NAVY MIL-A-25896 E-1983 ADAPTOR PRESSURE FUEL SERVICING NOMINAL 2 5 INCH DIAMETER《2 5英寸直径标定压力燃料服务电源适配器》.pdf
《NAVY MIL-A-25896 E-1983 ADAPTOR PRESSURE FUEL SERVICING NOMINAL 2 5 INCH DIAMETER《2 5英寸直径标定压力燃料服务电源适配器》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-A-25896 E-1983 ADAPTOR PRESSURE FUEL SERVICING NOMINAL 2 5 INCH DIAMETER《2 5英寸直径标定压力燃料服务电源适配器》.pdf(18页珍藏版)》请在麦多课文档分享上搜索。
1、MIL-A-25896E18 January 1983SupersedingMIL-A-25896D28 June 1976MILITARY SPECIFICATIONADAPTER, PRESSURE FUEL SERVICING,NOMINAL 2.5-INCH DIAMETERThis specification is approved for use by allDepartments and Agencies of the Department of Defense.1. SCOPE1.1 Scope This specification covers pressure fuel s
2、ervicing adapters having anominal line size of 2.5-inch diameter.2. APPLICABLE DOCUMENTS2.1 Government documents2.1.1 Specifications. standards, and handbooks. Unless otherwise specified,the following specifications, standards, and handbooks of the issue listed inthat issue of the Department of Defe
3、nse Index of Specifications and Standards(DODISS) specified in the solicitation form a part of this specification to theextent specified herein.SPECIFICATIONSFederalP-D-680 Dry Cleaning SolventQQ-P-416 Plating, Cadmium (Electrodeposited)TT-S-735 Standard Test Fluids; HydrocarbonPPP-B-601 Boxes, Wood
4、, Cleated-PlywoodPPP-B-636 Boxes, Shipping, FiberboardMilitaryMIL-P-116 Preservation, Methods OfMIL-G-5572 Gasoline, Aviation: Grades 80/87, 100/130, 115/145MIL-T-5624 Turbine Fuel, Aviation, Grades JP-4 and JP-5MIL-C-6021 Castings, Classification and Inspection ofMIL-I-8500 Interchangeability and R
5、eplaceability of component parts forAerospace VehiclesProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-A-25896EMIL-N-25027MIL-R-25988MIL-T-83133MIL-R-83248STANDARDSFederalFED-STD-151MilitaryMIL-STD-129MIL-STD-130MIL-STD-143MIL-STD-831MIL-STD-889MI
6、L-STD-1188MIL-STD-1523MS20995MS24484MS24694MS29520MS33540MS33588Nut, Self-locking, 250F, 450F and 800F, 125 KSI Ftu, 60 KSIFtu and 30 KSI FtuRubber, Fluorosilicone Elastomer, Oil- and Fuel-resistant,Sheets, Strips, Molded Parts, and Extruded ShapesTurbine Fuel, Aviation, Kerosene Type, Grade JP-8Rub
7、ber, Fluorocarbon Elastomer, High Temperature, Fluid andCompression Set ResistantMetals, Test MethodsMarking for Shipment and StorageIdentification Marking of U.S. Military PropertyStandards and Specifications, Order of Precedence for theSelection ofTest Reports, Preparation ofDissimilar MetalsComme
8、rcial Packaging of Supplies and EquipmentAge Controls of Age-sensitive Elastomeric MaterielWire, Safety or LockAdapter, Pressure Fuel Servicing, Nominal 2.5 Inch DiameterScrew, Machine, Flat Countersunk Head, 1000 Structural, CrossRecessed, UNC-3A and UNF-3AEnvelope Dimensions, Nozzle, Pressure fuel
9、 Servicing, Locking,Aircraft, Type D-1Safety Wiring and Cotter Pinning, General Practices forNut, Self-locking, Aircraft, Design and Usage; Limitations of (Copies of specifications, standards, drawings, and publications required bycontractors in connection with specific procurement functions should
10、beobtained from the procuring activity or as directed by the contractingofficer.)2.2 Order of precedence. In the event of a conflict between the text of thisspecification and the references cited herein, the text of this specificationshall take precedence.3. REQUIREMENTS3.1 Qualification. The adapte
11、rs furnished under this specification shall beproducts which are qualified for listing on the applicable qualified productslist at the time set for opening of bids (see 4.4 and 6.3).2Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-A-25896E3.2 Sel
12、ection of specifications and standards. Specifications and standardsfor necessary commodities and services not specified herein shall be selectedin accordance with MIL-STD-143, except as specified in 3.2.1 and 3.2.2.3.2.1 Commercial parts. Commercial parts having suitable properties may beused where
13、, on the date of invitation for bids or request for proposal, thereare no suitable standard parts. In any case, commercial utility parts, likescrews, bolts, nuts, and cotter pins having suitable properties may be used,provided:a. They can be replaced by the standard parts (AN, MS, or NAS) withoutalt
14、eration.b. The corresponding standard part numbers are referenced in the parts listand, if practicable on the contractors drawings.3.2.2 Standard parts. With the exceptions specified in 3.2.1, MS, AN, and NASstandard parts shall be used where they are suitable for the intended purpose.3.3 Materials.
15、 All materials shall be resistant to all fluids in accordancewith TT-S-735, MIL-G-5572, MIL-T-5624, and MIL-T-83133 as proven by successfulcompletion of the tests of 4.4.2.3.3.1 Metals. The portion of the adapter that supports the loads of 4.6.7shall have 40 KSI minimum yield strength. Metals shall
16、be inspected inaccordance with FED-STD-151. Alloys of magnesium and copper shall not be usedon parts that come into contact with fuel. Cadmium plating shall conform toclass 2, type II of QQ-P-416.3.3.2 Castings. Castings shall be clean, sound, and free from blowholes,porosity, cracks, or any other d
17、efects which would prevent the successfulcompletion of the tests of 4.6. The castings that support the loads of 4.6.7shall conform to MIL-C-6021, class 3, grade C.3.3.3 Dissimilar metals. Dissimilar metals in accordance with MIL-STD-889shall not be used in intimate contact unless they are protected
18、againstelectrolytic corrosion.3.3.4 Elastomers. Elastomers shall be in accordance with MIL-R-83248 orMIL-R-25988.3.3.5 Electrical conductivity. The resistance between the locking lugreference plane and the mounting surface shall be 0.010 ohms, maximum.3.4 Desire3.4.1 Interface. The adapter shall con
19、form to MS24484. When a MS29520 nozzleis secured to the adapter and opened or closed,the adapter shall open orclose, respectively. With the adapter installed in a test housing inaccordance with figure 1, the flow area around the adapter poppet when in thefull open position shall be a minimum of 4.8
20、square inches.3Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-A-25896EFIGURE 1 Test housing.4Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-A-258963.4.2 Locking of parts. All parts of the as
21、sembly shall be securely attached.Spring tension to hold parts in the assembly is not acceptable. All threadedparts shall be locked by safety wiring in accordance with MS20995, self-lockingnuts in accordance with MIL-N-25027, cotter pins, or other approved methods.Safety wire shall be installed in a
22、ccordance with MS33540. Self-locking nutsshall be used in accordance with MS33588; however, where loosening ordisengaging of a nut might result in the nut or other parts entering the fuelsystem, self-locking nuts shall not be used.3.4.3 Lubrication. The adapter shall require no lubricant.3.5 Perform
23、ance. The adapter shall be suitable for a temperature environmentas specified.a. Fuel: -55C (-67F) to +93C(+200F)b. Ambient: -55C (-67F) to +177C (+350F)The adapters shall satisfy the performance requirements when tested asspecified in section 4 herein.3.6 Interchangeability. Interchangeability shal
24、l be in accordance withMIL-I-8500.3.7 Weight. The weight of the adapter shall not exceed 1.0 pounds.3.8 Identification of product. Adapters shall be marked in accordance withMIL-STD-130. The minimum identification data is as follows:Adapter, Pressure Fuel ServicingMS24484-5Manufacturers identificati
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