SOLICITATION NOTICE
48 -- 48--VALVE,BALL, IN REPAIR/MODIFICATION OF
- Notice Date
- 7/1/2022 12:53:11 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
- N0010422QZB62
- Response Due
- 7/31/2022 10:00:00 PM
- Archive Date
- 08/16/2022
- Point of Contact
- Telephone: 7176054056
- E-Mail Address
-
TAMMY.LITTLE@NAVY.MIL
(TAMMY.LITTLE@NAVY.MIL)
- Description
- CONTACT INFORMATION|4|N742.2|GDHBB|7176054056|tammy.little@navy.mil| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2022)|19|||||||||||||||||||| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| TIME OF DELIVERY (JUNE 1997)|20|0001AA|2|330|||||||||||||||||| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Certifications - Stand-Alone Receiving Report Material - Receiving Report & Invoices |Certifications - Stand-Alone Receiving Report Material - Receiving Report & Invoices |TBD|N00104|TBD|TBD|N50286|TBD|||N/A||| ||| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|One year from delivery of item|one year from delivery of item||||| WARRANTY OF DATA--BASIC (MAR 2014)|2||| BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC(DEVIATION 2020-O0019) (MAR 2022))|3|||| NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (OCT 2020)(DEVIATION 2020-O0008)|1|| 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|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| 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| |D|0003.1 | Y|49998|0067198 DRAWING DATA=2621-827-05 |96169| Z| |D|0003.2 | Z|49998|0067997 DRAWING DATA=2621-827-05 |96169| Z| |D|0003.3 | Y|49998|0066584 DRAWING DATA=2621-827-05 |96169| Z| |D|0003.4 | Y|49998|0064848 DRAWING DATA=2621-827-05 |96169| Z| |D|0003.5 | Y|49998|0079962 DRAWING DATA=2621-827-05 |96169| Z| |D|0003.6 | Y|49998|0076925 DRAWING DATA=2621-827-05 |96169| Z| |D|0003.7 | Y|49998|0070166 DRAWING DATA=2621-827-05 |96169| Z| |D|0004 | S|49998|0048401 DRAWING DATA=2621-827-05 |96169| Z| |D|0004.1 | -|49998|0025321 DRAWING DATA=2621-827-05 |96169| Z| |D|0005 | K|49998|0053776 DRAWING DATA=2621-827-05 |96169| Z| |D|0005.1 | V|49998|0060374 DRAWING DATA=2621-827-05 |96169| Z| |D|0005.2 | Y|49998|0027296 DRAWING DATA=2621-827-05 |96169| Z| |D|0006 | S|49998|0060610 DRAWING DATA=2621-827-05 |96169| Z| |D|0007 | S|49998|0041136 DRAWING DATA=2621-827-05 |96169| Z| |D|0008 | Y|49998|0039834 DRAWING DATA=2621-827-05 |96169| Z| |D|0009 | S|49998|0059200 DRAWING DATA=2621-827-05 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S|49998|0065278 DRAWING DATA=2621-827-05 |96169| Z| |D|0185 | Y|49998|0044694 DRAWING DATA=2621-827-05 |96169| Z| |D|0186 | T|49998|0055911 DRAWING DATA=2621-827-05 |96169| Z| |D|0187 | S|49998|0050701 DRAWING DATA=2621-827-05 |96169| Z| |D|0188 | U|49998|0086937 DRAWING DATA=2621-827-05 |96169| Z| |D|0189 | Y|49998|0066843 DRAWING DATA=2621-827-05 |96169| Z| |D|0190 | T|49998|0067429 DRAWING DATA=2621-827-05 |96169| Z| |D|0191 | S|49998|0050349 DRAWING DATA=2621-827-05 |96169| Z| |D|0192 | S|49998|0062512 DRAWING DATA=2621-827-05 |96169| Z| |D|0193 | Y|49998|0047506 DRAWING DATA=2621-827-05 |96169| Z| |D|0194 | S|49998|0062403 DRAWING DATA=2621-827-05 |96169| Z| |D|0195 | Y|49998|0050812 DRAWING DATA=2621-827-05 |96169| Z| |D|0196 | S|49998|0063600 DRAWING DATA=2621-827-05 |96169| Z| |D|0197 | Y|49998|0051056 DRAWING DATA=2621-827-05 |96169| Z| |D|0198 | S|49998|0071191 DRAWING DATA=2621-827-05 |96169| Z| |D|0199 | S|49998|0048953 DRAWING DATA=2621-827-05 |96169| Z| |D|0200 | 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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|0266978 DRAWING DATA=5486332 |53711| G| |D|0001 | G|49998|0131198 DRAWING DATA=5486333 |53711| G| |D|0001 | G|49998|0285801 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 IF, 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 4 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 Self Locking Capscrew, Item 39 of drawing 5486331; 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 Hex Nuts, Items 21 and 22 of drawing 5486331; Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444 (Method C solvent removal techniques must not be used on thread) Acceptance - ;NASM25027; Attribute - Annealing and Age Hardening Item - ;Continuous Threaded Studs, Items 24 and 25 and Self Locking Cap Screw, Item 39 of drawing 5486331; Performance - QQ-N-286 Test - Weldability Test of ASTM-B369 material Item - ;Body, Item 6 and Tailpiece, Item 7 of drawing 5486332; Performance - ASTM-B369 Acceptance - ASTM-B369 Test - ;Hydrostatic Test; Item - ;Each Assembly; Performance - ;Paragraph 1.o of MS 5310-081-142; Acceptance - ;Paragraph 1.o of MS 5310-081-142; 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. 3.5 The pressure tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure tolerances arenot 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 / -0 PSIG. 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 the smallest graduation on an analog test pressure gauge, not to exceed 50 PSIG. For pressure tests 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. 3.6 Confidential Hydrostatic Test Pressures - When test pressures are confidential, certification must reference ;6984058 Rev A; and the item number to which the item was tested in lieu of the actual pressures. Any drawing requirement to mark the working pressure on the item does not apply and is strictly prohibited. 3.7 Ball Spherical Surface Waviness - Unless otherwise specified on drawing, all sealing area surfaces must have a spherical surface waviness which does not exceed 0.0005 inches of height per inch of spherical surface. Roughness and waviness ratings must apply in a direction which yields the maximum rating, normally perpendicular to the lay. 3.8 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.8.1 Fasteners that have been hot or cold headed or roll thread...
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