Attachment 3 - SOW.pdf

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Progressive Structural Inspection (PSI) and Depot Level Maintenance (DLM) for C-130J Aircraft
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70Z03820RH0000003
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70Z03820RH0000003

STATEMENT OF WORK (SOW)

FOR

Offsite PSI and Block 8.1 Upgrade for up to four (4) USCG HC-130J Aircraft

1.0 GENERAL

1.1 BACKGROUND

The United States Coast Guard (USCG) Aviation Logistics Center (ALC), Long Range Surveillance (LRS) Product Line Division (PLD), has a need to establish continued support for Progressive Structural Inspection (PSI) and Depot Level Maintenance (DLM) of C-130J aircraft.

The USCG ALC is responsible for providing aviation support in DLM, engineering, supply, procurement, information services, and acquisition project execution for the USCG’s aviation community. The C-130J aircraft are the USCG's LRS aircraft providing critical Search and Rescue, Law Enforcement, Logistics, and Marine Environmental Protection response to the United States of America.

1.2 SCOPE

The PSI is the depot level inspection and repairs of the C-130 series aircraft to ensure airworthiness through detailed non-destructive inspection procedures. Additionally, these inspections ensure compliance with Aircraft Structural Integrity Program (ASIP) requirements.

Due to the corrosive environment in which USCG aircraft operate, a PSI is required to be performed on each USCG C-130 every 48 months (previous PSI to new induction). The LRS PLD estimates a need to complete PSI for up to four (4) C-130J aircraft. The facility will be required to conduct PSI for up to two aircraft in flow at a time with additional space for at least one (1) aircraft in Unscheduled Depot Level Maintenance (UDLM). Avionics Modernization may be required for the C-130J in conjunction with the PSI. The period of performance for this contract will be October 2020 to October 2023. During the period of performance an UDLM may be required for additional C-130J aircraft which are not currently inducted into PSI.

1.3 OBJECTIVE

This effort will satisfy the structural overhaul requirements for these C-130J aircraft. The PSI services are divided into 9 Phases which include Induction, De-paint, Disassembly, Inspection, Repairs, Assembly, Operational Test, Functional Test Flights, and Paint. This effort will be accomplished in accordance with the USCG C-130 Depot Maintenance Procedure Cards (DMPC) in Attachment 2. The Contractor shall be responsible for the following functional areas:

PSI (and all de-painting and painting) of C-130J aircraft Depot Level repairs to a C-130J aircraft and system components Non-Routine Repairs Procurement, storage, stocking of inventory, control, accounting, issue, and shipping of supply parts and aeronautical equipment for a C-130J aircraft Preservation, storage, and maintenance of replacement aircraft parts Tracking and reporting the supply status on all parts associated with the PSI Aircraft sheet metal shop support and machine shop support

Maintenance on C130J AE 2100D engines and R391 propellers Avionics Modernization Line Ground and Flight Support of aircraft, to include repair of flight and non-flight generated discrepancies, hourly and calendar Maintenance Due List (MDL) items, aircraft fueling, de-fueling, and fireguard duties to launch aircraft

UDLM including Time Compliance Technical Order (TCTO) implementation as well as depot level structural repair and/or replacement of parts.

Ground and Flight Support of UDLM aircraft transferred to the contractor, to include repair of flight and non-flight generated discrepancies, hourly and calendar Maintenance Due List (MDL) items, aircraft fueling, de-fueling, and fireguard duties to launch aircraft

This contract is Firm Fixed-Price (FFP) with line items for completing specific milestones in the planned PSI schedule. In addition to the FFP there is a fully burdened labor hour cost Contract Line Item Number (CLIN) for items that may need to be completed, but are not currently identified in the basic scope of work for this contract; this will specifically be used for pricing unexpected work and UDLM in this basic Statement of Work (SOW).

In order to help ensure timely delivery of Contractor Furnished Material (CFM)/parts, the ALC will fund three (3) Contract Line Item Numbers (CLIN) for Materials (CLINs 0006, 1006, and 2006) for the aircraft in PSI. The Contracting Officer Representative (COR)’s approval is required before acquiring CFM/parts from the approved sources of supply and/or manufacturers from Aviation Maintenance Management Information System (AMMIS). If the Contractor desires to purchase a part from a non-AMMIS approved manufacturer or if the part is not loaded in AMMIS, the Contractor must initiate a Supply Item Change Record (SICR) in accordance with ALC Instruction, 5213.1(series) SICR Preparation and Routing Procedures.

The first PSI aircraft is to be inducted by the Contractor approximately 60 - 90 days after award.

The Government will provide the date on which the aircraft can be inducted at the time of the post-award meeting.

The Aircraft may be inducted earlier if both parties agree. The final delivery requirement for this effort is an aircraft that has undergone a complete depot maintenance and PSI process and has been fully tested. The Contractor shall complete the PSI within 220 calendar days from date of induction.

For aircraft undergoing PSI, the aircraft induction date is defined as the first full calendar day the aircraft is at the contractor facility for Induction. Flow days for PSI start accruing upon induction. Final delivery is defined as completion of paint and acceptance of the aircraft documented in a Form DD250 signed by the COR.

The Contractor may request additional days in accordance with FAR 52.212-4(f) if the Contractor believes that delays were Government caused, or are otherwise excusable delays. Any extension will be decided by the Contracting Officer and implemented via issuance of a contract modification. The issue will be handled through the disputes clause if there is a disagreement.

The USCG is the Airworthiness Authority for all actions performed under this contract.

1.4 APPLICABLE DOCUMENTS

See Attachment 1, for the Milestone Averages.

See Attachment 2, DMPC, for all applicable documents.

See Attachment 3, Government Furnished Material (GFM)

1.4.1 Reference Documents

See Attachments for all Reference Documents.

1.5 DEFINITIONS

The following definitions are necessary to describe the verbiage used throughout this document:

Non-Routine– Work within scope of estimated hours.

Unexpected Work – abnormal repairs that are outside of the scope of work, i.e. Major Structural Fittings.

2.0 SPECIFIC REQUIREMENTS/TASKS

2.1 GENERAL REQUIREMENTS

This contract is primarily a FFP contract with efforts such as de-paint, PSI milestones, aircraft weight and balance, and aircraft paint defined by FFP CLINs. The USCG schedule for PSI is every 48 months for USCG aircraft. This schedule may vary dependent upon aircraft availability and other factors related to mission readiness. The required timeline to complete the PSI shall be 220 calendar days from date aircraft induction. The Government may determine additional inspections are required in conjunction with PSI and will, if necessary, fund the additional costs and extend delivery time by issuance of a contract modification.

The Contractor shall purchase all consumable parts required for completion of each PSI evolution or other DLM. Any parts not listed in Attachment 3- GFM shall be purchased by the Contractor (subject to approval of the COR) and reimbursed by the Government at actual cost with no markup for overhead or profit.

Work generated by areas in the specification that direct the Contractor to proceed with correction of defects shall be performed as part of the inspection effort when the corrective action is merely cleaning or material removal within the limits specified by the applicable technical order. This effort includes corrosion removal within limits. All repairs shall be tracked in a manner approved by the Government.

Aircraft deficiencies noted on the Aircraft Condition Report (CG-103) that are not covered by the PSI shall be considered non-routine repairs.

2.1.1 Inspection and Acceptance

Inspection shall be performed by USCG Quality Assurance (QA) personnel and acceptance of the aircraft under this contract shall be by the COR, unless otherwise authorized by the Contracting Officer. Inspection and acceptance shall be performed by USCG ALC Elizabeth

City, NC, through its on-site representatives. The Contractor shall only tender for acceptance those items that conform to the requirements of the SOW/contract. The Government will inspect or test any supplies or services that have been tendered for acceptance in accordance with applicable publications. The Government may require repair or replacement of nonconforming supplies or re-performance of nonconforming services at no increase in price. If repair/replacement or re-performance will not correct the defects or is not possible, the Government may seek an equitable price reduction or adequate consideration for acceptance of nonconforming supplies or services. The Government must exercise its post-acceptance rights IAW FAR 52.212-4(a).

a) Within a reasonable time after the defect was discovered or should have been discovered; and

b) Before any substantial change occurs in the condition of the item, unless the change is due to the defect in the item.

2.1.2 Transport of Aircraft

The USCG shall be responsible for providing aircrews to conduct ferry flights to and from the contractor facility or other locations as required. Travel expenses for USCG provided aircrews will be the responsibility of the USCG. Flight hour charges for flights and travel expenses for USCG provided aircrews other than to/from a contractor facility (ex: re-work, warranty work) shall be negotiated on a case-by-case basis.

2.1.2.1 Fuel

The contractor should request a Government credit card to facilitate purchase of fuel for ground runs and flight activity. All fuel purchased with the Government credit card shall be used for engine runs and flight testing. Any additional fuel required for rework will be at no cost to the Government.

2.1.3 Material Inspection and Receiving Report

At the time of delivery of the aircraft, the Contractor shall prepare and furnish to the Government a properly completed DD Form 250 (DD 250), Material Inspection and Receiving Report. The original DD 250 shall be forwarded to the COR for acceptance. One copy of the DD 250 shall be attached to the original invoice when submitted to the payment office. Upon successful completion of the acceptance flight with no discrepancies, the USCG aircrew will communicate to the USCG COR that acceptance can occur. The COR is responsible for DD 250 signature.

Acceptance on the DD 250 will occur after the USCG flight crew departs for return to USCG destination.

In the event discrepancies are discovered during the acceptance flight (Section 2.2.11), the aircrew will return to the contractor’s facility for repair. Defects determined to be as a direct result of work accomplished by the Contractor, shall be resolved at no additional cost to the Government.

In the event a discrepancy is found at the operational unit as a result of work completed by the Contractor it will be the Government’s decision whether or not to complete repairs with a Contractor Field Team (CFT) or to bring aircraft to the contractor’s facility for resolution.

2.1.4 Government Furnished Property (GFP)

The Government reserves the right to supply any Ground Support Equipment (GSE), test equipment, parts or any other item required for PSI if it is deemed in the best interest of the Government. The Contractor may be entitled to an adjustment to the delivery schedule if availability of GFP results in a negative impact to the schedule. Any and all delivery schedule adjustments shall be made at the Government’s discretion and executed via a modification to the contract.

All Government property in the possession of the Contractor will be managed in accordance with FAR Part 45 and in accordance with FAR clause 52.245-1, Government Property (Jan 2017).

The Contractor shall be proper custodians of all assigned Government property through proper receipt, usage for the intended purpose, appropriate maintenance and repair, and disposition. All GFP is subject to inventory audits, and shall be returned to the Government upon completion of the project and/or contract. All property assigned to the Contractor for the sole purpose of performing the contract will be inventoried prior to commencement of contract performance.

The Government does not intend to provide any tools to complete the PSI. The Contractor shall notify the Government should special tools for the performance of this contract be required to be furnished by the Government. Should the Government provide special tools to the Contractor for the performance of this contract, they shall be controlled in the manner prescribed by ALCINST 13600.1(series), Aviation Tool Control Program. The current version, ALCINST 13600.1K, shall be provided to the Contractor prior to 01 July 2020. GFP shall be used for only USCG-assigned tasks. The Contractor shall be responsible for routine daily maintenance of the equipment/tooling loaned by the Government.

The Contractor shall report inadequacies or defective GFP by close of business the day the inadequacy or defective GFP is identified. The Contractor will not purchase or otherwise furnish any GFP for which Government reimbursement is to be made.

The Contractor shall notify the COR upon loss, destruction of, or damage to, Government property provided under this contract by close of business the day the discrepancy is identified.

The Contractor shall take all reasonable action to protect Government property from further damage by separating the damaged and undamaged Government property, putting all the affected Government property in the best possible order, and furnishing to the Contracting Officer and /or on-site COR a statement identifying:

a. The lost, destroyed, or damaged Government property;

b. The time and origin of the loss, destruction, or damage;

c. All known items in commingled (mingle, blend) property of which the Government property is a part; and

d. The insurance if any, covering any part of such commingled property.

The Contractor is responsible for preventing malicious acts or damages to USCG assets by Contractor employees.

Note: A list of peculiar support equipment will be provided up on written request.

2.1.5 Warranty

The Contractor warrants workmanship, including paint, for a minimum of twelve (12) months, from the date of final acceptance.

Further, Contractor warrants that all Contractor provided supplies and services furnished under this contract will be free from defects in material and workmanship and will conform to all requirements of this contract. With respect to Government Furnished Material (GFM) or GFP, the Contractor’s warranty shall extend only to its proper installation, unless the Contractor performs some modification or other work on the GFM or GFP, in which case the Contractor’s warranty shall extend to the modification or other work.

Warranties provided by a supplier to the Contractor for installation as CFM components in excess of this twelve (12) month warranty shall transfer to the USCG upon installation onto the aircraft and the remainder of such warranty shall endure to the benefit of the USCG.

If a defect is discovered during the warranty period, the USCG shall provide prompt notification to the Contractor via e-mail, specifying the nature of the defect in sufficient detail as the Contractor reasonably requests.

Upon receipt of such written warranty claim notice, Contractor at its option and with the assistance of the USCG if so requested shall perform a failure verification at the USCG’s location, or request the USCG to ship the item to Seller in order to ascertain and further confirm the nature of the purported defect. Shipping costs shall be at the Contractor’s expense. Contractor authorization in writing must be obtained for shipment coordination prior to the return of defective items. Contractor’s written authorization shall include packing, packaging, and shipping instructions to the repair facility designated by Seller.

Verification of warranty claim will be determined by contractor and government. After verification of the validity of the warranty claim, the Contractor shall at its discretion, and at its cost/expense, either repair or replace the defective item, provided that such repaired or replaced parts shall meet the original specification as to form, fit, function and cosmetic appearance.

Any repaired or replaced item shall enjoy the remaining, unexpired warranty period of the original item.

Warranty Exclusions: This warranty shall not apply and Contractor shall have no warranty obligation where the defect or failure is attributable to:

a. Normal wear and tear, or to parts and components of the deliverable items which are normally short-lived or not procured from Seller or to components which fail at or beyond their specified operating or shelf life;

b. Shipment, mishandling, installation, testing, or other act attributable to the USCG;

c. reasons which are beyond the control of, and without the fault of or negligence of the

Contractor, including but not limited to combat damage, fire, flood, crash, acts of God, explosion, misuse, or failures induced through interaction with Customer Owned and/or Customer Furnished Equipment (CFE) or other tactical or non-tactical equipment;

d. Cosmetic changes to surfaces including painted, stenciled and silk screened surfaces; or

e. Failure by USCG or any third party on USCG’s behalf to perform any routine or preventative maintenance as prescribed in the technical manuals.

No warranty is given with respect to those parts and components of equipment which are consumable or routine maintenance items.

Contractor warrants that the professional and technical services provided under the contract shall be performed by competent personnel with pertinent experience in the field of effort and shall be performed with that degree of care and diligence generally accepted in the international aerospace manufacturing industry in effect at the time of performance.

If a non-conformity is discovered within twelve (12) months after performance, then after providing prompt written notice within thirty (30) days after discovery, Contractor shall at its cost and expense re-perform such non-conforming services.

No other warranties/remedies shall apply.

The warranty remedies provided in the Contract shall be the USCG’s sole and exclusive remedies for breach of warranty and shall constitute Contractor’s sole liability with respect to breach of the warranty(ies) specified hereinabove.

The only warranties made by Contractor are those expressly enumerated in this Article. Any other statements of fact or descriptions or representations expressed in this Contract or any appendices or attachments hereto shall not deemed to constitute a warranty of the work or any part thereof. The warranties provided in the contract are the entire, sole and exclusive warranties made by seller and accepted by buyer in lieu of and to the exclusion of any other warranties, express, implied, statutory, or otherwise (including but not limited to implied warranties of merchantability and/or of fitness for a particular purpose, and all warranties arising from course of dealing and usage of trade).

Flight hour charges for flights and travel expenses for USCG provided aircrews to facilitate verified warranty work to/from contractor’s facility (ex: re-work, warranty work) shall be at the contractor’s expense.

Upon completion of warranty work, the Contractor shall prepare and furnish to the Government a properly completed DD 250 in accordance with SOW 2.1.3. The warranty period for any work performed under warranty shall be extended for twelve (12) months following the date on the

DD 250.

2.1.6 Quality Program

The Contractor shall possess and maintain an ISO AS 9110 certification for the life of the contract. Subcontractors shall comply with the Prime Contractor’s quality requirement but are not required to possess and maintain a separate certification. The Contractor shall also possess and maintain a Quality Control Plan; a current copy of which shall be available for review by USCG ALC in Elizabeth City, NC.

2.1.7 Ground and Flight Risk

Contractors shall base their procedures for conducting all aircraft flight and ground operations on Contract Service Guidance. Contract Service Guidance includes regulations, instructions, flight manuals, and technical publications as specified in the contract in effect on the date of contract award. USCG aircraft contracts Service Guidance includes, but are not limited to the following:

Coast Guard Air Operations Manual, COMDTIMST M3710.1 (series), and Aeronautical Engineering Maintenance Management Manual, COMDTINST

M13020.1(series).

Ground and Flight Operations Service Guidance COMDINST M13020.3 (series).This guidance will be provided upon written request.

A comprehensive list of applicable regulations, instructions, flight manuals, and technical publications which will be provided upon written request.

All Contractors and Subcontractors performing work on Government aircraft shall be subject to the Ground and Flight Risk Clause incorporated as an addendum to FAR 52.212-4.

The Contractor is responsible for all contract requirements subcontracted or delegated to other sources. The prime Contractor has the responsibility for ensuring that the subcontractor has procedures in place to implement the requirements of the Service Guidance. A prime Contractor is not relieved from liability for damage, loss, or destruction of aircraft while contract aircraft is in the possession or control of its subcontractors, except to the extent that the subcontract provides for relief from each liability.

2.1.8 Location of Government Flight Representative (GFR)

The GFR will be located at ALC. The Contractor will be notified in the event the POC information changes.

ALC Safety Officer Safety and Environmental Health Office, HMF1 252-334-5478 Mark.C.Haines@uscg.mil

2.1.9 Contracting Officer’s Authority

No oral or written statement of any person other than the Contracting Officer will in any manner or degree modify or otherwise affect the terms of this contract. The Contracting Officer is the only person authorized to approve changes in any of the requirements under this contract; and, notwithstanding any provisions contained elsewhere in this contract, said authority remains solely with the Contracting Officer. In the event the Contractor effects any such change at the direction of any person other than the Contracting Officer, the change will be considered to have been made without authority and no adjustment will be made in the contract price to cover any increase in cost incurred as a result thereof.

2.1.10 Contracting Officer’s Representative (COR)

The COR will be the primary conduit between the USCG and the Contractor.

a. The Contracting Officer hereby designates the following individual as the primary Contracting Officer’s Representative (COR) for this contract.

Mr. Todd Gerick USCG, ALC, Elizabeth City, NC Todd.M.Gerick@uscg.mil 252-335-6462

b. Technical surveillance will be performed by Technical Monitors who will serve to assist the COR in monitoring Contractor compliance with the SOW and ALC Policy applicable to the Contractor in performance of the contract. The Technical Monitors will be will be assigned at the time of Contract Award. The Technical Monitors will provide onsite surveillance IAW the DMPC and QA requirements. The Contractor shall contact the COR directly with any issues related to the Technical Monitors.

c. The COR will act as the Contracting Officer’s representative for technical matters (only), providing technical direction and discussion as necessary with respect to the SOW, monitoring the progress and quality of the Contractor performance. The COR is not a Contracting Officer and does not have authority to take any action, either directly or indirectly, that would change pricing, quantity, quality, place of performance, delivery schedule, personal services, or any other terms and conditions of the contract, or to direct the accomplishment of effort which goes beyond the scope of the statement of work in the contract. This also applies to the alternate COR and Technical Monitors.

d. It is emphasized that only a Contracting Officer has the authority to modify the terms of the contract; therefore, in no event will any understanding, agreement, modification, change order, or other matter deviating from the terms of the basic contract between the Contractor and any other person be effective or binding on the Government. When/if, in the opinion of the Contractor, an effort outside the existing scope of the contract is requested, the Contractor shall promptly notify the Contracting Officer in writing. No action shall be taken by the Contractor (under such direction) unless the Contracting Officer has issued a contractual change or otherwise resolved the issue.

2.1.11 Shipping Destination

All shipments to ALC for the LRS program shall be labeled with the following address:

Commanding Officer, USCG, ALC 1664 Weeksville Rd.

Bldg 63, Receiving Elizabeth City, NC 27909-5001

2.2 PSI PHASE REQUIREMENTS

The USCG expects the contractor to be in multiple phases simultaneously during a majority of the PSI; the below phases and days associated provided will be the general terms used when reporting progress of the aircraft.

2.2.1 Induction-Phase 1:

Induction is defined as the first full calendar day the aircraft is at the contractor facility. Flow days for PSI start accruing upon induction. The Contractor shall receive, inspect, process, store, preserve and provide inventory control of all material removed from the aircraft, including aircrew survival equipment left with the aircraft. The Contractor shall make all required logbook entries in accordance with applicable service directives and deliver the logbooks with the aircraft.

Phase 1 is completed when all induction Depot Maintenance Procedure Cards (DMPC) are at least 80% complete and work has commenced on the next phase.

2.2.2 De-paint-Phase 2:

The second phase of the PSI will be the de-painting of the aircraft which shall be completed by the Contractor at the Contractor’s facility.

This phase will include de-paint, disposal of de-paint waste, and all other aspects associated with de-painting. The Contractor shall de-paint the aircraft in accordance with the AFTO 1-1-8. The Contractor is responsible for following all current state, federal and Occupational Safety and Health Administration (OSHA) requirements. This requirement flows down to all subcontractors.

Phase 2 is completed when the aircraft is de-painted.

2.2.3 Disassembly-Phase 3:

Phase 3 involves aircraft teardown, including the removal of flight controls, avionics, wing fuel panels, engines and landing gear, and could involve large components (such as wings, vertical and horizontal stabilizers) of the external fuselage in accordance with the appropriate USCG depot maintenance guidance.

Phase 3 is completed when all DMPC cards in disassembly are at least 80% complete and work has commenced on the next phase.

2.2.4 Inspection- Phase 4:

During Phase 4 all applicable aircraft inspection DMPC cards and any additional CG103 entries shall be completed in accordance with the appropriate USCG and any additional CG103 entries and any additional CG103 entries specification documentation. The Contractor shall capture as many discrepancies as possible in the report. If several discrepancies are all related to one particular area of the aircraft, the founding may be reported to the COR as they are found (prior to the 60 day report). The Government will then make a determination and provide disposition for each repair within seven (7) calendar days. The primary deliverable of the inspection effort is the final report of all discrepancies noted on the 60-day PSI Inspection Report.

Phase 4 is completed when all DMPC cards in Inspection and any additional CG103 entries are complete.

2.2.4.1 Non-Destructive Inspections (NDI)

The contractor will provide certified NDI inspectors to perform all level two (2) and level three

(3) NDI inspections. Contractors shall perform detailed visual inspections IAW 1C-130J-36, DMPC, MPC, and TCTOs.

2.2.5 Repairs, Rework, Replace-Phase 5:

Phase 5 work encompasses repairs, rework, and replacement of components. These repairs will be considered non-routine and will be generated from the inspections completed in the Inspection phase. Non-routine repairs are included in the fixed-price CLIN three (3) for Phase 5.

The estimated hours for these repairs is 15,116 which is the average hours of repairs on the last five (5) C-130J aircraft through PSI. The Government does not predict any significant change in hours of repairs required for this PSI requirement. The funding for this phase does not include any major structural repairs such as rainbow and corner fittings, center wing replacement, and replacement of any major structural elements; this pricing will be negotiated at determination of the need for replacement. Work determined by the COR to be unnecessary shall be documented on the Contractor generated Noted but Not Corrected Report (NBNC). Only work authorized by the COR or specifically identified in the PSI DMPCs as being mandatory shall be accomplished during the repair phase effort.

Any damaged airframe structure shall be repaired and/or replaced. Labor-hours to be included in repair or replacement are those required to disassemble, remove damaged material/structure, prepare replacement material and parts for installation, prepare damaged area for installation of new or repair material and/or parts, and reassemble. Airframe structure damaged after induction into PSI due to Contractor negligence or error shall be repaired and/or replaced at no cost to the Government. The Contractor shall notify the COR within 24 hours when damage occurs. The Contractor is solely responsible for the acquisition of materials required for maintenance under this contract for C-130 aircraft with the exception of the components listed in Attachment 3.

Phase 5 shall be considered complete when 80% of the non-routine hours have been expended.

2.2.5.1 Technical Support

The C-130 aircraft inducted into the PSI inspection cycle often require major structural repairs or modifications that are not specifically addressed in the structural repair manuals. In order to ensure aircraft structural integrity is consistently maintained, the Technical Request Form (TRF) process will be used to document and design structural repairs. The Contractor will be provided with the LRS PLD TRF Instruction, for compliance. In no event shall the Contractor implement TRFs, processes or procedures that affect C-130J aircraft configuration (form, fit, or function) without Government approval. Any waivers/deviations from the specifics of the PSI basic specification and/or the technical orders shall be referred to the COR for Contracting Officer approval prior to beginning any work or repair.

The Contractor shall provide technical support that is inclusive of the following: determination of serviceability, installed structure compliance to drawings, and determination of flight critical/continued service for previously installed repairs.

The Contractor may also be called upon to assist with discrepancy evaluations, incorporate changes (e.g., Time Compliance Technical Orders (TCTOs), Special Compliance Technical Orders (SCTOs), Service Bulletins (SB)’s), and other services as deemed necessary.

All completed and signed-off DMPCs shall be retained via hard and soft copy and provided to the Government upon completion of the contract.

2.2.5.2 Aircraft Sheet Metal Repair/Overhaul Support

The Contractor shall make repairs and complete overhauls to flight controls and aircraft skin.

The Contractor shall perform C-130J enhanced cargo handling system inspections and repairs, C-130J flight control repairs and overhauls to include elevators, elevator trim tab, aileron, aileron trim tab, rudder, rudder trim tab and C-130J flap assemblies, wing leading edges, and landing gear door modifications and repairs.

2.2.5.3 Aircraft Component Repairs and Fabrication Support

When delivery of a component not listed in Attachment 3 is anticipated to adversely affect the aircraft production or delivery schedule, and where the capability exists, the Contractor shall request authority to repair, manufacture or request assistance in obtaining the component from the COR.

2.2.5.4 Depot maintenance for AE 2100D3 Engines and R391 Propellers The Contractor shall remove the AE 2100D3 engines and propellers from the C-130J aircraft and safely preserve and store the engines and propellers in an environmentally controlled area. The Contractor shall perform AE 2100D3 engine Quick Engine Change (QEC) inspections, routine maintenance, and component replacements. The AE 2100D3 engines are operated under a Power by the Hour (PBH) contract and all parts for the engines come directly from Rolls Royce. The Contractor shall notify the COR if GFM is required from the list of components covered by the Engine PBH contract which will be provided upon written request. The Contractor shall re-install and perform required operational checks. Additionally, the Contractor shall perform standard propeller maintenance, and remove and replace if necessary.

2.2.5.5 Avionics Modernization

The USCG will require the installation of several avionics components onboard the C-130J aircraft. Some of these upgrades are directly related to the 2020 Communications, Navigation and Surveillance/Air Traffic Management (CNS/ATM) system requirements. The Contractor shall provide avionics modification support for the USCG C-130J upon request, IAW a CG TCTO or OEM Technical Data Package. Pricing will be requested at the time the modification support is required.

2.2.5.6 Plating and Heat Treating

Cadmium plating, anodizing, and ion vapor deposition shall be accomplished in accordance with TO 1C-130J-23 and specification listed there in. Heat treat of steel and aluminum alloys shall be accomplished in accordance with TO 1-1A-9, TO 1C-130J-3 and or equivalent specification.

2.2.5.7 – Block 8.1 Upgrade Block 8.1 upgrade shall be completed in accordance with the following TCTO Numbers:

TCTO Estimated Hours

SCTO 1C-130J-I-4572 150

SCTO 1C-130J-I-4573 242

SCTO 1C-130J-I-4574 310

SCTO 1C-130J-I-4575 1832

SCTO 1C-130J-I-4576 5.5

SCTO 1C-130J-I-4577 3.5

2.2.6 Assembly-Phase 6:

In conjunction with the repair phase, the aircraft shall be re-assembled as repairs are completed in accordance with the appropriate USCG specification documentation. Specific areas of the aircraft will require paint prior to re-installation/re-assembly of components IAW applicable DMPCs.

Phase 6 shall be considered complete when a majority of assembly DMPCs are complete and the aircraft is off jacks and is mobile.

2.2.7 Operations Checks (Prior to Engine and Auxiliary Power Unit (APU) Runs)-Phase 7:

Once the aircraft is assembled, the Contractor shall complete a series of systematic tests of all aircraft systems, designed to ensure the aircraft is airworthy and safe to return to flight in accordance with appropriate USCG specification documentation prior to running Aircraft APU and Engines. During this phase, the Contractor should request a Government credit card to facilitate purchase of fuel for ground runs and flight activity. All fuel shall only be used for engine runs and flight testing. All fuel after this phase that is defueled from the aircraft will be credited back to the Government. Any additional fuel required for rework will be at no cost to the Government.

Phase 7 is complete when the aircraft is maintenance released for ground runs.

2.2.8 Ground Runs-Phase 8:

Operations Checks Ground Runs shall be completed by the Contractor’s personnel qualified in accordance with appropriate USCG specification documentation. At the completion of Operations Checks the Contractor shall enter all ground generated discrepancies in Aviation Logistics Management Information System (ALMIS).

All ground checks and operational checks, pre-flight and weekly inspections, and all work necessary to ensure aircraft integrity and reliability for flight shall be accomplished. This includes as many pre-flights and weekly inspections as are required to make the aircraft ready for acceptance. Prior to Functional Check Flight (FCF), USCG QA will spend the equivalent of one (1)work shift to do a complete aircraft QA inspection IAW DMPC 052000.D. Prior to the FCF the Contractor Supervisor shall conduct a QA brief with the test flight crew covering all the disassembly, reassembly and repairs during the PSI. The Contractor shall provide a letter stating they have completed a final check of the aircraft; the USCG QA inspection IAW DMPC 052000.D is complete, and aircraft is maintenance released for a FCF. Copies of this letter shall be given to the FCF pilots and COR at the QA brief.

Phase 8 is complete when the A/C is cleared for Flight Test Phase.

2.2.9 Aircraft Weight and Balance Requirements

Aircraft Weight and Balance (W&B) shall be performed by the Contractor at the completion of reassembly and prior to FCF IAW USCG specifications. W&B shall also be performed after completion of Final Paint, prior to USCG Acceptance. W&B for all aircraft shall be performed by the Contractor (or its subcontractor) IAW USCG specifications. The USCG Aircraft Weight and Balance System (AWBS) contains all pre-PSI W&B data. The Contractor is responsible for weighing aircraft and completion of W&B data.

2.2.10 Flight Test-Phase 9:

After the ground and operational checks are completed, the aircraft shall satisfactorily complete a full FCF IAW the appropriate USCG Technical Order (CGTO) to ensure the aircraft is ready for paint and acceptance with no record of flight discrepancies in the areas or systems included in the scope of work. Any discrepancies found during the FCF shall be corrected by the Contractor.

If a discrepancy is attributable to the Contractor’s workmanship, correction shall be made at the Contractor’s expense.

Phase 9 is considered complete when aircraft completes FCF with no discrepancies attributable to the PSI effort.

2.2.11 Paint and USCG Acceptance-Phase 10:

After all flight operation checks are finished, the Contractor shall complete the final application of primers, paint, and decals to the exterior aircraft surfaces in preparation for return of the aircraft to operational service. This Phase will include all aspects associated with painting. The Contractor shall be responsible for procuring paint, stencils and decals as called out in the paint drawings, which will be provided upon written request. The Contractor shall paint the aircraft in accordance with CGTOs, current USCG drawings, AFTOs and NAVAIR publications or other applicable publications. The Contractor is responsible for following all current state, federal and OSHA requirements. Applicable paint drawings for each aircraft must be requested from the ALC 30 days in advance of paint. The painting facility shall have climate control capability and the ability to control the relative humidity to ensure proper paint and primer adhesion.

This effort will be performed at the Contractor’s paint facility. Once the painting is completed, the Contractor shall accomplish aircraft final weighing evolution IAW USCG specifications.

Acceptance of the aircraft by the USCG will occur after the QA check for paint is completed, aircraft condition is communicated to the COR at ALC, and the aircraft is airborne from the Contractor’s facility for at least thirty (30) minutes. Acceptance will be by issuance of a Contactor prepared Form DD 250 signed by the COR.

2.2.12 Delivery Timeline

The Contractor shall complete all aspects of this SOW for each PSI aircraft within 220 calendar days from date of induction regardless of the amount of repairs or other work covered in this SOW unless Government delays are validated and documented by the Government. The induction date will be considered the first full day the aircraft is at the Contractor’s facility for induction and end upon USCG acceptance.

The aircraft shall be inducted by the Contractor within 60 to 90 days after award. Aircraft may be inducted earlier if both parties agree. The 60 to 90 days will provide ample time for the Contractor to obtain the required Applicable Documents, GFE, complete initial pre-inspection, and lay-in of parts. The Contractor may request a performance schedule adjustment if delays are Government caused, or are otherwise excusable delays. A performance schedule adjustment will also be made in the instance that a new TCTO is required as a result of the Government caused, or otherwise excusable delays.

2.2.13 Special Requirements

All deviations from technical and engineering data must be approved by USCG Engineering via the COR in accordance with USCG instructions. The USCG retains final Engineering Approval Authority for all repairs.

The Contractor shall document all removal/replacement of serial number tracked components in the Asset Computerized Maintenance System (ACMS), in accordance with Aeronautical Engineering Maintenance Management Process Guide, CGTO PG-85–00–110. The aircraft configuration report shall be reviewed by the COR for accuracy prior to FCF.

The Contractor shall ensure reinstallation of all door panels, fairings, fillets, parts, components and assemblies removed during the course of this contract, that have not been specifically called out.

All removed and repaired structural members of skin shall be installed/replaced/reinstalled with all fasteners and faying surfaces wet with MIL-S-81733 sealant IAW applicable TO 1C-130A-3 or 1C-130J-3.

The Contractor shall accomplish pressurization checks. The Ground and FCF flight crew shall test pressurization on ground and at altitude in accordance with 1C-130J-6CF as applicable. The Contractor shall correct leaks as necessary to obtain the required pressurization.

The Contractor shall ensure that maintenance records, forms, and publications applicable to each aircraft are updated to reflect maintenance accomplished and current status of aircraft in accordance with guidance in this SOW.

2.2.14 Unscheduled Depot Level Maintenance (UDLM)

The Contractor is advised that UDLM or “Drop In” work may be required on short notice. Such efforts could include TCTOs, installation of aircraft modifications/new equipment, extension inspections, and drop-in heavy maintenance. The type and quantity of aircraft will be determined as requirements are generated. When a UDLM is identified by the Government, a specific amount of hours will be negotiated and a detailed timeline for completion of work will be established. The Contractor will be provided a UDLM Work Specification and requested to submit a work request proposal. The Contractor’s proposal shall be submitted to the COR, and include the estimated number of labor hours required to accomplish the necessary tasks, delivery input, and completion date. All work shall be performed according to the UDLM specification provided at the hourly labor rates specified in the contract Schedule of Supplies/Services.

Work request proposals shall include: all preparation, inspection, removal and replacement of items to gain access to the job being performed, testing, functional or operational checks, de-sealing, de-painting, finishing, painting, resealing, cleaning, drilling, fitting, de-burring, trimming, sanding, rigging, lubrication, installation, reassembly, or any and all activities of similar nature required to perform the specific work identified. This includes all general ground servicing and aircraft flight support, repair of flight and non-flight generated discrepancies, hourly and calendar Maintenance Due List (MDL) items.

Aircraft delivery and associated work requests will occur after issuance of a funded task order.

The Contractor shall provide all services, indirect materials, and all technical support necessary to accomplish a complete job in accordance with the Government UDLM specification or work request and applicable technical orders. The Contractor shall be responsible for initiating a written request to the Contracting Officer for authorization to proceed with any work necessary, but not defined in the UDLM work specification, as soon as the need for such work becomes known.

Flight operations support (i.e. preflight, servicing, line maintenance, etc) are considered UDLM tasks under this contract.

2.3 PARTS SUPPORT

The Contractor is solely responsible for the acquisition of the components required for maintenance under this contract for C-130J aircraft with the exception of the components listed in Attachment 3. The Contractor will be provided access to AMMIS in order to view approved sources of supply and/or manufacturers for various components. The COR will assist the Contractor with obtaining access to Defense Logistics Agency (DLA) ordering applications as a resource for procuring materials for use in performance of this contract.

When late delivery of a CFM component may adversely affect the aircraft production or delivery schedule, and where the capability exists, the Contractor shall request authority to repair/overhaul the component, or request assistance in obtaining the component from the Government within ten (10) business days of determining the late delivery of the CFM component may affect the aircraft production or delivery schedule. Failing to notify the Government within ten (10) business days does not relieve the Contractor of performing the PSI by the required delivery date. Notification may be accomplished electronically and must include an identification of the item(s) needed, applicable part numbers, required date of delivery, a description of efforts made to secure the item(s), and proposed lead-times from other sources.

Any extension of the delivery date requires endorsement from the COR and authorization from the Contracting Officer.

Upon completion of the contractual period, any remaining GFM and GFP assets (supplied but not used) shall be returned to the USCG in the same condition in which they were received. The Contractor shall return all GFM and GFP components back to USCG within 30 days of the end of the contractual period as instructed.

2.3.1 Government Furnished Material (GFM) (Attachment 3)

Requests for components listed in Attachment 3 shall be submitted to the USCG COR as soon as the need is known or anticipated. The request shall include the part number(s) required, and shall include a required date of delivery. Delays in receiving GFM/GFE do not automatically result in an adjustment to the delivery schedule of an aircraft. In no case shall an acceptable required date of delivery be less than 14 calendar days in the future from the request of any/all GFM. Exceptions to this rule will be handled on a case by case basis by the COR.

The Contractor shall acknowledge actual receipt of all GFM provided. If the Contractor requests GFM which is not listed in Attachment 3 and the request is approved by the COR, the cost to the Government of the supplied GFM will not be billed to the Government. Delivery of GFM is considered complete when GFM is received by the Contractor. All non-RFI GFM shall be turned in within seven (7) business days of receipt of the replacement RFI GFM.

The Government shall be reimbursed for the repair or replacement of GFM components damaged due to Contractor negligence or error.

The Contractor will be responsible for receipting and shipping of all GFM provided for by the Government in AMMIS. AMMIS access will be provided to the Contractor to fulfill this requirement. RFI material receipts in AMMIS must be done prior to manifesting and shipping the non-RFI assets back to ALC.

2.3.2 Parts Procurement

CFM costs shall be supported by documentation of a competitive pricing process (i.e. a commercial invoice). Any agreements with material suppliers must have documentation supporting price reasonableness for all direct materials purchased. The Contractor shall be reimbursed for actual cost of Contractor-furnished direct parts and materials, along with related shipping charges (excluding handling fees or royalties and less any rebates, refunds, or discounts received by the contractor that are identifiable to the contract). The USCG reserves the right to review any costs associated with this effort and may require documentation of a competitive pricing process to support any invoices submitted for direct material cost and may reject invoices deemed unreasonable. These procedures for reimbursement of direct material costs shall govern the process for the entire contractual period.

The LRS PL at the ALC will work with the Contractor’s supply department to ensure all ALC SICR processes are followed for acquiring CFM components. All support material (including personal protection equipment (PPE) and administrative supplies) shall be the responsibility of the Contractor at no additional cost to the Government.

All replacement part(s) used in the PSI must either be from an approved manufacturer, source of supply in AMMIS, or be approved by LRS Engineering in accordance with ALC policies. Only parts that have traceability to the approved manufacturer of those specific part(s) or alternate part(s) shall be used. Airworthiness Certificates (8130-3 or alternate) must be provided for all flight critical parts. Alternate parts must satisfy all form, fit, and function requirements of the original parts and conform to the approved configuration of the assembly. USCG C-130 Engineering approval must be received prior to utilization of an alternate manufacturer or supplier not recognized as authorized in AMMIS. USCG Engineering shall respond within five

(5) business days.

The Contractor shall cooperate in the event that an investigation is…

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