1、 MIL-STD-1518D 25 August 2006 NOT MEASUREMENT SENSITIVE SUPERSEDING MIL-STD-1518C 1 February 2003 DEPARTMENT OF DEFENSE STANDARD PRACTICE STORAGE, HANDLING, AND SERVICING OF AVIATION FUELS, LUBRICATING OILS, AND HYDRAULIC FLUIDS AT CONTRACTOR FACILITIES AMSC N/A FSC 91GP DISTRIBUTION STATEMENT A. Ap
2、proved for public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-1518D FORWARD 1. This standard is approved for use by all Departments and Agencies of the Department of Defense (DOD). 2. Comments, suggesti
3、ons, or questions on this document should be addressed to DET 3, WR-ALC/AFTH, 2430 C Street, Bldg 70, Area B, Wright-Patterson AFB OH 45433-7632 or e-mailed to AFPET.AFTHwpafb.af.mil. Since contact information can change, you may want to verify the currency of this address information using the ASSI
4、ST Online database at http:/assist.daps.dla.mil. iiProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-1518D CONTENTS PARAGRAPH PAGEFOREWARD.ii 1 SCOPE .1 1.1 Scope .1 2 APPLICABLE DOCUMENTS .1 2.1 General.1 2.2 Government documents .1 2.2.1 Spec
5、ifications, standards, and handbooks.1 2.2.2 Other Government documents, drawings, and publications 1 2.3 Non-Government publications2 2.4 Order of precedence.3 3 DEFINITIONS.4 3.1 Bulk storage system .4 3.2 Conductivity additive.4 3.3 Corrosion inhibitor/lubricity improver 4 3.4 Filter differential
6、 pressure.4 3.5 Filter vessel.4 3.6 Fuel.4 3.7 Aviation turbine fuel 4 3.7.1 JP-4 (NATO F-40) 4 3.7.2 JP-5 (NATO F-44) 4 3.7.3 JP-8 (NATO F-34) 4 3.8 Fuel system icing inhibitor (FSII) 4 3.9 Gauge pressure4 3.10 Hydrant servicing units .4 3.11 Intragovernmental transfer .5 4 GENERAL REQUIREMENTS 5 4
7、.1 Safety summary5 4.2 Product quality5 4.3 Contamination 6 4.4 Water 6 4.4.1 Dissolved water 6 4.5 Sediment.6 4.6 Recycled, recovered, or environmentally preferable materials 6 5 DETAILED REQUIREMENTS6 5.1 Fuel equipment.6 5.1.1 Storage and handling system.6 5.1.2 Receipt strainers.6 5.1.3 Receipt
8、filtration6 5.1.4 Storage tanks6 5.1.5 Refueling truck product tank.7 5.1.6 Filtration7 5.1.6.1 Filtration with operating tanks.7 5.1.6.2 Filtration element replacement .7 5.1.7 Differential pressure .7 5.1.8 Pressure gauges 7 5.1.9 Meters.7 5.1.10 Hoses and couplings 7 iiiProvided by IHSNot for Res
9、aleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-1518D 5.1.11 Aircraft refueling nozzles 7 5.1.12 Identification markings7 5.1.12.1 Fuel handling equipment 7 5.1.12.2 Packaged products.7 5.1.13 Continuity resistance 8 5.2 Operations 8 5.2.1 Fuel tanks with water bottom
10、s8 5.2.2 Tank product exchange8 5.2.3 Settling time8 5.2.4 Servicing of drummed product8 5.2.5 Line displacing procedures.8 5.2.6 Handling of lubricants and hydraulic fluids 8 5.2.6.1 Turbine engine lubricating oil8 5.2.6.1.1 Cans 8 5.2.6.1.2 Drums 8 5.2.6.1.3 Equipment other than cans or drums .8 5
11、.2.6.2 Reciprocating engine oil .8 5.2.6.2.1 Drums .9 5.2.6.2.2 Cans .9 5.2.6.3 Aircraft hydraulic fluid .9 5.2.6.3.1 Cans .9 5.2.6.3.2 Drums .9 5.2.6.3.3 Unused fluid9 5.3 Safety requirements .9 5.4 Quality assurance at contractor facilities 10 5.4.1 Sample submission 10 5.4.1.1 Sample container 10
12、 5.4.1.2 Sample location 10 5.4.1.3 Analysis of sample 10 5.4.2 Sampling requirements. 10 5.4.3 Sampling procedures 10 5.4.4 Sample size 10 5.4.5 Questionable quality products 10 5.4.6 Disposal of samples . 10 5.4.7 Aircraft defueling. 11 5.4.8 Change of product grade 11 5.4.8.1 Controls and marking
13、 . 11 5.4.9 Records and quality checks required . 11 5.5 Additive blending 11 5.5.1 Handling precautions 11 5.5.2 Methods of blending . 12 5.5.2.1 Bulk storage tank 12 5.5.2.2 Product tanks of refueling trucks 12 5.5.2.3 Adding FSII to tanks . 12 5.5.2.4 Adding FSII during refueling. 12 6 NOTES . 12
14、 6.1 Intended use. 13 6.2 Acquisition requirements 13 6.3 Subject term (key word) listing . 13 6.4 Changes from previous issue. 13 TABLE I Sampling requirements and test limits . 14 II Minimum specification and use limits . 17 ivProvided by IHSNot for ResaleNo reproduction or networking permitted wi
15、thout license from IHS-,-,-MIL-STD-1518D CONCLUDING MATERIAL 18 vProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-1518D 1. SCOPE 1.1 Scope. This standard establishes the minimum performance and quality requirements for the storage, handling, a
16、nd servicing of aviation fuels, lubricating oils, and hydraulic fluids at contractor owned/operated aircraft maintenance facilities. 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in sections 3, 4, or 5 of this standard. This section does not include document
17、s cited in other sections of this standard 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 specified requirements of documents cited in sections 3, 4, or 5 of this
18、 standard, 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 herein. Unless otherwise specified, the issues of these documents are those
19、cited in the solicitation or contract. FEDERAL STANDARDS FED-STD-791 Lubricants, Liquid Fuels, and Related Products; Methods of Testing DEPARTMENT OF DEFENSE SPECIFICATIONS MIL-PRF-25017 Inhibitor, Corrosion/Lubricity Improver, Fuel Soluble MIL-PRF-52308 Filter-Coalescer Element, Fluid Pressure MIL-
20、DTL-5624 Turbine Fuel, Aviation, Grades JP-4, JP-5 MIL-DTL-83133 Turbine Fuels, Aviation, Kerosene Types, NATO F-34 (JP-8), NATO F-35, and JP-8 + 100 MIL-DTL-85470 Inhibitor, Icing, Fuel System, High Flash NATO Code Number S-1745 DEPARTMENT OF DEFENSE STANDARDS MIL-STD-161 Identification Methods for
21、 Bulk Petroleum Products Systems Including Hydrocarbon Missile Fuels MILITARY STANDARD MS24484 Adapter, Pressure Fuel Servicing, Nominal 2.5 Inch Diameter (Copies of these documents are available online at http:/assist.daps.dla.mil or from the Standardization Document Order Desk, 700 Robbins Avenue,
22、 Bldg 4D, Philadelphia PA 19111-5094.) 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 c
23、ited in the solicitation or contract. 1Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-1518D TECHNICAL ORDER 42B-1-1 Quality Control of Fuels and Lubricants 37-1-1 General Operation and Inspection of Installed Fuel Storage and Dispensing Syst
24、ems (Copies of these documents are available online at https:/afpet.wpafb.af.mil/ or from DET 3, WR-ALC/AFTT, 2430 C Street, Bldg 70, Area B, Wright-Patterson AFB OH 45433-7632.) UNIFIED FACILITIES CRITERIA UFC 3-460-03 Operation and Maintenance: Maintenance of Petroleum Systems (Copies of these doc
25、uments are available online at http:/dod.wbdg.org/ ) 2.3 Non-government 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 INS
26、TITUTE (API) API-STD-1529 Aviation Fueling Hose API-STD-1542 Identification Markings for Dedicated Aviation Fuel Manufacturing and Distribution Facilities, Airport Storage and Mobile Fueling Equipment API/IP SPEC 1581 Specifications and Qualification Procedures for Aviation Jet Fuel Filter/Separator
27、s IP SPEC 1583 Specification and Laboratory Tests for Aviation Fuel Filter Monitors with Absorbent Type Elements (Copies of these documents are available online at http:/assist.daps.dla.mil/quicksearch/ or http:/www.api.org or from the American Petroleum Institute, 1220 L Street, Northwest Washingto
28、n DC, 20005-4070.) AMERICAN SOCIETY FOR TESTING AND MATERIALS, INC. (ASTM) ASTM D910 Standard Specification for Aviation Gasolines ASTM D2276 Standard Test Method for Particulate Contaminant in Aviation Fuel by Line Sampling ASTM D2624 Standard Test Methods for Electrical Conductivity of Aviation an
29、d Distillate Fuels ASTM D3240 Standard Test Method for Undissolved Water in Aviation Turbine Fuel ASTM D3241 Standard Test Method for Thermal Oxidation Stability of Aviation Turbine Fuels ASTM D4057 Standard Practice for Manual Sampling of Petroleum and Petroleum Products ASTM D4171 Standard Specifi
30、cation for Fuel System Icing Inhibitors ASTM D4177 Standard Practice for Automatic Sampling of Petroleum and Petroleum Products ASTM D4306 Standard Practice for Aviation Fuel Sample Containers for Tests Affected by Trace Contamination 2Provided by IHSNot for ResaleNo reproduction or networking permi
31、tted without license from IHS-,-,-MIL-STD-1518D ASTM D5001 Standard Test Method for Measurement of Lubricity of Aviation Turbine Fuels by the Ball-On Cylinder Lubricity Evaluator (BOCLE) ASTM D5006 Standard Test Method for Measurement of Fuel System Icing Inhibitors (Ether Type) in Aviation Fuels AS
32、TM D5452 Standard Test Method for Particulate Contamination in Aviation Fuels by Laboratory Filtration ASTM D5854 Standard Practice for Mixing and Handling of Liquid Samples of Petroleum and Petroleum Products (Copies of these documents are available online at http:/www.astm.org or the American Soci
33、ety for Testing and Materials, 100 Barr Harbor Drive, West Conshohocken PA 19428-2959.) AIR TRANSPORT ASSOCIATION (ATA) ATA SPEC 103 Standards for Jet Fuel Quality Control at Airports (Copies of these documents are available online at http:/www.air-transport.org or from the Air Transport Association
34、 of America, 1301 Pennsylvania Ave. NW, Suite 1100, Washington, DC 20004.) INTERNATIONAL ORGANIZATION FOR STANDARDIZATION BS EN 1361 British Standard Specification for Rubber Hoses and Hose Assemblies for Aviation Fuel Handling (Copies of these documents are available online at http:/www.bsonline.bs
35、i- or from the British Standards Institution, No. 2 Park Street, London WIA 285, England or from the American National Standards Institute, 11 West 42ndSt., New York, New York 10036.) NATIONAL FIRE PROTECTION ASSOCIATION (NFPA) NFPA 407 Standard for Aircraft Fuel Servicing (Copies of these documents
36、 are available online at http:/assist.daps.dla.mil/quicksearch/ or http:/www.nfpa.org or from the National Fire Protection Association, 1 Batterymarch Park, P.O. Box 9101, Quincy, MA 02269-9101.) SOCIETY OF AUTOMOTIVE ENGINEERS SAE ARP5818 Design and Operation of Aircraft Refueling Tanker Vehicles S
37、AE AS5877 Detailed Specification for Aircraft Pressure Refueling Nozzle (Copies of these documents are available online at http:/www.sae.org or from the Society of Automotive Engineers, 400 Commonwealth Dr., Warrendale, PA USA 15096-0001.) 2.4 Order of precedence. In the event of a conflict between
38、the text 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. 3Provided by IHSNot for ResaleNo reproduction or networking permitted wi
39、thout license from IHS-,-,-MIL-STD-1518D 3. DEFINITIONS 3.1 Bulk storage system. Bulk storage systems consist of above or below ground storage tanks equipped for receiving and transferring product to truck fillstands and hydrant system operating tanks. 3.2 Conductivity additive. A conductivity addit
40、ive is added to, JP-8, and at some locations JP-5, turbine fuel to decrease the time required to relax any electrical charge accumulated in the fuel during movement, pumping or filtration. The usual concentration of this additive is one or two parts per million (PPM). The conductivity level of the f
41、uel on receipt at the using facility should be between 150 and 450 picosiemens or conductivity units (CU). Fuel serviced to aircraft should be between 50 and 700 CU. Commercial jet fuel procured outside the U.S. is usually supplied with conductivity levels between 50 and 450 CU. 3.3 Corrosion inhibi
42、tor/lubricity improver. This additive, conforming to MIL-PRF-25017, is required in JP-5 and JP-8 fuel to inhibit corrosion of steel surfaces in contact with fuel. Corrosion inhibitor also provides added lubricity to fuel for more effective operation of aircraft fuel components such as pumps and fuel
43、 controls. Since there are several qualified manufacturers of inhibitors, the amount blended into the fuel depends on the type used. This is governed by the Qualified Products List (QPL) for MIL-PRF-25017 and ranges from a minimum of 3.15 pounds to a maximum of 11.03 pounds per 1000 barrels of jet f
44、uel. 3.4 Filter differential pressure. The decrease in pressure as measured from the inlet to the outlet of a filter vessel. 3.5 Filter vessel. A cylindrical vessel housing filter elements (either coalesced/separator or absorption type) designed for removing solid contaminants and free water from fu
45、el. 3.6 Fuel. Aviation gasoline or aviation turbine fuels. 3.7 Aviation turbine fuels. 3.7.1 JP-5 (NATO F-44). JP-5 is a high flash point (140F) aviation turbine fuel. It is the primary fuel for naval aircraft and is used in aircraft of all services operating off of Navy ships. It is procured to the
46、 requirements of MIL-DTL-5624. JP-5 contains both fuel system icing inhibitor and corrosion inhibitor. 3.7.2 JP-8 (NATO F-34). JP-8 is the standard fuel for US Army and USAF turbine engine powered aircraft and for some shore based Navy aircraft. This fuel is similar to commercial Jet A-1 with the ad
47、dition of corrosion inhibitor, fuel system icing inhibitor and conductivity additives. It is procured to meet MIL-DTL-83133. JP-8 is the standard fuel for NATO use in Europe. 3.7.3 JP-8+100 (NATO F-37). JP-8 containing a thermal stability additive is referred to as JP-8+100 (NATO F-37). The additive
48、 improves the thermal stability of JP-8 by approximately 100F. It reduces aircraft engine nozzle injector coking and is used primarily in fighter/trainer and selected helicopter and C-130 aircraft. For downgrading/blending procedures involving JP-8+100 contact DET 3, WR-ALC/AFTH at (937) 255-8070, D
49、SN 785-8070, for guidance. 3.8 Fuel system icing inhibitor (FSII). FSII conforming to MIL-DTL-85470 (diethylene glycol monomethyl ether DIEGME) is added to JP-5 and JP-8 to inhibit the formation of ice. 3.9 Gauge pressure. Fuel pressure measured by a pressure measurement device containing a scale calibrated in pressure units, such as k
