N6449823R4000_RFP Conformed through 0002_LCS-1.pdf

SEE ADDENDUM

(No Collect Calls)

N6449823R4000 15-Mar-2023

b. TELEPHONE NUMBER

267-990-5870

8. OFFER DUE DATE/LOCAL TIME

04:00 PM 05 Jun 2025

5. SOLICITATION NUMBER 6. SOLICITATION ISSUE DATE

AUTHORIZED FOR LOCAL REPRODUCTION

PREVIOUS EDITION IS NOT USABLE

STANDARD FORM 1449 (REV. 2/2012)

Prescribed by GSA – FAR (48 CFR) 53.212

(TYPE OR PRINT)

(SIGNATURE OF CONTRACTING OFFICER)

ADDENDA ARE

26. TOTAL AWARD AMOUNT (For Gov t. Use Only )

23.

CODE 10. THIS ACQUISITION IS

SUCH ADDRESS IN OFFER

17b. CHECK IF REMITTANCE IS DIFFERENT AND PUT

BELOW IS CHECKED

TELEPHONE NO.

N644989. ISSUED BY

18b. SUBMIT INVOICES TO ADDRESS SHOWN IN BLOCK 18a. UNLESS BLOCK

7. FOR SOLICITATION

INFORMATION CALL:

a. NAME

MATTHEW D PARLETT

2. CONTRACT NO. 3. AWARD/EFFECTIVE DATE 4. ORDER NUMBER

(TYPE OR PRINT)

30b. NAME AND TITLE OF SIGNER 30c. DATE SIGNED 31b. NAME OF CONTRACTING OFFICER

30a. SIGNATURE OF OFFEROR/CONTRACTOR 31a.UNITED STATES OF AMERICA

27a. SOLICITATION INCORPORATES BY REFERENCE FAR 52.212-1. 52.212-4. FAR 52.212-3. 52.212-5 ARE ATTACHED.

25. ACCOUNTING AND APPROPRIATION DATA

1. REQUISITION NUMBER

20.

ADDITIONAL SHEETS SUBJECT TO THE TERMS AND CONDITIONS SPECIFIED.

OFFEROR TO COMPLETE BLOCKS 12, 17, 23, 24, AND 30

SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS

ARE NOT ATTACHED

27b. CONTRACT/PURCHASE ORDER INCORPORATES BY REFERENCE FAR 52.212-4. FAR 52.212-5 IS ATTACHED. ADDENDA ARE ARE NOT ATTACHED

(BLOCK 5), INCLUDING ANY ADDITIONS OR CHANGES WHICH ARE

SET FORTH HEREIN, IS ACCEPTED AS TO ITEMS:

. YOUR OFFER ON SOLICITATION

28. CONTRACTOR IS REQUIRED TO SIGN THIS DOCUMENT AND RETURN

% FOR:SET ASIDE:UNRESTRICTED ORX

SMALL BUSINESS

17a.CONTRACTOR/ CODE FACILITY

OFFEROR CODE

NAVAL SURFACE WARFARE CENTER PHILA

CODE 0231, MATTHEW PARLETT

267-990-5870, MATTHEW.D.PARLETT@NAVY.MIL

5001 SOUTH BROAD STREET

PHILADELPHIA PA 19112

18a. PAYMENT WILL BE MADE BY CODE

RATED ORDER UNDER

DPAS (15 CFR 700)

13a. THIS CONTRACT IS AX

13b. RATING

DO-A3

CODE15. DELIVER TO CODE 16. ADMINISTERED BY

SEE SCHEDULE

12. DISCOUNT TERMS11. DELIVERY FOR FOB DESTINA-

TION UNLESS BLOCK IS

MARKED

X SEE SCHEDULE

14. METHOD OF SOLICITATION

RFQ IFB RFPX

FAX:

TEL: 267-990-5870

SERVICE-DISABLED

VETERAN-OWNED

SMALL BUSINESS

8(A)

HUBZONE SMALL

BUSINESS

SIZE STANDARD:

$11,000,000

NAICS:

811310

OFFER DATED

29. AWARD OF CONTRACT: REF.

DELIVER ALL ITEMS SET FORTH OR OTHERWISE IDENTIFIED ABOVE AND ON ANY

COPIES TO ISSUING OFFICE. CONTRACTOR AGREES TO FURNISH AND

EMAIL:

TEL:

31c. DATE SIGNED

SEE SCHEDULE

SCHEDULE OF SUPPLIES/ SERVICESITEM NO. QUANTITY UNIT UNIT PRICE AMOUNT

24.22.21.19.

WOMEN-OWNED SMALL BUSINESS (WOSB)

ELIGIBLE UNDER THE WOMEN-OWNED

SMALL BUSINESS PROGRAM

EDWOSB

32g. E-MAIL OF AUTHORIZED GOVERNMENT REPRESENTATIVE

SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS

(CONTINUED)

PAGE 2 OF156

ACCEPTED, AND CONFORMS TO THE CONTRACT, EXCEPT AS NOTED: ______________________________________________________

32a. QUANTITY IN COLUMN 21 HAS BEEN

RECEIVED INSPECTED

32b. SIGNATURE OF AUTHORIZED GOVERNMENT

REPRESENTATIVE

32c. DATE 32d. PRINTED NAME AND TITLE OF AUTHORIZED GOVERNMENT

REPRESENTATIVE

32e. MAILING ADDRESS OF AUTHORIZED GOVERNMENT REPRESENTATIVE 32f . TELEPHONE NUMBER OF AUTHORIZED GOVERNMENT REPRESENTATIVE

37. CHECK NUMBER

FINALPARTIALCOMPLETE

36. PAYMENT35. AMOUNT VERIFIED

CORRECT FOR

34. VOUCHER NUMBER

FINAL

33. SHIP NUMBER

PARTIAL

38. S/R ACCOUNT NUMBER 39. S/R VOUCHER NUMBER 40. PAID BY

41a. I CERTIFY THIS ACCOUNT IS CORRECT AND PROPER FOR PAYMENT

41b. SIGNATURE AND TITLE OF CERTIFYING OFFICER 41c. DATE

42a. RECEIVED BY (Print)

42b. RECEIVED AT (Location)

42c. DATE REC'D (YY/MM/DD) 42d. TOTAL CONTAINERS

STANDARD FORM 1449 (REV. 2/2012) BACK

Prescribed by GSA – FAR (48 CFR) 53.212

AUTHORIZED FOR LOCAL REPRODUCTION

PREVIOUS EDITION IS NOT USABLE

SEE SCHEDULE

20.

SCHEDULE OF SUPPLIES/ SERVICES

21.

QUANTITY UNIT

22. 23.

UNIT PRICE

24.

AMOUNT

19.

ITEM NO.

N6449823R4000

Section A - Solicitation/Contract Form

NOTES

1. BASIS OF COMPETITION: A single Indefinite-Delivery, Indefinite-Quantity (IDIQ) Contract is intended to result from this solicitation. This requirement is being solicited on the basis of other than full and open competition to Rolls-Royce Marine North America, Inc. (RRMNA) in accordance with 10 U.S.C.

3204(a)(1).

2. MINIMUM & MAXIMUM: The guaranteed minimum is $500.00, to be satisfied by order of one (1) of

SLIN 0019AA. The contract maximum shall be the value of all CLINs to be determined at time of Contract award.

3. QUESTIONS: All questions regarding this solicitation shall be submitted in writing to

Michaela.C.DelRossi.civ@us.navy.mil, with a copy to Matthew.D.Parlett.civ@us.navy.mil, no later than

14 May 2025. Questions will be addressed during a subsequent pre-proposal teleconference on 21 May

2025.

mailto:Michaela.C.DelRossi.civ@us.navy.mil mailto:Matthew.D.Parlett.civ@us.navy.mil

Section B - Supplies or Services and Prices

ITEM NO SUPPLIES/SERVICES QUANTITY UNIT UNIT PRICE AMOUNT

TTE - 172AX MK1 Boost Waterjet

FFP

Teardown, Test, and Evaluation (TTE) for 172AX MK1 Boost Waterjet Assembly in accordance with the Performance Work Statement, Section C.

NSN: 2S 2010 01 622 3620

MFR PART NR: 6172252000

NET AMT

ITEM NO SUPPLIES/SERVICES MAX

QUANTITY

UNIT UNIT PRICE MAX AMOUNT

0001AA 2 Each Year 1 - TTE

FFP

Year 1 (from date of contract award through 12 months thereafter).

FOB: Origin (Shipping Point)

NSN: 2S 2010 01 622 3620

BRAND NAME/SOLE SOURCE: SS

PSC CD: J030

MAX

UNIT UNIT PRICE MAX AMOUNT

0001AB 4 Each Year 2 - TTE

FFP

Year 2 (from 12 months after date of contract award through 24 months thereafter).

FOB: Origin (Shipping Point)

NSN: 2S 2010 01 622 3620

BRAND NAME/SOLE SOURCE: SS

UNIT UNIT PRICE MAX AMOUNT

0001AC 6 Each Year 3 - TTE

FFP

Year 3 (from 24 months after date of contract award through 36 months thereafter).

FOB: Origin (Shipping Point)

NSN: 2S 2010 01 622 3620

BRAND NAME/SOLE SOURCE: SS

UNIT UNIT PRICE MAX AMOUNT

0001AD 6 Each Year 4 - TTE

FFP

Year 4 (from 36 months after date of contract award through 48 months thereafter).

FOB: Origin (Shipping Point)

NSN: 2S 2010 01 622 3620

BRAND NAME/SOLE SOURCE: SS

UNIT UNIT PRICE MAX AMOUNT

0001AE 6 Each Year 5 - TTE

FFP

Year 5 (from 48 months after date of contract award through 60 months thereafter).

FOB: Origin (Shipping Point)

NSN: 2S 2010 01 622 3620

BRAND NAME/SOLE SOURCE: SS

UNIT UNIT PRICE MAX AMOUNT

0002 UNDEFINED

TTE - 172AX MK1 Steerable Waterjet

FFP

Teardown, Test, and Evaluation for 172AX MK1 Steerable Waterjet Assembly in accordance with the Performance Work Statement, Section C.

NSN: 2S 2930 01 601 1649

MFR PART NR: 617252001

UNIT UNIT PRICE MAX AMOUNT

0002AA 2 Each TTE - Year 1

FFP

Year 1 (from date of contract award through 12 months thereafter).

FOB: Origin (Shipping Point)

NSN: 2S 2930 01 601 1649

UNIT UNIT PRICE MAX AMOUNT

0002AB 4 Each TTE - Year 2

FFP

Year 2 (from 12 months after date of contract award through 24 months thereafter).

FOB: Origin (Shipping Point)

NSN: 2S 2930 01 601 1649

UNIT UNIT PRICE MAX AMOUNT

0002AC 6 Each TTE - Year 3

FFP

Year 3 (from 24 months after date of contract award through 36 months thereafter).

FOB: Origin (Shipping Point)

NSN: 2S 2930 01 601 1649

UNIT UNIT PRICE MAX AMOUNT

0002AD 6 Each TTE - Year 4

FFP

Year 4 (from 36 months after date of contract award through 48 months thereafter).

FOB: Origin (Shipping Point)

NSN: 2S 2930 01 601 1649

UNIT UNIT PRICE MAX AMOUNT

0002AE 6 Each TTE - Year 5

FFP

Year 5 (from 48 months after date of contract award through 60 months thereafter).

FOB: Origin (Shipping Point)

NSN: 2S 2930 01 601 1649

UNIT UNIT PRICE MAX AMOUNT

0003 UNDEFINED

TTE - Impeller Drive Shaft

FFP

Teardown, Test, and Evaluation for Impeller Drive Shaft Assembly in accordance with the Performance Work Statement, Section C.

NSN: 7H 2010 01 632 6307

MFR PART NR: 617252003

UNIT UNIT PRICE MAX AMOUNT

0003AA 4 Each TTE - Year 1

FFP

Year 1 (from date of contract award through 12 months thereafter).

FOB: Origin (Shipping Point)

NSN: 7H 2010 01 632 6307

UNIT UNIT PRICE MAX AMOUNT

0003AB 8 Each TTE - Year 2

FFP

Year 2 (from 12 months after date of contract award through 24 months thereafter).

FOB: Origin (Shipping Point)

NSN: 7H 2010 01 632 6307

UNIT UNIT PRICE MAX AMOUNT

0003AC 12 Each TTE - Year 3

FFP

Year 3 (from 24 months after date of contract award through 36 months thereafter).

FOB: Origin (Shipping Point)

NSN: 7H 2010 01 632 6307

UNIT UNIT PRICE MAX AMOUNT

0003AD 12 Each TTE - Year 4

FFP

Year 4 (from 36 months after date of contract award through 48 months thereafter).

FOB: Origin (Shipping Point)

NSN: 7H 2010 01 632 6307

UNIT UNIT PRICE MAX AMOUNT

0003AE 12 Each TTE - Year 5

FFP

Year 5 (from 48 months after date of contract award through 60 months thereafter).

FOB: Origin (Shipping Point)

NSN: 7H 2010 01 632 6307

UNIT UNIT PRICE MAX AMOUNT

0004 24 Each Repair - 172AX MK1 Boost Waterjet

FFP

Repair of 172AX MK1 Boost Waterjet Assembly and Repackaging in accordance with the Performance Work Statement, Section C. To be negotiated at the Task

Order level once the Teardown, Test, and Evaluation work has been completed via delivery and approval CDRL # A006. To be ordered from date of contract award through 60 months thereafter.

NOTE: The requirements in DFARS 252.211-7003, Item Identification and

Valuation, are applicable for this line item. The contractor shall provide DoD unique identification or a DoD recognized unique identification equivalent.

FOB: Origin (Shipping Point)

NSN: 2S 2010 01 622 3620

UNIT UNIT PRICE MAX AMOUNT

0005 24 Each Repair - 172AX MK1 Steerable Waterjet

FFP

Repair of 172AX MK1 Steerable Waterjet Assembly and Repackaging in accordance with the Performance Work Statement, Section C. To be negotiated at the Task Order level once the Teardown, Test, and Evaluation work has been completed via delivery and approval CDRL # A006. To be ordered from date of contract award through 60 months thereafter.

NOTE: The requirements in DFARS 252.211-7003, Item Identification and

Valuation, are applicable for this line item. The contractor shall provide DoD unique identification or a DoD recognized unique identification equivalent.

FOB: Origin (Shipping Point)

NSN: 2S 2930 01 601 1649

UNIT UNIT PRICE MAX AMOUNT

0006 48 Each Repair - Impeller Drive Shaft

FFP

Repair of Impeller Drive Shaft Assembly and Repackaging in accordance with the

Performance Work Statement, Section C. To be negotiated at the Task Order level once the Teardown, Test, and Evaluation work has been completed via delivery and approval CDRL # A006.. To be ordered from date of contract award through

60 months thereafter.

NOTE: The requirements in DFARS 252.211-7003, Item Identification and

Valuation, are applicable for this line item. The contractor shall provide DoD unique identification or a DoD recognized unique identification equivalent.

FOB: Origin (Shipping Point)

NSN: 7H 2010 01 632 6307

UNIT UNIT PRICE MAX AMOUNT

0007 1 Lot

OVER & ABOVE

FFP

See DFARS 252.217-7028. To Be Negotiated (TBN). No pricing needed at this time.

FOB: Destination

UNIT UNIT PRICE MAX AMOUNT

0008 72 Each

TECHNICAL DATA - CDRL A001

FFP

Technical Data in accordance with Contract Data Requirements List (CDRL)

A001 – Contract Status Report - DD Form 1423. Not Separately Priced (NSP).

0009 1 Each

TECHNICAL DATA - CDRL A002

FFP

Technical Data in accordance with CDRL A002 – Inspection and Test Plan - DD

Form 1423. NSP.

See Exhibit B

0010 1 Each

TECHNICAL DATA - CDRL A003

FFP

Technical Data in accordance with CDRL A003 – Welding Procedure

Qualification Test Report - DD Form 1423. NSP.

See Exhibit C

UNIT UNIT PRICE MAX AMOUNT

0011 1 Lot

TECHNICAL DATA - CDRL A004

FFP

Technical Data in accordance with CDRL A004 – Request For Waivers - DD

Form 1423. NSP.

See Exhibit D

UNIT UNIT PRICE MAX AMOUNT

0012 192 Each

TECHNICAL DATA - CDRL A005

FFP

Technical Data in accordance with CDRL A005 – Visual Preservation Report -

DD Form 1423. NSP.

See Exhibit E

UNIT UNIT PRICE MAX AMOUNT

0013 96 Each

TECHNICAL DATA - CDRL A006

FFP

Technical Data in accordance with CDRL A006 – Pre-Repair Report - DD Form

1423. NSP.

See Exhibit F

UNIT UNIT PRICE MAX AMOUNT

0014 96 Each

TECHNICAL DATA - CDRL A007

FFP

Technical Data in accordance with CDRL A007 – Final Repair Report - DD Form

1423. NSP.

See Exhibit G

UNIT UNIT PRICE MAX AMOUNT

0015 96 Each

TECHNICAL DATA - CDRL A008

FFP

Technical Data in accordance with CDRL A008 – Certification Data Report - DD

Form 1423. NSP.

See Exhibit H

UNIT UNIT PRICE MAX AMOUNT

0016 96 Each

TECHNICAL DATA - CDRL A009

FFP

Technical Data in accordance with CDRL A009 – GFP Report Periodic - DD

Form 1423. NSP.

UNIT UNIT PRICE MAX AMOUNT

0017 96 Each

TECHNICAL DATA - CDRL A010

FFP

Technical Data in accordance with CDRL A010 – GFP Report Final - DD Form

1423. NSP.

See Exhibit K

UNIT UNIT PRICE MAX AMOUNT

0018 12 Each

TECHNICAL DATA - CDRL A011

FFP

Technical Data in accordance with CDRL A011 – Small Business Utilization

Report - DD Form 1423. NSP.

FOB: Origin (Shipping Point)

See Exhibit L

UNIT UNIT PRICE MAX AMOUNT

0019 UNDEFINED

TECHNICAL DATA - CDRL A012

FFP

Technical Data in accordance with CDRL A012 – Quality Management System -

DD Form 1423.

See Exhibit M

UNIT UNIT PRICE MAX AMOUNT

0019AA 1 Each

GUARANTEED MINIMUM - CDRL A012

FFP

To be ordered at time of base contract award.

UNIT UNIT PRICE MAX AMOUNT

0019AB 23 Each

TECHNICAL DATA - CDRL A012

FFP

Technical Data in accordance with CDRL A012 – Quality Management System -

DD Form 1423. NSP.

0020 1 Each

TECHNICAL DATA - CDRL A013

FFP

Technical Data in accordance with CDRL A013 – Thermal Spray Procedure - DD

Form 1423. NSP.

See Exhibit N

Section C - Descriptions and Specifications

Performance Work Statement (PWS) for

Repair of LCS-1 Class Waterjet and Impeller Drive Shaft Assemblies

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 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.

1.0.4.4.2 The Contracting Officer will, within five (5) calendar days after receipt of notice, respond to the notice in writing. In responding, the Contracting Officer will either:

(i) Confirm the conduct is in violation and when necessary direct the mode of further performance,

(ii) Countermand any communication regarded as a violation,

(iii) Deny that the conduct constitutes a violation and when necessary direct the mode of further performance, or

(iv) In the event the notice is inadequate to make a decision, advise the Contractor what additional information is required, and establish the date by which it should be furnished by the Contractor.

1.1 BACKGROUND

The Propulsion Systems Division, Code 42, of the Naval Surface Warfare Center, Philadelphia Division

(NSWPCD), is responsible for maintaining a ready-for-issue rotatable pool of waterjet and impeller shaft assemblies to support Freedom Class Littoral Combat Ship (LCS-1) hulls.

1.2 SCOPE OF WORK

The scope of this contract is to perform the repair of the following US Navy National Stock Numbers (NSN):

Asset NSN

172AX MK1 Boost Waterjet Assembly 2S 2010 01 622 3620

172AX MK1 Steerable Waterjet Assembly 2S 2930 01 601 1649

Impeller Drive Shaft Assembly 2S 2010 01 632 6307

Re-packaging of 172AX MK1 Boost and 172AX

MK1 Steerable Waterjet Assembly

Re-packaging of Impeller Drive Shaft Assembly

2.0 APPLICABLE DOCUMENTS

2.1 The following Specifications are considered part of this contract as specified herein.

REF SPECIFICATION NUMBER REV DATE

A NAVSEA T9074-AS-GIB-010/271

B NAVSEA S9074-AQ-GIB-010/248

C ASQ/ANSI/ISO 9001

D NAVSEA S9086-HR-STM-010

NSTM 247 Waterjets

E RRMNA NWI SP 4.1-003 1 23 AUG 2019

F MIL-STD-2035

G S9245-AR-TSM-010

H RRMNA NWI SP 4.1-009 1 07 AUG 2019

I RRMNA NWI SP 3-008 3 1 APR 2020

J RRMNA NWI SP 4.1-008 1 07 AUG 2019

K NAVSEA S9247-AT-MMC-010

L NAVSEA S9074-AR-GIB-010/278

M MIL-STD-2191

N RRNMA 172 Axial MKI Waterjet Overhaul and

Installation Kit

O ISO 1940/1

P RRMNA DWG 617252002 C 10 FEB 2012

Q NAVSEA DWG 53711-631-8534685

R DoD Manual 4140.65

S MIL-DTL-2845

T International Standards for Phytosanitary

Measures (ISPM) No. 15

U RRMNA DWG J-20-2-63 E 27 MAR 2023

V RRNMA DWG J-20-3-22 B 27 MAR 2023

W RRNMA DWG J-20-2-70 B 27 MAR 2023

2.2 The following forms are considered part of this contract as specified herein. All forms can be found at https://www.dcma.mil/NPP/forms.aspx

NUMBER TITLE

9247/005 LCS FRE Variant Impeller Drive Shaft Assembly Visual Preservation Inspection

9247/006 LCS FRE Variant Waterjet Assembly Visual Preservation Inspection Report

9247/007 LCS FRE Variant Waterjet and Impeller Drive Shaft Assembly Visual Technical

Inspection Report

2.3 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.

2.4 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.

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

3.0. REQUIREMENTS

3.1 General

3.1.1 Unless otherwise specified in the contract or task order, the Contractor is responsible for the performance of all inspection requirements as specified herein. Except as otherwise specified in the contract or task order, the Contractor may use its own or any other facilities suitable for the performance of the inspection requirements 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 If at any time during the pre-repair inspection or repair process, the Contractor determines that the

Impeller Drive Shaft Assembly, Waterjet Assembly, or any component which is not identified in

Reference N may be beyond economical repair (BER), the Contractor shall immediately notify the technical point of contact and provide a description of the Impeller Drive Shaft Assembly or

Waterjet Assembly condition. More than seventy-five percent (75%) of the Impeller Drive Shaft

Assembly or Waterjet Assembly replacement cost is considered BER for purposes of this paragraph.

3.1.3 If damage is identified due to shipping or packaging deficiencies or if the items are not preserved, packaged, packed, marked and transported in accordance with Reference D, the Contractor shall https://www.dcma.mil/NPP/forms.aspx submit a report of discrepancy (ROD), Form SF 364, in accordance with SECNAVINST 4355.18, within 30 days of receipt of any government furnished material (GFM).

3.1.4 For any work that is to be performed on the Impeller, the Contractor shall utilize personnel who have successfully completed the NAVSEA Propeller Visual Inspection Course. For cleaning, painting, packaging, and preserving, personnel do not have to successfully complete this course.

3.1.5 The Contractor shall utilize Nondestructive testing (NDT) personnel, procedures, and equipment, which are qualified in accordance with Reference A to be used for this contract, where necessary.

3.1.6 The Contractor shall utilize qualified welding procedures and operators in accordance with

Reference B, where necessary.

3.1.7 The Contractor shall utilize a qualified management system in accordance with Reference C.

3.1.8 The Contractor shall provide all drawings necessary to understand all results and reports that are provided per 3.2 and C.3.3.

3.1.9 The Contractor shall take and record all measurements in metric units.

3.1.10 Prior to any assessment, all non-weld filler material, previously applied shall be removed. Prior approved thermal spray does not need to be removed, unless repairs are necessary.

3.1.11 Non-weld filler material shall not be used as a repair method. Thermal spray may be considered for shaft repair, pending NAVSEA approval.

3.1.12 For all thread inspections, clean and inspect threaded parts for burnished, galled, crossed, torn, cracked, deformed or missing threads. All thread damage shall be documented. Thread damage may be acceptable if it can be repaired by handwork methods so that free fit threads engage by hand with no excessive play. Thread damage which extends to the root of a male thread is not acceptable. Stretched threads are also not acceptable. Use mating part to check threads.

3.1.13 Digital pictures of the entire Waterjet Assembly and Impeller Drive Shaft Assembly from two sides shall be taken before and after repair. Close-ups of any damaged areas, including painting, shall be provided throughout the pre-repair and repair stages. Digital pictures shall be taken depicting the before and after conditions of any area repaired. Pictures shall be labeled with asset serial number, location on asset, date, repair activity, and any other information to clearly identify the repair area and condition.

3.2 WATERJET ASSEMBLY AND IMPELLER DRIVE SHAFT ASSEMBLY REPAIR

3.2.1 Pre-Repair Inspection of Waterjet Assembly and Impeller Drive Shaft Assembly

3.2.1.1 Upon receipt of each Impeller Drive Shaft Assembly and Waterjet Assembly, the Contractor shall perform and document an initial Visual Preservation Inspection (VPI) in accordance with Reference D. Inspection results shall be documented using NAVSEA Forms 9247/5 and

9247/6 and reported in accordance with CDRL A005.

3.2.1.2 Each Impeller Drive Shaft Assembly and Waterjet Assembly shall be initially cleaned in accordance with Reference D. Initial cleaning shall remove all marine growth, but should leave any paint undisturbed.

3.2.1.3 After assemblies have been cleaned free of marine growth, a visual inspection of painted surfaces shall be performed. All defects shall be identified and size shall be quantified.

Documented results shall be reported in accordance with CDRL A006.

3.2.1.4 For locations where removal of paint is required to perform NDT inspections, cleanliness requirements shall be in accordance with NACE SSPC-SC 5 for abrasive blasting or NACE

SSPC-SC WJ-1 for hydroblasting. If abrasive blasting is used, blast media used shall be selected such that the blast process shall leave as much of the surface profile as possible while still being able to perform NDT inspections, with at least a blast profile of 2.0 to 4.0 mil. The blast process shall also minimize the need for additional blasting to re-establish the surface profile to allow for painting post repair.

3.2.1.5 Each Impeller Drive Shaft Assembly shall be inspected in accordance with Attachment 4.

Acceptance criteria shall be in accordance with the applicable component drawing and as outlined in Attachment 4. Results shall be reported in accordance with CDRL A006.

3.2.1.6 All paint and coatings shall be removed prior to pre-repair VTI inspections. The contractor is permitted to perform PT inspections on welded areas after paint and coatings are removed.

3.2.1.7 A complete Visual Technical Inspection (VTI) shall be performed for each Impeller in accordance with Reference D, and the applicable component drawing. All defects shall be identified. Results shall be documented using NAVSEA Form 9247/7 and reported in accordance with CDRL A006.

3.2.1.7.1 For the Impeller Sleeve, a thread inspection shall also be performed.

3.2.1.8 Liquid Penetrant (PT) inspection shall be performed for each Impeller and Impeller Sleeve in accordance with Reference A and applicable component drawing. Acceptance criteria shall be in accordance with Reference F table IV, Reference G Chapter 6 Class 2, and applicable component drawing. If there are any conflicting requirements, applicable component drawing shall take precedence. All defects shall be identified. Results shall be documented and reported in accordance with CDRL A006.

3.2.1.9 Each Impeller shall be dimensionally checked in accordance with Reference H. Acceptance criteria shall be in accordance with Reference H. Calculations associated with impeller mounting in Reference I shall be performed based on repair proposal to verify proposal will result in appropriate post-repair fit-up. Results shall be documented and reported in accordance with CDRL A006.

3.2.1.9.1 For the Impeller Sleeve, measure all critical sleeve dimensions in accordance with applicable component drawing. Calculations associated with impeller mounting in

Reference I shall be performed based on repair proposal to verify proposal will result in appropriate post-repair fit-up.

3.2.1.10 A complete Visual Technical Inspection (VTI) shall be performed for each Waterjet

Assembly in accordance with Reference D, and the applicable component drawing. In addition all sub-bullet tasks shall be performed. All defects shall be identified, and results shall be documented using NAVSEA Form 9247/7 and reported in accordance with CDRL

A006.

3.2.1.10.1 For each Stator, perform thread inspection of Stator End Cone mounting holes, Hub

Bearing cooling water fittings, and lift points.

3.2.1.10.2 For each Stator End Cone, perform thread inspection of lifting fixture hole.

3.2.1.10.3 For each Steerable Waterjet Steering Nozzle, perform thread inspection of mounting holes for covers of Slew Link and Upper Reversing Bucket connection joints.

3.2.1.10.4 For each Steerable Waterjet Upper Reversing Bucket, perform thread inspection of mounting holes for covers of Lower Reversing bucket connection joints.

3.2.1.10.5 For each Steerable Waterjet Lower Reversing Bucket, perform thread inspection of covers of Slew Link connection joint.

3.2.1.10.6 For each Steerable Waterjet Hydraulic Hose Manifold, perform thread inspection of all hose connection mounting holes.

3.2.1.10.7 For each Steerable Waterjet Steering and Reversing Cylinder, perform thread inspection of hose mounts, Lock Screw hole, Feed Pipe, Valve mount, Valve Cover mount, Feed Pipe block mount, and the Head.

3.2.1.10.8 For each Steerable Waterjet Guide Pin, Steering/Steering Cylinder Pin, Upper

Bucket Pin, Lower Bucket Pin, Slew Link Pin, Reversing Pin, Feedback Cable Pin, and Pump Alignment Pin, perform thread inspection of applicable puller holes.

3.2.1.11 Liquid Penetrant (PT) inspection shall be performed for each Waterjet Assembly in accordance with Reference A in the areas listed below. Acceptance criteria shall be in accordance with Reference F, Section 7, Class 2 and applicable component drawing. If there are any conflicting requirements, applicable component drawing shall take precedence.

Results shall be documented and reported in accordance with CDRL A006.

3.2.1.11.1 For each Stator, PT inspection shall be performed in critical areas as specified by applicable component drawing, as well as all Hub Bearing Assembly landing surfaces, Pump Alignment Pin recesses, Lift Points, Stator Flange Bushings, Guide

Pin holes, and Steering Pin holes.

3.2.1.11.2 For each Stator End Cone, PT inspection shall be performed on mating surface and mounting bolt holes.

3.2.1.11.3 For each Impeller Housing, PT inspection shall be performed in critical areas as specified by applicable component drawing. Calculations associated with impeller tip clearances shall be performed based on repair proposal to verify proposal will result in appropriate post-repair fit up.

3.2.1.11.4 For each Boost and Steerable Nozzle Extension, PT inspection shall be performed in critical areas as specified by reference E.

3.2.1.11.5 For each Shock Retention Bracket, PT inspection shall be performed on the entire bracket.

3.2.1.11.6 For each Boost Waterjet Pump Alignment Pin, PT inspection shall be performed on the entire pin.

3.2.1.11.7 For each Steerable Waterjet Steering Nozzle, PT inspection shall be performed in critical areas as specified by reference E, as well as all Guide Pin holes/holders, Steering Pin holes/holders, Reversing Pin holes, Upper Bucket Pin holes, Slewing

Link Pin holes, and welds around Nozzle Link Boss.

3.2.1.11.8 For each Steerable Waterjet Upper Reversing Bucket, PT inspection shall be performed on all Upper Bucket Pin holes, Lower Bucket Pin holes, Reversing Pin holes, and on all welds between Bucket Pivot Boss and Bucket Side Plates, Bucket

Side Plates and Bucket Beam, and Bucket Side Plates and Bucket Flow Plate.

3.2.1.11.9 For each Steerable Waterjet Lower Reversing Bucket, PT inspection shall be performed on all Lower Bucket Pin holes and Slewing Pin holes.

3.2.1.11.10 For each Steerable Waterjet Slewing Link, PT inspection shall be performed on all

Internal and Exterior Slewing Link Pin hole surfaces.

3.2.1.11.11 For each Steerable Waterjet Guide Pin, Steering/Steering Cylinder Pin, Upper and Pump Alignment Pin, PT inspection shall be performed on entire pin.

3.2.1.12 For each Waterjet Assembly, dimensional inspections shall be performed in accordance with

Reference D and all applicable drawings, in areas specified below. All results shall be reported in accordance with CDRL A006, and shall include design dimension, allowable tolerance, and measured dimension.

3.2.1.12.1 For each stator, dimensions shall be taken for all Hub Bearing Assembly landing surfaces, Pump Alignment Pin recesses, Lift Points, Guide Pin holes, and Steering

Pin holes.

3.2.1.12.2 For each Stator End Cone, dimensions shall be taken for interfacing pilot to the hub bearing assembly.

3.2.1.12.3 For each Impeller Housing, inside diameter shall be measured in accordance with component drawing.

3.2.1.12.4 For each Boost and Steerable Nozzle Extension, measure flatness and surface finish of flanges interfacing to the stator.

3.2.1.12.5 For each Steerable Waterjet Steering Nozzle, perform dimensional inspection of holes for guide pins, cylinder pins, and pins for upper reversing bucket and slew link joints.

3.2.1.12.6 For each Steerable Waterjet Upper Reversing Bucket, perform dimensional inspection of holes for guide pins, cylinder pins, and pins for upper reversing bucket and slew link joints.

3.2.1.12.7 For each Steerable Waterjet Lower Reversing Bucket, perform dimensional inspection of holes for pins for upper reversing bucket and slew link joints.

3.2.1.12.8 For each Steerable Waterjet Slewing Link, dimensions shall be taken for all Slewing

Link Pin holes.

3.2.1.12.9 For each Steerable Waterjet Steering and Reversing Cylinder, dimensions shall be taken in accordance with applicable component drawing.

3.2.1.12.10 For each Steerable Waterjet Guide Pin, Steering/Steering Cylinder Pin, Upper and Pump Alignment Pin, dimensions shall be taken of all applicable retaining ring grooves and pin shoulder details. Also, each pin’s overall diameter shall be taken at 3 locations, one in each third of the pin length.

3.2.1.12.11 A visual and dimensional inspection of the water lubricated bearing assembly shall be performed, including inside diameter measurements between diametrically opposed bearing pad surfaces (six total locations circumferentially) and surface finish of each bearing pad surface (twelve total locations circumferentially).

Diameter and surface finish measurements shall be repeated for a total of three sets of measurements along the length of the bearing (forward, middle, aft).

3.2.1.13 For sealing surfaces, acceptance criteria shall be in accordance with applicable component drawing. In addition, should a sealing surface contain a leakage path across

50% or greater of the seal contact width, that shall be deemed unsatisfactory.

3.2.1.14 If an unsatisfactory scan, visual, dimensional, or NDT inspection is due to product quality deficiencies, a product quality deficiency report (PQDR), Form SF 368 shall be submitted in accordance with CDRL A006.

3.2.1.15 The contractor shall submit a repair plan, including all anticipated repairs, cost, and estimated repair timeline with CDRL A006.

3.2.1.16 All design modifications that have been incorporated for new construction shall be incorporated during this overhaul period if modification has not been accomplished yet.

If the contractor believes a design modification should NOT be incorporated, justification should be provided as part of CDRL A006.

3.2.1.17 If there are any known or anticipated deviations the Contractor shall submit a Request for

Deviation/Waiver in accordance with CDRL A004 on a case by case basis. This shall include the effect on performance, function, reliability, durability, integrated logistics support, interface, and/or software. The contractor shall also include engineering rationale as to why such effects are technically acceptable.

3.2.1.18 Upon completion of all inspections, the Contractor shall prepare and submit a Pre-Repair

Inspection Report in accordance with CDRL A006.

3.2.2 Repair of Waterjet Assembly and Impeller Drive Shaft Assembly

3.2.2.1 Upon approval of CDRL A006, the Contractor shall repair Impeller Drive Shaft Assembly and Waterjet Assembly in accordance with approved repair plan, Reference K, the applicable component drawing, and Attachment 4. When repair tolerances are not specified, new manufacturing tolerances shall be met.

3.2.2.2 All welding shall be in accordance with Reference L, Class M-1, Category A.

3.2.2.2.1 For propulsion shafting, if welding is to be used as a repair method, requirements outlined in Attachment 4 apply.

3.2.2.3 If the Contractor would like to use thermal spray as a method of repairing the shaft, a procedure must be submitted and approved by NAVSEA prior to use.

3.2.2.4 For sealing surfaces, minor hand repair may be used to repair or restore a part to usable condition. Method of repair shall be stated in the repair proposal.

3.2.2.5 Internal threads may be repaired by re-tapping provided loss of threads does not exceed 10% or by welding, drilling, and tapping. External threads may be repaired by chasing or by welding and re machining. Replace nylon pellets. Threaded parts shall be replaced if repair is considered uneconomical. MolyKote and similar compounds shall not be used on threaded fasteners in contact with hydraulic fluid.

3.2.2.6 For each Impeller Sleeve and Hub Bearing Sleeve, if sleeve is installed and does not meet all acceptance criteria, the Contractor shall replace the sleeve.

3.2.2.7 For each Stator, Stator Vane leading edge gage profiles may be used to guide repair of those areas.

3.2.2.8 For each Stator, Impeller Housing, Nozzle Extension, Steering Nozzle, Upper Reversing

Bucket, Lower Reversing Bucket, and Slewing Link, masking for paint shall be accomplished in accordance with an instruction/specification that shall be submitted by RR for review and approval. Once approved, PWS will be updated with reference details.

3.2.2.9 The Contractor shall replace all components in Reference N.

3.2.2.10 Upon completion of repairs, the Contractor shall balance Impellers as a separate component in accordance to References O and P. All results, including original unbalance, remaining residual unbalance, and calculated allowable unbalance shall be documented and reported in accordance with CDRL A007.

3.2.2.11 Upon completion of all repairs, the Contractor shall perform all pre-repair inspections specified in C.3.2.1. All results shall be documented and reported in accordance with CDRL

A007.

3.2.2.12 Upon completion of all repairs and satisfactory post-repair inspections, the Contractor shall reassemble each Waterjet Assembly and Impeller Drive Shaft Assembly. Impeller Drive Shaft

Assembly shall be reassembled using Reference I.

3.2.2.13 Upon completion of reassembly, operational tests shall be performed in accordance with

Reference J. All results shall be documented and reported in accordance with CDRL A007.

3.2.2.14 The Contractor shall submit a Request for Deviation/Waiver in accordance with CDRL A004 on a case by case basis. This shall include the effect on performance, function, reliability, durability, integrated logistics support, interface, and/or software. The contractor shall also include engineering rationale as to why such effects are technically acceptable.

3.2.2.15 Upon completion of all repairs, balancing, post-repair inspections, reassembly, and operational tests, the Contractor shall prepare and submit a Final Repair Report in accordance with CDRL A007.

3.2.2.16 Upon approval of CDRL A007, the Contractor shall paint each Impeller Drive Shaft

Assembly and Waterjet Assembly in accordance with an instruction/specification that shall be submitted by RR for review and approval. Once approved, PWS will be updated with reference details.

3.2.2.17 Upon approval of CDRL A007, the Contractor shall preserve, package, pack, and mark the

Impeller Drive Shaft Assembly and Waterjet Assembly in accordance with References R, S, T, U, V, and W. If there is any conflicting information, References U, V, and W take precedence.

3.2.2.17.1 Each asset shall be stamped to include the following on each major component

3.2.2.17.1.1 Nomenclature:

3.2.2.17.1.2 NSN:

3.2.2.17.1.3 PN:

3.2.2.17.1.4 Government Assembly S/N:

3.2.2.17.2 Government Assembly S/N will be provided after approval of CDRL A006.

3.2.2.18 Waterjet Assembly and Impeller Drive Shaft Assembly crates shall be built in accordance with Reference S, U, V, and W.. The following conditions must also be met:

3.2.2.18.1 The ability to use sling points and fork lift points shall be required in the packaging design. Fork lift capabilities shall meet the following: fork spread of 60" and the forks themselves 12" wide and 4" thick.

3.2.2.18.2 Components deemed as “Crated for ship install,” as defined in Reference N, shall be packaged in accordance with References R, S, and T, and included in the Waterjet

Assembly crate to be used upon delivery to the ship.

3.2.2.19 Upon completion of preservation, packaging, packing, and marking of each Impeller Drive

Shaft Assembly and Waterjet Assembly, the Contractor shall perform a final VPI in accordance with Reference K. Inspection results shall be documented and reported in accordance with CDRL A005.

3.2.2.20 For each Impeller Drive Shaft Assembly and Waterjet Assembly, the contractor shall submit a

Certification Report in accordance with CDRL A008 and a copy of the report shall be attached to each Assembly container in accordance with Reference S.

3.2.2.21 A copy of the signed Certification Report, the latest VTI, VPI and final approved repair report of the Impeller Drive Shaft Assembly and Waterjet Assembly, shall be packaged with asset for final delivery.

3.3 ASSEMBLY RE-PACKAGING

3.3.1 If at any time an Assembly needs to be re-packaged outside of efforts explained in Sections C.3.1 and C.3.2, the following shall be utilized.

3.3.2 During packaging of each Impeller Drive Shaft Assembly and Waterjet Assembly, the Contractor shall perform and document an initial Visual Preservation Inspection (VPI) in accordance with

Reference D. An inventory of any loose parts shall be documented. Inspection results shall be documented and reported in accordance with CDRL A005.

3.3.3 The Contractor shall clean each Impeller Drive Shaft Assembly and Waterjet Assembly, in accordance with Reference D.

3.3.4 The Contractor shall preserve, package, pack, and mark the Impeller Drive Shaft Assembly and

Waterjet Assembly in accordance with References R, S, T, U, V, and W. If there is any conflicting information, References U, V, and W take precedence.

3.3.5 Waterjet Assembly and Impeller Drive Shaft Assembly crates shall be built in accordance with

Reference S, U, V, and W. The following conditions must also be met:

3.3.5.1 The ability to use sling points and fork lift points shall be required in the packaging design.

Fork lift capabilities shall meet the following: fork spread of 60" and the forks themselves 12" wide and 4" thick.

3.3.5.2 Components deemed as “Crated for ship install,” as defined in Reference M, shall be packaged in accordance with References R, S, and T, and included in the Waterjet Assembly crate to be used upon delivery to the ship.

3.3.6 Upon completion of preservation, packaging, packing, and marking of each Impeller Drive Shaft

Assembly and Waterjet Assembly, the Contractor shall perform a final VPI in accordance with

Reference K. Inspection results shall be documented and reported in accordance with CDRL

A005.

3.3.7 A copy of the latest VPI of the Impeller Drive Shaft Assembly and Waterjet Assembly shall be packaged with asset for final delivery.

3.4 Manufacturing Phase-Out or Discontinuation of Production, Diminishing Sources, and Obsolete

Materials or Components

3.4.1 The contractor shall notify the contracting officer immediately upon determining the unavailability of obsolete materials or components. The contractor may recommend a solution to include the impact on the contract price and delivery. The contractor shall not initiate any item redesign or incur any additional costs without the express, written authorization of the contracting officer.

4.0 DATA REQUIREMENTS

4.1. Contract Status Report (CDRL A001)

4.2. Inspection System Program and Test Report (CDRL A002)

4.2.1. The Contractor shall prepare and submit an Inspection System Program and Test Plan in accordance with Data Item Description DI-QCIC-81110, as modified, referenced on Contract Data Requirements

List DD Form 1423.

4.2.2. Plan shall include the contractor’s quality system procedures that meet the requirements of Reference

C.

4.2.3. The contractor shall submit inspection and test procedures for the inspection and testing of Impeller

Drive Shaft Assembly, and Waterjet Assembly in accordance with contract requirements. If the contractor wishes to make any changes to these documents after submittal, they shall make these proposals to the Government for review and approval.

4.2.4. Test Procedures. The Contractor shall submit procedures for all inspections and tests planned to demonstrate that the specified requirements will be met.

4.3. Weld Procedures and Qualification Test Report (CDRL A003)

4.3.1. The Contractor shall submit welding procedures that apply to the repair of Impeller Drive Shaft

Assembly and Waterjet Assembly. Prior to performing any welding (production or repair), the applicable welding procedure qualification data shall be submitted and approved in accordance with

Data Item Description DI-MISC-80876, as modified, listed on Contract Data Requirements List DD

Form 1423. Welding procedures shall be submitted for information with the supporting procedure qualification data.

4.3.2. Submit copies of all welding procedures and performance qualification data prior to performance of welding. The contractor shall submit welding procedures that apply only to the repair of Impeller

Drive Shaft Assembly, and Waterjet Assembly. In addition, provide a copy of any previous Navy approval of procedures relating to welding. The approval letter must reference the applicable welding procedure and/or welding procedure qualification data number. Submission of welding procedures and qualification data is not required for tack/spot welds.

4.3.3. Welder Performance Qualification. The Contractor shall submit welder performance qualification records in accordance with Reference B.

4.4. Request for Deviation / Waiver (CDRL A004)

4.4.1. The contractor shall submit a request for deviation/waiver for all anticipated unrepairable and/or out of tolerance conditions that are not recommended to be repaired. Format and content shall be in accordance with ANSI EIA-649. The contractor shall utilize DD Form 1694 for submission of all requests.

4.4.2. DD Form 1694 shall include the effect on performance, function, reliability, durability, integrated logistics support, interface, and/or software. The contractor shall also include engineering rationale as to why such effects are technically acceptable.

4.4.3. Requests shall be submitted for pre-existing conditions found during initial inspections and during any repair if necessary.

4.5. Visual Preservation Inspection (VPI) (CDRL A005)

4.5.1. The contractor shall submit visual inspection reports for pre and post repaired conditions.

4.5.2. For Impeller Drive Shaft Assembly, a visual preservation inspection (VPI) report, NAVSEA Form

9247/5 shall be completed and submitted.

4.5.3. Form Waterjet Assembly, a visual preservation inspection (VPI) report, NAVSEA Form 9247/6 shall be completed and submitted.

4.5.4. In addition to submittal in accordance with DD-1423-1, a copy of each Visual Inspection shall be submitted via email to NSWCPD C/427 & C/423.

4.6. Pre-Repair Report (CDRL A006)

4.6.1. A paint inspection of all painted surfaces shall be completed and submitted.

4.6.2. For each Impeller Drive Shaft Assembly, a pre-repair visual technical inspection (VTI) report, NAVSEA form 9247/7 shall be completed and submitted.

4.6.3. For each Waterjet Assembly, a pre-repair visual technical inspection (VTI) report, NAVSEA form

9247/7 shall be completed and submitted.

4.6.4. Each pre-repair Dimensional Inspection Report shall include all data, information, and associated calculations from measurements of the items to demonstrate the conformance to all dimensions, inspections, tolerances, and other requirements specified by the applicable technical requirements.

4.6.4.1. For Impeller Shaft, a dimensional inspection report in the Contractor’s format shall be completed and submitted. Report format shall be prior approved by NAVSEA C/427.

4.6.4.2. For Impeller, a dimensional inspection report in the Contractor’s format shall be completed and submitted. Report format shall be prior approved by NAVSEA C/427.

4.6.4.3. For Waterjet Assembly, a dimensional inspection report in the Contractor’s format shall be

4.6.5. If an unsatisfactory visual or dimensional inspection is due to product quality deficiencies, a product quality deficiency report (PQDR), Form SF 368 shall be submitted.

4.6.6. A complete list of anticipated requests for deviation/waiver shall be completed and submitted.

4.6.7. A repair plan, including all anticipated repairs and estimated repair timeline shall be completed and submitted.

4.7. Final Repair Report (CDRL A007)

4.7.1. A summary of all accomplished repairs shall be submitted in the Contractor’s format. Report format shall be prior approved by NAVSEA C/427.

4.7.2. All applicable stress relief documentation shall be included in the Final Repair Report.

4.7.3. For Impeller Drive Shaft Assembly, a post-repair visual technical inspection (VTI) report, NAVSEA

Form 9247/7 shall be completed and submitted.

4.7.4. For Waterjet Assembly, a post-repair visual technical inspection (VTI) report, NAVSEA Form

9247/7 shall be completed and submitted.

4.7.4.1. A post-repair VTI report shall be completed prior to final coating and submitted with CDRL

A007.

4.7.4.2. A post-repair visual inspection shall be completed after final coating is applied and submitted with CDRL A007.

4.7.5. Each post-repair Dimensional Inspection Report shall include all data, information, and associated calculations from measurements of the items to demonstrate the conformance to all dimensions, inspections, tolerances, and other…