreign Object

Damage (FOD) Prevention

NAVAIR 5100.21B NAVAIR Risk Management Policy

NAVAIRINST 4355.19 Systems Engineering Technical Review Process

NAVAIRINST 13034.1 Flight Clearance Policy for Air Vehicles and Aircraft Systems

SECNAVINST 5510.36 Department of the Navy Information Security Program

P-8 PFSD MOU dated 20

March 2012

Memorandum of Understanding between the U.S. DOD and the Australia

DOD Concerning Cooperation in the P-8A Production, Sustainment and

Follow-on Development Project

P-8 Safety of Flight

Checklist

FRCSE LPS 2110C

Fleet Readiness Center South East local processing specification manual and portable machine hole manufacturing

MIL-STD 7179A

DoD Standard Practices Finishings, Coatings, and Sealants for the

Protection of Aerospace Weapons

INTEGRATED MAINTENANCE AGE EXPLORATION PLAN DEPOT 3.0

SPECIFICATION

The Contractor shall accomplish all Depot inspections and maintenance requirements IAW the

Naval Air Systems Command (NAVAIR) P-8A AEPD Specification (Attachment (5)), A1-

P8AAA-PMIC-000, A1-P8AAA-MTC-000 Maintenance Task Cards, and A1-P8AAA-AMM-

100/200. The Contractor shall remove all equipment/racks necessary to perform AEPD inspection requirements. The Contractor shall conform to the safety of flight inspections in accordance with the safety of flight checklist. The Contractor will validate and verify the PMIC

Task Cards, AMMs and the AEPDs, throughout the depot process to ensure accuracy. The

Contractor shall identify any technical data deficiencies by delivering a Technical Data

Discrepancy record (TDDR) (CDRL A007/C007/E007/G007/J007/L007/N007).

For the purposes of technical inconsistencies between the AEPD Specification and this SOW, the inconsistencies shall be resolved by giving precedence in the following order: (1) SOW; (2)

AEPD Specification. The Contractor shall document and notify the COR of any discrepancy found.

AEPD Induction 3.1

(FFP CLINs X002, X003, X007, X008, X030) The contractor shall perform in accordance with the Naval Air Systems Command (NAVAIR) P-8A AEPD Specification (Attachment (5)).

Aircraft induction for Depot occurs at the scheduled induction month as set forth in the P-8A

Maintenance Inspection Schedule in the contract. The Government will schedule the Induction

Readiness Review (IRR) for each BUNO with the Contractor no later than (NLT) 90 calendar days prior to an AEPD induction to review the required scope of work. See Attachment 19 for anticipated Airframe Induction Schedule. The Government has the flexibility to adjust the induction dates plus or minus two weeks to meet fleet requirements.

Equipment Removal 3.2

(FFP CLINs X002, X003, X007, X008, X030) During disassembly for AEPD inspections the

Contractor shall inspect removed equipment and panels for visible damage, if damaged the contractor shall document the damage using the discrepancy record (Attachment (2) to the contract), the report shall be submitted to the Integrated Maintenance Concept/Plan (IMC/P)

Site Coordinator for repair disposition. The Contractor shall preserve and store all removed equipment and panels. When required for aircraft reassembly, removed equipment and panels will be de-preserved for reinstallation.

The Contractor shall track items that have been removed and retained by BUNO. Upon completion, items removed will be reinstalled on the same BUNO unless otherwise directed by the Government.

Initial Assessment Report Estimate to Completion 3.3

(FFP CLINs X002, X003, X007, X008, X030) Upon completion of the AEPD basic inspection, the Contractor shall deliver an Initial Assessment Report for each aircraft. The information in this report shall establish the Contractual Delivery Date (CDD) and Turn Around Time (TAT) for each aircraft and shall be submitted IAW CDRL

A00L/C00L/E00L/G00L/J00L/L00L/N00L/ B00L/D00L/ F00L/H00L/K00L/ M00L/ P00L

Age Exploration Plan Depot Discrepancies 3.4

(T&M CLINs X004, X009, X031) All Discrepancies found as the result of the AEPD inspection and classified as critical or major in accordance with the Naval Air Systems

Command (NAVAIR) P-8A AEPD Specification (Attachment (5)) shall be repaired IAW the

P-8A Structural Repair Manual (SRM)/AMM using the O&A process as found in section “I” of the contract. All discrepancies will be evaluated by the IMC/P Coordinator for Work/No Work decision. All non-standard repairs shall be reviewed and approved by the Fleet Support Team

(FST) and NAVAIR engineering. If a conflict should occur between the SRM and the AMM, final guidance will be provided by the FST and NAVAIR engineering.

Delay Notifications 3.5

(FFP CLINs X002, X003, X007, X008, X030) After the Initial CDD/TAT is established the

Contractor shall notify the Government of any delays affecting the critical path and delivery of an aircraft. The Contractor shall utilize the Delay Notification Form (DNF) Attachment (7).

Delay Notification Report shall be submitted IAW CDRL

A00J/C00J/E00J/G00J/J00J/L00J/N00J/ B00J/D00J/F00J/H00J/K00J/M00J/P00J.

Records and Documentation 3.6

(FFP CLINs X002, X003, X007, X008, X030) The Contractor shall update the aircraft and engine logbooks in accordance with the Naval Air Systems Command (NAVAIR) P-8A AEPD

Specification (Attachment (5)).

At the completion of each Depot event the Contractor shall complete and submit a Maintenance

History Summary and Corrosion Inspection Report (CDRL

A00C/C00C/E00C/G00C/J00C/L00C/N00C), Structural Alteration Report (CDRL

A009/C009/E009/G009/J009/L009/N009/ B009/D009/F009/H009/K009/M009/P009/), to document repairs that reduce the fatigue life of a fatigue critical component/assembly or will require unscheduled inspection to reach the components fatigue life limit and Depot Completion

Report (CDRL A00D/C00D/E00D/G00D/J00D/L00D/N00D/

B00D/D00D/F00D/H00D/K00D/M00D/P00D/.

AEPD Completion 3.7

(FFP CLINs X002, X003, X007, X008, X030) The contractor shall perform all AEPD completion tasks in accordance with the Naval Air Systems Command (NAVAIR) P-8A AEPD

Specification (Attachment (5)). The Contractor shall notify the Gov’t 10 days prior to the completion of the AEPD to schedule the Flight Readiness Review (FRR). The Contractor shall debrief the completed repair(s) and conduct an FRR using NAVAIRINST 4355.19 as guidance.

See Paragraph 8.18 for Disturbed System procedures.

Acceptance 3.8

(FFP CLINs X002, X003, X007, X008, X030) After completion of all repairs, the Contractor shall sign off all open work orders and provide Certificate of Conformance (CoC) documentation to the Government. The Contractor shall provide a final report detailing the repairs performed IAW CDRLs A009/C009/E009/G009/J009/L009/N009/

B009/D009/F009/H009/K009/M009/P009/.

UNSCHEDULED MAINTENANCE 4.0

Unscheduled Drop-in Depot Maintenance 4.1

(T&M CLINs X020, X021, X033, X043) The work performed hereunder includes unscheduled maintenance performed at the contractor’s facility. This work is beyond the capability of the O-

Level that cannot be accomplished in the field. The PCO will provide direction to induct and initiate the initial assessment report IAW 4.1.2.

Induction Requirements 4.1.1

The Government will notify the Contractor prior to an unscheduled maintenance event to review the required scope of work. The contractor shall perform induction activities to include:

The Contractor shall perform preservation in accordance with NA 15-01-500 and the

AMMs based on the expected TAT for the work being performed on P-8A aircraft.

Joint Government/Contractor inventory of all items aboard the aircraft utilizing the Aircraft

Inventory Record (AIR) (Office of the Chief of Naval Operations (OPNAV) 4790/111 and

112) and Weight & Balance Chart "C" inventory (DD Form 365-3) and annotate any shortages.

Conduct ferry flight discrepancy/documentation review with the Government and prepare the aircraft for maintenance.

If required the Contractor shall schedule defueling upon arrival and prior to induction; any fuel removed at the depot facility may be scrapped at the depot’s discretion. The Contractor shall provide a Point of Contact (POC) to enable status discussion to Program Management

Activity (PMA-290).

The Government will remove sensitive/controlled flight essential equipment that was installed for ferry purpose prior to induction. The Government will provide Engine, Auxiliary Power Unit, and Aircraft Logs.

Aircraft access shall be restricted to personnel requiring access to perform maintenance or otherwise in direct support of maintenance and meet ITAR criteria.

Initial Assessment Report Estimate to Completion 4.1.2

The Contractor shall perform an assessment of the inducted aircraft and deliver an Initial

Assessment Report. The information in this report shall be submitted IAW CDRL

A00L/C00L/E00L/G00L/J00L/L00L/N00L/ B00L/D00L/F00L/H00L/K00L/M00L/P00L

/AG0L/AJ0L/AM0L/AP0L/AR0L/AT0L. The CDD/TAT will be established via issuance of a contract modification by the PCO.

Delay Notifications 4.1.3

After the Initial CDD/TAT is established the Contractor shall notify the Government of any delays affecting the critical path and the delivery of an aircraft. The Contractor shall utilize the

Delay Notification Form (DNF) Attachment (7) to support all Impact Assessments. The Delay

Notification Forms (DNF) shall be used to document delays. Impact Delay Notification Report

Assessment shall be submitted IAW CDRL

A00J/C00J/E00J/G00J/J00J/L00J/N00J/Q00J/B00J/D00J/F00J/H00J/K00J/M00J/P00J/R0

0J /AG0J/AJ0J/AM0J/AP0J/AR0J/AT0J

Discrepancy Record(s) 4.1.4

The Contractor shall submit a discrepancy record (Attachment (2)) for all airframe defects discovered during the unscheduled depot event that is not related to the unscheduled work scope. The records shall be submitted to the Integrated Maintenance Concept/Plan (IMC/P) Site

Coordinator for disposition.

Completion of Unscheduled Depot Maintenance 4.1.5

Return to Service 4.1.5.1

Upon completion of all aircraft repairs and post repairable activities, the Contractor shall perform depreservation in accordance with NA 15-01-500 as required and present the aircraft to the Government Air Crew for post Depot inspection and acceptance. The Contractor shall review, with the Government Air Crew, a listing of all work performed and discrepancies discovered, corrected or noted but not corrected (NBNC) during the Depot process. The

Contractor shall perform post-repair activities to include the following paragraphs:

Flight Readiness Review Debrief 4.1.5.2

The Contractor shall debrief the completed repair(s) and conduct a Flight Readiness Review using NAVAIRINST 4355.19 as guidance. The Contractor shall notify the Gov’t 10 days prior to the completion of the maintenance to schedule the Flight Readiness Review (FRR). The

Contractor shall debrief the completed repair(s) and conduct an FRR using NAVAIRINST

4355.19 as guidance. See Paragraph 8.18 for Disturbed System procedures.

Updated Logs and Forms 4.1.5.3

After completion of all aircraft repairs the Contractor shall provide appropriate documentation entries into the aircraft/engine logs in accordance with (CNAFINST 4790.2 Series) 4790.2

Series. Contractor shall conduct a Joint Government/Contractor inventory of all items aboard the aircraft utilizing the Aircraft Inventory Record (OPNAV 4790/111 and 112) and Weight &

Balance Chart "C" inventory (DD Form 365-3) and annotate any shortages.

The contractor shall provide the ferry crew a completed FAA Form 337 (or succeeding FAA

Form), NBNC List, Weight and Balance Chart A (DD Form 365-1) if applicable, at completion of each Maintenance Repair and Overhaul (MRO) visit. One copy of each will be retained in the aircraft or engine logs and one copy will be retained by the Contractor. A Depot Completion

Report shall be provided per (CDRLs A00D/C00D/E00D/ G00D/J00D/L00D/N00D/

B00D/D00D/F00D/H00D/K00D/M00D/P00D/ AG0D/AJ0D/AM0D/AP0D/AR0D/AT0D).

Upon completion of the Depot visit, a FAA A&P or Avionics Mechanic with Inspector

Authorization (Part 145 Certified) shall sign an entry for the USN aircraft logbook documentation, certifying inspection completion and configuration status of the aircraft.

Functional Check Flight (FCF) Support 4.1.5.4

If necessary, the Contractor shall prepare the aircraft for the FCF and all post-FCF support requirements to deliver the aircraft.

Certificate of Conformance 4.1.6

After completion of all repairs, the Contractor shall sign off discrepancies and provide FAA

Form 337 (if applicable) or Certificate of Conformance (CoC) documentation to the

Government. The Contractor shall provide a Structural Alteration report detailing the fatigue critical repairs performed (if applicable) IAW CDRLs

A009/C009/E009/G009/J009/L009/N009/ /B009/D009/F009/H009/K009/M009/P009/

AG09/AJ09/AM09/AP09/AR09/AT09).

Unscheduled In-Field Maintenance 4.2

(T&M CLINs X020, X021, X033, X043) The work performed hereunder includes any unscheduled depot maintenance that can be accomplished in the field. All “O” level activities such as preparing the aircraft for maintenance are the responsibility of the “O” level.

Field Team Requirements 4.2.1

Prior to contractor travel to the aircraft site (T&M CLINs X017, X038, X044), contractor shall participate in a joint meeting with the FST and squadron maintenance personnel to ensure that the scope of work is defined and understood. This meeting shall establish all of the material and tooling required. Any material and tooling not available at the “O” level shall be provided by the Contractor. Prior to commencing work, the Contractor shall check-in with squadron maintenance control and is required to follow all local maintenance processes and procedures.

The contractor shall provide the Gov’t a field assessment report in accordance with CDRLs

A00F/C00F/E00F/G00F/J00F/L00F/N00F/ B00F/D00F/F00F/H00F/K00F/M00F/P00F/

AG0F/AJ0F/AM0F/AP0F/AR0F/AT0F).

Completion 4.2.2

After completion of all repairs, the Contractor shall sign off discrepancies and provide FAA

Form 337 (if applicable) and/or Certificate of Conformance (CoC) documentation to the

Government. The Contractor shall provide an In-field Completion report detailing repairs performed IAW CDRLs A00D/C00D/E00D/G00D/J00D/L00D/N00D/ B00D/D00D/

F00D/H00D/K00D /M00D/P00D/ AG0D/AJ0D/AM0D/AP0D/AR0D/AT0D). The

Contractor shall also provide a Structural Alteration report detailing the fatigue critical repairs performed (if applicable) IAW CDRLs A009/C009/E009/ G009/J009/L009/N009/

B009/D009/F009/H009/K009/M009/ P009/ AG09/AJ09/AM09/AP09/AR09/AT09).

Flap Track Attach Fitting Concurrent with AEPD 4.3

(FFP CLINs X019, X041) The Contractor shall remove and replace the fitting in accordance with the P-8A AMM. The Contractor shall follow the procedures under paragraph 3.0.

After completion of the Flap Track replacements, the Contractor shall provide FAA Form 337

(if applicable) and/or Certificate of Conformance (CoC) documentation to the Government. If necessary, the Contractor shall provide an In-field Completion report detailing repairs performed IAW CDRLs A00D/C00D/E00D/G00D/J00D/L00D/N00D/ B00D/D00D/

F00D/H00D/K00D /M00D/P00D.

Stand-alone Flap Track Attach Fitting 4.4

(T&M CLINs X015, X042X043) The Contractor shall remove and replace the fitting in accordance with the P-8A AMM. The Contractor shall follow the procedures under paragraphs

3.0, 4.1, or 4.2 above depending on aircraft location.

After completion of the Flap Track replacements, the Contractor shall provide FAA Form 337

(if applicable) and/or Certificate of Conformance (CoC) documentation to the Government. If necessary, the Contractor shall provide an In-field Completion report detailing repairs performed IAW CDRLs A00D/C00D/E00D/G00D/J00D/L00D/N00D/

B00D/D00D/F00D/H00D/K00D /M00D/P00D/ AG0D/AJ0D/AM0D/AP0D/AR0D/AT0D).

TECHNICAL DIRECTIVE (TD) INCORPORATION 5.0

Requirements 5.1

(T&M CLINs X012, X014, X034 and FFP CLINs X013 and X035) Contractor shall incorporate depot level TDs, including mission systems avionics upgrades at the system level, not at the component level, as directed by the Government either concurrent with AEPD, as a depot drop-in or in the field. Contractor shall have the ability to install multiple TDs concurrent with a single AEPD, depot drop-in, or in field event. Boeing Service Letters and Service

Bulletins that have not been converted to US NAVY technical directive format shall comply with the references FRCSE LPS 2110C and MIL-STD 7179A.

TD Incorporation Concurrent with AEPD 5.2

(T&M CLINs X012, X014, X034 and FFP CLINs X013 and X035) To improve fleet readiness and reduce aircraft out-of-service time, the Government will identify TDs to be incorporated concurrent with AEPD maintenance. TDs will be identified by the Government during the IRR process described under paragraph 3.1. All TDs, service letters, and service bulletins are identified in Attachment (8). This Attachment is a living document and shall be updated as new TDs, service letters, and service bulletins are issued. Emergent TDs or TDs that have not been validated and verified are not on Attachment (8) and will be executed as Time and Material efforts. Once validated and verified, these TDs will be added to Attachment (8) as firm fixed price efforts through bilateral modification. An Aircraft shall be inducted for TD incorporation using AEPD or Unscheduled Maintenance CLINs: X002, X003, X007, X008, X020, X021, X030, or X033.

TD Incorporation Non-Concurrent with AEPD (Drop-In DEPOT) 5.3

(T&M CLINs X012, X014, X034 and FFP CLINs X013 and X035) The work performed hereunder includes any Technical Directive (TD) incorporation to be accomplished in depot non-concurrent with AEPD. The Government will coordinate with the Contractor prior to a

Depot TD Incorporation induction to review the required scope of work. An Aircraft shall be inducted using AEPD or Unscheduled Maintenance CLINs: X002, X003, X007, X008, X020, X021, X030, or X033.

The Contractor shall perform induction activities:

The Contractor shall perform preservation in accordance with NA 15-01-500 and the

AMMs based on the expected TAT for the work being performed on P-8A aircraft.

Joint Government/Contractor inventory of all items aboard the aircraft utilizing the Aircraft

Inventory Record (AIR) (Office of the Chief of Naval Operations (OPNAV) 4790/111 and

112) and Weight & Balance Chart "C" inventory (DD Form 365-3) and annotate any shortages.

Conduct ferry flight discrepancy/documentation review with the Government and prepare the aircraft for maintenance.

If required based on the magnitude of the effort, the Contractor shall schedule defueling upon arrival and prior to induction; any fuel removed at the depot facility may be scrapped at the depot’s discretion The Contractor shall provide a Point of Contact (POC) to enable status discussion to Program Management Activity-290 (PMA-290).

The Government will remove sensitive/controlled flight essential equipment that was installed for ferry purpose prior to induction. The Government will provide Engine, Auxiliary Power Unit, and Aircraft Logs.

Aircraft access shall be restricted to personnel requiring access to perform maintenance or otherwise in direct support of maintenance and meet ITAR criteria.

Reserved 5.3.1

Discrepancy Record(s) 5.3.2

(T&M CLINs X012, X014, X034 and FFP CLINs X013 and X035) The Contractor shall submit a discrepancy record (Attachment (2)) for all defects discovered during the Technical

Directive incorporation. The report shall be submitted to the Integrated Maintenance

Concept/Plan (IMC/P) Site Coordinator for disposition.

Completion of Drop-In Depot TD Incorporation 5.3.3

Return to Service 5.3.3.1

(T&M CLINs X012, X014, X034 and FFP CLINs X013 and X035) Upon completion of all technical directive incorporation, the Contractor shall perform depreservation in accordance with NA 15-01-500 and present the aircraft to the Government Air Crew for post Depot inspection and acceptance. The Contractor shall review, with the Government Air Crew, a listing of all work performed and discrepancies discovered, corrected or NBNC during the

Depot process. A Depot Completion Repair Report shall be provided per CDRL

A00D/C00D/E00D/G00D/J00D/L00D/N00D/ B00D/D00D/F00D/H00D/K00D/M00D/P00D.

The Contractor shall perform post-repair activities to include to the following paragraphs below:

Aircraft Inventory Record 5.3.3.2

(T&M CLINs X012, X014, X034 and FFP CLINs X013 and X035)) Joint

Government/Contractor inventory of all items aboard the aircraft utilizing the Aircraft Inventory

Record (OPNAV 4790/111 and 112) and Weight & Balance Chart "C" inventory (DD Form

365-3) and annotate any shortages.

Flight Readiness Review Debrief 5.3.3.3

(T&M CLINs X012, X014, X034 and FFP CLINs X013 and X035) The Contractor shall debrief the completed repair(s) and conduct a Flight Readiness Review using NAVAIRINST

4355.19 as guidance. The Contractor shall notify the Gov’t 10 days prior to the completion of the maintenance to schedule the Flight Readiness Review (FRR). The Contractor shall debrief the completed repair(s) and conduct an FRR using NAVAIRINST 4355.19 as guidance. See

Paragraph 8.18 for Disturbed System procedures.

Updated Logs and Forms 5.3.3.4

(T&M CLINs X012, X014, X034 and FFP CLINs X013 and X035) After completion of all aircraft repairs the Contractor shall provide appropriate documentation entries into the aircraft/engine logs in accordance with CNAFINST 4790.2 Series. The contractor shall provide the ferry crew a completed FAA Form 337 (or succeeding FAA Form) or CoC, NBNC List, Weight and Balance Chart A (DD Form 365-1) if applicable, at completion of each

Maintenance Repair and Overhaul (MRO) visit. One copy of each will be retained in the aircraft or engine logs and one copy will be retained by the Contractor. Upon completion of the

Depot visit, a FAA A&P or Avionics Mechanic with Inspector Authorization (Part 145

Certified) shall sign an entry for the USN aircraft logbook documentation, certifying inspection completion and configuration status of the aircraft.

Functional Check Flight (FCF) Support 5.3.3.5

(T&M CLINs X012, X014, X034 and FFP CLINs X013 and X035) If necessary, the

Contractor shall prepare the aircraft for the FCF and all post-FCF support requirements to deliver the aircraft.

Certificate of Conformance 5.3.4

(T&M CLINs X012, X014, X034 and FFP CLINs X013 and X035) After completion of all

Technical Directives the Contractor shall provide a Certificate of Conformance (CoC) to the

Government to document the incorporation of all TDs.

In-Field TD Incorporation 5.4

(T&M CLINs X012, X014, X034 and FFP CLINs X013 and X035) The work performed hereunder includes any Technical Directive (TD) incorporation to be accomplished in the field.

All “O” level activities such as preparing the aircraft for TD incorporation are the responsibility of the “O” level.

Field Team Requirements 5.4.1

Prior to contractor travel to the aircraft site (T&M CLINs X017, X038), contractor shall participate in a joint meeting with the Program Office and squadron maintenance personnel to ensure that the scope of work is defined and understood. Meeting shall establish all of the material and tooling required. Any material and tooling not available at the “O” level shall be provided by the Contractor. Prior to commencing work, the Contractor shall check-in with squadron maintenance control and is required to follow all local maintenance processes and procedures.

Completion 5.4.2

(T&M CLINs X012, X014, X034 and FFP CLINs X013 and X035) After completion of all

Technical Directives the Contractor shall provide a Certificate of Conformance (CoC) to the

Government to document the incorporation of all TDs.

CONTRACTOR AIRCRAFT ON GROUND (AOG) DEPOT FIELD TEAM 6.0

(T&M CLINs X017, X018, X036, X038, X045)

Aircraft on Ground (AOG) maintenance support is emergent maintenance efforts that are beyond the technical expertise or authorization of the squadron.

Assessment and Repair 6.1

To activate an AOG event the squadron will send a request to the P-8A FST IAW CNAFINST

4790.2 Series. Upon PCO authorization, the Contractor shall coordinate a planned response with the Program Office within 12 hours. Upon travel and arrival to the AOG location (T&M

CLINs X017, X038, X044); the Contractor shall meet with the squadron maintenance control to coordinate O-level assistance and to gain access to the aircraft. At the conclusion of the assessment, the contractor shall provide the Gov’t a field assessment report in accordance with

CDRLs A00F/C00F/E00F/G00F/J00F/L00F/N00F/

B00F/D00F/F00F/H00F/K00F/M00F/P00F/ AG0F/ AJ0F/ AM0F/ AP0F/ AR0F/ AT0F

Upon review of the field assessment report, the Government (P-8A FST) and the Contractor shall agree on the repair specification and all coordinating details (i.e. HAZMAT, Maintenance responsibility, location, etc). The contractor shall provide the Government an estimate that includes hours per task, a Priced Bill of Material (PBOM), and HAZMAT requirements. Upon authorization by the PCO, the Contractor shall begin repair work in accordance with the negotiated repair specification.

Discrepancies 6.2

For aircraft structural and aircraft system discrepancies, the Contractor shall use authorized P-

8A Aircraft Maintenance Manual (AMM) / Structural Repair Manual (SRM) repair procedures.

Non-standard repairs or maintenance not detailed in the P-8A AMM/SRM will require

NAVAIR/FST engineering approval. Additionally, a determination by the FST may be made to either accomplish a repair in place or make a temporary repair and fly the aircraft to a MOB /

PDS and/or drop-in to a Depot facility for final repairs. Drop-in repairs shall be directed by the

Government in accordance with Unscheduled Depot Maintenance requirements (Paragraph 4.1)

Critical Safety Items 6.3

See Paragraph 8.12.

Completion 6.4

After completion of all repairs, the Contractor shall sign off discrepancies and provide FAA

Form 337 (if applicable) and/or a Certificate of Conformance (CoC) to the Government. An In-field Completion Repair Report shall be provided per CDRLs

A00D/C00D/E00D/G00D/J00D/L00D/N00D/ B00D/D00D/F00D/H00D/K00D/M00D/P00D/

AG0D/AJ0D/AM0D/AP0D/AR0D/AT0D). The Contractor shall also provide a Structural

Alteration report detailing the fatigue critical repairs performed (if applicable) IAW CDRLs

A009/C009/E009/G009/J009/L009/N009/ B009/D009/F009/H009/K009/M009/P009/

AG09/AJ09/AM09/AP09/AR09/AT09/AV09.

PROGRAM MANAGEMENT 7.0

The Contractor shall manage all technical and contractual performance, including program planning and control, Logistics Support , cost, schedule, and data delivery requirements related to this SOW.

The contractor shall provide functional resources and technical processes in support of program execution. The contractor shall provide an Integrated Master Schedule (IMS) in accordance with

CDRL A003/C003/E003/G003/J003/L003/N003, for each aircraft induction to the Government program manager and P-8A Program Office to effectively execute and track the progress. The contractor is responsible for financial reporting, supplier management, and management of

Government Furnished Property (GFP) / Government Furnished Equipment (GFE) / Government

Furnished Information (GFI). The contractor shall support Government periodic reviews including

Program Management Reviews (PMRs), Technical Interchange Meetings (TIMs), and IRRs. An

Integrated Baseline Review (IBR) will be conducted 180 days after contract award at the Contractor’s site.

Program Management Reviews 7.1

The Contractor shall conduct a PMR at the Contractor’s site 30 days after the first induction and quarterly thereafter (no more than four per year). The Contractor shall prepare and deliver an agenda (CDRL A001) and meeting minutes (CDRL A002). The items for presentation and discussion at each PMR shall include, at a minimum:

A brief overview and status of the program cost, schedule, and performance by each delivery order (to include BUNO number);

Updates to the Integrated Master Schedule (IMS);

An update and analysis of Technical Performance Measures and associated metrics as defined in the Contractor Quality Assurance Program Plan (QAPP) (CDRL A004); and an overall Quality brief including any contractor-generated damage;

An assessment of the program schedule and risks to include critical path analysis, missed milestones, and corrective action plans;

Status of outstanding CDRLs, with detailed explanation for any that are past due;

A summary of program data, including production status, engineering status and issues;

Status and discussion of open action items resulting from the previous PMRs, milestone presentations, and technical coordination meetings;

Over and Above labor and material funding status;

Copies of all presentation material (e.g., charts, graphs, etc.) (CDRL A002).

Meeting Agenda 7.2

The Contractor shall prepare for each meeting by drafting an agenda and presentation material.

The Contractor shall submit a Meeting Agenda IAW CDRL

A001/C001/E001/G001/J001/L001/N001.

Meeting Minutes 7.3

The Contractor shall track all action items, agreements, and all pertinent information for each meeting and submit meeting minutes IAW CDRL A002/C002/E002/G002/J002/L002/N002.

Post-Award Conference 7.4

The Contractor shall conduct one Post Award Conference approximately 30 calendar days after the initial contract award at the Contractor’s site. The purpose is to allow the Contractor and the

Government to establish lines of communication, set program objectives, priorities, and address any issues. The Contractor shall prepare and deliver an agenda (CDRL

A001/C001/E001/G001/J001/L001/N001) and meeting minutes IAW CDRL

A002/C002/E002/G002/J002/L002/N002.

Induction Readiness…