1、*USACE / NAVFAC / AFCESA / NASA UFGS-33 52 43.28 (February 2010)-Preparing Activity: USACEUNIFIED FACILITIES GUIDE SPECIFICATIONSReferences are in agreement with UMRL dated April 2010*SECTION TABLE OF CONTENTSDIVISION 33 - UTILITIESSECTION 33 52 43.28FILTER SEPARATOR, AVIATION FUELING SYSTEM02/10PAR
2、T 1 GENERAL1.1 REFERENCES1.2 SUBMITTALS1.3 PREPRODUCTION TESTING1.3.1 Inspection and Testing1.3.2 Deviations from API Spec 15811.3.3 Data Required Prior to Tests1.3.4 Submittal of Test Documents1.3.5 Required Preproduction Tests1.4 DESIGN CONDITIONS1.5 WORKMANSHIP1.6 CLEANINGPART 2 PRODUCTS2.1 WELDI
3、NG2.2 MATERIALS AND EQUIPMENT2.2.1 Housing2.3 FILTER SEPARATOR CONSTRUCTION2.3.1 Housing Vessel2.3.2 Legs2.3.3 Inlet and Outlet Connections2.3.4 Manual Drain Valve2.3.5 Sight Gauge2.3.6 Differential Pressure Gauge2.3.7 Automatic Air Eliminator and Pressure Relief Valves2.3.8 Sampling Connections2.3.
4、9 Spider Assembly2.3.10 Coalescer and Separator Cartridges2.3.11 Control Valve Accessories2.3.11.1 Float Control Pilot and Tester2.3.12 Identification of Product2.3.13 Assembly2.4 MICRONIC PRE-FILTER CONSTRUCTION2.4.1 Product Submittals2.4.2 Housing VesselSECTION 33 52 43.28 Page 1Provided by IHSNot
5、 for ResaleNo reproduction or networking permitted without license from IHS-,-,-2.4.3 Legs2.4.4 Inlet and Outlet Connections2.4.5 Manual Drain Valve2.4.6 Sight Gauge2.4.7 Differential Pressure Gauge2.4.8 Automatic Air Eliminator and Pressure Relief Valves2.4.9 Sampling Connections2.4.10 Spider Assem
6、bly2.4.11 Filter Cartridges2.4.12 Identification of Product2.4.13 Assembly2.5 ACCESSORIES2.5.1 Manual Drain Valve2.5.2 Sight Gauge2.5.3 Differential Pressure Gauge2.5.4 Automatic Air Eliminator and Pressure Relief Valves2.5.5 Sampling ConnectionsPART 3 EXECUTION3.1 INSTALLATION3.1.1 Anchoring3.1.2 G
7、routing3.1.3 Leveling and Aligning3.1.4 Painting- End of Section Table of Contents -SECTION 33 52 43.28 Page 2Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-*USACE / NAVFAC / AFCESA / NASA UFGS-33 52 43.28 (February 2010)-Preparing Activity: USACEUN
8、IFIED FACILITIES GUIDE SPECIFICATIONSReferences are in agreement with UMRL dated April 2010*SECTION 33 52 43.28FILTER SEPARATOR, AVIATION FUELING SYSTEM02/10*NOTE: This guide specification covers the requirements for filter separators and fuel quality monitors used in aircraft refueling systems cons
9、tructed to the requirements of the DoD Type III/IV/V, and Cutn Cover Hydrant Refueling System Standards. DoD Type III systems shall conform to Standard Design 078-24-28 PRESSURIZED HYDRANT FUELING SYSTEM (TYPE III). DoD Type IV/V systems shall conform to Standard Design 078-24-29 AIRCRAFT DIRECT FUE
10、LING SYSTEM (TYPE IV) DESIGN.Edit this guide specification for project specific requirements by adding, deleting, or revising text. For bracketed items, choose applicable items(s) or insert appropriate information.Remove information and requirements not required in respective project, whether or not
11、 brackets are present.Comments and suggestion on this specification are welcome and should be directed to the technical proponent of the specification. A listing of the technical proponents, including their organization designation and telephone number, is on the Internet.*PART 1 GENERAL1.1 REFERENC
12、ES*NOTE: This paragraph is used to list the publications cited in the text of the guide specification. The publications are referred to in the text by basic designation only and listed in this paragraph by organization, designation, date, and title.Use the Reference Wizards Check Reference feature w
13、hen you add a RID outside of the Sections SECTION 33 52 43.28 Page 3Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Reference Article to automatically place the reference in the Reference Article. Also use the Reference Wizards Check Reference featur
14、e to update the issue dates.References not used in the text will automatically be deleted from this section of the project specification when you choose to reconcile references in the publish print process.*The publications listed below form a part of this specification to the extent referenced. The
15、 publications are referred to in the text by basic designation only.AMERICAN PETROLEUM INSTITUTE (API)API Spec 1581 (2002; Addenda 2006) Specifications and Qualification Procedures for Aviation Jet Fuel Filter/SeparatorsASME INTERNATIONAL (ASME)ASME B16.5 (2009) Standard for Pipe Flanges and Flanged
16、 Fittings: NPS 1/2 Through NPS 24ASME B31.3 (2008) Process PipingASME BPVC SEC VIII D1 (2007; Addenda 2008; Addenda 2009) Boiler and Pressure Vessel Code; Section VIII, Rules for Construction of Pressure Vessels Division 1ASTM INTERNATIONAL (ASTM)ASTM C 827 (2001a; R 2005) Change in Height at Early
17、Ages of Cylindrical Specimens from Cementitious MixturesSOCIETY OF AUTOMOTIVE ENGINEERS INTERNATIONAL (SAE)SAE AMS-P-5315 (2001, Rev A) Butadiene - Acrylonitrile (NBR) Rubber For Fuel-Resistant Seals 60 To 70U.S. DEPARTMENT OF DEFENSE (DOD)MIL-HDBK-831 (1999; Not 1) Preparation of Test ReportsMIL-PR
18、F-4556 (1999; Rev F; Am 1) Coating Kit, Epoxy, for Interior of Steel Fuel TanksMIL-STD-130 (Rev N) Identification Marking of U.S. Military PropertyU.S. GENERAL SERVICES ADMINISTRATION (GSA)CID A-A-1923 (Rev A; Notice 1) Shield, Expansion (Lag, Machine and Externally Threaded Wedge Bolt SECTION 33 52
19、 43.28 Page 4Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Anchors)1.2 SUBMITTALS*NOTE: Review submittal description (SD) definitions in Section 01 33 00 SUBMITTAL PROCEDURES and edit the following list to reflect only the submittals required for t
20、he project. Submittals should be kept to the minimum required for adequate quality control.A “G” following a submittal item indicates that the submittal requires Government approval. Some submittals are already marked with a “G”. Only delete an existing “G” if the submittal item is not complex and c
21、an be reviewed through the Contractors Quality Control system. Only add a “G” if the submittal is sufficiently important or complex in context of the project.For submittals requiring Government approval on Army projects, a code of up to three characters within the submittal tags may be used followin
22、g the “G“ designation to indicate the approving authority. Codes for Army projects using the Resident Management System (RMS) are: “AE“ for Architect-Engineer; “DO“ for District Office (Engineering Division or other organization in the District Office); “AO“ for Area Office; “RO“ for Resident Office
23、; and “PO“ for Project Office. Codes following the “G“ typically are not used for Navy, Air Force, and NASA projects.Choose the first bracketed item for Navy, Air Force and NASA projects, or choose the second bracketed item for Army projects.*Government approval is required for submittals with a “G“
24、 designation; submittals not having a “G“ designation are for Contractor Quality Control approval. information only. When used, a designation following the “G“ designation identifies the office that will review the submittal for the Government. Submit the following in accordance with Section 01 33 0
25、0 SUBMITTAL PROCEDURES:SD-02 Shop DrawingsFilter Separator; G; G, _.Micronic Pre-filter; G; G, _.SD-03 Product DataFilter Separator; G; G, _.Micronic Pre-filter; G; G, _.SD-07 CertificatesFilter Separator.Micronic Pre-filter.SECTION 33 52 43.28 Page 5Provided by IHSNot for ResaleNo reproduction or n
26、etworking permitted without license from IHS-,-,-SD-10 Operation and Maintenance DataFilter Separator; G; G, _.Micronic Pre-filter; G; G, _.1.3 PREPRODUCTION TESTING*NOTE: Contact the Naval Facilities Engineering Command (NAVFACENGCOM) or the Coprs of Engineers (COE) for direction on selection. For
27、COE projects, include in the MOU the specific Air Force representatives to be notified when factory filter separator test dates are submitted to the Contracting Officer.Er.*Prior to construction of filter separators (FSI-1 THROUGH FSI-_, FSR-_, THROUGH FSR-_) for the project, preproduction tests sha
28、ll have been conducted in the presence of Det 3, WR-ALC/AFTH Technical Assistance Team Air Force Petroleum Office Wright-Patterson AFB, OH NAVAIR/NAFAC Army Petroleum Center representative. Notify the Contracting Officer _ days prior to conductance of factory tests in order to schedule witnessing by
29、 representative.1.3.1 Inspection and TestingThe inspection and testing of the preproduction filter separator shall be conducted on a full-scale test system in accordance with API Spec 1581 and as specified herein. The test sample shall consist of a complete filter separator with elements installed.
30、Elements shall be representative of a production lot. The filter separator, coalescers, and separator screens shall be identified with the manufacturers part number.1.3.2 Deviations from API Spec 1581No deviations are allowed.1.3.3 Data Required Prior to TestsSubmit installation data to enable Gover
31、nment representative to verify that the equipment has been installed and operated correctly. Submit certification from the manufacturer that the test vessel has passed a hydrostatic pressure test, and that the design conforms to API Spec 1581, Category M M100, Type S. Submit two sets of assembly dra
32、wings of the test vessel and accessories for approval.1.3.4 Submittal of Test Documents*NOTE: Contact NAVFACENGCOM or COE for direction on selection. For NAVFACENGCOM Projects, the designer must consult with the engineer in charge (EIC) to determine the review input of the appopriate service. For CO
33、E projects, coordinate with appopriate service to determine which service agency will review test documents and ensure that mou and submittal register contain these requirements.SECTION 33 52 43.28 Page 6Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-
34、,-*The test report shall be submitted to the Command Fuel Facilities Engineer or Det 3, WR-ALC/AFTHNAVAIR/NAFAC Army Petroleum Center for Government approval. Prepare report in accordance with MIL-HDBK-831. In addition to results, the report shall contain complete records of the tests including data
35、 sheets, performance curves, chronological test records, photographs, sample calculations, test procedures, and a description of the test apparatus. Submit color photographs of the sample elements before and after tests. Submit one new coalescer element and one new separator element.1.3.5 Required P
36、reproduction Testsa. Examination. A visual examination of the filter separator housing and each element shall be performed to ensure compliance with the drawings and verify workmanship requirements.b. Hydrostatic Pressure Tests. The filter separator shall be subjected to a hydrostatic pressure test
37、in accordance with API Spec 1581, Section 3.2.2.11.1.c. Full Scale Performance Test. API Spec 1581 The filter/separator with a full set of coalescer and separator elements shall be tested in accordance with API Spec 1581 section 4.4 at 38 _ L/s 600 _ gpm (FSI-1 through FSI-_ ; FSR-1 and FSR-2) and75
38、 _ L/s 1200 _ gpm (FSR-1 and FSR-2).d. Coalescer Structural Test. A coaleser structural test shall be conducted in accordance with API Spec 1581 Section 4.5.e. Disassembly Inspection. Upon completion of the tests specified above, the filter separator shall be disassembled and inspected to determine
39、the condition of the coalescer and separator elements. Defects in the element such as swelling of the elements, or damaged gaskets shall be noted. Swelling of or damage to the elements or other parts shall be cause for rejection.1.4 DESIGN CONDITIONSDesign conditions shall be as specified in Section
40、 33 52 43.11 AVIATION FUEL MECHANICAL EQUIPMENT and as modified herein.1.5 WORKMANSHIPEach filter separator, including all parts and accessories, shall be free from blemishes, defects, burrs and sharp edges. The vessel shall exhibit accuracy of dimensions, accurate radii of fillets and complete mark
41、ing of parts and assemblies.1.6 CLEANINGComponents of the filter separators shall be cleaned to remove dirt; excess soldering; brazing, and welding flux; welding slag; loose, spattered, or excess solder; metal chips; and other foreign materials before, during and after assembly.SECTION 33 52 43.28 P
42、age 7Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-PART 2 PRODUCTS2.1 WELDINGWelding shall be in accordance with ASME B31.3.2.2 MATERIALS AND EQUIPMENT2.2.1 Housinga. Carbon steel with internal epoxy coating3003 or 6061 aluminum alloyType 304 or 31
43、6 stainless steel.b. Float Assembly. Stainless steel.c. Manual Drain Valve. Stainless steel.d. Sight Glass. Armored clear pyrex with nickel-copper alloyball checks.e. Differential Gauge. Corrosion resistant piston with stainlesssteel valves.f. Seperators. 75 um200 mesh stainless steel wire cloth, Te
44、flon coated on both sides, or synthetic mesh cloth.2.3 FILTER SEPARATOR CONSTRUCTION*NOTE: As required by the Command Fuels Facility Engineer or service headquarters. Coated carbon steel shall not be used for filter separator vessels on Navy/Marine Corps projects. Specify internally coated carbon steel vessel construction for Air Force projects.Indicate the operating height of the unit on the drawings. Note that the units support system (legs) may have to be structurally designed to meet pr
