1、 AMSC N/A FSC4920 MIL-PRF-83323C 15 March 2010 SUPERSEDING MIL-PRF-83323B 1 November 1997 PERFORMANCE SPECIFICATION TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specificati
2、on covers a type of universal aerial refueling receptacle ground tester (UARRGT) to be used in functionally testing receiver aircraft using the boom-receptacle method of aerial refueling. 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in sections 3, 4, or 5 o
3、f this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specifi
4、ed requirements of documents cited in sections 3, 4, or 5 of this specification, whether or not they are listed. 2.2 Government documents. 2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handbooks form a part of this document to the extent specified herei
5、n. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. FEDERAL STANDARDS FED-STD-595/26173 Ocean Gray, NAVSEA DEPARTMENT OF DEFENSE SPECIFICATIONS MIL-A-25896 Adapter, Pressure Fuel Servicing, Aircraft, Nominal 2-1/2 Inch Diameter MIL-A-8625 Ano
6、dic Coatings for Aluminum and Aluminum Alloys MIL-C-8605 Cap; Pressure Fuel Servicing MIL-DTL-83413/7 Connectors and Assemblies, Electrical, Aircraft Grounding, Grounding Clamp MIL- DTL -83413/10 Connectors and Assemblies, Electrical, Aircraft Grounding, Jumper Cable Comments, suggestions, or questi
7、ons on this document should be addressed to 642 CBSG/GBEC, 460 Richard Ray Blvd, Suite 200, Robins AFB, GA 31098-1813. Since contact information can change, you may want to verify the currency of this address information using the ASSIST Online database at https:/assist.daps.dla.mil/online . INCH-PO
8、UND Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-83323C 2 MIL-F-8615 Fuel System Components, General Specification for (ASG) MIL-DTL-83511 Headset Microphone and Headset Electrical (Medium Nose Attenuation, Hearing Protective), General Spe
9、cifications For MIL-DTL-83511/2 Headset - Microphone, H-157A/AIC MIL-DTL-3661 Lamp holders, Indicator Lights, Indicator-Light Housings, and Indicator- Light Lenses, General Specification for MIL-L-3661/35 Lenses, Indicator Light, Watertight, Style Lc3 MIL-DTL-3661/47 Lamp holders, Housing, Indicator
10、-Light, Watertight, Style LH89 MIL-PRF-10304/32 Meter, Electrical Indicating, Panel Type, Ruggedized; Voltmeter, DC (Flush Mounting, Round Flange, 1 inch), Styles, 05,06 and 07. MIL-PRF-23377 Primer Coating: Epoxy, High-Solids MIL-PRF-94/3 Resistor, Variable, Composition General Specific Style RV6 M
11、IL-DTL-5624 Turbine Fuel, Aviation, Grades JP-4, JP-5, and JP-5/JP-8 ST MIL-PRF-7024 Calibrating Fluids, Aircraft Fuel System Component MIL-PRF-85285 Coating: Polyurethane, High-Solids MIL-R-27521 Receptacle, Flying Boom, Aerial Refueling MIL-DTL-8834 Switch, Toggle, Positive Break General Specifica
12、tion for MIL-S-38449 Signal and Signal/Intercommunication Amplifiers, Universal, Aerial Refueling MIL-DTL-83133 Turbine Fuels, Aviation, Kerosene Types, NATO F-34 (JP-8) and NATO F-35 DEPARTMENT OF DEFENSE STANDARDS MIL-STD-130 Identification Marking of US Military Property MIL-STD-464 Electromagnet
13、ic Environmental Effects Requirements For Systems MS24484 Adapter, Pressure Fuel Servicing, Nominal 2.5 Inch Diameter MS27604 Nozzle-Universal Aerial Refueling Tanker Boom MS29520 Envelope Dimensions Nozzle, Pressure Fuel Servicing Locking Aircraft, Type D-1, D-1R, D-2 and D-2R MS29526 Cap-Pressure
14、Fuel Servicing, Nominal 2-1/2 Inch Diameter Non-Flush Type MS8005 Hose Assembly Permanently Attached Fittings, Tetrafluoroethylene High Temperature, MS90310 Switch, Toggle, Positive Break, Miniature, Toggle Sealed, Solder Lug, Single Pole, 469 Mounting Bushing (Copies of these documents are availabl
15、e online at https:/assist.daps.dla.mil/quicksearch/ or https:/assist.daps.dla.mil/online . or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.) 2.2.2 Other Government documents, drawings, and publications. The following other Government docu
16、ments, drawings, and publications form a part of this specification, to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. AIR FORCE GUIDE SPECIFICATION AFGS-87154 FUEL SYSTEMS GENERAL DESIGN SPECIFICATION FOR (Copi
17、es of Guide Specifications are available from Global Engineering Documents, or at http:/ . Phone number: 1-800-854-7179.) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-83323C 3 2.3 Non-Government publications. The following document forms a
18、 part of this document to the extent specified herein. Unless otherwise specified, the issues of the documents which shall be DoD adopted are those listed in the Acquisition Streamlining and Standardization Information System (ASSIST) database, cited in the solicitation. Unless otherwise specified,
19、the issues of documents not listed in the ASSIST database, cited in the solicitation (see 6.2). AMERICAN SOCIETY OF MECHANICAL ENGINEERS (ASME) ASTM D 471 Standard Test Method for Rubber Property Effect of Liquids (ASTM standards may be obtained from ASTM International, 100 Barr Harbor Drive, P.O. B
20、ox C700, West Conshohocken, PA 19428-2959. Electronic copies of ASTM standards may be obtained from http:/www.astm.org ) XAR INDUSTRY DRAWING XAR INDUSTRIES 7034 RECEPTACLE, UNIVERSAL, UARRSI (Copies of the above drawing are available by contacting X A R Industries Inc, 711 E Walnut St Ste 102, Pasa
21、dena, CA 91101-4401) SOCIETY AEROSPACE ENGINEERING (SAE) SAE-ARP 868 Pressure Drop Test for Fuel system Components SAE-AS31061 Connector, Plug, Electric, Straight, Solder Contacts, AN Type SAE-AS50151 Connectors, Electrical, Circular Threaded, AN Type, General Specification for SAE-AS5877 Detailed s
22、pecification for aircraft pressure refueling nozzle. (SAE documents may be obtained at http:/www.sae.org/servlets/index or from SAE, Inc., 400 Commonwealth Drive, Warrendale PA 15096.) 2.4 Order of precedence. Unless otherwise noted herein or in the contract, in the event of a conflict between the t
23、ext of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 3. REQUIREMENTS 3.1 First Article. First article testing is required unless o
24、therwise specified. 3.2 Components. The tester and its container shall consist of the following components which shall be integral or included parts of the assembly: Tester a. Universal Aerial Refueling (AR) Nozzle b. Nozzle Dust Cover c. Pressure Fuel Servicing Adapter d. Adapter Dust Cap e. Body (
25、Reducer) with Bleed Valve Provisions f. Handle Assembly g. Electrical box (1) Oscilloscope connector (2) Telephone jack or other suitable headset connection (3) Electrical harness and connector (4) Recharging connection (5) On-off/reset switch (6) Voltmeter and voltage switch (7) Indicator lights Pr
26、ovided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-83323C 4 (8) Intercommunication switch (9) Signal switch (10) Signal amplifier (11) 28-Volt (28V) rechargeable batteries (nickel-cadmium sealed) (12) Headset amplifier with volume control (13) Bat
27、tery charger h. Bleed Valve Assembly Container a. Battery Charging Harness b. Charging Indicator Light - (Incorporated in Electric Box Item #14) c. Pedestal/Sliding Valve Assembly Removal Tool d. Headset, Adapter, Cable 3.3 Materials and manufacturing processes. All materials and processes used in t
28、he manufacturing of the tester and the tester container shall be resistant to fuel conforming to MIL-DTL-5624(JP-4), MIL-DTL-83133 (JP-8), or to fluid conforming to ASTM D 471 (types I and III having an aromatic content from 0 to 30 percent), or to fluid conforming to MIL-C-7024, Type III, calibrati
29、ng fluid, where environmental testing with aromatics is not required. The use of magnesium and copper or alloys of either of these metals is prohibited. Teflon shall not be used for gaskets, seals or packings in any location where an impact load is encountered. Castings shall be capable of withstand
30、ing the structural loads as specified in 3.5.11 and shock loads of 4.4.12.1 3.4 Design. The tester shall be designed to engage with a boom receptacle slipway installation conforming to MIL-R-27521 and MIL-F-87154. The opposite end shall permit the engagement of a Type D-1 nozzle, conforming to SAE-A
31、S5877 and MS29520, for fuel transfer. Upon engagement by ground personnel, the tester shall be held in place by the hydraulic toggles of the receptacle. The use of the tester shall permit checking of the electrical circuitry, the intercommunications capability via use of the headset/headset amplifie
32、r and the receptacle induction coil, and the function of the receptacle toggles and contact and latch switches. Use of the tester shall also permit transferring of fuel to perform leakage checks and other related receptacle and aerial refueling system checks. Maximum envelope size and angular relati
33、onship shall be in accordance with Figure 1. The tester shall include a fluid bleed valve, which allows evacuation of air from the unit prior to usage. A drain hose shall be provided. Also provided will be a utility carrying handle, attached to the body and handle assembly. (3.6.6). 3.4.1 Finish. Al
34、l aluminum-alloy parts shall be anodized or adequately treated in some other acceptable manner for corrosion prevention. The nozzle head (MS27604) shall be hard-coat anodized. The pedestal/sliding valve assembly removal tool (3.6.26) shall be non-dyed red and utility carrying handle which shall be d
35、yed black. Steel parts, not in moving contact with other parts, shall be chrome plated or adequately treated in some other acceptable manner for corrosion prevention. Cadmium plating shall not be used. Corrosion-resisting steel parts shall be passivated. The electrical box (3.6.10) shall be electrod
36、eposited, tin lead or solder dip plating, using mattered flow or flow brightened finish procedure. 3.4.2 Paint. Areas which require paint, except for the electrical box, shall receive two coats of zinc chromate primer for aluminum surfaces. The tester shall be color coded to indicate fuel use. The e
37、lectrical box shall be primed per MIL-P-23377, Type 1, Class 1, and painted with FED-STD-595/26173 Ocean Gray, NAVSEA. No paint shall be permitted in areas where it could be introduced into the fuel passage. 3.5 Operating requirements. The tester shall be capable of operating under the following con
38、ditions and be capable of meeting the following requirements: 3.5.1 Dielectric Strength. The tester electrical system and induction coal shall be capable of withstanding a surge of 1,000V rms, 60 Hz, between test points for 1 minute. 3.5.2 Noise Susceptibility. The tester shall not advance from READ
39、Y to CONTACT or from CONTACT to DISCONNECT when the signal leads are subjected to high-frequency noise bursts (broad band RF) for a maximum time duration of one millisecond and a minimum voltage amplitude of 200V peak-to-peak. These bursts are Provided by IHSNot for ResaleNo reproduction or networki
40、ng permitted without license from IHS-,-,-MIL-PRF-83323C 5 generally associated with the actuation of reactive solenoids. 3.5.3 Fuel Pressure and Leakage. The tester shall be capable of withstanding operating, proof, and burst pressures of 120, 240, and 360 lbs per square inch gage (psig) respective
41、ly under the conditions specified herein. There shall be no fuel leakage during any pressure and transfer conditions except during disconnects. The leakage during a normal disconnect without pressure shall not exceed 25 cubic centimeters (cc). The leakage during disconnects initiated under pressure
42、shall not exceed 50 cc. 3.5.4 Pressure Drop. The pressure drop shall not exceed 18 psig, at a fuel flow of 600 gallons per minute (gpm), when the tester is engaged with the receptacle and the D-1 refueling nozzle is connected to the tester. 3.5.5 Fuel Resistance and Extreme Temperature. The tester s
43、hall withstand the fuel resistance and extreme temperature test as specified herein without fuel leakage or malfunction. 3.5.6 Contaminated Fuel Endurance. The tester shall withstand the contaminated fuel endurance test as specified herein without fuel leakage or malfunction. 3.5.7 Endurance. The te
44、ster shall be capable of operating for 5,000 cycles as specified in Section 4, without deterioration, deformation, corrosion, fuel leakage, or malfunction. 3.5.8 Compatibility. The tester shall be capable of meeting all performance requirements when engaged with the various receiver aircraft using t
45、he boom receptacle method of aerial refueling. 3.5.9 Bonding. The tester shall meet the requirements of MIL-B-5087 and this specification when tested as specified herein. 3.5.10 Induction Coil. The induction coil shall withstand immersion in fluid conformation to ASTM D 471, types I and III, without
46、 disintegration or deterioration and shall be capable of meeting the dielectric strength requirements specified herein after such immersion. 3.5.11 Structural Requirements. The tester shall be capable of withstanding the following loads: a. Tension limit load, body and nozzle - 3,000 lbs. b. Bending
47、 limit load, handles and structural attach points - 3,000 lbs. c. Compression limit load, nozzle - 6,000 lbs. NOTE: The tester shall be capable of withstanding the bending limit load applied to the outermost end of each handle. Any structural attach points shall also be capable of withstanding the 3
48、,000-pound tension limit load. The nozzle striker plates and nozzle tip shall be capable of withstanding the compression limit load. d. Tension, compression, and bending limit loads; elbow and index handle assembly - 1,000 lbs NOTE: The tester shall be capable of withstanding the tension, compressio
49、n, and bending limit loads when applied separately at the center of the elbow openings as follows: (1) Tension and compression loads applied in a direction parallel to the centerline of the elbow, and (2) Bending loads applied perpendicular to the centerline of the elbow and, by indexing the elbow assembly, in the three directions producing the greatest bending loads on the elbow. 3.5.12 Temperature and altitude.
