1、AMSC N/A FSC 1660 MIL-DTL-5886H 30 January 2009 SUPERSEDING MIL-DTL-5886G 19 June 2000 DETAIL SPECIFICATION CYLINDER, AIRCRAFT OXYGEN, LOW PRESSURE, NONSHATTERABLE INCH-POUND This document remains Inactive for New Design. Comments, suggestions, or questions on this document should be addressed to: O
2、klahoma City Air Logistics Center/ENSDAA, 3001 Staff Drive, Tinker AFB, OK. 73145-3036 or emailed to af71tinker.af.mil. Since contact information can change, you may want to verify the currency of this address information using ASSIST Online database at http:/assist.daps.dla.mil. Provided by IHSNot
3、for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-5886H 2 This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification covers low pressure storage cylinders for compressed gas with a w
4、orking pressure of 450 psi for aerospace application. 1.2 Part or Identifying Number (PIN). PINs to be used for cylinders acquired to this specification are created as follows: M 5886 - X 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in sections 3, 4, or 5 o
5、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 these lists, document users are cautioned that they must meet all speci
6、fied 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, and standards. The following specifications and standards form a part of this document to the extent specified herein. Unless otherwise s
7、pecified, the issues of these documents are those cited in the solicitation or contract. FEDERAL SPECIFICATIONS BB-A-1034 - Compressed Air, Breathing FEDERAL STANDARDS FED-STD-595/13655 - Yellow, Gloss COMMERCIAL ITEM DESCRIPTIONS A-A-58092 - Tape, Antiseize, Polytetrafluorethylene A-A-59503 - Nitro
8、gen, Technical M prefix Specification number Configuration (see table IV) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-5886H 3 DEPARTMENT OF DEFENSE SPECIFICATIONS MIL-PRF-27210 - Oxygen, Aviators Breathing, Liquid and Gas (Copies of these
9、 documents are available online at http:/assist.daps.dla.mil/quicksearch/ or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.) 2.3 Non-Government publications. The following documents form a part of this document to the extent specified here
10、in. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. AEROSPACE INDUSTRIES ASSOCIATION of AMERICA, INC. (AIA) AIA NAS847 - Caps and Plugs, Protective, Dust and Moisture Seal (NA/NAS documents may be obtained at www.aia-aerospace.org/ or from A
11、erospace Industries Association 1000 Wilson Boulevard, Suite 1700 Arlington, VA 22209-3928.) AMERICAN SOCIETY FOR QUALITY (ASQ) ANSI/ASQ-Z1.4 - Sampling Procedures and Tables For Inspections By Attributes (ASQC documents may be obtained at http:/asq.org or addressed to the American Society for Quali
12、ty P.O. Box 3005 Milwaukee, WI 53201-3005 or 600 North Plankinton Avenue, Milwaukee, Wisconsin, 53203, USA) AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM D 7091 - Standard Practice for Nondestructive Measurement of Dry Film Thickness of Nonmagnetic Coatings Applied to Ferrous Metals and Non
13、magnetic, Nonconductive Coatings Applied to Non-Ferrous Metals ASTM D 2247 - Testing Water Resistance of Coatings in 100% Relative Humidity ASTM D 3359 - Standard Test Methods for Measuring Adhesion by Tape Test ASTM E 8 - Standard Test Methods for Tension Testing of Metallic Materials Provided by I
14、HSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-5886H 4 (ASTM documents may be obtained at or addressed to the American Society for Testing and Materials, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959) AMERICAN WELDING SOCIETY (AWS) AWS D17.1 Sp
15、ecification with Fusion Welding for Aerospace Applications (AWS documents may be obtained at or from American Welding Society, 550 N.W. LeJeune Road, Miami, Florida 33126.) METALS AND ALLOYS IN THE UNIFIED NUMBERING SYSTEM (UNS) S30403 - Austenitic Cr-Ni Stainless Steel (Low Carbon) S31600 - Austeni
16、tic Cr-Ni Mo Stainless Steel (SAE documents may be obtained at or from Society of Automotive Engineers, Inc., 400 Commonwealth Drive, Warrendale PA 15096.) SOCIETY OF AUTOMOTIVE ENGINEERS (SAE) SAE ARP1176 - Oxygen System and Component Cleaning and Packaging SAE AS4863 - Plug, Pipe, External Thread
17、(SAE documents may be obtained at or from Society of Automotive Engineers, 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 text of this document and the references cited herein, the
18、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. When specified (see 6.2), a sample shall be subjected to first article inspection in accordance with
19、 4.3. 3.2 Materials. The materials used in all parts of the cylinders shall be in accordance with Metals And Alloys in The Unified Numbering System S30403, S31600, or stainless maraging steel conforming to the following chemical composition: C 0.05 percent max Provided by IHSNot for ResaleNo reprodu
20、ction or networking permitted without license from IHS-,-,-MIL-DTL-5886H 5 Mn 0.5 percent max Si 0.3 percent max P 0.03 percent max S 0.02 percent max Cr 14.0 18.0 percent Ni 6.0 7.0 percent Ti 0.70 0.95 percent Fe Remainder 3.2.1 Recycled, recovered, or environmentally preferable materials. Recycle
21、d, recovered, or environmentally preferable materials should be used to the maximum extent possible, provided that the material meets or exceeds the operational and maintenance requirements, and promotes economically advantageous life cycle costs. 3.3 Design and construction. The design and construc
22、tion of the cylinders shall be in accordance with the applicable part number of Table IV and Figure 2, as specified in the contract or order (see 6.2). 3.3.1 Welding. Welding shall be performed in accordance with AWS D17.1, Class A (see 4.5.7). 3.3.2 Closures. Cylinders with two openings shall have
23、one plug conforming to SAE-AS4863, CRES type 304 or 316, while the other opening shall be closed with a removable metal threaded plug or cap conforming to NAS847. The cylinder with one opening shall be closed with a removable metal threaded plug or cap conforming to NAS847 or a commercially equivale
24、nt metal plug or cap. These plugs or caps shall protect the threads and prevent entrance of foreign matter or moisture (see 4.5.1). 3.3.3 Forming by pressurization. Forming by pressurization up to 900 psi as a manufacturing process is allowed. The permanent volumetric expansion test (see 4.5.4) is a
25、 separate requirement. 3.4 Performance. 3.4.1 Cleanliness. The cylinders, when tested as specified (see 4.5.1), shall pass the requirements in Table I as specified (see 4.5.2). 3.4.2 Leakage. The cylinder shall show no evidence of leaks when tested as specified (see 4.5.3). 3.4.3 Permanent volumetri
26、c expansion. The cylinder shall have a permanent volumetric Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-5886H 6 expansion not greater than 10 percent of the total volumetric expansion when tested as specified (see 4.5.4). 3.4.4 Burst pres
27、sure. The cylinder shall burst at a pressure not less than 1,000 PSI when tested as specified (see 4.5.5). 3.4.4.1 Cyclic endurance. The cylinder shall hold pressure during the cyclic endurance portion of the test as specified (see 4.5.5.1). 3.4.5 Macrostructure defects. The cylinder shall show no e
28、vidence of abnormal segregation, pipes, cracks, carbide defects, seams or abnormal change in structure from the surface to the center when tested as specified (see 4.5.6). 3.4.6 Fragmentation. The cylinder shall remain in one piece and exhibit no evidence of shattering when tested as specified (see
29、4.5.8). 3.4.7 Physical properties. The cylinder material sample shall have an ultimate tensile strength that is not greater than 165,000 pounds per square inch and the elongation shall be not less than 12 percent when tested as specified (see 4.5.10). 3.5 Weight. The weight of the cylinders shall be
30、 not greater than the values specified in Table IV (see 4.5.1). 3.6 Exterior finish. The color of the finish shall be gloss yellow in accordance with color number 13655 of FED-STD-595. The .375 X .750 hexagonal, wrench-flat surfaces and the adjacent end of the bottle between the threads and these wr
31、ench flats may be left unpainted .The external finish of all cylinders shall have a paint thickness not less than 0.001 inches. The paint shall not crack, chip, or scale during normal service life or under extreme environmental conditions (see 4.5.9). 3.6.1 Humidity. The exterior finish when exposed
32、 to humidity shall not show evidence of corrosion, blistering, wrinkling or loss of adhesion (see 4.5.9.1). 3.6.2 Adhesion. The cured film coating shall have a classification not less than 4B as specified in ASTM-D2247 (see 4.5.9.2). 3.7 Identification of product. Decals, if used in lieu of paint, s
33、hall be approved by the procuring activity. The cylinders shall be marked for identification in accordance with MIL-STD-130 and shall include the following information (see 4.5.1) and the color shall be a durable dull (lusterless) black: Oxygen Cylinder, Nonshatterable M5886- *1 MIL-DTL-5886 Volume
34、or method of application; markings not the same on the interior and exterior containers. Packaging and packing materials Any non-conforming component; any component missing, damaged, or otherwise defective. Workmanship Inadequate application of the components such as incomplete closure of the unit p
35、ackage, intermediate package, container flaps, loose strappings, etc.; bulging or distortion of the containers. Exterior and interior weight or content Number per container is more or less than required; gross or net weight exceeds the requirements Provided by IHSNot for ResaleNo reproduction or net
36、working permitted without license from IHS-,-,-MIL-DTL-5886H 17 TABLE IV. Cylinder characteristics PIN (Superseded Type) INTERNAL VOLUME IN3 (MIN) WEIGHT POUNDS (MAX) LENGTH INCHES (MAX) DIAMETER INCHES (MAX) NUMBER OF OPENINGS M5886-1 (A-6) 280 3.75 14.500 5.750 1 M5886-2 (B-3) 280 3.75 15.000 5.75
37、0 2 M5886-3 (D-2) 500 5.75 23.500 5.750 2 M5886-4 (F-1) 1000 10.00 18.000 10.125 2 M5886-5 (F-2) 1000 11.00 44.500 5.750 2 M5886-6 (G-1) 2100 18.00 24.500 12.562 2 M5886-7 (J-1) 18000 155.00 49.250 24.500 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS
38、-,-,-MIL-DTL-5886H 18 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-5886H 19 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-5886H 20 Provided by IHSNot for ResaleNo reproduction or
39、networking permitted without license from IHS-,-,-MIL-DTL-5886H 21 Custodians: Preparing activity Air Force - 71 Air Force - 71 Army - AV Navy - AS (Project 1660-2008-003) Reviewer activities: Air Force - 11 DLA - GS NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST database at http:/assist.daps.dla.mil/. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
