ARMY MIL-A-45947-1972 ARMAMENT SUBSYSTEM HELICOPTER 7 62MM MACHINE GUN RAMP MOUNTED LIGHT WEIGHT M41 (LESS M60D MACHINE GUN)《M24型直升机装备子系统7 62mm大门装重量轻高射机枪(少于M60D机枪)》.pdf
《ARMY MIL-A-45947-1972 ARMAMENT SUBSYSTEM HELICOPTER 7 62MM MACHINE GUN RAMP MOUNTED LIGHT WEIGHT M41 (LESS M60D MACHINE GUN)《M24型直升机装备子系统7 62mm大门装重量轻高射机枪(少于M60D机枪)》.pdf》由会员分享,可在线阅读,更多相关《ARMY MIL-A-45947-1972 ARMAMENT SUBSYSTEM HELICOPTER 7 62MM MACHINE GUN RAMP MOUNTED LIGHT WEIGHT M41 (LESS M60D MACHINE GUN)《M24型直升机装备子系统7 62mm大门装重量轻高射机枪(少于M60D机枪)》.pdf(14页珍藏版)》请在麦多课文档分享上搜索。
1、-_ _- - MIL-A-45747 10 m 7777706 0307554 4 m I 1. SCOPE 1.1 This cpeclficatiofi covers one typ lignt we5gh-k srtraxeak szbsystes providing a pintle nounted 7.62.n?i, X603 xacktine gdr: for raia? incta1iat:z on CS-47A heicopter . 2 APPLICABLE rnCl%W2S 2.1 The following docuwntc, O? Tne issue in ezlec
2、t 03 te of in- vitation for bids or request For proposal, form a part of che specificatior to the extent specified hereiri. SPECIFICATIONS Military MIL-P- i16 - MIL- I- 6866 - MIL- I- 6868 - MIL-w- 8611 - MIL-W-12332 - Preservation, Nethods of. Inspection, Penetrant Xetno o?. Inspection Process, Yag
3、retic Particle. Welding, %etzliL-e aixi Gas, Steels arrd Corrosior, and Heat Resfstant Alloys; Process for. Welding, iiesfc-kance, S-goz, Seam an6 Pro jecixion, For Fabrication Asceuhlfec of Lm Carbon Steel. WZBOC, Snial Ay% an kiafiF-p*- LC .i L, Subcystens, General SgeciLicatkn fe Insp ct ioti Eq-
4、rrt-gnent tenafice aad Dispositi oa, or. Ac cycec8436675 and drawings a3.se sec225ed (se 6., prior to production CT any weXrr;entc, tiiz corri*aeto2 OF m:xacww shall have Government agroni1 0% rel5.ng procedfires an6 ;ces% specfxens e Welding of Parts and subassemblies shaii be in accorancs with zhe
5、 EL?- plicable drawing ana as specified herein. 3.3.1.2 Welded joints, Ail welded joints o2 parts an6 sIzbssenhiies shall be sound and free Pom cracks, particle ins-oected in accordance with ,1-13868 and penetrant iccpecteg in accordance with PEIL-Lo800 as a;splicable: Weled joints shall be mignetlc
6、, F Ff 3.3.2 Gur- mount assembly, 3.3,2.1 Po.st assembly, The post assembly sbzli be capable of Essrrfibly to the rear ramp mount of the aircraft and be securely attached %o .the rear ramp mount by the two (2) mounting pins and the quick release pin. Welding of the post assembly shall be in accordan
7、ce with KiL-w-86L. 3.3.2.1.1 Cam and stops. The post assembly shall incorporate mechan- ical cam and stops to preclude firing of the weap6n into azy park of the aircraft. 3.3.2.2 Quick release pin. The quick release pin shall rcaciily 8s- semble to and disassemble from the rear rsnp mount of the air
8、craft, and when assembled shall be retained in the rear ramp mount by Yne bail detez%. The quick release pin shall be securely attache6 to tne post asserobly by the cable (see 3.3.7). 3.3.2.3 Pintle. Tne pintle shall ascerable in the post asserrAXy a36 be retained in the post assembly by the split b
9、earing and syring pin. 5% -pintle shall rotate throughout its fu-l range of travelwiLhouLL Oindirg. 3.3.3 Amnition box. Tne ammunition box shall reaily assembly to and disacsemble from the weapon and be re-tainea on the weaTon Sracket as- sembly. range of travel and be held securely j=n pocitiafi by
10、 the SLW CLP LIS ejector plunger shall move freei? throughout it; fuil. range of travel rt-rdge bag frW aSSemb2y- 3.3.5 Xmpty cartridge bag frame asseably. The errpty cartridge bag frame assembly shall be capable. of being attached to an6 reniove frm t3e weapon. binding, and when released shall retu
11、rn to its origiml position by s-pirlg action. . RIIL- STD- 1261. . The ammunition retaining rod shsll. move Freely thr?ug;ho$ ifis, ?Jridge bag shall be capcbe The a-t;ch shall move freely through its fi111 range of travel trithout Weling of the cartriage bag fraze shall be in accor6mce with c 4- .
12、Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. XPL-8- 4 594 7 (wc ) 3.3.6 Shstic cozAsssezi3ly. Ilne ekistic cord asr;ex3; sk-z*rZ se - 1“ “LX ine elas- securely retained OK the sxnxfit, bracket. s gradual applied stretch Load of 75 pounGs f 5 pou
13、xs wlthout 6a:mge Gr permanent stetch, Tfie crirQe6 ceeves Gfi the cable shall be capable 05 withstanciirg the tencie lor an6 .k.i-%lsanCiIl.g IO cycies 02 rough handling without mlfunctions, unserviceable prts, or crackir-g ai“ welded Joints with a 10 pe_rceE%-.-onilSence leyel. specified in 4.4.3.
14、k 1.- to the mount shall have .an r;zixnuth of 1Olo -40 inciuaed angle, En ei_evsi“,-ion of 12.5O, to 69O depression, and shall meet the target reqtiiremefits fiefineit In Figures la and lb (see 4.4.2.4). 36 Marking. Each armament suScystem shall be clearly marked in accordance with the applicable d
15、rawings und ML-W-13855. 3.7 Workroanship. Workmanship shall be in accordance with the work- manship requirements of MIL-W-13855. Yesting shall be as specified in h-.h.3.2 3.3.7 Cable and sleeve cirQ tensile load. Testing ski1 be as t 3 . 5 Targeting. The armatnent sctbsyctem with M03 mchine -; sii-m
16、ystem, prts en6 packbgirg shal: be 5n accordance with XiL-STD-LC5. practicable in consideration of qmlity histoy, tmufaccw5fig conSftlcr-c, and contractors delivery schedule, and t7ithln the Er,t2%e-L$oas of K5-X 13855. parts that bve met all inspection requirements specified I=ereLr:. Znspection io
17、ts c%cS se SC -crge as Armament subsystazs shall be asseikdeii ?rom hts of coqmz,er 4.k.2 Exmination: 4.4.2.1 Corn-pnent pzircs arid c-oncurrenz ?eFi-r ar-cs . ExzzSzacior I of component parts and concurrefit, repzi-r prts shall Ge p3SorxeZ ir, accordance with the criteria specifie in the coatrsct (
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