AIR FORCE MIL-C-3095 G-1988 CAP SERVICE MAN'S AIR FORCE《空军男式服役制服帽》.pdf

上传人:roleaisle130 文档编号:427574 上传时间:2018-11-07 格式:PDF 页数:43 大小:1.58MB
下载 相关 举报
AIR FORCE MIL-C-3095 G-1988 CAP SERVICE MAN'S AIR FORCE《空军男式服役制服帽》.pdf_第1页
第1页 / 共43页
AIR FORCE MIL-C-3095 G-1988 CAP SERVICE MAN'S AIR FORCE《空军男式服役制服帽》.pdf_第2页
第2页 / 共43页
AIR FORCE MIL-C-3095 G-1988 CAP SERVICE MAN'S AIR FORCE《空军男式服役制服帽》.pdf_第3页
第3页 / 共43页
AIR FORCE MIL-C-3095 G-1988 CAP SERVICE MAN'S AIR FORCE《空军男式服役制服帽》.pdf_第4页
第4页 / 共43页
AIR FORCE MIL-C-3095 G-1988 CAP SERVICE MAN'S AIR FORCE《空军男式服役制服帽》.pdf_第5页
第5页 / 共43页
亲,该文档总共43页,到这儿已超出免费预览范围,如果喜欢就下载吧!
资源描述

1、i l L L k !- i I I I b a i I f t L I , I L i I i r Beneficial connnents (recomnendations, additions, deletions) and any pertinent data vuhich may be of use in improving this document should be addressed to: ASD/ENES, Wright-Patterson AFB OH 45433-6503 by using the self-addressed Standardization Docu

2、mont Improvement Proposal (DD Form 1426) appearing at the end of this document or bv letter. A I INCH-POUND I MIL-C3095G (USAFI 25 November 1988 SUPERSEDING MIL-C-3095F (USAF) 25 January 1985 MILITARY SPECIFICATION -CAF, SERVICE, MANS, AIR FORCE t This specification is approved for use by the Depart

3、ment of the Air Force, and is available for use by all Departments and Agencies of the Department of Defense. -3 I 1. SCOPE A 1.1 Scope. This specification covers the requirements for a mans Air Force service cap. * 1.2 Classification. The cap shall be of one type in the following classes, as specif

4、ied (see 6.2): Class 1 - Polyester/wool tropical cloth, USAF Blue 1578, 10.00 oz. Class 2 - Polyester/wol tropical cloth, USAF Blue 1608, 10.25 oz. 1.2.1 Size. The cap shall be furnished in the following sizes, as specified (see 6.2) : 6-3/8 6-3/4 7-1/8 7- 1/2 7-7/8 6-1/2 6-718 7-114 7-5/ 6-5/8 7 7-

5、3/8 7-3/4 FSC 8405 * AMXC N/A * DISTRIBUTION STATEMENT A. Approved for public release; distribution is un1 imi ted. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-3095G 84 m 9999906 0373536 B MIL-c-30958 (USAF) 2. APFLICABLJI DOCUMENTS 2.1 Gov

6、ernment documents * 2.1.1 Specifications and standards. The fol lowing specifications and standards form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these docwnts are those listed in the issue of the Department of Defense Index of Specifications

7、and Standards (DoDISS) and supplement thereto, cited in the solicitation (see 6.2). SPECIFICATIONS FEDERAL C-F-206 H-S-95 1 Felt Sheet: Synthetic Fi For L-P-375 L-P-390 V-T-276 V-T-295 NN-P-7 1 UU-P-258 UU-P-553 ccc-c-432 DDD-L-20 PPP-B-60 1 PPP -B - 63 6 PPP-T-45 MILITARY MIL-C-368 MIL-B-593 MIL-B-

8、346 1 MIL-s-3577 MIL-P-15011 MIL-(2-21115 MIL-(3-41831 MIL-L-43541 MIL-T-43548 Cloth, Felt, Wool, Pressed aments for Brushes; General Spec-fication Plastic Film, Flexible, Vinyl Chloride Plastic Molding and Extrusion Material, Polyethylene and Copolymers (Low, Medium, and High Density) Thread, Cotto

9、n Thread, Nylon Pallets, Material Handling, 2-Way And 4-Way (Partial) Paper, Index Paper, Wrapping, Tissue Wood, Stringer Construction, Cloth, Sheeting, Cotton, (Ur.dleached, Bleached, and Dyed) Label: For Clothing, Equipage, and Tentage, (General Use) Boxes, Wood, Coated-Plymod Boxes, Shipping, Fib

10、erboard Tape, Gunmed, Paper, Reinforced and Plain, for Sealing and Securing C.loth, Satin, Rayon and Cloth, Twill, Rayon Braid, Textile (Flat) Button, Insignia, Metal, Uniformand Cap Sweatband, Headmar, Leather Pallets, Material Handling, Wood Post Construction, the requirements for colorfastness to

11、 light and to laundering and for seam efficiency shall not apply: and the shrinkage shall not exceed 6 percent in the warp or the filling. The cotton sheeting shall be dyed to approximate the shade of the lining mterial specified in 3.3.2. The lining mterial or the cotton sheeting for the crown seam

12、 tape shall be bias cut 1-5/8 inches wide, with the raw edges overlapping 1/16 21/32 inch on the underside, to form binding. 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-3075G BLt 7779906 0373537 3 MIL-C-3095G (USAF) 3.3.4 Interlining for

13、-crown seam tape. The interlining for the crown seam tape shall be bias cut, 3/4 11/16 inch wide, fromnatural or dyed nylon mesh. The nylon mesh shall be knitted on a single needle bar raschel and shall weigh 6 20.5 ounces per square yard. The stiffness, the length parallel to the wales of the finis

14、hed cloth, shall be 0.08 (minimud and 0.1 (niaxirrnn) load pound. The stiffness, the length across or perpendicular to the wales of finished cloth, shall be 0.04 (minimum) and 0.06 (niaXimm9 load pound (see 4.4.1). 3.3.5 Crown protector, personal label pocket, and binding. The mterial for the crown

15、protector, the personal label pocket, and the binding for the front interlining shall conform to type II, class 1 of L-P-375 and shall be 0.004 +0.0004 inch thick. 3.3.6 Visor cushion. The material for the visor cushion shall conform to type I, classification 9R4 of C-F-206 except that the niaterial

16、 shall be 114 inch thick and shall have fair colorfastness to wet dry cleaning. The visor cushion shall be cut 3/4 21/8 inch wide and shall be the length of the visor. In lieu of the felt pad, a 3/8 inch wide and 1/4 inch thick expanded foam polyvinyl chloride pad my be used. adhesive (see 4.4.1). .

17、 .3 It shall be attached with self 3.3.7 Swatband wlt. The material for the sweatband shall be pressed fiber. The pressed fiber shall weigh 1/5 to 2 ounces per square foot; shall be 0.015 to 0.2 inch thick; and shall be natural, red, or black (see 4.4.1). 3.3.8 Interlining for front. The interlining

18、 for the front shall be constructed of cloth, knitted, nylon raschel conforming to MIL-C-41831. 3.3.9 Inner body band. The niaterial for the inner body band shall be composed of a high alpha cellulose wood pulp sheet impregnated with an oil- resistant and perspiration-resistant synthetic rubber bind

19、er and shall conform to the requirements specified in table I or the inner body band shall be of high density (linear) polyethylene plastic material conforming to type III, class H, grades 1 or 2 of L-P-390, except that the low temperature brittleness, dielectric constant, dissipation factor and the

20、rml-stress cracking resistance properties shall not apply. shall be cut, extruded, stripped or slit 2 +i/lS inches in width and 0.030 - +0.002 inch in thickness. As an additional alternate the band my be made from imitation (mlded) linear polyethylene patterned on one or both sides, interlaced in a

21、chair seat design: shall be black; and shall finish 2 51/16 inches in width. The thickness of the material shall be 0.050 to 0.075 inch (see 4.4.1). The band 3.3.10 Wadding. The wdding shall be a good comercial cotton wadding that conforms to the requirements specified herein. The wadding shall be g

22、ray or vrihite, shall weigh not less than 2 ounces nor more than 2.5 ounces per square yard, and shall have good colorfastness to mt dry cleaning (see 4.4.1). Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-3075G 84 7777706 0373520 T MIL-C-3095

23、G (US 3.3.11 Thread. The cotton thread for seaming and stitching the caps shall ccnformto V-T-276 as indicated in table II or as an alternate, cotton- co%yre polyester threads, in equivalent sizes, conforming to MIL-T-43548 my be bed. The thread for fel 1 ing the sweatband to the band shall be black

24、 wd shall conform to type IV, letter size C of V-T-295. The thread for bartacking the front stiffener shall be either cotton-covered or rayon- . . covered polyester conforming to MIL-T-43548. 3.3.11.1 Colorfastness. The vat dyed threads shall show fastness to light and laundering equal to or better

25、than the standard sample. When no standard sample is avaifable, the dyed thread shall show good fastness to light, wet dry cleaning, and perspiration. / _ .A- -. JX 3.3.12 Sweatband. The sweatband shall be 1-5/8 21/8 inches wide, conforming to MIL-S-3577, and shall be dyed brown. The finished sweatb

26、and shall have evenly spaced perforations. 3.3.13 Braid. The braid shall be 1-3/4 inches wide, USAF Color Blue, Shade No. 1095 (see 6.41, conforming to type I, class 3 of MIL-B-593 except that the braid shall have fair colorfastness to light, mt dry cleaning, crocking, and perspiration when tested (

27、see 4.4.1). 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. =. Co 1 or MIL-C-3075G 4 = 777770b 0373523 3 Type TABLE II. Cotton thread. Ply Ticket No. Black Pearl gray Blue L/ Russet Black Black 3 3 3 4 IC2 IC2 IC2 IC2 IB3 IA3 (bobbin only) A A A

28、16 or 24 31 A 16 4l I t - 1/ The color shall conform to Navy Blue AT, C.A. 66060 (see DoD Standard Color Card). * 3.3.14 Visor and chin strap. The rnaterial for the top piece of the visor and for the chin strap shall be leather conforming to type I of MIL-L-43541 and shall be 3 to 4 ounces thick. co

29、nstructed of 2 or 3 layers of reconstituted leather 5.5 to 6.0 ounces thick The visor bottom piece shall be meting the requiremnts of betwen the top and the inch thick. Nitro water repellency and Spot resistance in in MIL-L-43541. chin strap may be 3.3.14.1 Poromric homogeneous 100 percent polyureth

30、ane structure containing no free plastisizers. equal to the standard sample (see 6.4). The physical characteristics shall be as follows: The material shall be black and have a lazy calf grain finish Characteristics Requirements Thickness .O60 2.005 Weight Abrasion resistance (Taber) Very slight wear

31、 at 100 cycles Tensile strength (cut strip mthod): 23.5 51.5 ounces per yard Leng th 70 pounds Width 60 pounds A 3.3.15 Visor binding., The binding strip shall be made from black vinyl chloride flexible plastic film, 0.012 inch thick, having a smoth finish, approximate to the -finish of the top piec

32、e conforming to- type I, class 2 of L-P-375. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-3095G 84 W 7777706 0373522 3 W mL-C-3095G (USAFI 3.3.16 Buttons. The buttons shall conform to type II, style 1, 25-line size of MIL-B-3461. 3.3.17 Eyel

33、ets. The eyelets shall be brass and shall conform to the dimensions show on figure 1. of 0.250 to 0.285 inch. The brims or flanges of the eyelets shall be enameled or lacquered black. Prior to coating, the eyelets shall be thoroughly cleaned and degreased. 3.3.18 Washers. The -hers for backing the e

34、yelets shall be brass. Each washer shall fit over the barrel of the eyelet to ensure a secure clinch of the eyelet. The front eyelet shall have a barrel length 3.3.19 Sweatband reinforcement strip. The material for the sweatband reinforcement shall be a strip of coated print cotton cloth or sheeting

35、 that is 5/8 to 3/4 inch wide. - w V 3.3.19.1 Sweatband welt. When the sweatband is joined by mchine (see Operation 19) a sweatband welt conforming to type I, class 2, 0.010 inch thick of L-P-375, a brown shade, shall be used. It shall be cut 3/4 21/16 inch in width. If this wlt is used, the sweatba

36、nd welt cited in 3.3.7 shall not apply or be used. 3.3.20 Front stiffener. The materials for the front stiffener shall be a comnercial twin or wire tape: one ply or undyed, stiff, comnercial crinoline; and one ply of either haircloth or cotton warp-fused rayon filling cloth. provided that the conmer

37、cial front stay conforhs to the requiremnts specified herein. 3.3.20.1 Twin wire tape. The twin wire tape for the front stiffener shall be 3 7/16 +1/8 inches long by 1 inch wide. The wire used in the tape shall be hard-rol led, cold-f inished carbon steel, galvanized, flat wire, and shall be 0.016 2

38、0.001 inch thick by 0.090 50.004 inch wide. A corkrcial front stay my be used for the front stiffener 3.3.20.2 Crinoline. The crinoline for the front stiffener shall wigh 1.5 to 2.5 ounces per square yard, shall have not less than 25 threads per inch in the warp or the filling, and shal-l conform to

39、 the specified patterns. 3.3.21 Staples. The staples shall be stamped from steel, monel metal, brass, or stainless-steel wire. The wire shall be 0.025 L0.0005 inch thick. Ordinary carbon-steel wire used for the staples shall have a noncorrosive finish that will withstand exposure to salt spray for n

40、ot less than 25 hours when tested (see 4.4.1). The staples for fastening the front stiffener to the inner body band shall be 118 21/64 inch in overall width and shall have divergent prongs 1/4 to 3/8 inch long. 3.3.21.1 Staples for closing the loops of the chin strap. The staples for closing the loo

41、ps of the chin strap shall be approximtely 114 51/16 inch in overall width and shall have divergent prongs that are 318 21/64 inch long. 8 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-3075G AL( m 7777906 0373523 5 a MIL-C-3095G (USAFI DIA I

42、Ir NOTE: Dimensions in inches. +.O18 187 -*O17 L. O10 2.003 FIGURE 1. Eyelet. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-3095G 4 W 979990b 0373524 7 W MIL-C-3095G(USAF) 3.3.21.2 Staples for button Dosts. The staples for fastening the botto

43、m of the posts to the inner body band shall be a heavy duty, flat, standard clinch type and shall be 0.05 inch wide by 0.025 inch thick, 1/4 21/64 inch long leg with a 1/2 inch wide crown. 3.3.21.3 Staples for securing front welt and ends of stitching thereon. The staples for securing the front welt

44、 and the ends of the stitching thereon shall be a flat type measuring 1/4 21/64 inch leg, 0.0018 - +0.0003 inch wide by 0.0054 +0.0009 inch thick. 3.3.22 Crown support. The crown support shall consist of a steel wire inclosed in a braided grommet. 3.3.22.1 Steel wire. The steel wire for the crown su

45、pport shall be spring steel 5/16 21/16 inch wide, 0.020 +0.005 inch thick, and completely covered with a white pyroxylin coating. The cut length of the spring steel wire shall be as specified in table III. The coupling for joining the ends of the spring steel wiire shall be 1 t1/8 inch long and zinc

46、 or cadmiumcoated to withstand 25 hours of the salt spray test (See 4.4.1). 3.3.22.2 Braided grommet. Clear nylon mnofilmnt filling yarn and carded cotton warp yarns shall be braided to form a gromt approximately 3.4 inch in diameter. The filling yarns shall be 0.012 L0.0005 inch in diameter and sha

47、ll confrmto class N, type II of H-X-951 except that the cut length designation shall not apply. The mrp yarns shall be 12 +1/2 count singles. The gromt shall be made on a 48-carrier braider or 44-carrier braider with carriers braiding in pairs with a 1/1 weave with one 0.012-inch diameter nylon mono

48、filamnt end per carrier or 24-carrier braider with carriers braiding in pairs on a 1/1 wave with tm 0.012-inch diameter nylon monofilanrint ends per carrier. Not less than eight warps of tm ends each of cotton yarn shall be intermittently spaced around the circumference interlacings. There shall be

49、no less than 8 picks per inch in the relaxed state. The ends of the gromt shall be joined by mod or cork plugs, laminated paper rings, or other suitable material to ensure proper closure of the gromt. The length of the gromriet shall be governed by the size of the cap (see 4.4.1). 3.3.23 Labels. Each cap shall have a combination instruction, identification and size label and a personal identification label conforming to DDD-L-20. The c

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 2068-1989 Aerospace Series Rod-Ends with Self-Lubricating Self-Aligning Bearings Technical Specification Issue P 1《航空航天系列.带螺纹自润滑自对心滚球轴承技术规范P.第1版》.pdf AECMA PREN 2068-1989 Aerospace Series Rod-Ends with Self-Lubricating Self-Aligning Bearings Technical Specification Issue P 1《航空航天系列.带螺纹自润滑自对心滚球轴承技术规范P.第1版》.pdf
  • AECMA PREN 2069-1-1994 Inspection and Testing Requirements for Steel Wrought Products Part 1 - General Requirements Aerospace Series Edition 2 [Refer To ASD-STAN PREN 4235-1]《航空航天系.pdf AECMA PREN 2069-1-1994 Inspection and Testing Requirements for Steel Wrought Products Part 1 - General Requirements Aerospace Series Edition 2 [Refer To ASD-STAN PREN 4235-1]《航空航天系.pdf
  • AECMA PREN 2069-2-1994 Inspection and Testing Requirements for Steel Wrought Products Part 2 Inspection and Testing Requirements for Sheets Strips and Plates Aerospace Series Editi.pdf AECMA PREN 2069-2-1994 Inspection and Testing Requirements for Steel Wrought Products Part 2 Inspection and Testing Requirements for Sheets Strips and Plates Aerospace Series Editi.pdf
  • AECMA PREN 2069-3-1994 Inspection and Testing Requirements for Steel Wrought Products Part 3 Inspection and Testing Requirements for Bars and Sections Aerospace Series Edition 2 [R.pdf AECMA PREN 2069-3-1994 Inspection and Testing Requirements for Steel Wrought Products Part 3 Inspection and Testing Requirements for Bars and Sections Aerospace Series Edition 2 [R.pdf
  • AECMA PREN 2069-4-1994 Inspection and Testing Requirements for Steel Wrought Products Part 4 - Inspection and Testing Requirements for Tubes Aerospace Series Edition 2 [Refer To AS.pdf AECMA PREN 2069-4-1994 Inspection and Testing Requirements for Steel Wrought Products Part 4 - Inspection and Testing Requirements for Tubes Aerospace Series Edition 2 [Refer To AS.pdf
  • AECMA PREN 2069-5-1994 Inspection and Testing Requirements for Steel Wrought Products Part 5 - Inspection and Testing Requirements for Wires Aerospace Series Edition 2 [Refer To AS.pdf AECMA PREN 2069-5-1994 Inspection and Testing Requirements for Steel Wrought Products Part 5 - Inspection and Testing Requirements for Wires Aerospace Series Edition 2 [Refer To AS.pdf
  • AECMA PREN 2069-6-1994 Inspection and Testing Requirements for Steel Wrought Products Part 6 Inspection and Testing Requirements for Bars and Wires for Fasteners Aerospace Series E.pdf AECMA PREN 2069-6-1994 Inspection and Testing Requirements for Steel Wrought Products Part 6 Inspection and Testing Requirements for Bars and Wires for Fasteners Aerospace Series E.pdf
  • AECMA PREN 2070-1-1984 Aluminium and Aluminium Alloy Wrought Products - Technical Specification - Part 1 - General Requirements Aerospace Series Edition 1《航空系列.铝和铝合金锻制品的检验和试验要求.第1部.pdf AECMA PREN 2070-1-1984 Aluminium and Aluminium Alloy Wrought Products - Technical Specification - Part 1 - General Requirements Aerospace Series Edition 1《航空系列.铝和铝合金锻制品的检验和试验要求.第1部.pdf
  • AECMA PREN 2070-2-1984 Aluminium and Aluminium Alloy Wrought Products - Technical Specification - Part 2 - Sheet Strip Formed Profiles and Plate Aerospace Series Edition 1《航空系列.铝和铝.pdf AECMA PREN 2070-2-1984 Aluminium and Aluminium Alloy Wrought Products - Technical Specification - Part 2 - Sheet Strip Formed Profiles and Plate Aerospace Series Edition 1《航空系列.铝和铝.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1