SOW Prop Assy Repair Updated 1.18.23.pdf

ATTACHMENT B

STATEMENT OF WORK (SOW)

OVERHAUL AND REPAIR OF THE 14RF-37 PROPELLER ASSEMBLY AND COMPONENTS

1.0 BACKGROUND

1.1 The United States Coast Guard (USCG) currently operates Eighteen (18) HC-144 Maritime Patrol Aircraft each powered by two CT7-9C3 turboprop engines which use the model 14RF-37 Propeller. The aircraft is manufactured by AIRBUS MILITARY (formerly EADS CASA) in Seville, Spain. While the base CASA CN-235-300M Maritime Patrol & Surveillance Aircraft (MPSA) aircraft provides the foundation for the Coast Guard HC- 144, changes to the base aircraft configuration and the addition of supplementary systems have been combined resulting in a CG01 version of the CN-235300M MPSA. The HC- 144 aircraft is programmed to fly 1000 hours annually.

1.2 The MPSA are operated differently from general aviation in support of USCG operations which consist of Search and Rescue, Surveillance, and Reconnaissance missions. USCG HC-144 missions require frequent operation at lower altitudes and in salt–laden environments. These environments contribute to an increase of corrosion on airframe structures, engines and components of the aircraft. The Aircraft and its components are inspected by USCG personnel in accordance with (IAW) the Original Equipment Manufacturers’ (OEM) periodic requirements and in conjunction with the USCG’s specialized Asset Computerized Maintenance System (ACMS).

1.3 The original manufacturer, design authority and technical data rights owner of the components listed in the solicitation schedule was Hamilton Sundstrand Corporation.

Following corporate mergers with United Technologies Corporation and most recently Collins Aerospace, design authority and ownership of component technical data transferred to Collins Aerospace. For the purpose of this SOW, the term OEM refers to the component technical authority and data rights originally established by Hamilton Sundstrand but currently owned and managed by Collins Aerospace.

2.0 SCOPE

2.1 The scope is intended to establish overhaul and repair services for the listed Hamilton Sundstrand manufactured parts (listed in the solicitation schedule). All are listed and are hereafter known as Hamilton Sundstrand components unless otherwise specified. This would include the complete teardown, inspection, rework, repair, assembly, and testing of all items identified in the Schedule IAW OEM specifications. This SOW establishes the minimum USCG requirements necessary for overhaul and repairs, and is not intended to be all inclusive, nor detract from the procedures outlined in the manufacturer’s drawings, manuals, specifications, public & private Action Items (AI) and Service Bulletins (SB).

USCG configuration control requires that applicable SBs and Modifications (MOD) for all ACMS tracked Hamilton Sundstrand components not previously configured, shall not be incorporated without prior written approval from the USCG Contracting Officer.

3.0 REQUIREMENTS

3.1 The contractor shall be a certified Federal Aviation Administration (FAA) Part 145 authorized overhaul and repair center or equivalent to effectively inspect, test, troubleshoot, clean, overhaul, repair and preserve the listed Hamilton Sundstrand components within this scope and requirements; IAW the most current Hamilton Sundstrand or other OEM Component Maintenance Manuals (CMM), Public & Private AIs, revisions (REV), Temporary REVs (TRs), and specifications, including SBs, Service Information Release (SIR), amendments (AMD), and MODs to include any specified or proposed USCG publication(s). Maintain all USCG specific requirements for return to service in a Ready For Issue (RFI) condition and USCG operational use. The Hamilton Sundstrand components shall be complete and configured for installation on USCG HC-144 aircraft.

3.2 The contractor shall be formally recognized as an OEM licensee repair facility. OEM licensee repair facility shall be used throughout this SOW. The contractor shall be authorized and capable of performing all requirements of an OEM licensee repair facility as referenced in the Hamilton Sundstrand CMM with the exception of the blade Taper Bore Repair and taper bore tip shotpeening referenced in the CMM REV NO. 14 Dated APR 20/07, Repair 5-30, Pages 609/610. The contractor shall have access and authorization to perform proprietary repairs developed by the OEM to include, Major Repairs, and repairs indicated in the CMM AI Log for both Public and Private/Restricted status.

3.3 The contractor shall maintain this OEM licensee status for the duration of the contract and shall immediately report any loss of licensee status to the Contracting Officer.

3.3.1 The contractor shall have a formal agreement for technical assistance from the OEM which provides access to design level technical data, repair drawings and engineering authority required to develop or co-write new repairs, AIs and/or justify repairs/actions beyond that listed in the CMM to maximize the serviceability and longevity of USCG components. The formal agreement from the OEM shall be supported via the licensee designation which authorizes the contractor to perform repairs or deviations to Design Critical Characteristics when warranted/directed by the OEM.

3.3.2 The contractor shall have on-site capability to perform cut and cold roll rework processing per engineering drawing SK122836.

3.3.3 The contractor shall evaluate and recommend the application of existing or development of new Private/Restricted AIs where appropriate to address USCG specific damage, corrosion, and reliability issues. At a minimum, the contractor shall perform private AI D1155-AI10819 to all USCG propeller hubs during all repairs and/or overhauls.

3.4 The contractor shall receive and comply with all OEM Flight Safety Audits to include scheduled and unscheduled intervals set by the OEM. Regardless of OEM mandated intervals, the contractor shall complete an annual safety audit at a minimum and provide the OEM audit report to USCG Contracting Officer.

3.5 The contractor shall paint all 14RF-37 Propeller blade tips White (Paint Part Number (P/N) 55W002) 5.75 to 6.25 inches from the blade tip with White paint that meets MIL- PRF-85285 standard and FED-STD-595 (17925). Blade tips shall be painted when repaired or overhauled.

3.6 The contractor shall provide new blade seals for all 14RF-37 Propeller blades regardless of repair or overhaul.

3.7 The contractor shall provide a 100% replacement of the Outer Bearing Race (782674-1) and Race Barrel Retainers (789263-1), Shim (820475-1) and Glide Ring (790098-4), Dowel Pin Composite Bushing Shim (815597-1) during Overhaul (Airworthiness Inspection) on all 14RF-37 Propeller Hubs (814721-2). The contractor shall ensure that all RFI Prop Hubs (repaired or overhauled) are returned with races and retainers with matching Flight hours regardless if the hub was configured with these components upon receipt by the contractor.

3.8 If any parts are missing to include but not limited to those listed in sections 3.6 & 3.7, the contractor shall provide traceability and documentation supporting the absence of the missing parts. USCG contracting shall initiate an investigation and reimbursement for any missing parts.

3.9 The USCG does not own, nor can it provide access to or copies of OEM publications.

3.10 The contractor shall be responsible for all necessary functions to perform the contracted services requested. This includes, but is not limited to, required tooling, manuals, test equipment, parts, material, engineering services, management, personnel, documentation, preservation, shipping, etc.

3.11 Designated Engineering Representative (DER) Repair Procedures

3.11.1 DER Repair procedures may be authorized on a case-by-case basis after review and approval by the USCG Engineering Officer.

3.11.2 The contractor shall submit a complete technical package to the USCG Contracting Officer showing the DER repair procedure on a FAA form 8110-3 which shall meet the original OEM operational requirements. This information shall be treated as Procurement Sensitive and shall not be released to parties outside of the Government.

3.12 The USCG anticipates at least two levels of service; “Repair” and “Overhaul”.

3.12.1 “Repair” - “Return to Service,” which is considered inspect, repair, and test as necessary. This work consists of inspection and analysis usually of a specific defective condition, repair of that condition, replacement of defective parts only as necessary, and testing to meet the OEM’s functional return to service requirements. A repair shall not zero the “Time Since Overhaul” (TSO), component time continues for repaired items. All parts sent to the contractor under the repair level of service shall be returned to the USCG within forty five (45) calendar days After Receipt of Material at the contractor’s facility. Parts shall be returned in RFI condition, and be shipped to the USCG’s Aviation Logistics Center (ALC) facility unless directed otherwise by the USCG contracting Officer by contract MOD.

3.12.2 “Overhaul” (Major Inspection) - “High Time,” having reached one of the OEM’s airworthiness limitations for any life cycle limits or having some other general condition (out-of-limit/out-of-tolerance) such as excessive wear and tear, damage, or corrosion, as deemed to require a major inspection or overhaul level of service.

An “Overhaul” shall be considered over and above the “Repair” scope; it shall include the complete teardown, inspection, rework, assembly, and testing of components, to OEM original or rebuilt specifications. An overhaul shall zero the TSO and effectively restart restoration intervals and OEM component life cycle limits as applicable. All parts sent to the contractor under the overhaul level of service shall be returned to the USCG within sixty (60) calendar days After Receipt of Material at the contractors facility. Parts shall be returned in RFI condition, and be shipped to the USCG’s ALC facility unless directed otherwise by the USCG contracting Officer by contract MOD.

3.13 The contractor shall track and document calendar time, flight time, flight/life cycles, for all work and services performed on the Hamilton Sundstrand components as required under USCG ACMS. See Section 6.0 for specific information.

3.14 If the contractor for any reason loses its FAA part 145 certification or licensee status during the period of performance, this constitutes a material breach of contract which may, at the discretion of the USCG Contracting Officer, result in contract termination.

The contractor shall notify the Contracting Officer verbally and in writing, not later than five (5) calendar days after certification or licensee forfeiture and disclose all facts relevant to the forfeiture.

3.15 The contractor shall ensure that all Public & Private AIs, SBs, AMDs and MODs that have previously been incorporated remain incorporated unless otherwise appropriately superseded or as directed by the USCG Contracting Officer.

3.16 The contractor shall identify and recommend, new or additional AIs, SBs, AMDs, or MODs, as applicable, to be incorporated and specify how the AIs, SBs, AMDs, or MODs may affect components, P/Ns, and pricing. The contractor shall contact the USCG Contracting Officer, in writing, via FAX or e-mail for approval to incorporate the changes.

3.17 The contractor must be subscribed to receive notifications to all applicable OEM Hamilton Sundstrand or other OEM Manual publications: Component Maintenance Manuals (CMM), AI Log, REVs, TRs, SBs, SIR, MODs, AMDs, including contractor specifications and procedures applicable, to be used for the inspection, repairs or overhaul of the listed USCG Hamilton Sundstrand components.

3.18 The contractor shall attach information regarding weight and applicable blade balance information for the associated blade P/N RFA12A1POC and Serial Number (S/N) on the outside of the shipping container which matches the repair and balance documentation on the airworthiness form 8130-3.

3.18.1 The contractor must preserve and package propeller components IAW SIR:

PROPS GEN: 140 or as directed by other publication(s) to include any specified or proposed USCG publication(s) to ensure a minimum of two year shelf life with no corrosion damage. The contractor shall apply a corrosion preventative compound (CPC) which is approved by the OEM via AI or other means, that exceeds the requirements listed in the SIR: PROPS GEN: 140. The approved CPC shall provide a two year preservation performance. Protective caps and covers shall be installed on the hub P/N 814721-2 blade bores, actuator bore and all hub bolt ends.

The preservation date shall be attached to the outside of the shipping container which matches the preservation date on the airworthiness form 8130-3.

3.19 The contractor shall provide a current Capabilities list, REF: FAA part 145.215 and indicate the percentage of each repair/overhaul element(s) listed in the CMM for blades, hubs and actuators which can be performed at the vendor’s facility (in-house) for the identified operation.

3.20 If the contractor receives information more current than that previously provided to the USCG, the contractor shall identify the Hamilton Sundstrand or other OEM Manuals, CMMs, AIs, REVs, and specifications, including SBs, SIR, AMDs, and MODs, and provide a brief synopsis of the REVs and dates to the USCG’s Contracting Officer for review and disposition approval. Refer to paragraphs 2.1, 3.15, 3.16 and 3.23 for the incorporation of SBs and MODs.

3.21 Environmental Requirements

3.21.1 All parts must be thoroughly cleaned IAW applicable CMMs to ensure they are as free as practicable of all hazardous dust to include hexavalent chromium, cadmium, lead, etc., prior to being returned to ALC. ALC may take random samples of parts to ensure they are as free as practicable of all hazards.

Information on these hazards can be found in Occupational Safety and Health Standards 1910.1025 (lead), 1910.1026 (Hexavalent Chromium) and

1910.1027 (Cadmium)

3.22 Provide written delivery order receipts within five (5) working days for all Hamilton Sundstrand components.

3.22.1 Delivery order receipts shall include, but are not limited to, the following information: nomenclature, National Stock Numbers (NSN), P/Ns, S/Ns, contract number, delivery order numbers, Contract Line Item Numbers (CLIN), and dates of receipt.

3.22.2 Delivery order receipts via facsimile/email are acceptable and may contain single or multiple notification entries.

3.23 The contractor shall maintain all existing SBs (Mandatory and Optional), public & private AIs and other MODs previously incorporated on USCG components unless otherwise directed by the USCG Contracting Officer.

3.23.1 SB and AI configurations are subject to change during the course of the contract period. SBs, AIs (both public & private), and MODs not previously incorporated shall be identified in writing to the USCG Contracting Officer.

3.23.2 Within thirty (30) calendar days of OEM publication, the contractor shall obtain and notify the USCG Contracting Officer of any new SB or AI for disposition approval prior to incorporation. USCG HC-144 Engineering Officer or designated representative shall approve all newly published SBs and/or AIs.

3.23.3 SBs and AIs incorporated during performance of this requirement may create new P/N configurations, which supersede the previous configurations. In cases where the older configurations cannot be modified to the newer configurations, the new configuration P/Ns may be added to the contract. The contractor shall notify and request disposition instructions from the USCG Contracting Officer for superseded parts, which have been removed and replaced by newer configurations.

3.23.4 Upon receipt of notification from the OEM that a SB, AI (public & private), or MOD is published, the contractor shall notify and submit, within ten (10) calendar days after receipt of that notification, a firm-fixed price proposal for the SB or AI (public & private) to be incorporated in the component to the USCG. The proposal shall contain a breakdown of material and labor costs including hours, labor categories, labor rates, and applicable mark ups. Upon completion of negotiations, a contract MOD will be issued to reflect the change, and the SB shall be incorporated into each subsequent component received at the contractor’s facility for which the SB has not already been incorporated. When SB or AI (public & private) incorporation changes the CLIN P/N, the new P/N shall be added to the contract. The same procedures apply if removal of SBs is required.

Failure to supply a change notice shall forfeit the right to any increase as a result of the contractor’s failure to request a price change. Unless the contractor has a signed contract MOD permitting a change and bearing the signature of a USCG Contracting Officer, funding has not been authorized. Performance without written authority from the USCG Contracting Officer will not be authorized for payment.

3.24 Prepare and submit, component Teardown Inspection Reports (TIR) 3.24.1 TIRs, are occasionally requested by the USCG Contracting Officer, and are usually requested in support of a USCG Engineering incident, safety investigation, warranty determination, or for other failure analysis.

3.24.2 Upon request, the contractor shall within ten (10) calendar days provide a copy of the TIR to the Contracting Officer. TIRs, when requested, shall be forwarded to the USCG Contracting Officer prior to commencement of repair or overhaul work.

3.24.3 TIRs shall include: nomenclature, NSNs, P/Ns, S/Ns, Contract number, Delivery Order numbers, CLINs, including descriptions, photos, illustrations, and drawings, as necessary before and during teardown, for documentation of the failure, and list all parts and costs as would be required for repair/overhaul of the component or assembly. The TIR shall also list all tolerances, and/or specification(s) which are out of limits to include CMM reference and the exact location on the component with the associated discrepancy measurements.

3.25 Replacement Parts:

3.25.1 The contractor is responsible for all replacement parts required for repairs/overhauls, including hightime, life, or cycle limited parts.

3.25.2 Per section 3.12 above, a component classified as “High Time” results in the classification of associated assembly parts as “High Time” to include but not limited to those listed in 3.7 above.

3.25.3 High time, life, or cycle limited assembly parts which have reached their respective limits IAW paragraph 3.25.2 above, shall not be repaired or overhauled, but shall be replaced with other USCG serviceable parts or replaced with new OEM parts. The non-conforming parts shall be labeled and returned to the USCG on a separate manifest.

3.25.4 Replacement parts shall be new and have full traceability to the OEM, Hamilton Sundstrand. See Paragraph 3.25.5 concerning PMA parts (Parts Manufacturer Approval).

3.25.5 PMA

3.25.5.1 PMA parts may be authorized on a case by case basis after review of technical documentation and approval by the USCG Engineering Officer.

3.25.5.2 The contractor shall submit a complete technical package to the USCG contracting officer showing that the PMA part meets or exceeds the original OEM specifications. This information will be treated as proprietary information; the USCG will not release this information to other sources outside of the Government.

3.25.6 Defective parts: The cost of repair or replacement of defective parts is inclusive to the component repair contract price. Defective parts which cannot otherwise be repaired IAW OEM specifications, shall be reported to the Item Manager (IM) and labeled as scrapped IAW ALCINST 4100.1 dated 08 September 2016, and replaced with new OEM parts (See Paragraph 3.25.5 concerning PMA parts). The IM shall provide direction on all scrapped parts.

3.26 Beyond Economical Repair (BER):

3.26.1 When the cost of returning the CLIN part to serviceable condition, exceeds the current replacement cost of that part; or when the part cannot be repaired or overhauled due to damage or wear beyond the material properties, characteristic, or specifications of the item, the following procedures shall apply:

The contractor shall contact the USCG Contracting Officer, in writing, via FAX or e-mail, with specific rationale for the BER condition. The rationale shall include and provide: TIR, nomenclature, NSN, P/N, S/N, contract number, delivery order number, and CLIN along with a cost breakdown of additional parts and labor as would be necessary to repair the component to serviceable status. Propeller Hubs deemed BER shall have damage, limitations, measurements, tolerances and the corresponding reference(s) listed on the TIR. If requested by the USCG, the contractor shall have the Propeller Hub evaluated by the OEM and produce in writing, OEM documentation of the evaluation to include any OEM repair guidance or repair instructions.

3.26.2 If the contract line item (received at the contractor's facility) is later determined to be in a BER condition. The USCG Contracting Officer shall be notified immediately following the BER determination and provided with the BER determination rationale. Refer to paragraph 3.25 for further disposition and rationale.

3.26.3 Once the contract line item is determined to be BER, no further repair/overhaul work on that item shall be performed and the item in question shall be placed in a bonded storage room for safekeeping until written authorization to proceed or other disposition instructions are received from the USCG Contracting Officer.

3.27 Missing or Cannibalized Components

3.27.1 Missing Components: Within ten (10) working days after the receipt and inspection of the components the contractor shall notify the USCG Contracting Officer in writing of any missing parts or sub-assemblies required for final inspection and acceptance. The USCG Contracting Officer will then have forty five (45) calendar days to provide formal disposition instructions to the contractor. The

USCG reserves the right to provide RFI or repairable parts to replace the missing parts.

3.27.2 Cannibalized Components: Upon receiving components exhibiting cannibalization, the contractor shall notify the USCG Contracting Officer, in writing and in detail, within ten (10) working days and discontinue all actions until receipt of written authorization to proceed from the USCG Contracting Officer. The USCG Contracting Officer reserves the right to appoint a USCG Representative who shall witness the remaining teardown and inspection of the component. A letter of notification and a TIR shall be submitted to the Contracting Officer for disposition.

3.27.3 Turn-Around-Time (TAT) stops as of the date on the correspondence giving notification that work must cease due to missing/cannibalized parts. Unless the USCG Contracting Officer elects to have the component returned to the USCG as is, the TAT will re-start effective as of the mutually agreeable date stated in the bilateral

MOD.

3.28 Corrosion

3.28.1 Low altitude flight over salt water contributes to greater corrosion damage in USCG components than that experienced in commercial aircraft components. The contractor shall consider the presence and effects of corrosion to be "normal" in this case and provide for correction and removal of corrosion in the firm fixed repair/overhaul price. During inspection and functional testing, the presence of corrosion in an item or part shall constitute reason for a more thorough disassembly and inspection.

3.28.2 Corroded parts shall be replaced, except in those cases where removal of corrosion from a part will not impair the efficiency or safe operation of the part. Corrosion removal and treatment of any affected areas shall be accomplished IAW the applicable CMM repair procedures.

3.29 Exclusions; Components received in the following conditions are to be considered exclusions and may indicate an exclusion from the price in the contract schedule: 3.29.1 Catastrophic crash damage, foreign object damage, domestic object damage traceable to a USCG documented repair on the Hamilton Sundstrand components, Acts of God, war, and accidents attributable to the USCG responsibility.

3.29.2 Alteration, MOD or repairs that were not completed by the USCG IAW technical data approved by the FAA, OEM, or the USCG.

3.29.3 If a component is considered (by the contractor) to fit the exclusion description, the contractor shall notify the USCG Contracting Officer within ten (10) working days and discontinue all actions until the Contracting Officer makes a determination. The USCG reserves the right to appoint a USCG Representative to witness the remaining teardown and inspection of the component. A letter of notification and the TIR shall be submitted to the USCG Contracting Officer for disposition of the component. The contractor shall make the affected equipment available to a USCG Representative to view the exclusionary damage. If the Government elects not to physically view the equipment, the contractor’s findings report shall stand.

3.29.4 Upon request by the USCG’s Contracting Officer, the contractor shall submit a firm fixed price proposal to include an itemized breakdown of material including nomenclature, P/N, cost, and quantity of replacement parts, replacement percentages used to develop the original firm fixed contract price and the number of labor hours using established labor rates necessary to repair and/or restore exclusionary damage.

This proposal shall include all necessary supporting rationale and shall be submitted within forty-five (45) calendar days after notification is given to the USCG Contracting Officer. Upon completion of negotiations, the USCG Contracting Officer may authorize repair/overhaul, via contract MOD.

4.0 APPLICABLE DOCUMENTS

4.1 All Hamilton Sundstrand CMMs, CMM AI Log, REVs, MODs, and SBs and SIRs as applicable to the Hamilton Sundstrand components. It is noted that the service of this contract shall adhere to, but is not limited to these publications, as other OEM applicable documentation or specifications revealed, published, or updated prior to award or during the course of the contract period, shall be considered as being within the scope of this requirement and may be added to the contract as agreed upon by both parties.

4.2 All other OEM CMMs and REVs as applicable to the Hamilton Sundstrand components.

4.3 Hamilton Sundstrand and other OEM CMMs, REVs, SBs, MODs, AMDs, and Specifications are proprietary; the USCG does not own or possess rights in data, or distribution authority, and they cannot be provided by the USCG.

5.0 DEFINITIONS

5.1 ACMS tracking provides an effective means of configuration control to maintain the integrity of OEM overhaul/high time hourly intervals including flight and life cycle limits as applicable to Hamilton Sundstrand components. See section 6.0 for specific information on the incorporation of USCG ACMS requirements.

5.2 TSO shall be zeroed after an overhaul and may effectively restart some sub-assembly time intervals; while the total time, and OEM component life cycle limits may continue as applicable.

5.3 MOD is defined as the incorporation of FAA approved SBs, Spare Parts Bulletins, and Airworthiness Directives. This also includes USCG Time Compliance Technical Order (TCTO), and Special Compliance Technical Orders (SCTO), that are based on the FAA approved documents listed above. See paragraph 2.1, 3.15, 3.16 and 3.23 for incorporation of SBs and MODs.

5.4 BER: When the cost of returning the component to serviceable condition, exceeds the current replacement cost of that component; or when the component cannot be repaired or overhauled due to damage or wear beyond the material properties, characteristic, or specifications of the item. See paragraph 3.26 for specific information on USCG BER requirements.

5.5 SB (Mandatory and Optional): An Official statement from the OEM to correct issues or improve efficiency of systems within the aircraft. The contractor shall be responsible for obtaining and notifying the USCG Contracting Officer of all SB changes and MODs, for disposition approval prior to incorporation of those changes and MODs. See paragraphs 2.1, 3.15, 3.16 and 3.23 for incorporation of SBs and MODs.

5.6 Public and Private AIs:

5.6.1 Private AI: Available only to the OEM or OEM licensed repair facilities. These AIs contain approved manufacturer data for continued airworthiness and may be used to supplement OEM technical publications. The information contained in these documents is proprietary to the OEM and is for OEM or OEM licensed facility use only.

5.6.2 Public AI: Publicly available to MRO with appropriate technical data subscriptions. These AIs contain approved manufacturer data for continued airworthiness and may be used to supplement OEM technical publications. The intent of these AIs will be incorporated in the appropriate publication during future REVs.

6.0 ACMS Requirements

6.1 The contractor shall comply with all USCG ACMS documentation requirements.

6.1.1 Some Hamilton Sundstrand components are S/N tracked under USCG ACMS.

This tracking provides historical records of repairs, MODs, overhauls, flight times, cycles, item location, status, and an effective method of configuration control.

Components that are S/N tracked under USCG ACMS should, at the time of receipt, have a blank Component Repair Record (CRR), and a current Significant Component History Report (SCHR) attached to the component.

6.1.2 For configuration control, prior written approval of the USCG Contracting Officer shall be obtained for any configuration changes to Hamilton Sundstrand components. See paragraph 2.1, 3.15, 3.16 and 3.23 for specific information on the incorporation of SBs and MODs.

6.1.3 Verify the SCHR and CRR correspond with the NSN, P/N, and S/N of the component received. Promptly report discrepancies to the USCG Contracting Officer prior to performing any work.

6.2 Complete the CRR or a contractor proposed form preapproved by the USCG, describing the work performed, the technical data used to perform the work, and any significant parts replaced.

6.2.1 The CRR shall provide a complete description of the work performed, the component status (repaired, modified, overhauled, BER, scrap, etc.) and include, but not be limited to: the Contract number, Delivery Order number, CLIN, the contractor’s Work Order number, the date work was completed, any changes to the TSO, and total time, landings, or cycles as applicable.

6.2.2 The information provided in the CRR will be used by the USCG to update the component SCHRs.

6.3 Provide two copies of the completed CRR as follows:

6.3.1 One copy of the CRR shall remain with the material and is to be returned with the component upon completion of the repair MOD or overhaul.

6.3.2 A second copy of the CRR shall be mailed to:

USCG ALC (ATTN: ACMS)

1664 WEEKSVILLE ROAD, BLDG. 63 ELIZABETH

CITY, NC 27909-5001 alc

6.3.3 The CRR is considered a deliverable under the contract, and noncompliance with instructions will result in the delay or nonpayment of the invoice.

6.4 Provide one copy of an approved FAA Airworthiness Form 8130-3 or other FAA authorized form (e.g. EASA Form 1).

6.4.1 Attach one copy to the component along with the CRR.

6.4.2 The FAA airworthiness Form 8130-3, the OEM Certificate of Conformance or a

Certificate of Conformance IAW FAR 52.246-15 is considered a deliverable under the contract, and noncompliance with instructions herein, will result in the delay or nonpayment of the invoice.

7.0 MARKING, PACKAGING, AND PRESERVATION

7.1 For preservation and packaging see sections 3.18 and 3.18.1. All containers must be labeled on the outside with the NSN, P/N, S/N, nomenclature, contract number, delivery order number, CLIN, and vendor Commercial and Government Entity (CAGE) Code.

7.2 For propeller blade P/N RFA12A1POC, the associated S/N, blade weight and balance information matching the 8130-3 shall be attached to the outside of the shipping container.

7.3 The Propeller Blades, Hubs and Actuators shall be returned in the original OEM or USCG constructed Wooden Crate.

7.4 The internal packaging material shall be sufficient to prevent damage during shipment, handling, and storage. Preservation protection must be sufficient to prevent corrosion, deterioration or decay during warehouse storage for a period of not less than two years, see section 3.18.1 for specific preservation procedures.

7.5 Packaging matter shall not consist of the following materials: popcorn, shredded paper, Styrofoam or any type of peanut packaging.

7.6 Bar coding is authorized but not required.

8.0 INSPECTION AND ACCEPTANCE

8.1 Notwithstanding any requirement for specific inspections to be performed solely by the Government, the contractor shall perform all inspections, tests, and checks as required to substantiate that the supplies and services provided under the contract conform to the latest drawings, specifications, CMMs, and contract requirements listed herein.

8.2 Final inspection and acceptance shall be performed by ALC quality assurance personnel for quantity, condition, and compliance with the contract SOW.

9.0 ACRONYMS

ACMS Asset Computerized Maintenance System AI Action Item

ALC Aviation Logistics Center AMD Amendment

BER Beyond Economical Repair

CAGE Commercial and Government Entity CLIN Contract Line Item Number

CMM Component Maintenance Manual CRR Component Repair Record

DER Designated Engineering Representative FAA Federal Aviation Administration

IAW In Accordance With IM Item Manager

MOD Modification MPSA Maritime Patrol & Surveillance Aircraft

NSN National Stock Number

OEM Original Equipment Manufacturer P/N Part Number

PMA Parts Manufacturer Approval REV Revision

RFI Ready For Issue S/N Serial Number

SB Service Bulletin SCHR Significant Component History Report

SIR Service Information Release

SOW Statement of Work

TAT Turn-Around-Time

TIR Teardown Inspection Report TR Temporary Revision

TSO Time Since Overhaul USCG United States Coast Guard

Engineering Review/Approval: