ARMY MIL-STD-209 K-2005 INTERFACE STANDARD FOR LIFTING AND TIEDOWN PROVISIONS《吊挂和固定束缚装置接口标准》.pdf

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1、DEPARTMENT OF DEFENSEINTERFACE STANDARD FORLIFTING AND TIEDOWN PROVISIONSINCH-POUNDMIL-STD-209K22 February 2005SUPERSEDINGMIL-STD-209J28 January 1998AMSC N/A FSC 2540DISTRIBUTION STATEMENT A. Approved for public release;Distribution is unlimited.Provided by IHSNot for ResaleNo reproduction or networ

2、king permitted without license from IHS-,-,-iiMIL-STD-209KFOREWORD1. This interface standard is approved for use by all Departments and Agencies of theDepartment of Defense.2. This standard covers the design and testing of lifting, tiedown, and cargo tiedownprovisions. The requirements in this stand

3、ard are military-unique interface requirementsdeveloped specifically for ensuring that the lifting and tiedown provisions on militaryequipment meet the physical, functional and operational environment attributes fortransportation assets of the Defense Transportation System (DTS). These requirementsa

4、re necessary to permit the interoperability between transported military equipment andthe transportation system available for military movements. Changes incorporated in thisrevision include the addition of a new type of provision to the standard, supplemental airtransport tiedown provisions. This r

5、evision also redefines the definitions for the types ofequipment that require provisions, and combines cargo bed tiedowns and flatbed/flatracktiedowns into one type of provision that is simply called “cargo tiedown” provisions.Additionally, this revision of the standard has been reformatted so that

6、it is easier to findthe specific requirements for each type of provision covered under this standard.3. The following service points of contact can provide assistance with questionsconcerning this military standard:U.S. Army - SDDCTEA (for questions concerning intepretating this standard, and onhigh

7、way, rail, and marine transport), dpemailtea.army.mil, (757) 599-1109.U.S. Air Force - ASC/ENFC (ATTLA) (for questions concerning transport on Air Forcefixed wing aircraft), ATTLAwpafb.af.mil, (937) 255-2330.U.S. Navy/Marine Corps (for questions concerning transport on Navy/Marine Corpsaircraft), (3

8、01) 342-9392 (internal transport), (732) 323-2578 (external transport).U.S. Army - Natick (for questions concerning Helicopter Sling Load (HSL) and internaltransport on U.S. Army helicopters), (508) 233-5289.4. Comments, suggestions, or questions on this document should be addressed toDirector, Surf

9、ace Deployment and Distribution Command Transportation EngineeringAgency (SDDCTEA), ATTN: SDTE-DPE, 720 Thimble Shoals Blvd, Suite 130, NewportNews, VA 23606-4537 or emailed to DPEmailtea.army.mil. Since contact informationcan change, you may want to verify the currency of this address information u

10、sing theASSIST Online database at http:/assist.daps.dla.mil.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-iiiMIL-STD-209KTable of Contents1. SCOPE.11.1 Coverage 11.1.1 Excluded equipment 11.1.2 Military equipment for helicopter sling loading. 11.1.

11、3 Military equipment for airdrop. . 11.2 Application. .11.3 Equipment types. . 22. APPLICABLE DOCUMENTS. 22.1 Specifications and standards. 22.2 Other Government documents, drawings, and publications. 32.3 Order of precedence. . 33. DEFINITIONS 33.1 Cargo tiedown provision. 33.2 Container spreader b

12、ar. 33.3 Design limit load. 33.4 Equipment. . 43.5 Equipment tiedown provision. 43.6 Gross weight (GW). 43.7 Gross Vehicle Weight Rating (GVWR). 43.8 Helicopter flight testing. 43.9 Helicopter sling loading (HSL). . 43.10 Helicopter sling load weight (HSLWT). . 43.11 Largo cargo tiedown provision. 4

13、3.12 Lifting provision. . 43.13 Multipurpose provision. 53.14 Permanent deformation 53.15 Plane of the provisions. 53.16 Static lift test. 53.17 Static load.53.18 Supplemental air transport tiedown provision. . 53.19 Ultimate load. . 53.20 Yield load54. GENERAL REQUIREMENTS 54.1 Restraint of Item. 5

14、4.2 Surface of provisions 64.3 Shackles.64.4 Hub and axle attachments 64.5 Removable provisions. . 6Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ivMIL-STD-209K4.6 Freezing and jamming. . 64.7 Stowable lifting provisions. . 64.8 Spreader bars. 74.9

15、 Deviations. . 74.10 Strength of Provisions. . 74.11 Provision dimensions 74.12 Supplemental air transport tiedown provisions. 74.13 Testing. . 84.14 Transport on Navy/Marine Corps aircraft 84.15 Option for Type II equipment. . 84.16. Large cargo tiedown provisions. 85. DETAILED REQUIREMENTS 95.1 Li

16、fting provisions. 95.1.1 Number 95.1.2 Location.95.1.3 Strength. 105.1.3.1 For equipment with a helicopter/tiltrotor sling load requirement and a crane liftrequirement 105.1.3.2 For equipment with only a crane lift requirement. 115.1.4 Provision Dimensions 125.1.5 Testing. 125.2 Equipment tiedown pr

17、ovisions 135.2.1 Number 135.2.2 Location. 135.2.3 Strength. 145.2.3.1 Option for equipment weighing 50,000 pounds or more. 155.2.3.2 Strength of helicopter equipment tiedown provisions. . 155.2.4 Provision Dimensions 155.2.5 Testing. 165.3 Multipurpose provisions. 165.4 Cargo tiedown provisions. 165

18、.4.1 Number 165.4.2 Location. 165.4.3 Strength. 175.4.3.1 Ultimate design load. 175.4.3.1 Transport on Navy/Marine Corps aircraft 175.4.4 Provision Dimensions 175.4.5 Testing. 175.4.6 Directional capabilities. 185.4.7. Unique cargo tiedown provisions. 19Provided by IHSNot for ResaleNo reproduction o

19、r networking permitted without license from IHS-,-,-vMIL-STD-209K5.5 Large Cargo Tiedown Provisions. 195.5.1 Number 195.5.2 Location 195.5.3 Strength. . 195.5.3.1 Ultimate design load. 205.5.3.2 Transport on Navy/Marine Corps aircraft 205.5.4 Provision dimensions. 205.5.5 Testing. 205.6 Supplemental

20、 air transport tiedown provisions 215.6.1 Number 215.6.2 Location. 215.6.3 Strength. 215.6.4 Provision Dimensions. . 235.6.5 Qualification. . 235.6.6 Directional capabilities. 245.7 Marking. . 245.7.1 Shipping data plate. 245.7.2 Identification. . 246. NOTES 256.1 Intended use. . 256.2 Issue of DODI

21、SS. . 256.3 Associated Data Item Descriptions (DIDs). 256.4 Tiedown system. 256.5 Subject term (keyword) listing: . 256.6 International interest. 266.7 Changes from previous issue. 266.8 Tailoring. .266.9 Computer aided engineering (CAE) structural analysis 266.10 Checklist for Program Managers and

22、Contractors. 27FiguresFigure 1. Approximate Location of the Six Different Types of Provisions. 29Figure 2. Example of a Nonremovable, Dual-Purpose Provision. 29Figure 3. Lifting, Equipment Tiedown, Multipurpose, and Large Cargo TiedownProvision Openings and Clearance Dimensions. 30Figure 4. Range of

23、 Sling Leg Orientations. 31Figure 5. Location of Lifting Provisions. . 31Figure 6. Apex Height . 32Figure 7. Working Angles for Equipment Tiedown Provisions 32Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-viMIL-STD-209KFigure 8. Example of an Equip

24、ment Tiedown Provision with Two Openings 33Figure 9. Example of resulting cross-section that must be inscribed in a 2 inch diametercircle 33Figure 10. Required Dimensions of Cargo Tiedown Provisions. 34Figure 11. Directional Capabilities of Cargo Tiedown Provisions. 34Figure 12. Center cargo tiedown

25、 provisions for cargo areas 40 feet or longer. 35Figure 13. Range of restraint capabilities of supplemental air transport tiedown provi-sions. . 35Figure 14. Resultant direction of pull for testing supplemental air transport tiedownprovisions. 36Figure 15. Sample Dataplate with Required Information

26、37TablesTable I - Load Requirements for Equipment Tiedown Provisions (transport by highway,rail, marine, USAF fixed-wing aircraft, and internally by CH-47 helicopter) and LargeCargo Tiedown Provisions. 14Table II - Load Requirements for Cargo Tiedown Provisions. . 18Table III. Number of Supplemental

27、 Air Transport Tiedown ProvisionsRequired Per Side 22AppendicesAPPENDIX AHelicopter Sling Load Materiel Lift Point Load Factor A-1APPENDIX BSample Problem for Determining the Required Test Sling Lengths and Strength of theLifting Provisions B-1APPENDIX CSample problem for Determining the Required St

28、rength of the Tiedown Provisions C-1APPENDIX DTransport by Navy/Marine Corps Aircraft D-1Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-1MIL-STD-209K1. SCOPE1.1 Coverage.This standard establishes dimensional limits, design considerations, positionin

29、grequirements, and strength requirements for lifting (to include helicopter sling load(HSL) and tiedown provisions for lifting or tying down tanks and other tracked vehicles,tactical wheeled vehicles, helicopters, and other military equipment shipped assembledor disassembled in unboxed or uncrated c

30、ondition, and for restraining cargo oraccessories to such equipment. The lifting and tiedown requirements in this standardare necessary to permit compatibility between military equipment and the transportationsystems used for deployments.1.1.1 Excluded equipment.This standard excludes internal cargo

31、 tiedown provisions on helicopters and fixed-wing aircraft, and cargo equipment and containers/flatracks built to InternationalOrganization for Standardization (ISO) standards and meeting the requirements forConventions for Safe Containers (CSC) certification. However, ISO corner castings arenot acc

32、eptable as a substitute for lifting and tiedown provisions on equipment nothaving CSC certification.1.1.2 Military equipment for helicopter sling loading.Although the design of lifting provisions is covered in this standard, items ofequipment requiring helicopter sling loading certification must als

33、o meet the static liftand helicopter flight-test requirements of MIL-STD-913.1.1.3 Military equipment for airdrop.Even though airdrop design criteria for military equipment are specified in MIL-STD-814, equipment must also be transported by surface modes. Therefore, lifting andtiedown provisions for

34、 airdrop-designed equipment should meet both the requirementsof this standard and MIL-STD-814.1.2 Application.This standard applies to the following:a. All new commercial, modified commercial, nondevelopmental, developmental,and re-procurements weighing more than 500 pounds, and any removed componen

35、tsfrom such equipment weighing more than 500 pounds, as noted above in paragraph1.1.b. Modified equipment, when the modifications result in changes to lifting ortiedown requirements (for example, provision relocation, item weight increase, shift incenter of gravity, or the addition of something to t

36、he equipment that interferes with liftingor tiedown), or when the modified equipment was not previously equipped with liftingand tiedown provisions that meet the requirements of this standard.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-2MIL-STD-2

37、09K1.3 Equipment types.Equipment is classified as follows:Type I. All equipment issued to Table of Organization and Equipment (TOE)units (for example, combat, tactical and tactical support vehicles, armored carriers, self-propelled artillery, tanks, recovery vehicles, semi-trailers, trailers, trucks

38、, constructionequipment, and helicopters).Type II. Equipment can be classified as Type II equipment only if thespecification explicitly states that the equipment qualifies as Type II equipment for thepurpose of meeting this standard. If a statement to this effect is not contained in thespecification

39、, then the equipment is Type I equipment. In general, Type II equipmentwill be equipment that is not TOE equipment (for example, unmodified materialshandling equipment and commercial construction equipment, and items that areshipped unboxed or uncrated and lifted separately as individual units).2. A

40、PPLICABLE DOCUMENTS2.1 Specifications and standards.The following specifications and standards form a part of this document to theextent specified herein. Unless otherwise specified, the issues of these documents arethose listed in the issue of the Department of Defense Index of Specifications andSt

41、andards (DODISS) and supplement thereto cited in the solicitation (see paragraph6.2).SPECIFICATIONSFEDERALA-A-50271 Plate, IdentificationRR-C-271 Chains and Attachments, Welded and WeldlessSTANDARDSDEPARTMENT OF DEFENSEMIL-STD-913 Requirements for the Certification of SlingLoaded Military Equipment

42、for ExternalTransportation by Department of DefenseHelicopters.MIL-STD-814 Requirements for Tiedown, Suspension andExtraction Provisions on Military Material for AirdropMIL-STD-1366 Interface Standard for Transportability CriteriaProvided by IHSNot for ResaleNo reproduction or networking permitted w

43、ithout license from IHS-,-,-3MIL-STD-209K(Unless otherwise indicated, copies of above specifications and standards areavailable from the Documentation Automation and Production Service, Building 4/D,700 Robbins Avenue, Philadelphia, PA 19111-5094, phone number (215) 697-6257, orhttp:/assist.daps.dla

44、.mil/online/start.)2.2 Other Government documents, drawings, and publications.The following documents form a part of this document to the extent specifiedherein. Unless otherwise indicated, the issues of these documents are those current onthe date of the solicitation.Code of Federal Regulations Tit

45、le 49 - Transportation(CFR Title 49 can be obtained from the Superintendent of Documents, USGovernment Printing Office, Washington, DC 20402, (202) 512-1800, or http:/bookstore.gpo.gov.)2.3 Order of precedence.In the event of a conflict between the text of this document and the references citedherei

46、n, the text with the most restrictive requirement will take precedence. Additionally,illustrations do not supercede requirements that are otherwise specified in this standardor in the equipment specification.3. DEFINITIONS3.1 Cargo tiedown provision.A padeye, fixture, or attachment integral to the c

47、argo areas of trucks and trailers,flatbed trailers, or flatracks (used as a demountable truck or trailer bed) for securingcargo or accessories (see Figure 1).3.2 Container spreader bar.Material handling equipment specifically designed for lifting standard AmericanNational Standards Institute/Interna

48、tional Organization for Standardization (ANSI/ISO)containers.3.3 Design limit load.The applied force, or maximum probable force, that a provision, including itsconnecting structural members, will be subjected to in its most severe transportenvironment. For lifting, the design limit load is the stati

49、c load times the load factor(LF). For equipment tiedown, the design limit load is 4.0 times the gross weight in thelongitudinal direction, 2.0 times the gross weight in the vertical direction, and 1.5 timesthe gross weight in the lateral direction.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-4MIL-STD-209K3.4 Equipment.The item