1、Comments, suggestions, or questions on this document should be addressed to: WR-ALC/GRVEB, 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 AMSC N/A FSC 2320
2、Distribution Statement A. Approved for public release; distribution is unlimited. MIL-PRF-32080A 01 November 2011 SUPERSEDING MIL-PRF-32080 1 March 2001 PERFORMANCE SPECIFICATION TRUCK, AIRCRAFT FUELING-DEFUELING, 6,000 GALLON, A/S32R-11 This specification is approved for use by the Department of th
3、e Air Force and is available for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification covers the requirements for one type of aircraft refueling cargo tank truck capable of refueling and defueling military and commercial aircraft on Government inst
4、allations worldwide. The aircraft refueling truck is compliant with all applicable Department of Transportation (DOT) regulations for transportation and is air transportable in C-130, C-17, and C-5 aircraft. 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in s
5、ections 3, 4, or 5 of 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 m
6、ust meet all specified requirements of documents cited in sections 3, 4, or 5 of this specification, whether or not they are listed. NOT MEASUREMENT SENSITIVE Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32080A 2 2.2 Government documents.
7、2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. FEDERAL STANDARDS FED-STD-297
8、 Rustproofing of Commercial (Nontactical) Vehicles FED-STD-595/14052 Green, Gloss FED-STD-595/24052 Green, Semi-gloss FED-STD-595/31136 Red, Flat or Lusterless FED-STD-595/33446 Tan FED-STD-595/37038 Black, Flat or Lusterless FED-STD-595/37875 White, Flat or Lusterless FED-STD-807 Trucks: Heavy Comm
9、ercial, 6X4 and 6X6, 19,500 to 30,000 KG (43,000 to 66,000 pounds) Gross Vehicle Weight Rating (GVWR) COMMERCIAL ITEM DESCRIPTIONS A-A-393 Extinguisher, Fire, Dry Chemical (Hand Portable) A-A-50696 Reels, Static Discharge, Grounding, 50 and 75 Foot Cable Lengths A-A-52557 Fuel Oil, Diesel; for Posts
10、, Camps, and Stations A-A-52624 Antifreeze, Multi Engine Type A-A-59326 Coupling Halves, Quick Disconnect, Cam locking Type DEPARTMENT OF DEFENSE SPECIFICATIONS MIL-DTL-5624 Turbine Fuel, Aviation, Grades JP-4 and JP-5 MIL-A-8625 Anodic Coatings for Aluminum and Aluminum Alloys MIL-B-18013/1 Battery
11、, Storage, Support Equipment MIL-DTL-25524 Turbine Fuel, Aviation, Thermally Stable MIL-A-25896 Adapter, Pressure Fuel Servicing, Nominal 2.5 Inch Diameter MIL-DTL-25959 Tie Down, Tensioners, Cargo, Aircraft MIL-PRF-27260 Tie Down, Cargo, Aircraft, CGU-1/B MIL-PRF-52308 Filter-Coalescer Element, Flu
12、id Pressure MIL-DTL-53030 Primer Coating, Epoxy, Water Based, Lead and Chromate Free MIL-DTL-53039 Coating, Aliphatic Polyurethane, Single Component, Chemical Agent Resist MIL-DTL-83133 Turbine Fuel, Aviation, Kerosene Type, JP-8 (NATO F-34), NATO F-35, and JP-8+100 (NATO F-37) Provided by IHSNot fo
13、r ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32080A 3 MIL-DTL-83413/10 Connectors and Assemblies, Electrical, Aircraft Grounding: Jumper Cable Assembly, Aircraft to Fuel Nozzle, Discharger, Electrostatic DEPARTMENT OF DEFENSE STANDARDS MIL-STD-130 Identificati
14、on Marking of U.S. Military Property MIL-STD-461 Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment MIL-STD-810 Environmental Engineering Considerations and Laboratory Tests MIL-STD-882 Standard Practice for System Safety MIL-STD-889 Dissimilar M
15、etals MIL-STD-1366 Transportability Criteria MIL-STD-1472 Human Engineering DEPARTMENT OF DEFENSE HANDBOOKS MIL-HDBK-470 Designing and Developing Maintainable Products and Systems MIL-HDBK-781 Reliability test methods, plans, and environments for engineering development, qualification, and productio
16、n MIL-HDBK-1223 Nontactical Wheeled Vehicles Treatment, Painting, Identification Marking and Data Plate Standards MIL-HDBK-1791 Designing for Internal Aerial Delivery in Fixed Wing Aircraft MIL-HDBK-1791 C-17 Appendix Designing for Internal Aerial Delivery in Fixed Wing Aircraft C-17 Appendix (Copie
17、s of these documents, except for MIL-HDBK-1791 C-17 Appendix, are available online at https:/assist.daps.dla.mil/quicksearch or https:/assist.daps.dla.mil or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094. A copy of MIL-HDBK-1791 C-17 Appen
18、dix can be obtained from the Procuring Contracting Officer (PCO) or requested by contacting Air Transportability Test Loading Agency (ATTLA) at 937-255-6296.) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32080A 4 FOREIGN SPECIFICATIONS EUR
19、O-ASIAN COUNCIL FOR STANDARDIZATION, METROLOGY AND CERTIFICATION GOST 10227 Fuels for Jet Engines, Specifications (Copies of these documents are available online at http:/www.gost.ru/wps/portal/pages.en.Main, from the Leninsky prospect, 9, Moscow, V-49, GSP-1, 119991, Russian Federation or English t
20、ranslations are available from various specification and standards publication technical services) UNITED KINGDOM MINISTRY OF DEFENSE Standard 91-87 Turbine Fuel, Aviation, Kerosine Type: Containing Fuel System Icing Inhibitor NATO Code: F-34 Joint Service Designation: AVTUR/ FSII Standard 91-91 Spe
21、cification and Qualification Procedures for Aviation Jet Turbine Fuel, Aviation Kerosine Type, Jet A-1 NATO Code: F-35 Joint Service Designation: AVTUR (Copies of these documents are available online at http:/www.dstan.mod.uk or from the UK Defence Standardization Room 1138, Kentigern House, 65 Brow
22、n Street, Glasgow G2 8EX) 2.2.2 Other Government documents, drawings, and publications. The following other Government documents, drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the s
23、olicitation or contract. DRAWINGS MS24484 Adapter, Pressure Fuel Servicing, Nominal 2.5 Inch Diameter LAWS AND REGULATIONS Code of Federal Regulations (CFR) 49CFR172.302 General Marking Requirements for Bulk Packaging 49CFR393 49CFR178 Federal Motor Carrier Safety Regulations Specifications for Pack
24、agings 49CFR178.346 Material and Thickness of Material 29CFR1910 Labor, Section XVII Occupational Safety and Health Administration (OSHA) Parts 1900-1999 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32080A 5 Federal Acquisition Regulation
25、(FAR) FAR 23.404 Agency Affirmative Procurement Programs National Institute of Standards and Technology (NIST) HDBK44 Section 3.31/S.1.1.4-5 Advancement of Indicating and Recording Elements (Copies of The Code of Federal Regulations (CFR) may be obtained at http:/www.gpoaccess.gov/cfr/index.html or
26、available from the Superintendent of Documents, U.S. Government Printing Office, Washington, DC, 20402.) (Copies of FAR and DFARS may be obtained from the Superintendent of Documents, P.O. Box 371954, Pittsburgh, PA 15250-7954. Electronic copies of the FAR may be obtained from https:/www.acquisition
27、.gov/far/ . Electronic copies of the DFARS may be obtained from http:/www.acq.osd.mil/dpap/dars/dfars/index.htm .) (Copies of Government documents required by the contractor in connection with this acquisition functions should be obtained from or as directed by the contracting activity.) 2.3 Non-Gov
28、ernment publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. AMERICAN PETROLEUM INSTITUTE API 579-1/ASME FFS-1 Fitness for Service API RP 2003 Prot
29、ection Against Ignitions Arising out of Static, Lightning, and Stray Currents (Copies of API specifications are available from the American Petroleum Institute, 1220 L Street, NW Washington, DC 20005-4070 1220 or at http:/www.api.org ). AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM D1655 Av
30、iation Turbine Fuels ASTM D975 Oil, Diesel Fuel ASTM B241/B241 Aluminum and Aluminum-Alloy Seamless Pipe and Seamless Extruded Tube ASTM A312/A312M ASTM D910 ASTM D4306 Pipes, Stainless Steel, Seamless, Welded and Heavily Cold Worked Austenitic, Standard Specification for High Temperature and Genera
31、l Corrosive Service Gasolines, Aviation Aviation Fuel Sample Containers for Tests Affected by Trace Contamination Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32080A 6 ASTM D 4057 ASTM D 4177 ASTM D5001 ASTM D5006 ASTM D3241 ASTM D6615 AST
32、M D7467 ASTM D7566 Practice for Manual Sampling of Petroleum and Petroleum Products Practice for Automatic Sampling of Petroleum and Petroleum Products. Aviation Turbine Fuels by the Ball-on-Cylinder Lubricity Evaluator (BOCLE), Measurement of Lubricity of, Standard Test Method for Fuel System Icing
33、 Inhibitors (Ether Type) in Aviation Fuels, Measurement of Oxidation, Thermal, Stability of Aviation Turbine Fuels (JFTOT Procedure) Standard Specification for Jet B Wide-Cut Aviation Turbine Fuel Standard Specification for Diesel Fuel Oil, Biodiesel Blend (B6 to B20) Standard Specification for Avia
34、tion Turbine Fuel Containing Synthesized Hydrocarbons (Copies of ASTM standards may be obtained from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959. Electronic copies of ASTM standards may be obtained from http:/www.astm.org ) AMERICAN SOCIETY OF MECHANICA
35、L ENGINEERS (ASME) ASME Boiler and Pressure Vessel Code Section VIII Rules for Construction of Pressure Vessels (Copies are available from the American Society of Mechanical Engineers, United Engineering Center, 345 East 47th Street, New York, NY 10017 - Electronic copies may be obtained from http:/
36、www.asme.org) AMERICAN WELDING SOCIETY (AWS) D1.1/D1.1M Structural Welding CodeSteel D1.2/D1.2M Structural Welding CodeAluminum (Application for copies should be addressed to American Welding Society, 550 N.W. LeJeune Road, Miami FL 33126. Electronic copies may be obtained from http:/www.aws.org) EN
37、ERGY INSTITUTE EI 1529 Aviation Fueling Hose EI 1581 Specification and Qualification Procedures for Aviation Jet Fuel Filter Separators EI 1584 Four-Inch Hydrant System Components and Arrangements Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P
38、RF-32080A 7 (Copies are available from the Energy Institute, 61 New Cavendish Street, London W1G 7AR, UK or at http:/www.energyinst.org). NATIONAL FIRE PROTECTION ASSOCIATION (NFPA) NFPA 385 Tank Vehicles for Flammable and Combustible Liquids NFPA 407 Aircraft Fuel Servicing (Application for copies
39、should be addressed to American Welding Society, 550 N.W. LeJeune Road, Miami FL 33126. Electronic copies may be obtained from http:/www.aws.org) SOCIETY OF AUTOMOTIVE ENGINEERS (SAE) SAE J534 Lubrication Fittings SAE AMS 336 Silicone Rubber, Extreme Low Temperature Resistant 55 65 Duro For Sheeting
40、 see 3.13 ). 3.3 Design and construction. The aircraft refueling truck shall be designed and constructed so that no parts will work loose in service. It shall be built to withstand the strains, jars, vibrations, and other conditions incident to shipping, storage, installation, and service. It shall
41、be weatherproof and designed to prevent the intrusion of water and sand into critical operating components. The aircraft refueling truck shall be designed to optimize energy efficiency while minimizing engine fuel consumption. Unless otherwise specified, SAE ARP 1247 requirements for aerospace groun
42、d support equipment, as applicable to a refueling truck, shall apply. 3.3.1 Materials, protective coatings, and finish. All components which come into contact with fuel shall be compatible with all fuels in accordance with ASTM D910, ASTM D1655, MIL-DTL-5624, MIL-DTL-25524, MIL-DTL-83133, GOST 10-22
43、7, Def Stan 91-91, Def Stan 91-87, ASTM D6615, and ASTM D7566. Magnesium alloys, wood products, polyvinyl chloride (PVC), polyester, room temperature vulcanizing rubber (yielding acetic acid), or asbestos shall not be used in any component or assembly of this truck. Zinc coated metals, brass, bronze
44、, or other copper bearing alloys shall not come in direct contact with fuel. 3.3.1.1 Recycled, recovered, or environmentally preferable materials. Recycled, recovered, or environmentally preferable materials should be used to the maximum extent possible provided that the material meets or exceeds th
45、e operational and maintenance requirements, and promotes economically advantageous life cycle costs. 3.3.1.2 Green Procurement Program (GPP). GPP is a mandatory federal acquisition program that focuses on the purchase and use of environmentally preferable products and services. GPP requirements appl
46、y to all acquisitions using appropriated funds, including services and new requirements. FAR 23.404(b) applies and states the GPP requires 100 percent of Environmental Protection Agency designated product purchase that are included in the Comprehensive Procurement Guidelines list that contains recov
47、ered materials (see 6.3.1), unless the item cannot be acquired: a. Competitively within a reasonable timeframe, b. Meet appropriate performance standards, or c. At a reasonable price. The prime contractor is responsible for ensuring that all subcontractors comply with this requirement. Provided by I
48、HSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32080A 9 3.3.1.3 Metals. All materials in contact with the fuel and not specified elsewhere in this document shall be corrosion resistant and shall not be adversely affected by or affect the fuel. All compon
49、ents and piping downstream of the filtration system shall be of aluminum or stainless steel. All aluminum components in direct contact with fuel, except the tank, shall be anodized or chemically conversion coated. Brass components shall be minimized but accepted in hose couplings/hose reducers and drain valves. Copper components will be minimiz
