1、MIL-DTL-83798/7C INCH-POUND18 August 2008 SUPERSEDING MIL-DTL-83798/7B 18 September 2000 DETAIL SPECIFICATION SHEET FITTINGS, RUBBER HOSE, LIGHTWEIGHT, MEDIUM PRESSURE, SWIVEL FLANGE, STRAIGHT This specification is approved for use by all Departments and Agencies of the Department of Defense. The re
2、quirements for acquiring the product described herein shall consist of this specification sheet and MIL-DTL-83798. FIGURE 1. Fitting, swivel flange straight. AMSC N/A FSC 4730 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83798/7C 2 A (max)
3、 Weight (max) Dash Number inch mm lbs. grams -8 1.82 46.23 0.099 44.91 -10 1.87 47.50 0.122 55.34 -12 2.29 58.17 0.165 74.84 -16 2.60 66.04 0.251 113.85 -20 2.82 71.63 0.368 166.92 -24 2.74 69.60 0.454 205.93 -32 3.08 78.23 0.739 335.20 NOTES: 1. Dimensions are in inches. 2. Metric equivalents are g
4、iven for information only. FIGURE 1. Fitting, swivel flange straight - Continued. REQUIREMENTS: Design and construction: Dimensions and configuration: See figure 1. Materials and finishes. Materials and finishes for the flange, nipple, and socket shall be as specified in table I. The swivel flange s
5、hall be in accordance with MS20756 and shall mate with MS33786. TABLE I. Material and finish. Component Material Finish Socket Nipple Flange Aluminum in accordance with MIL-DTL-83798 Anodize in accordance with MIL-A-8625, type II. All Titanium in accordance with SAE-AMS4928 (alloy 6AI-4V) Annealed P
6、rovided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83798/7C 3 Part or Identifying Number (PIN) example: M 83798 /7 -10 TSize (see figure 1)Specification sheet number M prefix Material code (see table II)Specification number M83798/7-10L-T indicat
7、es: Straight swivel flange, 7/8 inch, titanium annealed. Flange, nipple, and socket material and finish code is specified in table II. TABLE II. Flange, nut and socket material code. PIN code dash letter Material Plating finish Blank Aluminum Anodize -T Titanium Annealed Changes from previous issue.
8、 Marginal notations are not used in this revision to identify changes with respect to the previous issue due to the extent of the changes. Referenced documents. In addition to MIL-DTL-83798, this document references the following: MIL-A-8625 MS20756 MS33786 SAE-AMS4928 Provided by IHSNot for ResaleN
9、o reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83798/7C 4 CONCLUDING MATERIAL Custodians: Preparing activity: Army - AV DLA - CC Navy - AS Air Force - 99 (Project 4730-2007-124) DLA - CC Review activities: Army - AT Navy-SA Air Force - 71, 85 NOTE: The activities listed
10、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 Online database at http:/assist.daps.dla.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
