Draft SOW_CPP and Monobloc Propeller Repair Services.docx

Statement of Work (SOW) US Navy Surface Ship Propeller Inspection and Repair

1.0 INTRODUCTION

1.0.1 The Naval Surface Warfare Center Philadelphia Division (NSWCPD) is a Department of Defense entity responsible for research and development, test and evaluation, engineering and fleet support organization for the Navy’s ships, submarines, military watercraft and unmanned vehicles. This requirement is for NSWCPD Code 42, which is responsible for U.S. Naval ship propulsion systems.

1.0.2 This contract is for non-personal services. It does not create employment rights with the U.S. Government whether actual, inherent, or implied

1.0.3 Government/Contractor Relationship:

1.0.3.1 The services to be delivered under this Contract are non-personal services and the parties recognize and agree that no employer-employee relationship exists or will exist under the Contract between the Government and the Contractor's personnel. Therefore, it is in the best interest of the Government to provide both parties a full understanding of their respective obligations.

1.0.3.2 The Contractor employees shall identify themselves as Contractor personnel by introducing themselves or being introduced as Contractor personnel and displaying distinguishable badges or other visible identification for meetings with Government personnel. In addition, Contractor personnel shall appropriately identify themselves as Contractor employees in telephone conversations and in formal and informal written correspondence.

1.0.3.3 Contractor personnel under this Contract shall not engage in any of the inherently Governmental functions listed at FAR Subpart 7.5 or DFARS Subpart 207.5.

1.0.4 Employee Relationship:

1.0.4.1 The services to be performed under this Contract do not require the Contractor or its personnel to exercise personal judgment and discretion on behalf of the Government. Rather the Contractor's personnel will act and exercise personal judgment and discretion on behalf of the Contractor.

1.0.4.2 Rules, regulations, directives, and requirements that are issued by the U. S. Navy and NSWCPD under its responsibility for good order, administration, and security are applicable to all personnel who enter a Government installation or who travel on Government transportation. This is not to be construed or interpreted to establish any degree of Government control that is inconsistent with a non-personal services contract.

1.0.4.3 Inapplicability of Employee Benefits: This Contract does not create an employer-employee relationship. Accordingly, entitlements and benefits applicable to such relationships do not apply.

1.0.4.4 It is the Contractor's, as well as the Government's, responsibility to monitor Contract activities and notify the Contracting Officer if the Contractor believes that the intent of this Section has been or may be violated.

1.0.4.4.1 The Contractor shall notify the Contracting Officer in writing via letter or email within three (3) calendar days from the date of any incident that the Contractor considers to constitute a violation of this Section. The notice should include the date, nature, and circumstances of the conduct; the name, function, and activity of each Government employee or Contractor official or employee involved or knowledgeable about such conduct; identify any documents or substance of any oral communication involved in the conduct; and the Contractor's estimated date when, absent a response, cost, schedule or performance will be impacted.

1.1 BACKGROUND

1.1.1 The Propulsion Systems Division, Code 42, of the Naval Surface Warfare Center, Philadelphia Division (NSWCPD), is responsible for maintaining a ready-for-issue rotatable pool of propeller assets for Controllable Pitch and Fixed Pitch Propellers

1.2 SCOPE OF WORK

1.2.1 List of Common Acronyms

· TPOC – Technical Point of Contact

· BER – Beyond Economical Repair

· GFP – Government Furnished Property

· VPI – Visual Preservation Inspection

· VTI – Visual Technical Inspection

· RFV – Request For Variance

· O&A – Over & Above

1.2.1 The scope of this Contract is to perform the repair of the following US Navy Propeller type and applicable drawings

2.0 APPLICABLE DOCUMENTS

2.0.1 The Contractor may contact the TPOC for copies of any references.

2.0.2 The Contractor shall reference and utilize the latest version available when performing tasks within this SOW.

2.0.3 If during the performance of this contract the Contractor believes that the contract contains outdated or different versions of any specifications or standards, the Contractor may request that the contract be updated to include the current version of the applicable specification or standard. The Contractor should submit update requests to the Contracting Officer for approval. The Contractor shall perform the contract in accordance with the existing specifications and standards until notified by the Contracting Officer of the disposition of the request. Any approved alternate or updated specifications and standards will be incorporated into the contract.

2.0.4 In the event of a conflict between the text of this document and the references and/or drawings, the text of this document shall take precedence. Nothing in this document, however, shall supersede applicable laws and regulations unless a specific exemption has been obtained.

3.0 REQUIREMENTS

3.1 GENERAL

3.1.1 Unless otherwise specified, the Contractor is responsible for the performance of all work requirements herein. The Contractor may use its own or any other facilities suitable for the performance of the work specified herein, unless disapproved by the Government. The Government reserves the right to perform any of the inspections set forth in the specification where such inspections are deemed necessary to assure supplies and services conform to prescribed requirements.

3.1.2 Material is considered BER if the repair costs exceed 75% of the replacement cost. If at any time during the period of performance, the Contractor determines that the condition of the GFP may indicate it is BER, the Contractor shall immediately notify the Contracting Officer, Contracting Officer’s Representative, and TPOC with a description of the condition. Replacement costs can be provided to the Contractor upon request.

3.1.4 Visitations by the government. Visits by US Navy personnel will be coordinated with the Contractor based on appropriate production milestones, or when the Government deems such a visit appropriate. The Government reserves the right to conduct a facility audit at any time during the Contract period of performance.

3.2 CLIN 0001: FULL OVERHAUL, CPP SINGLE BLADE (1 BLADE)

3.2.1 For the duration of any order involving this CLIN, submit a monthly status update, in accordance with CDRL A001.

3.2.2 For the duration of any order involving this CLIN, submit a monthly GFP inventory report in accordance with CDRL A004.

3.2.3 Within two weeks of awarding any order involving this CLIN, initiate a kickoff meeting with the TPOC to review contract requirements, in accordance with CDRL A001.

3.2.4 Photos of non-confidential GFP are highly encouraged as an aid to the visual inspection reports. The Contractor shall NOT take or transmit photos of confidential GFP under any circumstances.

3.2.5 Unload the CPP single blade from the delivery truck.

3.2.6 Unload the propeller blade gage set from the delivery truck.

3.2.7 Unload the CPP dummy hub assembly from the delivery truck.

3.2.8 Within two weeks of receipt of the CPP single blade, complete a pre-repair VPI in accordance with Reference E. Inspection results shall be documented using Reference M and submitted in accordance with CDRL A002.

3.2.9 Within two weeks of receipt of the propeller blade gage set, complete a pre-repair Visual Inspection in accordance with Reference E. Inspection results and photos shall be documented using Reference P and submitted in accordance with CDRL A002.

3.2.9.1 This requirement may be omitted if the GFP is already located at the Contractor’s facility upon award (due to prior awarded work), the GFM has not left the Contractor facility in the last 6 months, and the Contractor already submitted a valid inspection report for the GFP to the Government within the last 6 months.

3.2.10 Within two weeks of receipt of the CPP dummy hub assembly, complete a pre-repair Visual Inspection in accordance with Reference E. Inspection results and photos shall be documented using Reference Q and submitted in accordance with CDRL A002.

3.2.10.1 This requirement may be omitted if the GFP is already located at the Contractor’s facility upon award (due to prior awarded work), the GFP has not left the Contractor facility in the last 6 months, and the Contractor already submitted a valid inspection report for the GFP to the Government within the last 6 months.

3.2.11 If results of the visual inspections are unsatisfactory, contact the TPOC immediately.

3.2.12 Clean the CPP single blade in accordance with Reference F.

3.2.13 Dispose of all existing packaging, preservation, and crating.

3.2.14 Complete a pre-repair PT-aided VTI of the CPP single blade, in accordance with References E. Inspection results and photos shall be documented using Reference N and submitted in accordance with CDRL A002.

3.2.15 Complete a pre-repair dimensional inspection of the CPP single blade, in accordance with Reference E and as modified below. Inspection results shall be documented using Reference O and submitted in accordance with CDRL A002. Results for inspections that do not have existing government forms shall be documented and reported in approved contractor format using Reference O as guidance.

3.2.15.1 Complete and document a pre-repair UT plate thickness inspection in accordance with Reference E.

3.2.15.2 Complete and document a pre-repair PRAIRIE flow test inspection in accordance with Reference E.

3.2.15.3 Complete and document a pre-repair weight inspection in accordance with Reference E.

3.2.16 If the results of the CPP single blade VTI or dimensional inspection are unsatisfactory due to product quality deficiencies (i.e. features that differ from design), contact the TPOC immediately.

3.2.17 Complete a repair plan for the CPP single blade. The repair plan shall include a numbered list of all non-conformances noted in the VTI and dimensional inspection reports, along with a corresponding recommended repair action, applicable RFV, or applicable request for O&A for each. Document and submit in accordance with CDRL A002 using a TPOC-provided template.

3.2.18 Upon approval of the repair plan in WAWF and any applicable O&A requests submitted with it, complete all indicated repairs in accordance with Reference E and as directed below, via straightening, material removal, and/or weld build-up.

3.2.19 Complete a post-repair dimensional inspection of the CPP single blade in accordance with Reference E. Inspection results shall be documented using Reference O and submitted in accordance with CDRL A002. Results for inspections that do not have existing government forms shall be documented and reported in approved contractor format using Reference O as guidance.

3.2.19.1 The dimensional inspection report shall include a weld-map with the size and location of all new welds.

3.2.20 Re-stamp the palm data on the CPP single blade using existing stamp data and the data format below as guidance in accordance with References E. If information is missing or needs clarification, contact the TPOC prior to stamping.

· A. SN [XXXX-XX]

· B. HN [Heat number]

· C. DN [NAVSEA drawing number and rev as indicated on existing stamping]

· D. [SHIP CLASS]

· E. [PORT/STBD/CENTER, RH/LH]

· F. DES DIA [FT and IN]

· G. DES PITCH AT 0.70R [FT and IN]

· H. MFR [Name and Date]

· I. CN [full manufacture contract number]

· J. WT [actual weight with palm weights added] LBS

· K. NSN [XXXX-XX-XXX-XXXX]

· L. MAT [material, alloy, and spec]

· REP/BAL [Company name, MM/YY, including any previous history]

3.2.21 Complete a PT-aided post-repair VTI of the CPP single blade, in accordance with Reference E. Inspection results and photos shall be documented using Reference N and submitted in accordance with CDRL A002.

3.2.22 Document and submit all applicable RFV’s using Reference R in accordance with CDRL A003.

3.2.23 Upon approval of the CPP single blade post-repair VTI and post-repair dimensional inspection reports in WAWF, preserve, package, crate, and mark the CPP single blade in accordance with Reference A and Reference B.

3.2.23.1 Replace all original packaging, preservation, and crating with new.

3.2.24 Complete a post-repair VPI of the CPP single blade in accordance with Reference E. Inspection results and photos shall be documented using Reference M and submitted in accordance with CDRL A002.

3.2.25 Complete a post-repair Visual Inspection of the propeller blade gage set in accordance with Reference E. Inspection results and photos shall be documented using Reference P and submitted in accordance with CDRL A002.

3.2.26 Complete a post-repair Visual Inspection of the CPP dummy hub assembly in accordance with Reference E. Inspection results and photos shall be documented using Reference Q and submitted in accordance with CDRL A0002.

3.2.27 Document and submit a CPP single blade certification report using Reference L in accordance with CDRL A002.

3.2.28 Attach signed copies of the CPP single blade VPI and Certification reports to the upright blade face as well as the outside of the crate in a transparent, waterproof, greaseproof, re-sealable bag in accordance with Reference A.

3.2.29 Attach a signed copy of the propeller blade gage set VI report to both the inside and outside of the crate in a transparent, waterproof, greaseproof, re-sealable bag in accordance with Reference A.

3.2.30 Attach a signed copy of the CPP dummy hub assembly VI report to the dummy hub as well as outside of the crate in a transparent, waterproof, greaseproof, re-sealable bag in accordance with Reference A.

3.2.31 When directed, load the CPP single blade onto the delivery truck.

3.2.32 When directed, load the propeller blade gage set onto the delivery truck.

3.2.33 When directed, load the CPP dummy hub assembly onto the delivery truck.

3.2.34 All GFP shall be shipped to the destination(s) specified on the individual task order.

3.2.35 The following conditions are considered O&A for this CLIN. If the Contractor suspects any of these conditions are necessary, contact the contracting officer, contracting specialist, and TPOC immediately to initiate O&A negotiations in accordance with clause 252.217-7028.

3.3 CLIN 0002: FULL OVERHAUL, CPP BLADE SET (5 BLADES)

3.3.1 For the duration of any order involving this CLIN, submit a monthly status update, in accordance with CDRL A001.

3.3.2 For the duration of any order involving this CLIN, submit a monthly GFP inventory report in accordance with CDRL A004.

3.3.3 Within two weeks of awarding any order involving this CLIN, initiate a kickoff meeting with the TPOC to review contract requirements, in accordance with CDRL A001.

3.3.4 For the purpose of this CLIN, a CPP blade set is defined as 5x CPP single blades that are or will be balanced together.

3.3.5 Photos of non-confidential GFP are highly encouraged as an aid to the visual inspection reports. The Contractor shall NOT take or transmit photos of confidential GFP under any circumstances.

3.3.6 Unload the CPP blade set from the delivery truck.

3.3.7 Unload the propeller blade gage set from the delivery truck.

3.3.8 Unload the CPP dummy hub assembly from the delivery truck.

3.3.9 Within two weeks of receipt of the CPP blade set, complete a pre-repair VPI in accordance with Reference E. Inspection results shall be documented using Reference M and submitted in accordance with CDRL A002.

3.3.10 Within two weeks of receipt of the propeller blade gage set, complete a pre-repair Visual Inspection in accordance with Reference E. Inspection results and photos shall be documented using Reference P and submitted in accordance with CDRL A002.

3.3.10.1 This requirement may be omitted if the GFP is already located at the Contractor’s facility upon award (due to prior awarded work), the GFP has not left the Contractor facility in the last 6 months, and the Contractor already submitted a valid inspection report for the GFP to the Government within the last 6 months.

3.3.11 Within two weeks of receipt of the CPP dummy hub assembly, complete a pre-repair Visual Inspection in accordance with Reference E. Inspection results and photos shall be documented using Reference Q and submitted in accordance with CDRL A002.

3.3.11.1 This requirement may be omitted if the GFP is already located at the Contractor’s facility upon award (due to prior awarded work), the GFP has not left the Contractor facility in the last 6 months, and the Contractor already submitted a valid inspection report for the GFP to the Government within the last 6 months.

3.3.12 If results of the visual inspections are unsatisfactory, contact the TPOC immediately.

3.3.13 Clean the CPP blade set in accordance with Reference F.

3.3.14 Dispose of all existing packaging, preservation, and crating.

3.3.15 Complete a pre-repair PT-aided VTI of the CPP blade set, in accordance with Reference E. Inspection results and photos shall be documented using Reference N and submitted in accordance with CDRL A002.

3.3.16 Complete a pre-repair dimensional inspection of the CPP blade set, in accordance with Reference E and as modified below. Inspection results shall be documented using Reference O and submitted in accordance with CDRL A002. Results for inspections that do not have existing government forms shall be documented and reported in approved contractor format using Reference O as guidance.

3.3.16.1 Complete and document a pre-repair UT plate thickness inspection in accordance with Reference E.

3.3.16.2 Complete and document a pre-repair PRAIRIE flow test inspection in accordance with Reference E.

3.3.16.3 Complete and document a pre-repair balance inspection in accordance with Reference E.

3.3.17 If the results of the CPP blade set VTI or dimensional inspection are unsatisfactory due to product quality deficiencies (i.e. features that differ from design), contact the TPOC immediately.

3.3.18 Complete a repair plan for the CPP blade set. The repair plan shall include a numbered list of all non-conformances noted in the VTI and dimensional inspection reports, along with a corresponding recommended repair action, applicable RFV, or applicable request for O&A for each. Document and submit in accordance with CDRL A002 using a TPOC-provided template.

3.3.19 Upon approval of the repair plan in WAWF and any applicable O&A requests submitted with it, complete all indicated repairs in accordance with Reference E, and as directed below, via straightening, material removal, and/or weld build-up.

3.3.20 Complete a post-repair dimensional inspection of the CPP blade set in accordance with Reference E. Inspection results shall be documented using Reference O and submitted in accordance with CDRL A002. Results for inspections that do not have existing government forms shall be documented and reported in approved contractor format using Reference O as guidance.

3.3.20.1 The dimensional inspection report shall include a weld-map with the size and location of all new welds.

3.3.21 Re-stamp the palm data on each CPP blade using the existing stamp data and the data format below as guidance in accordance with Reference E. If information is missing or needs clarification, contact the TPOC prior to stamping.

· A. SN [XXXX-XX]

· B. HN [Heat number]

· C. DN [NAVSEA drawing number and rev as indicated on existing stamping]

· D. [SHIP CLASS]

· E. [PORT/STBD/CENTER, RH/LH]

· F. DES DIA [FT and IN]

· G. DES PITCH AT 0.70R [FT and IN]

· H. MFR [Name and Date]

· I. CN [full manufacture contract number]

· J. WT [actual weight after balance] LBS

· K. NSN [XXXX-XX-XXX-XXXX]

· L. MAT [material, alloy, and spec]

· REP/BAL [Company name, MM/YY, including any previous history]

3.3.22 Complete a PT-aided post-repair VTI of the CPP blade set, in accordance with Reference E. Inspection results and photos shall be documented using Reference N and submitted in accordance with CDRL A002.

3.3.23 Document and submit all applicable RFV’s in accordance with CDRL A003 using Reference R.

3.3.24 Upon approval of the CPP blade set post-repair VTI and post-repair dimensional inspection reports in WAWF, preserve, package, crate, and mark the CPP blade set in accordance with Reference A and Reference B.

3.3.24.1 Replace all original packaging, preservation, and crating with new.

3.3.25 Complete a post-repair VPI of the CPP blade set in accordance with Reference E. Inspection results and photos shall be documented using Reference M and submitted in accordance with CDRL A002.

3.3.26 Complete a post-repair Visual Inspection of the propeller blade gage set in accordance with Reference E. Inspection results and photos shall be documented using Reference P and submitted in accordance with CDRL A002.

3.3.27 Complete a post-repair Visual Inspection of the CPP dummy hub assembly in accordance with Reference E. Inspection results and photos shall be documented using Reference Q and submitted in accordance with CDRL A002.

3.3.28 Document and submit a CPP blade set certification report in accordance with CDRL A002 using Reference L.

3.3.29 Attach signed copies of the CPP blade set VPI and Certification reports to each upright blade face as well as the outside of each crate in a transparent, waterproof, greaseproof, re-sealable bag in accordance with Reference A.

3.3.30 Attach a signed copy of the propeller blade gage set VI report to both the inside and outside of the crate in a transparent, waterproof, greaseproof, re-sealable bag in accordance with Reference A.

3.3.31 Attach a signed copy of the CPP dummy hub assembly VI report to the dummy hub as well as outside of the crate in a transparent, waterproof, greaseproof, re-sealable bag in accordance with Reference A.

3.3.32 When directed, load the CPP blade set onto the delivery truck.

3.3.33 When directed, load the propeller blade gage set onto the delivery truck.

3.3.34 When directed, load the CPP dummy hub assembly onto the delivery truck.

3.3.35 All GFP shall be shipped to the destination(s) specified on the individual task order.

3.3.36 The following conditions are considered O&A for this CLIN. If the Contractor suspects any of these conditions are necessary, contact the contracting officer, contracting specialist, and TPOC immediately to initiate O&A negotiations in accordance with clause 252.217-7028.

3.3.36.1 Need for more than (5x) dowel pin sleeve repairs and more than (3x) blade palm skim cuts to restore flatness.

3.4 CLIN 0003: FULL OVERHAUL, MONOBLOC PROPELLER

3.4.1 For the duration of any order involving this CLIN, submit a monthly status update, in accordance with CDRL A001.

3.4.2 For the duration of any order involving this CLIN, submit a monthly GFP inventory report in accordance with CDRL A004.

3.4.3 Within two weeks of awarding any order involving this CLIN, initiate a kickoff meeting with the TPOC to review contract requirements, in accordance with CDRL A001.

3.4.4 For the purpose of this CLIN, a propeller assembly is defined by the following items, in the quantities specified in the applicable propeller drawing:

· Propeller

· Gland Ring

· Lifting Eyebolts (FWD/AFT)

· Lifting Eyebolt (SIDE)

· Lifting Eyebolt Hole Plugs (FWD)

· Lifting Eyebolt Hole Plug (SIDE)

· Fill/Vent Hole Plugs

· Cap Studs

· Cap Stud Nuts

· Gland Studs

· Gland Stud Nuts

· Filler Guide Blocks

3.4.5 Photos of non-confidential GFP are highly encouraged as an aid to the visual inspection reports. The Contractor shall NOT take or transmit photos of confidential GFP under any circumstances.

3.4.6 Unload the propeller assembly from the delivery truck.

3.4.7 Unload the propeller blade gage set from the delivery truck.

3.4.8 Unload the propeller plug gage assembly from the delivery truck.

3.4.9 Within two weeks of receipt of the propeller assembly, complete a pre-repair Visual Preservation Inspection (VPI) in accordance with Reference E. Inspection results and photos shall be documented using Reference M and submitted in accordance with CDRL A002.

3.4.10 Within two weeks of receipt of the propeller blade gage set, perf complete orm a pre-repair Visual Inspection in accordance with Reference E. Inspection results and photos shall be documented using Reference P and submitted in accordance with CDRL A002.

3.4.10.1 This requirement may be omitted if the GFP is already located at the Contractor’s facility upon award (due to prior awarded work), the GFP has not left the Contractor facility in the last 6 months, and the Contractor already submitted a valid inspection report for the GFP to the Government within the last 6 months.

3.4.11 Within two weeks of receipt of the propeller plug gage assembly, complete a pre-repair Visual Inspection in accordance with Reference E. Inspection results and photos shall be documented using Reference K and submitted in accordance with CDRL A002.

3.4.11.1 This requirement may be omitted if the GFP is already located at the Contractor’s facility upon award (due to prior awarded work), the GFP has not left the Contractor facility in the last 6 months, and the Contractor already submitted a valid inspection report for the GFP to the Government within the last 6 months.

3.4.12 If results of the visual inspections are unsatisfactory, contact the TPOC immediately.

3.4.13 Clean the propeller assembly in accordance with Reference F.

3.4.14 Dispose of all existing packaging, preservation, and crating.

3.4.15 Dispose of the following items – these items do not need to be included in the pre-repair VTI or pre-repair dimensional Inspection:

· Lifting Eyebolt Hole Plugs (FWD)

· Lifting Eyebolt Hole Plug (SIDE)

· Fill/Vent Hole Plugs

· Cap Studs

· Cap Stud Nuts

· Gland Studs

· Gland Stud Nuts

3.4.16 Complete a pre-repair PT-aided VTI of the remaining propeller assembly, in accordance with Reference E. Inspection results and photos shall be documented using Reference N and submitted in accordance with CDRL A002.

3.4.17 Complete a pre-repair dimensional inspection of the propeller assembly, in accordance with Reference E and as modified below. Inspection results shall be documented using Reference O and submitted in accordance with CDRL A002. Results for inspections that do not have existing government forms shall be documented and reported in approved contractor format using Reference O as guidance.

3.4.17.1 Complete and document a pre-repair hub pressure test in accordance with Reference E.

3.4.17.2 Complete and document an assembly fit-up with all remaining propeller assembly components in accordance with Reference E.

3.4.17.3 Complete and document a pre-repair balance inspection in accordance with Reference E.

3.4.18 If the results of the VTI or dimensional inspection are unsatisfactory due to product quality deficiencies (i.e. features that differ from design), contact the TPOC immediately.

3.4.19 Complete a repair plan for the propeller assembly. The repair plan shall include a numbered list of all non-conformances noted in the VTI and dimensional inspection reports, along with a corresponding recommended repair action, applicable RFV, or applicable request for Over and Above (O&A) for each. Document and submit in accordance with CDRL A002 using a TPOC-provided template.

3.4.20 Upon approval of the repair plan in WAWF and any applicable O&A requests submitted with the repair plan, complete all repairs detailed in the repair plan in accordance with Reference E and as directed below, via straightening, material removal, and/or weld build-up:

3.4.20.1 Replace full quantities of all following items in accordance with Reference E:

· Gland Ring

· Lifting Eyebolts (FWD/AFT)

· Lifting Eyebolt (SIDE)

· Lifting Eyebolt Hole Plugs (FWD)

· Lifting Eyebolt Hole Plug (SIDE)

· Fill/Vent Hole Plugs

· Cap Studs

· Cap Stud Nuts

· Gland Studs

· Gland Stud Nuts

3.4.21 Complete a post-repair dimensional inspection of the propeller assembly in accordance with Reference E. Inspection results shall be documented using Reference O and submitted in accordance with CDRL A002. Results for inspections that do not have existing government forms shall be documented and reported in approved contractor format using Reference O as guidance.

3.4.21.1 The dimensional inspection report shall include a weld-map with the size and location of all new welds.

3.4.22 Re-Stamp the propeller assembly using the existing stamp data and the data format below, in accordance with Reference E. If information is missing or needs clarification, contact the TPOC prior to stamping.

· A. SN [XXXXX]

· B. DN [NAVSEA drawing number and rev as indicated on existing stamping]

· C. [SHIP CLASS]

· D. [PORT/STBD/CENTER, RH/LH]

· E. DES DIA [FT and IN]

· F. DES PITCH AT 0.70R [FT and IN]

· G. MFR [Name and Date]

· H. CN [full manufacture contract number]

· I. WT [actual weight after balance] LBS

· J. NSN [XXXX-XX-XXX-XXXX]

· K. MAT [material, alloy, and spec]

· REP/BAL [Company name, MM/YY, including any previous history]

3.4.23 Complete a PT-aided post-repair VTI of the propeller assembly, in accordance with Reference E. Inspection results and photos shall be documented using Reference N and submitted in accordance with CDRL A002.

3.4.24 Document and submit all applicable RFV’s in accordance with CDRL A003 using Reference R.

3.4.25 Upon approval of the propeller assembly post-repair VTI and post-repair dimensional inspection reports in WAWF, preserve, package, crate, and mark the propeller assembly in accordance with Reference A and Reference B and as modified below:

3.4.25.1 Replace all original preservation, packaging, and crating with new.

3.4.25.2 All eyebolts shall be installed in their respective propeller eyebolt holes with anti-seize compound and thread sealant.

3.4.26 Complete a post-repair VPI of the propeller assembly in accordance with Reference E. Inspection results and photos, shall be documented using Reference M and submitted in accordance with CDRL A002.

3.4.27 Complete a post-repair Visual Inspection of the blade gage set in accordance with Reference E. Inspection results and photos shall be documented using Reference P and submitted in accordance with CDRL A002.

3.4.28 Complete a post-repair Visual Inspection of the propeller plug gage assembly in accordance with Reference E. Inspection results and photos shall be documented using Reference K and submitted in accordance with CDRL A002.

3.4.29 Document and submit a propeller assembly certification report in accordance with CDRL A002 using Reference L.

3.4.30 Attach signed copies of the propeller assembly VPI and Certification report to the outer diameter of the hub (in line with the side eyebolt hole) in a transparent, waterproof, greaseproof, re-sealable bag in accordance with Reference A.

3.4.31 Attach a signed copy of the propeller blade gage set VI report to both the inside and outside of the crate in a transparent, waterproof, greaseproof, re-sealable bag in accordance with Reference A.

3.4.32 Attach a signed copy of the propeller plug gage assembly VI report to both the inside and outside of the crate in a transparent, waterproof, greaseproof, re-sealable bag in accordance with Reference A.

3.4.33 When directed, load the propeller assembly onto the delivery truck.

3.4.34 When directed, load the propeller blade gage set onto the delivery truck.

3.4.35 When directed, load the propeller plug gage onto the delivery truck.

3.4.36 All GFP shall be shipped to the destination(s) specified on the individual task order.

3.4.37 The following conditions are considered O&A for this CLIN. If the Contractor suspects any of these conditions are necessary, contact the contracting officer, contracting specialist, and TPOC immediately to initiate O&A negotiations in accordance with clause 252.217-7028.

3.4.37.1 Machining or casting replacement components beyond those listed in Para 3.4.20.1

3.4.37.2 Machining of the existing propeller assembly beyond what is necessary to repair out of tolerance threaded holes.

3.4.37.3 Weld repair of more than (2x) eyebolt holes and more than (2x) other threaded holes.

3.5 CLIN 0004: FULL OVERHAUL, MONOBLOC PROPELLER CAP

3.5.1 For the duration of any order involving this CLIN, submit a monthly status update, in accordance with CDRL A001.

3.5.2 For the duration of any order involving this CLIN, submit a monthly GFP inventory report in accordance with CDRL A004.

3.5.3 Within two weeks of awarding any order involving this CLIN, initiate a kickoff meeting with the TPOC to review contract requirements, in accordance with CDRL A001.

3.5.4 For the purpose of this CLIN, a propeller cap assembly is defined by the following items, in the quantities specified in the applicable propeller drawing:

· Propeller Cap

· Cap Cover Plates

· Cap Baffle Plate

· Cap Eyebolt Hole Plug

· Cap Cover Plate Fasteners

· Cap Fill/Vent Plugs

· Cap Eyebolt

· Foam (if propeller drawing specifies)

· Balance Weights (may not be listed in drawing)

3.5.5 Photos of non-confidential GFP are highly encouraged as an aid to the visual inspection reports. The Contractor shall NOT take or transmit photos of confidential GFP under any circumstances.

3.5.6 Unload the propeller cap assembly from the delivery truck.

3.5.7 Within two weeks of receipt of the propeller cap assembly, perform a pre-repair Visual Preservation Inspection (VPI) in accordance with Reference E. Inspection results and photos shall be documented using Reference M and submitted in accordance with CDRL A002.

3.5.7.1 If results of the VPI are unsatisfactory, contact the TPOC immediately.

3.5.8 Clean the propeller cap assembly in accordance with Reference F.

3.5.9 Dispose of all existing packaging, preservation, and crating.

3.5.10 Dispose of the following items – these items do not need to be included in the pre-repair Visual Technical Inspection (VTI) or pre-repair Dimensional Inspection:

· Cap Eyebolt Hole Plug

· Cap Cover Plate Fasteners

· Cap Fill/vent Plugs

· Cap eyebolt

3.5.11 Complete a pre-repair PT-aided VTI of the remaining cap assembly, in accordance with Reference E. Inspection results and photos shall be documented using Reference N and submitted in accordance with CDRL A002.

3.5.11.1 For caps that are supposed to have foam per the applicable propeller drawing, complete a foam inspection by removing the baffle plate and inspecting the cap foam for rigidity and loss of volume. Results of the foam inspection, including photos, shall be documented and submitted as part of the VTI report.

3.5.11.2 In addition to the acceptance criteria in Reference E, the following additional visual inspection acceptance criteria apply:

3.5.11.2.1 Reference D, Table IV, Weldments: criteria for “All Surfaces” shall apply to all surfaces of the cap.

3.5.11.2.2 Reference D, Table IV, CASTINGS: criteria for all “Hub outside diameter (OD)” shall apply to outside diameter of the cap.

3.5.11.2.3 Reference D, Table IV, CASTINGS: criteria for “The remaining surfaces of the blades” shall apply to the remaining cap surfaces.

3.5.11.2.4 The propeller cap shall be free of any defect that could permit leakage into the propeller cap interior.

3.5.12 Complete a pre-repair dimensional inspection of the propeller cap assembly, in accordance with Reference E and as directed below. Inspection results shall be documented using Reference O and submitted in accordance with CDRL A002. Results for inspections that do not have existing government forms shall be documented and reported in contractor format using Reference O as guidance. Dimensional inspections shall include the following. Tolerances are as defined in the applicable propeller cap drawing:

3.5.13 If the results of the VTI or dimensional inspection are unsatisfactory due to product quality deficiencies (i.e. features that differ from design), contact the TPOC immediately.

3.5.14 Complete a repair plan for the propeller cap assembly. The repair plan shall include a numbered list of all non-conformances noted in the VTI and Dimensional inspection reports, along with a corresponding recommended repair action or Request for Variance (RFV) for each. Document and submit in accordance with CDRL A002 using a TPOC-provided template.

3.5.15 Upon final approval of the repair plan in WAWF, complete all repairs detailed in the repair plan in accordance with Reference E and as directed below, via straightening, material removal, weld build-up, and/or machining:

3.5.15.1 Replace full quantities of all following items in accordance with Reference E:

· Cap eyebolt hole plug

· Cap cover plate fasteners

· Cap fill/vent plugs

· Cap eyebolt

· Foam

· Balance weight(s)

3.5.16 Complete a post-repair dimensional inspection of the propeller cap assembly in accordance with Reference E. Dimensional inspections shall include everything from Para. 3.5.12. Inspection results shall be documented using Reference O and submitted in accordance with CDRL A002. Results for inspections that do not have existing government forms shall be documented and reported in contractor format using Reference O as guidance.

3.5.16.1 The dimensional report shall include a weld-map with the size and location of all new welds.

3.5.17 Re-stamp the propeller cap using the existing stamp data and the data format below, in accordance with Reference E. If information is missing or needs clarification, contact the TPOC prior to stamping:

· SN [XXXXX]

· DN [DN and REV]

· NSN [XXXX-XX-XXX-XXXX]

· [As-stamped material]

· [As-stamped material spec]

· [Final weight after balance] LBS

· REP/BAL [Company name, MM/YY]

3.5.18 Complete a PT-aided post-repair VTI of the propeller cap assembly, in accordance with Reference E. Inspection results and photos shall be documented using Reference N and submitted in accordance with CDRL A002.

3.5.19 Document and submit all applicable RFVs in accordance with CDRL A003 using Reference R.

3.5.20 Upon approval of the post-repair VTI and post-repair dimensional reports in WAWF, preserve, package, crate, and mark the propeller cap assembly in accordance with Reference A and Reference B.

3.5.20.1 Replace all original preservation, packaging, and crating with new.

3.5.21 Attach signed copies of the propeller cap assembly post-repair VTI and Dimensional Inspection reports inside the cap crate in a transparent, waterproof, greaseproof, re-sealable bag.

3.5.22 Complete a post-repair VPI in accordance with Reference E. Inspection results, including photos, shall be documented using Reference M and submitted in accordance with CDRL A002.

3.5.23 Document and submit a propeller cap certification report in accordance with CDRL A002 using Reference L.

3.5.24 Attach signed copies of the VPI and Certification report to the outside of the crate in a transparent, waterproof, greaseproof, re-sealable bag.

3.5.25 Load the crated propeller cap assembly onto the delivery truck.

3.5.26 Equipment shall be shipped to the destination specified on the individual task order.

3.5.27 The following conditions are considered O&A for this CLIN. If the Contractor suspects any of these conditions are necessary, contact the contracting officer, contracting specialist, and TPOC immediately to initiate O&A negotiations in accordance with clause 252.217-7028.

3.5.27.1 Machining or casting replacement components beyond those listed in Para 3.5.15.1.

3.5.27.2 Machining of the existing propeller cap assembly beyond what is necessary to repair out of tolerance threaded holes.

3.6 CLIN 0005: BALANCE, CPP BLADE SET

3.6.1 For the duration of any order involving this CLIN, submit a monthly status update, in accordance with CDRL A001.

3.6.2 For the duration of any order involving this CLIN, submit a monthly GFP inventory report in accordance with CDRL A004.

3.6.3 Within two weeks of awarding any order involving this CLIN, initiate a kickoff meeting with the TPOC to review contract requirements, in accordance with CDRL A002.

3.6.4 For the purpose of this CLIN, a CPP blade set is defined as 5x CPP single blades that are or will be balanced together.

3.6.5 Photos of non-confidential GFP are highly encouraged as an aid to the visual inspection reports. The Contractor shall NOT take or transmit photos of confidential GFP under any circumstances.

3.6.6 Unload the CPP blade set from the delivery truck.

3.6.7 Unload the CPP dummy hub assembly from the delivery truck.

3.6.8 Within two weeks of receipt of the CPP blade set, complete a pre-repair Visual Preservation Inspection (VPI) in accordance with Reference E. Inspection results shall be documented using Reference M and submitted in accordance with CDRL A002.

3.6.9 Within two weeks of receipt of the CPP dummy hub assembly, complete a pre-repair Visual Inspection in accordance with Reference E. Inspection results and photos shall be documented using Reference Q and submitted in accordance with CDRL A002.

3.6.9.1 This requirement may be omitted if the GFP is already located at the Contractor’s facility upon award (due to prior awarded work), the GFP has not left the Contractor facility in the last 6 months, and the Contractor already submitted a valid inspection report for the GFP to the Government within the last 6 months.

3.6.9.2 If results of the VPI are unsatisfactory, contact the TPOC immediately.

3.6.10 Clean the CPP blade set in accordance with Reference F.

3.6.11 Complete a pre-repair PT-aided VTI of the CPP blade set, in accordance with Reference E. Inspection results and photos shall be documented using Reference N and submitted in accordance with CDRL A002.

3.6.11.1 Complete the VTI before balancing and re-stamping occur to provide early indication if UNSAT visual conditions are present. If visual inspection results indicate UNSAT conditions are present, notify the TPOC immediately. Submit the VTI report after balance and re-stamping are complete so updated stamp data can be included.

3.6.11.2 If results of the VTI are unsatisfactory, contact the TPOC immediately.

3.6.12 Complete a balance inspection and balance the blade set in accordance with Reference E. Document final results using Reference O and submit in accordance with CDRL A002.

3.6.13 Re-stamp palm data on each CPP blade using existing stamp data and the data format below as guidance in accordance with References E. Update each blade’s total weight as applicable and update the serial number with one provided by the TPOC. If information is missing or needs clarification, contact the TPOC prior to stamping.

· A. SN [XXXX-XX]

· B. HN [Heat number]

· C. DN [NAVSEA drawing number and rev as indicated on existing stamping]

· D. [SHIP CLASS]

· E. [PORT/STBD/CENTER, RH/LH]

· F. DES DIA [FT and IN]

· G. DES PITCH AT 0.70R [FT and IN]

· H. MFR [Name and Date]

· I. CN [full manufacture contract number]

· J. WT [actual weight after balance] LBS

· K. NSN [XXXX-XX-XXX-XXXX]

· L. MAT [material, alloy, and spec]

· REP/BAL [Company name, MM/YY, including any previous history]

3.6.14 Document and submit all applicable RFV’s in…