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ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19||||||||||||||||||||
HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specification sections C and E.|
INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2|||
TIME OF DELIVERY (JUNE 1997)|20|0001AA|5 EA.|540 DAYS |0001AB|20 EA.|540 DAYS|||||||||||||||
STOP-WORK ORDER (AUG 1989)|1||
GENERAL INFORMATION-FOB-DESTINATION|1|B|
WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Stand-Alone Receiving Report- Certifications Combo- Receiving Report & Invoice- Material |N/A|TBD|N00104|TBD|N39040 - Certifications, S4306A - Material |N50286|TBD|133.2|N/A|N/A|N39040 - Certifications |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||
EQUAL OPPORTUNITY (SEP 2016)|2|||
INTEGRITY OF UNIT PRICES (NOV 2021)|1||
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|||
EQUAL OPPORTUNITY FOR WORKERS WITH DISABILITIES (JUN 2020)|2|||
TRANSPORTATION OF SUPPLIES BY SEA (JAN 2023)|2|||
BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC (FEB2024))|11||||||||||||
PROGRESS PAYMENTS (NOV 2021)|4|||||
NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1||
LIST OF SOLICITATION ATTACHMENTS|5|x|x|x|x|x|
ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2023)|13||||||||||||||
BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024))|5||||||
BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024)|1||
ROYALTY INFORMATION (APR 1984)|1||
ANNUAL REPRESENTATIONS AND CERTIFICATIONS (FEB 2024)|13|336612|1000||||||||||||
TYPE OF CONTRACT (APR 1984)|1|Firm Fixed Price |
NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||x|
Please follow instructions outlined in Section L: of this solicitation.
WSSTERMLZ02: Offerors shall provide a Quality Assurance Manual. Only those sources with an acceptable Quality Assurance Manual are eligible for award under this solicitation.
This solicitation uses LPTA criteria outlined in this solicitation.
If drawings are included in the solicitation, access needs to berequested on the individual solicitation page on Contracts Opportunities on the Governments beta.SAM website. After requesting access, send an email to the Primary POC listed on the solicitation.
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 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions.
2.2.1 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.
2.2.2 Documents, drawings, and publications supplied are listed under "Drawing Number". These items should be retained until an award is made.
2.2.3 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order.
DRAWING DATA=EB-2937 |96169| B|SP |D|0001 | B|49998|0568465
DRAWING DATA=EB-2937 |96169| B|SP |D|0002 | B|49998|0262311
DRAWING DATA=EB-2937 |96169| B|SP |D|0003 | B|49998|0457001
DRAWING DATA=EB-2937 |96169| B|SP |D|0004 | B|49998|0494479
DRAWING DATA=EB-2937 |96169| B|SP |D|0005 | B|49998|0557624
DRAWING DATA=EB-2937 |96169| B|SP |D|0006 | B|49998|0572669
DRAWING DATA=EB-2937 |96169| B|SP |D|0007 | B|49998|0588302
DRAWING DATA=EB-2937 |96169| B|SP |D|0008 | B|49998|0487356
DRAWING DATA=EB-2937 |96169| B|SP |D|0009 | B|49998|0641401
DRAWING DATA=EB-2937 |96169| B|SP |D|0010 | B|49998|0609048
DRAWING DATA=EB-2937 |96169| B|SP |D|0011 | B|49998|0332061
DRAWING DATA=H261-0102D74 |53711| A|ER |D|0001 | |00026|0000000
DRAWING DATA=H621-0102A01 |53711| A|ER |D|0001 | A|49998|0037852
DRAWING DATA=H621-0102A01 |53711| A|ER |D|0002 | A|49998|0022265
DRAWING DATA=H621-0102A01 |53711| A|ER |D|0003 | A|49998|0045427
DRAWING DATA=H621-0102A01 |53711| A|ER |D|0004 | A|49998|0032629
DRAWING DATA=H621-0102A01 |53711| A|ER |D|0005 | A|49998|0033163
DRAWING DATA=H621-0102A01 |53711| A|ER |D|0006 | A|49998|0041453
DRAWING DATA=H621-0102A01 |53711| A|ER |D|0007 | A|49998|0122787
DRAWING DATA=H621-0102A01 |53711| A|ER |D|0008 | A|49998|0075868
DRAWING DATA=H621-0102A02 |53711| A|ER |D|0001 | A|49998|0038259
DRAWING DATA=H621-0102A02 |53711| A|ER |D|0002 | A|49998|0014346
DRAWING DATA=H621-0102A02 |53711| A|ER |D|0003 | A|49998|0053725
DRAWING DATA=H621-0102A02 |53711| A|ER |D|0004 | A|49998|0063527
DRAWING DATA=H621-0102A02 |53711| A|ER |D|0005 | A|49998|0064236
DRAWING DATA=H621-0102A02 |53711| A|ER |D|0006 | A|49998|0037645
DRAWING DATA=H621-0102A02 |53711| A|ER |D|0007 | A|49998|0036363
DRAWING DATA=H621-0102A02 |53711| A|ER |D|0008 | A|49998|0037448
DRAWING DATA=H621-0102A02 |53711| A|ER |D|0009 | A|49998|0039414
DRAWING DATA=H621-0102A02 |53711| A|ER |D|0010 | A|49998|0160700
DRAWING DATA=H621-0102A02 |53711| A|ER |D|0011 | A|49998|0134109
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001 | A|49998|0021078
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001.1 | A|49998|0019129
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001.2 | A|49998|0025775
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001.3 | A|49998|0039912
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0001.4 | A|49998|0026761
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0002 | A|49998|0057736
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0003 | A|49998|0069402
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0004 | A|49998|0052923
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0005 | A|49998|0044205
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0006 | A|49998|0053927
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0007 | A|49998|0039873
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0008 | A|49998|0047671
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0009 | A|49998|0042694
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0010 | A|49998|0039885
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0011 | A|49998|0044703
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0012 | A|49998|0042919
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0013 | A|49998|0037692
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0014 | A|49998|0039760
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0015 | A|49998|0041011
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0016 | A|49998|0048557
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0017 | A|49998|0014830
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0018 | A|49998|0013294
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0019 | A|49998|0166561
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0020 | A|49998|0139744
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0021 | A|49998|0189793
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0022 | A|49998|0139891
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0023 | A|49998|0121265
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0024 | A|49998|0105221
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0025 | A|49998|0114189
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0026 | A|49998|0198610
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0027 | A|49998|0115665
DRAWING DATA=H621-0102A03 |53711| A|ER |D|0028 | A|49998|0083415
DRAWING DATA=H621-0102A05 |53711| A|ER |D|0001 | A|49998|0034604
DRAWING DATA=H621-0102A05 |53711| A|ER |D|0001.1 | A|49998|0012203
DRAWING DATA=H621-0102A05 |53711| A|ER |D|0002 | A|49998|0064744
DRAWING DATA=H621-0102A05 |53711| A|ER |D|0003 | A|49998|0127671
DRAWING DATA=H621-0102A07 |53711| A|ER |D|0001 | A|49998|0043518
DRAWING DATA=H621-0102A07 |53711| A|ER |D|0001.1 | A|49998|0014077
DRAWING DATA=H621-0102A07 |53711| A|ER |D|0002 | A|49998|0063639
DRAWING DATA=H621-0102A07 |53711| A|ER |D|0003 | A|49998|0044605
DRAWING DATA=H621-0102A07 |53711| A|ER |D|0004 | A|49998|0044015
DRAWING DATA=H621-0102A108 |53711| A|ER |D|0001 | A|49998|0918547
DRAWING DATA=H621-0102A11 |53711| A|ER |D|0001 | A|49998|0043094
DRAWING DATA=H621-0102A11 |53711| A|ER |D|0001.1 | A|49998|0018658
DRAWING DATA=H621-0102A11 |53711| A|ER |D|0002 | A|49998|0060012
DRAWING DATA=H621-0102A11 |53711| A|ER |D|0003 | A|49998|0035375
DRAWING DATA=H621-0102A11 |53711| A|ER |D|0004 | A|49998|0055587
DRAWING DATA=H621-0102A11 |53711| A|ER |D|0005 | A|49998|0037265
DRAWING DATA=H621-0102A11 |53711| A|ER |D|0006 | A|49998|0039785
DRAWING DATA=H621-0102A11 |53711| A|ER |D|0007 | A|49998|0041585
DRAWING DATA=H621-0102A11 |53711| A|ER |D|0008 | A|49998|0036148
DRAWING DATA=H621-0102A11 |53711| A|ER |D|0009 | A|49998|0208132
DRAWING DATA=H621-0102A121 |53711| A|ER |D|0001 | A|49998|0709114
DRAWING DATA=H621-0102A125 |53711| A|ER |D|0001 | A|49998|0435504
DRAWING DATA=H621-0102A168 |53711| A|ER |D|0001 | A|49998|1501235
DRAWING DATA=H621-0102A17 |53711| A|ER |D|0001 | A|49998|0037341
DRAWING DATA=H621-0102A17 |53711| A|ER |D|0001.1 | A|49998|0019205
DRAWING DATA=H621-0102A17 |53711| A|ER |D|0002 | A|49998|0066302
DRAWING DATA=H621-0102A17 |53711| A|ER |D|0003 | A|49998|0062923
DRAWING DATA=H621-0102A17 |53711| A|ER |D|0004 | A|49998|0126037
DRAWING DATA=H621-0102A188 |53711| A|ER |D|0001 | |49998|1432274
DRAWING DATA=H621-0102A22 |53711| C|ER |D|0001 | |49998|0855198
DRAWING DATA=H621-0102A22 |53711| C|ER |D|0001.1 | B|49998|0028535
DRAWING DATA=H621-0102A22 |53711| C|ER |D|0001.2 | B|49998|0033887
DRAWING DATA=H621-0102A22 |53711| C|ER |D|0001.3 | B|49998|0012002
DRAWING DATA=H621-0102A22 |53711| C|ER |D|0002 | B|49998|0077551
DRAWING DATA=H621-0102A22 |53711| C|ER |D|0003 | B|49998|0038816
DRAWING DATA=H621-0102A22 |53711| C|ER |D|0004 | B|49998|0120742
DRAWING DATA=H621-0102A22 |53711| C|ER |D|0005 | B|49998|0068506
DRAWING DATA=H621-0102A22 |53711| C|ER |D|0006 | B|49998|0120902
DRAWING DATA=H621-0102A39 |53711| A|ER |D|0001 | A|49998|0043492
DRAWING DATA=H621-0102A39 |53711| A|ER |D|0001.1 | A|49998|0033724
DRAWING DATA=H621-0102A39 |53711| A|ER |D|0002 | A|49998|0062801
DRAWING DATA=H621-0102A39 |53711| A|ER |D|0003 | A|49998|0071199
DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001 | B|49998|0037377
DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001.1 | B|49998|0024643
DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001.2 | B|49998|0022539
DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001.3 | B|49998|0027931
DRAWING DATA=H621-0102A48 |53711| B|ER |D|0001.4 | B|49998|0036544
DRAWING DATA=H621-0102A48 |53711| B|ER |D|0002 | B|49998|0071446
DRAWING DATA=H621-0102A48 |53711| B|ER |D|0003 | B|49998|0035428
DRAWING DATA=H621-0102A48 |53711| B|ER |D|0004 | B|49998|0039985
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0001 | A|49998|0041731
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0001.1 | A|49998|0029231
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0001.2 | A|49998|0036383
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0002 | A|49998|0054429
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0003 | A|49998|0030654
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0004 | A|49998|0061856
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0005 | A|49998|0057108
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0006 | A|49998|0056135
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0007 | A|49998|0060035
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0008 | A|49998|0059823
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0009 | A|49998|0023352
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0010 | A|49998|0040524
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0011 | A|49998|0051452
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0012 | A|49998|0057922
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0013 | A|49998|0022848
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0014 | A|49998|0035871
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0015 | A|49998|0038701
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0016 | A|49998|0028302
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0017 | A|49998|0088297
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0018 | A|49998|0155682
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0019 | A|49998|0124972
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0020 | A|49998|0118121
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0021 | A|49998|0077344
DRAWING DATA=H621-0102A50 |53711| A|ER |D|0022 | A|49998|0128466
DRAWING DATA=H621-0102A51 |53711| A|ER |D|0001 | A|49998|0040110
DRAWING DATA=H621-0102A51 |53711| A|ER |D|0001.1 | A|49998|0027168
DRAWING DATA=H621-0102A51 |53711| A|ER |D|0002 | A|49998|0060056
DRAWING DATA=H621-0102A51 |53711| A|ER |D|0003 | A|49998|0061789
DRAWING DATA=H621-0102A52 |53711| A|ER |D|0001 | A|49998|0039953
DRAWING DATA=H621-0102A52 |53711| A|ER |D|0001.1 | A|49998|0032355
DRAWING DATA=H621-0102A52 |53711| A|ER |D|0002 | A|49998|0062662
DRAWING DATA=H621-0102A52 |53711| A|ER |D|0003 | A|49998|0037395
DRAWING DATA=H621-0102A52 |53711| A|ER |D|0004 | A|49998|0035793
DRAWING DATA=H621-0102A57 |53711| A|ER |D|0001 | A|49998|0168427
DRAWING DATA=H621-0102A71 |53711| A|ER |D|0001 | A|49998|0169469
DRAWING DATA=H621-0102A99 |53711| B|ER |D|0001 | B|49998|5824730
DRAWING DATA=H775-1512A1 |53711| A|ER |D|0001 | |00026|0000000
DRAWING DATA=H775-1512A10 |53711| A|ER |D|0001 | |49998|1565029
DRAWING DATA=H775-1512A2 |53711| A|ER |D|0001 | |00026|0000000
DRAWING DATA=H775-1512A3 |53711| A|ER |D|0001 | |00026|0000000
DRAWING DATA=H775-1512A4 |53711| A|ER |D|0001 | |00026|0000000
DRAWING DATA=H775-1512A5 |53711| A|ER |D|0001 | |49998|0228403
DRAWING DATA=H775-1512A6 |53711| A|ER |D|0001 | |49998|0063013
DRAWING DATA=H775-1512A7 |53711| A|ER |D|0001 | |49998|0176895
DRAWING DATA=H775-1512A8 |53711| A|ER |D|0001 | |49998|0271962
DRAWING DATA=H775-1512A9 |53711| A|ER |D|0001 | |49998|0335202
DRAWING DATA=6984052 |53711| D| |D|0001 | D|00026|0000000
DRAWING DATA=6985426 |53711| A| |D|0000.A | A|49998|0035751
DRAWING DATA=6985426 |53711| A| |D|0001 | A|49998|0074079
DRAWING DATA=6985426 |53711| A| |D|0002 | A|49998|0062500
DRAWING DATA=6985426 |53711| A| |D|0003 | A|49998|0008982
DRAWING DATA=6985426 |53711| A| |D|0004 | A|49998|0010717
DRAWING DATA=6985426 |53711| A| |D|0005 | A|49998|0030344
DRAWING DATA=6985426 |53711| A| |D|0006.1 | A|49998|0061541
DRAWING DATA=6985426 |53711| A| |D|0006.10 | A|49998|0022748
DRAWING DATA=6985426 |53711| A| |D|0006.2 | A|49998|0061465
DRAWING DATA=6985426 |53711| A| |D|0006.3 | A|49998|0055809
DRAWING DATA=6985426 |53711| A| |D|0006.4 | A|49998|0059727
DRAWING DATA=6985426 |53711| A| |D|0006.5 | A|49998|0059513
DRAWING DATA=6985426 |53711| A| |D|0006.6 | A|49998|0023040
DRAWING DATA=6985426 |53711| A| |D|0006.7 | A|49998|0040218
DRAWING DATA=6985426 |53711| A| |D|0006.8 | A|49998|0051132
DRAWING DATA=6985426 |53711| A| |D|0006.9 | A|49998|0057425
DRAWING DATA=6985426 |53711| A| |D|0007.1 | A|49998|0024885
DRAWING DATA=6985426 |53711| A| |D|0007.10 | A|49998|0037342
DRAWING DATA=6985426 |53711| A| |D|0007.11 | A|49998|0032807
DRAWING DATA=6985426 |53711| A| |D|0007.12 | A|49998|0037061
DRAWING DATA=6985426 |53711| A| |D|0007.13 | A|49998|0036308
DRAWING DATA=6985426 |53711| A| |D|0007.14 | A|49998|0040683
DRAWING DATA=6985426 |53711| A| |D|0007.15 | A|49998|0028030
DRAWING DATA=6985426 |53711| A| |D|0007.2 | A|49998|0038133
DRAWING DATA=6985426 |53711| A| |D|0007.3 | A|49998|0037181
DRAWING DATA=6985426 |53711| A| |D|0007.4 | A|49998|0035304
DRAWING DATA=6985426 |53711| A| |D|0007.5 | A|49998|0035595
DRAWING DATA=6985426 |53711| A| |D|0007.6 | A|49998|0035487
DRAWING DATA=6985426 |53711| A| |D|0007.7 | A|49998|0032536
DRAWING DATA=6985426 |53711| A| |D|0007.8 | A|49998|0038400
DRAWING DATA=6985426 |53711| A| |D|0007.9 | A|49998|0042559
DRAWING DATA=6985426 |53711| A| |D|0008.1 | A|49998|0029133
DRAWING DATA=6985426 |53711| A| |D|0008.2 | A|49998|0046621
DRAWING DATA=6985426 |53711| A| |D|0008.3 | A|49998|0014013
DRAWING DATA=6985426 |53711| A| |D|0008.4 | A|49998|0012670
DRAWING DATA=6985426 |53711| A| |D|0009 | A|49998|0088388
DRAWING DATA=6985426 |53711| A| |D|0010 | A|49998|0157697
DRAWING DATA=6985426 |53711| A| |D|0011 | A|49998|0138726
DRAWING DATA=6985426 |53711| A| |D|0012 | A|49998|0189061
DRAWING DATA=6985426 |53711| A| |D|0013 | A|49998|0134718
DRAWING DATA=6985426 |53711| A| |D|0014 | A|49998|0123397
DRAWING DATA=6985426 |53711| A| |D|0015 | A|49998|0118040
DRAWING DATA=6985426 |53711| A| |D|0016 | A|49998|0113699
DRAWING DATA=6985426 |53711| A| |D|0017 | A|49998|0118200
DRAWING DATA=6985426 |53711| A| |D|0018 | A|49998|0071113
DRAWING DATA=6985426 |53711| A| |D|0019 | A|49998|0068598
DRAWING DATA=6985426 |53711| A| |D|0020 | A|49998|0116804
DRAWING DATA=6985426 |53711| A| |D|0021 | A|49998|0075838
DRAWING DATA=6985426 |53711| A| |D|0022 | A|49998|0097724
DRAWING DATA=6985426 |53711| A| |D|0023 | A|49998|0069126
DRAWING DATA=6985426 |53711| A| |D|0024 | A|49998|0155576
DRAWING DATA=6985426 |53711| A| |D|0025 | A|49998|0143738
DRAWING DATA=6985426 |53711| A| |D|0026 | A|49998|0127085
DRAWING DATA=6985426 |53711| A| |D|0027 | A|49998|0123826
DRAWING DATA=6985426 |53711| A| |D|0028 | A|49998|0109249
DRAWING DATA=6985426 |53711| A| |D|0029 | A|49998|0121330
DRAWING DATA=6985426 |53711| A| |D|0030 | A|49998|0087896
DRAWING DATA=6985426 |53711| A| |D|0031 | A|49998|0124616
DRAWING DATA=6985426 |53711| A| |D|0032 | A|49998|0234515
DRAWING DATA=6985426 |53711| A| |D|0033 | A|49998|0126707
DRAWING DATA=6985426 |53711| A| |D|0034 | A|49998|0128215
DRAWING DATA=6985426 |53711| A| |D|0035 | A|49998|0072619
DRAWING DATA=6985426 |53711| A| |D|0036 | A|49998|0076247
DRAWING DATA=7069152 |53711| A| |D|0001 | A|49998|2185285
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=ASTM-B150 | | | |190401|A| | |
DOCUMENT REF DATA=ASTM-A193 | | | |200515|A| | |
DOCUMENT REF DATA=ASTM-B209 | | | |070801|A| | |
DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A| 2| |
DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | |
DOCUMENT REF DATA=ASTM-B564 | | | |191101|A| | |
DOCUMENT REF DATA=ASTM-A574 | | | |120401|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=ASME-B18.3 | | | |120101|A| | |
DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | |
DOCUMENT REF DATA=ASTM-D4066 | | | |130701|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=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=SAE AMS-QQ-A-200 | | |A |980901|A| | |
DOCUMENT REF DATA=SAE AMS-QQ-A-200 |0008| |A |150501|A| | |
DOCUMENT REF DATA=SAE AMS-QQ-A-250 | | |A |040801|A| | |
DOCUMENT REF DATA=SAE AMS-QQ-A-250 |0011| | |970801|A| | |
DOCUMENT REF DATA=SAE AMS-QQ-S-763 | | |D |150301|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| | |
DOCUMENT REF DATA=T9074-BD-GIB-010/0300 | | |2 |121218|A| | |
3. REQUIREMENTS
3.1 ;The Aft Desurger Assembly is required to be in accordance with Naval Sea System Command Drawing 6985426 Part Number A2 and all EB ERs invoked in this contract, except as amplified or modified herein.;
3.2 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise:
Part - ;Desurger Head, Part 2-1;
Material - ;T9074-BD-GIB-010/0300, Appendix E, Grade HY-80, Forged;
Part - ;Tailpiece, Part 2-2;
Material - ;SAE AMS-QQ-S-763, CL 304, COND A;
Part - ;Bushing, Part 6-1;
Material - ;ASTM-B150, UNS C63200, TQ50 OR TQ55;
Part - ;Barrel, Part 22;
Material - ;ASTM-B564 forged, UNS N06625, Condition Annealed and meeting the mechanical properties of General Note 7006. Chrome Plated in accordance with General Note 7021;
Part - ;Piston, Part 23;
Material - ;SAE AMS-QQ-A-250/11, Alloy 6061, Temper T651 or ASTM B209, Alloy 6061, Temper T651. Anodized in accordance with General Note 2221;
Part - ;Tie Rod, Part 24;
Material - ;ASTM A193, Grade B7;
Part - ;Piston Rod, Part 25;
Material - ;SAE AMS-QQ-A-200/8, Alloy 6061, Temp T6. Anodized in accordance with General Note 2221 and plated in accordance with General Note 7202;
PART - ;Self-Locking Nut, Part 78;
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 - ;Self-Locking Cap Screw, Part 79;
Material - ;MIL-DTL-1222, Type II, QQ-N-286, Solution Annealed and Age Hardened and marked .K. Self-locking element to be in accordance with MIL-DTL-18240. Cross drill 2 holes IAW ASME-B18.3;
3.3 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 - 5x Visual Magnification or Dye Penetrant Inspection (root layer)
Item - Weldments
Performance - T9074-AS-GIB-010/271
Acceptance - MIL-STD-2035
Test - Visual and Dye Penetrant Inspection (final layer)
Item - Weldments
Performance - T9074-AS-GIB-010/271
Acceptance - MIL-STD-2035
Test - Intergranular Corrosion Test (Only for SAE-AMS-QQ-S-763, Classes 304-condition A, 304L, 316-condition A, 316L, 317-condition A, 321 and 347 material. Test must be performed prior to fabrication/machining)
Item - ;Tailpiece, Part 2-2;
Performance - SAE-AMS-QQ-S-763
Acceptance - SAE-AMS-QQ-S-763
Test - ;Ultrasonic Inspection;
Item - ;Bushing, Part 6-1 (with a diameter or minimum distance between parallel surfaces of 4 inches or greater of the starting material);
Performance - ;T9074-AS-GIB-010/271;
Acceptance - ;General Note 125 of Drawing 6985426;
Test - ;Ultrasonic Inspection;
Item - ;Barrel, Part 22 (starting material);
Performance - ;EB-2937, paragraph 4.5.4;
Acceptance - ;EB-2937, paragraph 4.5.4;
Test - ;Ultrasonic Inspection;
Item - ;HY-80 Forged Material;
Performance - ;T9074-BD-GIB-010/0300, Appendix E;
Acceptance - ;T9074-BD-GIB-010/0300, Appendix E;
Test - ;Magnetic Particle Inspection;
Item - ;HY-80 Forged Material;
Performance - ;T9074-BD-GIB-010/0300, Appendix E;
Acceptance - ;T9074-BD-GIB-010/0300, Appendix E;
Test - ;Liquid Penetrant Inspection;
Item - ;Tie Rod, Part 24;
Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222
Acceptance - MIL-DTL-1222
Test - ;Dye Penetrant Inspection for Non-Magnetic Grades;
Item - ;Self-Locking Nut, Part 78;
Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444
(Method C solvent removal techniques must not be used on thread)
Acceptance - ;NASM25027;
Test - Quality Conformance/Compliance Inspection
Item - ;HY-80 starting material;
Performance - ;T9074-BD-GIB-010/0300, Appendix E;
Acceptance - ;T9074-BD-GIB-010/0300, Appendix E;
Test - Quality Conformance Tests
Item - Self-Locking Nuts
Performance - ;NASM25027;
Acceptance - ;NASM25027;
Attribute - Certificate of Completion
Item - Self-Locking Nut Nonmetallic Insert
Performance - ;ASTM-D4066, Group 01, Class 1, Grade 1;
Attribute - Certificate of Compliance
Item - Self-Locking Nuts
Performance - This Certificate must state that self-locking nuts were manufactured by an approved source. Approved sources are those listed on QPL-25027 for the appropriate fastener. This QPL may also be considered as approved sources for Heavy Hex
self-locking nuts.
Test - ;Liquid Penetrant Inspection;
Item - ;Self-Locking Cap Screw, Part 79;
Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222
Acceptance - MIL-DTL-1222
Attribute - Annealing and Age Hardening
Item - ;Self-Locking Cap Screw, Part 79;
Performance - QQ-N-286
Test - ;Hydrostatic Test;
Item - ;Each Assembly;
Performance - ;Note 7400 of Drawing 6985426;
Acceptance - ;Note 7400 of Drawing 6985426;
3.4 The pressure tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the
following must be used:
For pressure tests below 100 PSIG, the pressure tolerance must be +1 PSIG/-0PSIG.
For pressure tests at or above 100 PSIG up to and including 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG rounded off to the nearest multiple of thesmallest graduation on an analog test pressure gauge, not to exceed 50 PSIG.
30 minutes / - 0 minutes. above 2500 PSIG, the pressure tolerance must be +2%/-0 PSIG, rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 200 PSIG.
The pressure test time tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure test time tolerances are not provided by drawings, specifications or specified elsewhere in
this contract, the following must be used:
For a test duration up to and including 1 hour, the tolerance must be +5 minutes / - 0 minutes.
For a test duration of more than 1 hour up to and including 24 hours, the tolerance must be +30 minutes / - 0 minutes.
For a test duration of more than 24 hours, the tolerance must be + 60 minutes/- 0 minutes.
3.5 K-MONEL Fasteners - Material must be heat treated per QQ-N-286.
3.5.1 Fasteners that have been hot or cold headed or roll threaded must be solution annealed followed by age hardening subsequent to all heading and thread rolling operations. The mechanical properties on certifications must be actual properties of the
annealed and age hardened material and must meet the requirements of QQ-N-286.
3.5.2 QQ-N-286 fasteners that have been headed and/or roll threaded must not beage hardened unless the material has been solution annealed subsequent to the heading and threading operations. Threads formed after the final age hardening heat treatment must be
cut or ground only.
3.6 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable.
3.7 K-MONEL Fasteners - K-MONEL externally threaded fasteners must have mechanical properties determined in accordance with MIL-DTL-1222. Test results must include Tensile, Yield, Elongation and Hardness as required by MIL-DTL-1222. (The Hardness tests must be
performed on a full size fastener.)
3.7.1 Studs require an Axial Tensile test in accordance with MIL-DTL-1222.
3.7.2 Headed fasteners require a Wedge Tensile test as specified elsewhere in this contract/purchase order.
3.8 Slow Strain Rate Tensile Test Laboratories - The Slow Strain Rate Tensile Test of QQ-N-286 must be performed by one of the following laboratories:
Huntington Alloys, a Special Metals Company
Attn: Bill Bolenr
3200 Riverside Drive
Huntington, WV 257059
Phone: (304) 526-5889
FAX: (304) 526-5973
Metallurgical Consultants, Inc.
Attn: W. M. Buehler
4820 Caroline
PO Box 88046
Houston, TX 77288-0046
Phone: (713) 526-6351
FAX: (713) 526-2964
Naval Surface Warfare Center, Carderock Division
Attn: Eric Focht Code 614
9500 Macarthur Blvd
West Bethesda, MD 20817-5700
Phone: (301) 227-5032
FAX: (301) 227-5576
Teledyne Allvac
Attn: Dr. W. D. Cao
2020 Ashcraft Ave.
Monroe, NC 28110
Phone: (704) 289-4511
FAX: (704) 289-4269
Westmoreland Mechanical Testing and Research Inc.
Attn: Andrew Wisniewski
P.O. Box 388
Youngstown, PA 15696-0388
Mannesmann Rohrenwerke
Mannesmann Forschungsinstitut (MFI)
Attn: Dr. Weiss
Postfach 251160
47251 Duisburg
Germany
Phone: 011-49-0203-9993194
FAX: 011-49-0203-9994415
ThyssenKrupp VDM USA, Inc.
Attn: D. C. Agarwal
11210 Steeplecrest Drive, Suite 120
Houston, TX 77065-4939
Phone: (281) 955-6683
3.9 Wedge Tensile Test Specimens (Headed fasteners) - A wedge tensile test must be conducted on a Full Size Fastener for each production lot and reported aspart of the Mechanical Properties. The required specimens for the Wedge Tensile Test must be separate
fasteners from those required for the Yield Test.
3.9.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1.
3.9.2 Testing for all other Headed Fasteners with a nominal diameter greater than 1/4-inch must be in accordance with ASTM-F606 for grades 5, 8, B7, and B16.For all other grades, the following wedge angles must be used.
a. Except as specified in item c below, fasteners with a nominal diameter of 1/4-inch through 1-inch (inclusive) must be tested with a ten degree wedge.
b. Except as specified in item c below, fasteners with a nominal diameter over 1-inch must be tested with a six degree wedge.
c. Fasteners that are of grades 8, B7, B16, 410, 416, 416Se, 431, and 630 and are threaded within one diameter to the underside of the head must be tested as follows:
Sizes 1/4 inch through 3/4 inch (inclusive) Use a six degree wedgeSizes over 3/4 inch Use a four degree wedge
d. Fasteners which have passed testing with wedge angles greater than those specified should be considered acceptable.
3.9.3 For fasteners having a length less than the minimum specified in Table 1 of ASTM-F606, one "test specimen fastener" must be manufactured from each lot of fasteners and tested to represent that lot. The length of these test specimen fasteners must meet
the minimum specified in table 1 of ASTM-F606 but must not exceed it by more than 1/4 inch. Test specimen fasteners must be the same type, style, and diameter as the production lot and must be manufactured from the same starting material, using the same
manufacturing techniques as the production lot, and must be heat treated (if required) along with the production lot.
3.10 Thread Inspection Requirements - All threads on threaded parts must be inspected using appropriate inspection methods, inspection systems, and inspection gages/instruments in accordance with FED-STD-H28 series. Substitution of thecommercial equivalent
inspection in accordance with ASME B1 series is acceptable.
3.10.1 System 21 of FED-STD-H28/20 must be used as a minimum inspection requirement for threads when the design drawing or design specification does not specify an inspection requirement.
3.10.2 For Navy and Shipyard drawings, system 21 of FED-STD-H28/20 may be substituted for System 22 without further Navy approval when the design drawing invokes System 22 and does not cite governing specifications that specifically require system 22. System
22 of FED-STD-H28/20 must be used when the drawing references other governing specifications that specifically require System 22, such as certain thread types of MIL-DTL-1222.
3.10.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system.
3.11 Certification is required for the following as identified further below:
- Process Control Plan
- Qualification Plan
- Qualification Testing (First Article)
All manufacturing facilities which have been approved to an earlier revision of this specification are required to meet the recertification requirements of T9074-BD-GIB-010/0300 Revision 2. An updated Process Control Plan incorporating any changes necessary to
meet the requirements of T9074-BD-GIB-010/0300 Revision 2 must be submitted.
Re-certification of the first article approval of vendor facilities, processes, and manufacturing methods is required every 5 years and must meet all the requirements of T9074-BD-GIB-010/0300. The certification must be current at the delivery date of procured
products.
3.11.1 Qualification Testing (First Article Inspection) - See DI-NDTI-80809 (First Article Test Report) - Certification is required for the following test on the items listed below:
Test - First Article Inspection
Item - ;HY-80 starting material;
Performance - T9074-BD-GIB-010/0300
Acceptance - T9074-BD-GIB-010/0300
Previous FAT approvals that were based upon previous specifications are not valid for meeting the requirements of T9074-BD-GIB-010/0300 Revision 2, unless otherwise approved by NAVSEA.
The Contractor may request the FAT submission requirement be waived by providing the PCO with evidence of NAVSEA approval, provided it meets the requirements of this contract/purchase order.
3.11.2 Process Control Plan - See DI-NDTI-80809 (Process Control Plan) - Certification is required for the following attribute on the items listed below:
Attribute - Process Control Plan
Item - ;HY-80 starting material;
Performance - T9074-BD-GIB-010/0300
The PCP must be reviewed and approved by NAVSEA prior to initiating First Article Testing. The Contractor may request the PCP submission requirement be waived by providing the PCO with evidence of NAVSEA approval.
3.11.3 Qualification Plan - See DI-NDTI-80809 (Qualification Plan) - Certification is required for the following attribute on the items listed below:
Attribute - Qualification Plan
Item - ;HY-80 starting material;
Performance - T9074-BD-GIB-010/0300
The QP must be reviewed and approved by NAVSEA prior to initiating First Article Testing. The Contractor may request the QP submission requirement be waived by providing the PCO with evidence of NAVSEA approval.
3.12 ;See CDRL DI-FORG-80412 (Forging Manufacturing Sketches) - Forging Sketches are required for the Desurger Head, Part 2-1, per T9074-B-GIB-010/0300, Appendix E.;
3.13 Welding or Brazing - When welding, brazing, and allied processes are required, as invoked by Section C paragraph 3 requirements, they must be in accordance with S9074-AR-GIB-010A/278, (S9074-AQ-GIB-010/248 for brazing) by personnel and procedures
qualified under S9074-AQ-GIB-010/248 for all production and repair welding and brazing. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing.
3.14 O-ring grooves and mating sealing surfaces must be inspected per the contractually invoked drawings or specifications. When the drawings or specifications do not provide specific defect criteria or state that no defects are allowed, the General
Acceptance Criteria (GAC) standard must be used for inspecting O-ring grooves and mating sealing surfaces only. Repairs to sealing surfaces and O-ring grooves with unacceptable defects may be accomplished within the limits of the size and tolerances provided
in the applicable drawing. Repairs thatwould exceed these limits require approval (including final dimensions). The data that is red lined (crossed out) is excluded from the GAC for this contract and is not to be used for acceptance or rejection criteria.
The GAC document is identified as Contract Support Library Reference Number CSD008 at https://register.nslc.navy.mil/
3.15 Specification Change - For QQ-N-281, Class B material:
1 - Footnote 9 to Table II of QQ-N-281 does not apply.
2 - When starting material is Round Bar greater than 3" dia,
the mechanical properties of Hex Bar apply.
3.16 Certificate of Compliance - (SPECIAL EMPHASIS MATERIAL) The Contractor must prepare and submit a certificate of compliance certifying that the items/components furnished under this contract comply with the requirements of the procurement document,
including any/all invoked specifications and drawings.
3.17 Configuration Control - The Contractor must maintain the total equipment baseline configuration. For items of proprietary design, Contractor drawings showing the latest assembly configuration must be provided to the Government in electronic (C4) format.
Definitions are provided elsewhere in the Contract/Purchase Order.
3.17.1 Waivers/Deviations - All waivers and deviations, regardless of significance or classification require review and approval by the Contracting Officer. Waivers and Deviations must be designated as Critical, Major, or Minor. The Contractor must provide
a copy of this request to the QAR. Requests must include the information listed below.
a. A complete description of the contract requirement affected
and the nature of the waiver/deviation (non-conformance),
including a classification of Critical, Major, or Minor.
b. Number of units (and serial/lot numbers) to be delivered in this
configuration.
c. Any impacts to logistics support elements (such as software,
manuals, spares, tools, and similar) being utilized by Government
personnel or impacts to the operational use of the product.
d. Information about remedial action being taken to prevent reoccurrence
of the non-conformance.
3.17.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted using the ECDS (Electronic Contractor Data Submission) system at https://register.nslc.navy.mil/
3.17.3 ECPs - The Government will maintain configuration control and change authority for all modifications or changes affecting form, fit, function, or interface parameters of the Equipment and its sub-assemblies. The Contractor must submit an Engineering
Change Proposal (ECP) for any Class I or II changes that impact the Equipment covered by this contract. ECPs must be prepared in Contractor format, and must include the following information:
a. The change priority, change classification (Class I or Class II),
and change justification.
b. A complete description of the change to be made and the need for
that change.
c. A complete listing of other Configuration Items impacted by the
proposed change and a description of the impact on those CIs.
d. Proposed changes to documents controlled by the Government.
e. Proposed serial/lot number effectivities of units to be
produced in, or retrofitted to, the proposed configuration.
f. Recommendations about the way a retrofit should be accomplished.
g. Impacts to any logistics support elements (such as software,
manuals, spares, tools, and similar) being utilized by Government
personnel in support of the product.
h. Impacts to the operational use of the product.
i. Complete estimated life-cycle cost impact of the proposed change.
j. Milestones relating to the processing and implementation of the
engineering change.
3.18 Mercury Free - Mercury and mercury containing compounds must not be intentionally added or come in direct contact with hardware or supplies furnished under this contract. Mercury contamination of the material will be cause for rejection.
3.19 NAVSEA 0948-LP-045-7010 - Any applicable requirements of NAVSHIPS 4410.17,NAVSEA 0948-LP-045-7010, or 0948-045-7010 which the contractor must meet are included in this contract/purchase order. The above documents are for GovernmentUse Only. Further
application of the above documents is prohibited.prohibited.
3.19.1 Marking of material with a Material Designator per the Drawing is also prohibited, with the exception of Fasteners. Fasteners must be marked with a Material Symbol/Designator as specified elsewhere in this contract.
^ QUALITY ASSURANCE REQUIREMENTS ^
3.20 See CDRL DI-MISC-80678 (Test Certification) - A statement of tests performed, listing the pieces tested must be furnished along with a copy of the test results. Certification must include the contractor's name, address and date, quantity inspected,
identified to the contract/purchase order and item number, and the Contractor's or authorized personnel's signature. Test certifications must reference the standard/specification, including the revision, to which the testing was performed and the acceptance
criteria used. Test procedure numbers may also be referenced on test reports. Test reports on weldments must be identified to weld joint and layer.
3.21 See CDRLs DI-MISC-80875 (welding procedures) and DI-MISC-80876 (weld procedure qualification data) - When production or repair welding is required, the applicable welding procedure(s) and qualification data must be submitted for review and approval. In
addition, the CONSUMED WELD METAL C of C as defined below must be submitted as part of the certification OQE package submitted by the Contractor.
Note: These requirements do not apply to tack/spot welds.
3.21.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair).
3.21.2 If the Contractors qualification data has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the procedures and qualification data report to expedite the approval process. The
approval letter must reference the applicable welding procedure and qualification data report identification/number. Prior approval does not guarantee acceptance for this or any future contracts. As far as practical, all procedures for the contract must be
submitted at the same time. Welding procedures and qualification data must be submitted in a commercially available electronic format such as Adobe Acrobat PDF. The contractor must state the applicability of each weld procedure and qualification data submitted,
citing the drawing number and pieces to be welded. (i.e. "WP-123 and QD-123 are submitted for the weld joint between pieces 1 and 2 on drawing ABC." WP-456 and QD-456 are submitted for the hardfacing of piece 3 on drawing XYZ.")
3.21.3 The PCO's authorization for the use of weld procedure(s) and qualification data for the specific application as submitted does not mitigate the vendors responsibility to comply with the requirements of S9074-AQ-GIB-010/248, S9074-AR-GIB-010A/278, and
the contract.
3.21.4 Authority for the repair of Special Repairs in castings, the repair of wrought material, or the repair of forged material must be obtained via request for waiver from the Procurement Contracting Officer. This request must describe the defect; including
size, depth, location, and a description of the proposed repair. Repairs deemed minor or nominal in accordance with S9074-AR-GIB-010/278 can be made at contractor discretion in accordance with S9074-AR-GIB-010/278 requirements; however, Weld Procedure
Specification (WPS) and Procedure Qualification Record (PQR) submittals are still required. This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application.
3.21.5 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 72 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 72 hour time limit may be modified upon mutual
agreement between the vendor and DCMA.
3.21.6 When drawings require hardfacing surface Iron or Nickel content not to exceed 5%, the contractor must verify surface Iron or Nickel content by performing chemical testing as defined by the applicable drawing. The chemical test results must be submitted
as part of the qualification data.
3.21.7 Additional qualification requirements for production hardfacing thickness less than 1/8-inch: Macro-etch (or legible photomacrographs clearly showing the fusion area) must be submitted for review and show consistent, minimized dilution. All essential
elements and any elements not listed in S9074-AQ-GIB-010/248 that influence dilution must be in the qualification data and weld procedure, with strict limits placed on each essential element.
3.21.8 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of S9074-AR-GIB-010A/278.
3.21.9 When production or repair welding is required on titanium materials, the applicable fabrication plan, facilities procedure, training plan, and active welder qualification must also be submitted for review and approval.
3.21.10 If the contractor's fabrication plan, facilities procedure, training plan, or active welder qualification has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the applicable
documentation to expedite the approval process. The approval letter must reference the applicable documentation. Prior approval does not guarantee acceptance for this or any future contracts. The contractor's fabrication plan, facilities procedure, training
plan, and active welder qualification must be submitted at the same time as the applicable welding procedure(s) and weld procedure qualification data. All documentation must be submitted in a commercially available electronic format, such as Adobe Acrobat PDF.
3.21.11 See CDRL DI-MISC-80678 (Consumed Weld Metal) - A Certificate of Compliance is required for all weld filler metals used for production or repair welding, and must include the following:
a) Filler Metal LOT number(s)
b) Specification and Type
c) A positive statement that the vendor has obtained OQE and verified that each LOT of weld filler material conforms to specification requirements.
d) A positive statement verifying that the weld filler metals were the correct material type or grade prior to consumption.
3.21.12 When production welds or repair welds are performed by a subcontractor, the requirement for submission of all certification documentation required herein must be passed down to the subcontractor.
3.22 See CDRLs DI-MISC-80875 (Brazing Procedures) and DI-MISC-80876 (Braze Proc Qual Data) - Prior to performing any brazing, the applicable brazing procedure qualification data must be submitted. Brazing procedures must be submitted for information with
the supporting procedure qualification data. Brazing Procedures and Qualification Data must be submitted in a commercially available electronic format, such as Adobe Acrobat PDF. If the Contractor's qualification data has previously been approved by the Navy
for this or other contracts, a copy of the original approval letter must besubmitted in lieu of the qualification data. (Note: Letters extendingapproval of qualification data based on previous approvals are not acceptableto fulfill this requirement. The
approval letter must reference the applicable brazing procedure and/or brazing procedure qualification data number.)
3.23 Quality System Requirements - The Contractor furnishing items under this contract/purchase order must provide and maintain a quality system in accordance with ISO-9001 as amplified or modified herein, with the calibration system requirements of ISO-10012
or ANSI-Z540.3 with ISO-17025. A Quality System in accordance with MIL-I-45208, with the calibration system requirements of MIL-STD-45662, is acceptable as an alternate.
3.23.1 The Contractor's quality system and products supplied under the system are subject to evaluation, verification inspection, and acceptance/nonacceptance by the Government representative to determine the system's effectiveness in meeting the quality
requirements established in the Contract/Purchase Order.
3.23.2 The Contractor's quality system must be documented and must be available for review by the Contracting Officer or his representative prior to initiation of production and throughout the life of the contract. The Prime Contractor must, upon
notification, make his facilities available for audit by the contracting Officer or his authorized representative.
3.23.3 See CDRL DI-QCIC-81110 (Inspection System Procedures) - All suppliers of Level I/SUBSAFE (LI/SS) material are required to submit a copy of their current documented quality system procedures to the Procurement Contracting Officer (PCO) prior to award of
any contract/purchase order. Suppliers that have a copy of their current quality system procedures on file at the Procuring Activity may request the PCO waive this requirement.
3.23.4 This contract provides for the performance of Government Quality Assurance at source. The place or places of performance may not be changed without the authorization of the Procurement Contracting Officer. Upon receipt of this order, promptly
notify the Government representative who normally services your plant so that appropriate planning for Government inspection can be accomplished. If you do not have an assigned Government representative, notify the nearest Defense Contract Management Agency
(DCMA) Office. In the event that a local Government representative or DCMA Office cannot be located, our purchasing agent should be notified immediately.
3.23.5 Any changes made by the Contractor to a qualified quality system will require re-submittal to the PCO and concurrence by the Government Quality Assurance Representative prior to adoption.
3.24 Contractor Inspection Requirements - The Contractor must maintain adequate records of all inspections and tests. The records must indicate the nature and number of observations made, the number and type of deficiencies found, the quantities approved and
rejected and the nature of corrective action taken as appropriate. Inspection records must be traceable to the material inspected.
3.24.1 The supplier's gages, measuring and test equipment must be made available for use by the Government representative when required to determine conformance with Contract requirements. When conditions warrant, the supplier's personnel must be made
available for operations of such devices and for verification of their accuracy and condition.
3.24.2 All documents and reference data applicable to this contract must be available for review by the Government representative. Copies of documents required for Government inspection purposes must be furnished in accordance with the instructions provided
by the Government representative.
3.25 Subcontractor Inspection Requirements - The Government has the right to inspect at source, any supplies or services that were not manufactured or performed within the contractor's facility. Such inspection can only be requested by or under authorization
of the Government representative. Any purchasing documents to a subcontractor must cite the applicable portions of the contractually invoked quality system (e.g. calibration requirements), plus any product requirements that apply to the supplies being
purchased. When the Government elects to perform source inspection at the subcontractor's facility, applicable purchase documents must be annotated with the following statement: "A Government inspection is required prior to shipment from your plant. Upon
receipt of this order, promptly notify the Government representative who normally services your plant so that appropriate planning for Government inspection can be accomplished. If you do not have an assigned Government representative, notify the nearest
Defense Contract Management Agency (DCMA) Office. In the event that a local Government representative or DCMA Office cannot be located, our purchasing agent should be notified immediately."
3.25.1 The prime contractor's program must include procedures to assess the capability of the prospective suppliers to produce the products or supply the services in accordance with the contract, prior to the issuance of any purchase document.
3.25.2 Each sub-tier supplier of material or services for items in Section 3 of this contract must be subjected to a periodic review or audit by the Prime to determine the continued capability of the supplier to control the quality of the products or services
specified in the purchase order or contract.
3.25.3 The prime contractor must ensure that the purchased product conformsto specified purchase requirements and this contract. The type and extent of control applied to the supplier and the purchased product must be dependent upon the effect of the
purchased product on the end item represented by this contract.
3.25.4 The prime contractor must evaluate the requirements of the contractand select suppliers based on their ability to supply the product in accordance with the prime contractor's requirements and the contract. Criteria for selection and evaluation must be
established. Records of this effort must be available for review by the government.
3.25.5 The prime contractor's supplier quality assurance program must provide for a review of purchase documents to assure applicable quality requirements are included or referenced in the documentation for compliance by the supplier.
3.26 Government Furnished Material and/or Equipment (GFM/GFE) - When material or equipment is furnished by the Government, the Contractor must develop documented control procedures that require at least the following:
3.26.1 Visual examination upon receipt to detect damage during transit.
3.26.2 Inspection for completeness and proper type.
3.26.3 Verification of material quality received.
3.26.4 Periodic inspection and precautions to assure adequate storage conditions and to guard against damage from handling and deterioration during storage.
3.26.5 Functional testing, either prior to or after installation, or both, as required by the Contract to determine satisfactory operation.
3.26.6 Identification and protection from improper use or disposition.
3.26.7 Reporting to the Government, any GFM or GFE property found damaged, malfunctioning, or otherwise unsuitable for use. In the event of damage or malfunction during or after installation, the supplier must determine and record probable cause and
necessity for withholding the material from use.
3.26.8 For GFE material, and as required by the terms of the bailment agreement, the supplier must establish procedures for adequate storage, maintenance, and inspection of bailed Government material. Records of all inspection and maintenance performed on
bailed property must be maintained.
3.26.9 Material returned to the contractor must be handled as GFM.
3.27 Traceability and Certification Requirements - To assure that correct materials are installed in Level I/SUBSAFE systems, it is imperative that traceability be maintained from the material to the material certification test report and other required
Objective Quality Evidence (OQE). The material certification report must completely and accurately reflect that the material supplied meets the specified requirements. Materials requiring Traceability and Certification Data are identified within Paragraph 3,
Section C of this contract/purchase order.
3.27.1 The following provides the minimum requirements for maintaining material traceability and supplements the requirements

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