SOLICITATION NOTICE
48 -- 48--VALVE,BALL, IN REPAIR/MODIFICATION OF
- Notice Date
- 7/5/2022 8:31:48 AM
- Notice Type
- Solicitation
- NAICS
- 333999
— All Other Miscellaneous General Purpose Machinery Manufacturing
- Contracting Office
- NAVSUP WEAPON SYSTEMS SUPPORT MECH MECHANICSBURG PA 17050-0788 USA
- ZIP Code
- 17050-0788
- Solicitation Number
- N0010422QZB82
- Response Due
- 7/31/2022 9:00:00 PM
- Archive Date
- 08/16/2022
- Point of Contact
- Telephone: 7176057562
- E-Mail Address
-
AMANDA.SWIGONSKI@NAVY.MIL
(AMANDA.SWIGONSKI@NAVY.MIL)
- Description
- CONTACT INFORMATION|4|N742.4|WV2|(717) 605-7562|amanda.a.swigonski.civ@us.navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2022)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|see specification sections C & E | INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8|X||X|||||| INSPECTION/ACCEPTANCE POINT|6||||||| REPAIR DELIVERY (FIRM FIXED PRICE)|1|90| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Material - Invoice & Receiving Report (COMBO) Certifications - Stand-Alone Receiving Report|Material - Inspection & Acceptance at SOURCE Certifications - Inspection at DESTINATION & Accept ance at OTHER |TBD|N00104|TBD|Material-S4306A; Certifications-N39040|N50286|TBD|Code 133.2|N/A|N/A|Certifications-N39040|N/A|N/A|See DD Form 1423|PORT_PTNH_WAWF_Notification@navy.mil| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| FIRM FIXED PRICE REPAIR PURCHASE ORDERS|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|one year from date of delivery|one year from date of delivery ||||| WARRANTY OF DATA--BASIC (MAR 2014)|2||| BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC(DEVIATION 2020-O0019) (MAR 2022))|3|||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE (DEVIATION 2020-O0019) (JUL 2020))|3|||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2014)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAY 2022)|13|332911|750 (# of employees)|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| 1. This is a limited competitive repair requirement. This part requiresengineering source approval by the design control activity in order to maintain the quality of the part. Existing unique design capability,engineering skills, and manufacturing knowledge by the qualified source(s) require acquisition of the part from approved source(s). The approved source(s) retain data rights, manufacturing knowledge, or technical data that are not economically available to the Government. 2. The resultant award of this solicitation shall be issued bilaterally,requiring the contractors written acceptance prior to execution. 3. The following proposed delivery schedule applies: Submission of Certification Data CDRLs will be on or before 20 days prior toscheduled delivery. PNSY review/acceptance of Certification CDRLs 6 workingdays after receipt of Certification DD 1423 CDRLs. Final delivery of material shall be on or before 250 days after the effective date of the resulting contract. 4. Drawings associated with this solicitation will be made available athttps://sam.gov/content/home. Drawings have restricted access which needs to be approved. Once access hasbeen requested, interested vendors should email the POC listed on thesolicitation to inform them of the request. 5. All transportation to/from the repair site will be paid for by the US Navy. 6. The contract shall comply with the Comercial Asset Visibility (CAV) of theasset(s) in the order in accordance with NAVSUPWSSFA24. 7. Offers shall be submitted as Firm Fixed Price for the full repair effortbased on the Repair Instruction or SOW. Please include the following: a. Teardown and Evaluation rate: b. RTAT: c. Throughput Constraint: d. Induction Expiration Date: A cost of new price shall also be provided in addition to the repair price. 8. All contractual documents (i.e. contracts, purchase orders, task orders,delivery orders, and modifications) related to the instant repair areconsidered to be ""issued"" by the Government when copies are either deposited in the mail, transmitted by facsimile, or send by other electronic commercemethods, such as email. The Government's acceptance of the contractor's proposal constitutes bilateral agreement to ""issue"" contractual details as detailed herein. 9. Any contract/order awarded as a result of this solicitation will be a ""DO""rated order certified for national defense use under the Defense Priorities and Allocations System (DPAS). See 52.211-14, Notice of Priority Rating forNational Defense, Emergency Preparedness, and Energy Program Use. 10. When submitting offers, make sure to specify any exceptions, i.e. MIL-STDpackaging, MIL-STD labeling, inspection and acceptance locations, packaginghouses, surplus material, etc. If no exceptions are indicated or received,award will be issued upon the solicitation requirements. Changes or requestsfor changes after award will require consideration costs deducted from the unit price. 11. If supplies will be packaged at a location different from the offeroraddress, the offeror shall provide the name, street address, and cage code ofthe packaging facility. 12. This is a Level 1 Repair. 13. This requirement requires access to classified drawings. These drawings are not required to submit a quote, however, in the event of an award, a facility clearance may be required in accordance with FAR 52.204-2. \ 1. SCOPE 1.1 The material covered in this contract/purchase order will be used in a crucial shipboard system. The use of incorrect or defective material would create a high probability of failure resulting in serious personnel injury, loss of life, loss of vital shipboard systems, or loss of the ship itself. Therefore, the material has been designated as SPECIAL EMPHASIS material (Level I, Scope of Certification, or Quality Assured) and special control procedures are invoked to ensure receipt of correct material. 2. APPLICABLE DOCUMENTS 2.1 Order of Precedence - In the event of a conflict between the text of this contract/purchase order and the references and/or drawings cited herein, the text of this contract/purchase order must take precedence. Nothing in this contract/purchase order, however, must supersede applicable laws and regulations unless a specific exemption has been obtained. 2.2 Identification of Classified Documents - This contract/purchase order requires the Contractor to have authorized access to classified documents in accordance with the attached Contract Security Classification Specification (DD Form 254). The classified documents and security level are: ;6984058 - CONFIDENTIAL; 2.3 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.3.1 Specification Revisions - The specification revisions listed under ""Documents References"" below are the preferred revision. Older and/or newer r evisions are acceptable when listed within Contract Support Library Reference Number CSD155 in ECDS (Electric Contractor Data Submission) at: ht tps://register.nslc.navy.mil/. This is to allow Contractors to use certain acceptable older specification revisions to purge their existing stock of material certified to those older revisions or to use newer specification revisions when material is certified to newly released revisions,without requiring the submittal of waiver/deviation requests for each specification revision on every contract. Revisions of specifications reflecting editorial and/or re-approval (e.g. E2009, R2014, etc.) are considered inconsequential, but are acceptable when their revisions are listedwithin CSD155 or elsewhere within this contract. 2.3.2 Documents, drawings, and publications supplied are listed under ""Drawing Number"". These items should be retained until an award is made. 2.3.3 ""Document References"" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. DRAWING DATA=26M65-0001H1 |53711| A|ER |D|0001 | |49998|1019235 DRAWING DATA=26M65-0001H2 |53711| A|ER |D|0001 | |49998|1070271 DRAWING DATA=26M65-0003G01 |53711| A|ER |D|0001 | A|49998|0305523 DRAWING DATA=2621-827-05 |96169| Z| |D|0001 | Z|49998|0084952 DRAWING DATA=2621-827-05 |96169| Z| |D|0001.1 | R|49998|0128957 DRAWING DATA=2621-827-05 |96169| Z| |D|0001.2 | F|49998|0085426 DRAWING DATA=2621-827-05 |96169| Z| |D|0001.3 | K|49998|0065651 DRAWING DATA=2621-827-05 |96169| Z| |D|0001.4 | K|49998|0060834 DRAWING DATA=2621-827-05 |96169| Z| |D|0002 | G|49998|0106348 DRAWING DATA=2621-827-05 |96169| Z| |D|0002.1 | M|49998|0092018 DRAWING DATA=2621-827-05 |96169| Z| |D|0002.2 | S|49998|0095871 DRAWING DATA=2621-827-05 |96169| Z| |D|0002.3 | S|49998|0081542 DRAWING DATA=2621-827-05 |96169| Z| |D|0002.4 | W|49998|0089226 DRAWING DATA=2621-827-05 |96169| Z| |D|0002.5 | Z|49998|0055086 DRAWING DATA=2621-827-05 |96169| Z| |D|0003 | Z|49998|0063398 DRAWING DATA=2621-827-05 |96169| Z| 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Y|49998|0044551 DRAWING DATA=2621-827-05 |96169| Z| |D|0218 | T|49998|0048466 DRAWING DATA=2621-827-05 |96169| Z| |D|0219 | T|49998|0049644 DRAWING DATA=2621-827-05 |96169| Z| |D|0220 | T|49998|0041601 DRAWING DATA=5486331 |53711| H| |D|0001 | H|49998|0200647 DRAWING DATA=5486332 |53711| G| |D|0001 | G|49998|0131198 DRAWING DATA=5486333 |53711| G| |D|0001 | G|49998|0238779 DRAWING DATA=6984058 |53711| A| |D|0001 | A|00026|0000000 DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=FED-STD-H28 |0020| |B |941221|A| |01| DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A|2 | | DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-B369 | | | |200401|A| | | DOCUMENT REF DATA=ASTM-B446 | | | |190401|A| | | DOCUMENT REF DATA=ASTM-A574 | | | |211201|A| | | DOCUMENT REF DATA=ASTM-F606 | | | |191115|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=ASTM-E1417 | | | |160615|A| | | DOCUMENT REF DATA=ASTM-E1444 | | | |160601|A| | | DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | | DOCUMENT REF DATA=SAE AMS 6931 | | |D |171201|A| | | DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-DTL-18240 | | |F |000313|A|1 | | DOCUMENT REF DATA=MIL-C-24679 | | | |880506|A| | | DOCUMENT REF DATA=QPL 25027 | | |17 |000207|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A|1 | | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=A-A-59004 | | |B |181118|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=AIA/NAS NASM 17828 | | |1 |130430|A| | | DOCUMENT REF DATA=AIA/NAS NASM 25027 | | |1 |121221|A| | | DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | |1 |191112|A| | | DOCUMENT REF DATA=T9074-AS-GIB-010/271 | | |1 |140911|A| | | DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | 3. REQUIREMENTS 3.1 REFURBISHED MATERIAL STATEMENT OF WORK (REPAIR SOW) - 3.1.1 INSPECTION - Clean and determine if refurbishment is possible. At disassembly, the Contractor must record all identifying markings found on the parts of each assembly. The Contractor must maintain traceability of these markings to each unit throughout refurbishment. 3.1.2 IDENTIFYING MARKINGS - Part must have a MIC (Material Identification a and Control) code, heat/heat lot code, or unique Contractor traceability number/code that is visible on the part. See Material Traceability in paragraph 3 (Quality Assurance Provisions) of this contract for traceability requirements. The MIC code can consist of a 2, 3, or 4 letter material identifier, 4 or 5 digit Julian date, 3 digit lot serial number, and Certifying Activity Designator (CAD) which will be 1 or 2 letters; the 4 parts are normally separated by hyphens; examples: TIA-3089-30-QQ and ST-06262-506-A. 3.1.3 RE-USEABLE PARTS - - Any parts of the original assembly that are useable (replacement is not necessary), that are properly marked as identified above, and that have material certifications available may be utilized as initially supplied. Certifications are not required to be resubmitted by the contractor. - Any parts of the original assembly that are useable (replacement is not necessary), are properly marked as identified above, but material certifications are not available at the contractor's facility, a waiver must be submitted in accordance with Waiver/Deviation (Configuration Control) requirements specified elsewhere in the Contract. 3.1.4 NON-USEABLE PARTS - -Any parts of the original assembly that are not properly marked as identified above must be replaced and the required certifications must be submitted. - Any parts of the original assembly that are not usable (replacement is necessary) must be replaced and the required certifications must be submitted. 3.1.5 REFURBISHMENT - Upon completion of inspection, this item must be refurbished to be in accordance with ;Naval Sea Systems Command drawing 517-5486331 Assembly IE, ER26M65-0001H1, ER26M65-0001H2, ER26M65-0003G1, and MS NO. 5310-081-142 REV - CHG-13 (CSD363); , except as amplified or modified herein. This applies to all ""Parts Requiring Certification"" as identified elsewhere in this Contract/Purchase Order. 3.1.6 ADDITIONAL SOW REQUIREMENTS - ;N/A; 3.1.7 ;Notes 9.A and 9.H on NAVSEA drawing 5486333 do not apply. The pre-manufactured Kamatics bearings listed on sheet 1 of Electric Boat engineering report ER26M65-0003G1 must be used in this valve.; 3.1.8 ;Stress relief per General Note 9 of drawing 5486332 is not required. Stress relief may be performed, at the option of the manufacturer, provided that all dimensional requirements are met. Stress relief, if performed, must be at 575 +/- 25 degrees Fahrenheit for one hour then air cooled.; 3.1.9 ;The material for the washer, Item 12 of NAVSEA drawing 5486333 and item 14 of NAVSEA drawing 5486331, must be per AMS 5906 and meet the spring load requirements of drawing 5486333 zone 17-B (The load at 0.023 inside height is to be 375 lbs ? 10%). Chemical and mechanical certification is not required. Any revision of AMS 5906 may be used.; 3.1.10 ;Note: For piece 7A of drawing 2621-827-05, allow thread machining relief between end of thread form and head of .045 min to .104 max.; 3.1.11 ;Note: Use Monoplex DOS (HallStar or equal) as the replacement for Plexol referenced in Note 8 on Drawing 5486331.; 3.2 Contract Support Library - Additional requirements for this item are identified as Contract Support Library Reference Number ;CSD363; in ECDS at https://register.nslc.navy.mil/ 3.3 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Body, Item 6 and Tailpiece, Item 7 both of drawing 5486332; Material - ;ASTM-B369, Alloy UNS C96400; Part - ;Trunnion Ball (Q3), Item 3 of drawing 5486333; Material - ;ASTM B446, Grade 1, Alloy UNS N06625, annealed; Part - ;Bonnet, Item 2 of drawing 5486333; Material - ;MIL-C-24679, Alloy C71500; Part - ;Self Locking Cap Screws, Item 39 of drawing 5486331; Material - ;MIL-DTL-1222, Type II, QQ-N-286, Annealed and Age Hardened and marked .K. and Self locking element to be in accordance with MIL-DTL-18240; Part - ;Continuous Threaded Studs, Items 24 and 25 of drawing 5486331; Material - ;MIL-DTL-1222, QQ-N-286, Type IV, Annealed and Age Hardened and marked .K.; Part - ;Vent Valve, Piece 7A of drawing 2621-827-05; Material - ;QQ-N-281 with Mechanical properties in accordance with Note 22 of drawing 2621-827-05; PART - ;Self-locking Hex Nuts, Items 21 and 22 of drawing 5486331; MATERIAL - QQ-N-281, class A annealed (hot finished or cold drawn) or class B cold drawn. All material must be from the same class. SELF-LOCKING ELEMENT- ASTM-D4066, Group 01, Class 1 or 2, Grade 1 Part - ;Stem, Item 3 of drawing 5486331; Material - SAE-AMS-6931 Note: Mechanical properties for bars, forgings and forging stock over 10"" must be as specified in the applicable drawing. If the mechanical properties are not provided in the drawing, the mechanical properties specified in SAE-AMS-6931 Table 2 for material 6"" to 10"", must be applied. Part - ;Seats (Q3), Item 7 of drawing 5486333; Material - Delrin: Dupont AF DE588 (Teflon Filled Acetal) (Properties Specified Below Only) ITEM PROPERTY ASTM TEST METHOD VALUE (A) Specific Gravity D792 (Note 1) 1.50 - 1.57 (B) Melting Point D2133 or D3418 172 - 184 deg C (342 - 363 deg F) (C) Tensile Strength (MIN) D638 (Notes 1 & 5) 6100 PSI (D) Tensile Impact (MIN) D1822 Type S (Notes 1 & 5) 5 FT-LB/SQ IN (E) Compressive Stress D695 2100 @ 1% DEF. (MIN - PSI) (Notes 1 & 5) 11,000 @ 10% DEF. (F) Water Absorption D570 .30% MAX 24 Hours (G) Rockwell Hardness (R) D785 (Note 1) 115 +/- 15 (H) Teflon Fiber Content (Note 2) 18 - 23% (I) Dimensional Change (Note 4) .7% MAX NOTES: 1. Material conditioning prior to test is at the vendor's option. 2. Teflon Fiber Content - As certified by DuPont (raw material). 3. Visual and Dimensional Inspection of Product (Final Machined Condition) - White Teflon string inclusions must not exceed the following: A.Diameter 1/32"" B. Length 1/8"" C. Density 6 indications per 100 SQ IN 4. The test method to determine dimensional stability must be performed as follows: The test specimens (finished pieces) tested must be measured at 23 +/- 3 deg C (73 +/- 5F) and placed in a mineral oil bath maintained at 160 +/- 3 deg C (320 +/- 5F) the specimens must remain in the bath for six (6) hours at temperature and allowed to slow cool in the bath at a rate not to exceed 23 +/- 3 deg C (73 +/- 5F) per hour. When the bath reaches 23 +/- 3 deg C (73 +/- 5F), the test specimens must be removed and measured. The percent change in each dimension, outside diameter, inside diameter and thickness must not be greater than the value specified. ^Mineral oil meets the specification as listed below: Description.......................Passes U.S.P. Test (USP XX, P.1143) Solubility........................Passes U.S.P. Test (USP XX, P.1143) Neutrality........................Passes U.S.P. Test (USP XX, P.532) Readily Carbonizable Substances...Passes U.S.P. Test (USP XX, P.532) Limit of Polynuclear Compounds....Passes U.S.P. Test (USP XX, P.532) Solid Paraffin....................Passes U.S.P. Test (USP XX, P.532) Specific Gravity @ 25 deg C (77 deg F).0.8600 to 0.8900 Viscosity @ 37.8 deg C (100F).....73.6 to 84.4 Centistokes (340-390 SUS) Flash Point Cleveland Open Cup....420 deg F (216C) (Typical) Refractive Index @ 20C (68F)......1.480 (Typical) 5. Values are minimum mean values. Individual specimen values may not vary more than 25% below the specified minimum mean value. Should one specimen exceed the 25% criteria, retest is required. Failure to meet the above criteria a second time is cause for rejection. 3.4 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below. Test - ;Liquid Penetrant Inspection; Item - ;Continuous Threaded Studs, Items 24 and 25 and Sel...
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