欢迎来到麦多课文档分享! | 帮助中心 海量文档,免费浏览,给你所需,享你所想!
麦多课文档分享
全部分类
  • 标准规范>
  • 教学课件>
  • 考试资料>
  • 办公文档>
  • 学术论文>
  • 行业资料>
  • 易语言源码>
  • ImageVerifierCode 换一换
    首页 麦多课文档分享 > 资源分类 > PDF文档下载
    分享到微信 分享到微博 分享到QQ空间

    NAVY MIL-R-48416-1974 REMOVER AIRCRAFT CANOPY RAU-1 A METAL PARTS ASSEMBLY《RAU-1 A飞机座舱盖金属装配件清洗剂》.pdf

    • 资源ID:981283       资源大小:870.42KB        全文页数:20页
    • 资源格式: PDF        下载积分:10000积分
    快捷下载 游客一键下载
    账号登录下载
    微信登录下载
    二维码
    微信扫一扫登录
    下载资源需要10000积分(如需开发票,请勿充值!)
    邮箱/手机:
    温馨提示:
    如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
    如需开发票,请勿充值!如填写123,账号就是123,密码也是123。
    支付方式: 支付宝扫码支付    微信扫码支付   
    验证码:   换一换

    加入VIP,交流精品资源
     
    账号:
    密码:
    验证码:   换一换
      忘记密码?
        
    友情提示
    2、PDF文件下载后,可能会被浏览器默认打开,此种情况可以点击浏览器菜单,保存网页到桌面,就可以正常下载了。
    3、本站不支持迅雷下载,请使用电脑自带的IE浏览器,或者360浏览器、谷歌浏览器下载即可。
    4、本站资源下载后的文档和图纸-无水印,预览文档经过压缩,下载后原文更清晰。
    5、试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。

    NAVY MIL-R-48416-1974 REMOVER AIRCRAFT CANOPY RAU-1 A METAL PARTS ASSEMBLY《RAU-1 A飞机座舱盖金属装配件清洗剂》.pdf

    1、Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Provid

    2、ed by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NIL-R-48416 (?m) 4.2.1.2 _ Initialqroduction sainnle failure.-Failure of the sample to comply with requirements of the drawings and specifications shall result in sample disapproval. 4.3 Inspectio_n_provision

    3、. 4.3.1 - Lot. 4.3.1.1 Submission of poduct.-The product shall be submitted in accordance with MIL-STD-105. = 4.3.1.2 - Size of lot.-For - the purpose of identification and siiipnent, the shipping lots of metal parts assemblies shall consist of 12U units maximum, exclusive of test samples, provided

    4、the homogeneity of manufacturing process has been retained throughout the inspection lot. shipped upon approval of the contractin? officer. A smaller lot may be 4.3.2 - Esamination.-One hundred percent exaaination shall be performed for all critical defects. performed on a defect basis in accordance

    5、 with the classification of defects contained herein, using the samnling plan and associated criteria in Tables IV and V. For an individual defect (sinzle characteristic) the criteria in Table IV shall be used. in Table V shall be used. Inspection for O-rings shall be in accordance with :lIL-STD-413

    6、. The roughness comparison specimens prescribed in ANSI 846.1 shall be used as a basis of com- parison for surface roughness determination. may be used in performing visual examination for such defects as burr and foreign matter. Examination for major and minor defects shall be For total defects wit

    7、hin a najor or minor group the criteria All nonconforming rnaterial shall be rejected. Four power (4X) nagnification TAirLC IV Accept :umbers Xaj or Hinor Lot Size Sainple Size Accepr Reject ibly shall be subjected . to the &est for excessive residual magnetism. with the requirements of 3.9 shall be

    8、 cause for rejection of the assembly. equipment lisced on LI-11751076, Failure of any unit to coiiiply. 4.3.4 Jsj-esggo-qequipment. -+i -The exaniination and tests shall be made uskiig - 4 4 _T-s_t_met_ho_bc _and_2r!-cs!xe- 4.4.1 -I.- Hardness,-Prior -.I_ - to the application of protective finish. a

    9、 hardness - e used to detemine comnliance with the hardness requiremen he detail drawings. 4 4.2 Xvd roc_tt-c-_. -Or ior to the application o f pro t ec t ive finish , the inside and outside tubes shall be inaividiially mounted in a test device, using the fixture for sealinq all ogeninrs, and subj e

    10、cted to the hydrostatic pressure to determine conpliance with 3.4. seal the components at the prescribed seal surfeces without applying an axial load other than that applied by the liquid pressure. pin shall be subjected to the shear strenatli test to cicteriaine coapliance the requirements of 3.5 .

    11、 The test shall be pcrfor1w.d iii tiie fixture in con junction with a tensile testing i!iachine. The test device useci shall inteynally 4.4.3 sh-e-ax ELE %t-rbe:n3Lh.-Af ter applicatior, of protective finish, the 4.4.4 -ucrl-t-ent!, -The remover shall be placed in tlie teIIsile testing machine and s

    12、ubjected to tlie specified tension aiici conpression load for deterisinatiori of compliance with the requirements of 3 . The test siia be perfonded as follows : a. Apply a preload of 500 pouncs so us to move tile iriounting points away frois each other and adjust the dial iiiclicator to zero inches.

    13、 b. Apply the specified load in tension. c. Decrease the load to 590 pounds and recori! tiic dial indicator reading. d. Rcgeat steps “b and “c“, e. Apply a preload of 500 pounds so as to move the mounting points toward each other and adjust the dial indicator to zero inches. AVsly the specified load

    14、 in Compression. Decrease the load to 500 pounds and record the dial indicator f. p. reading, A - #&* li. Repeat steps “f“ and gii. 19 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-


    注意事项

    本文(NAVY MIL-R-48416-1974 REMOVER AIRCRAFT CANOPY RAU-1 A METAL PARTS ASSEMBLY《RAU-1 A飞机座舱盖金属装配件清洗剂》.pdf)为本站会员(jobexamine331)主动上传,麦多课文档分享仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文档分享(点击联系客服),我们立即给予删除!




    关于我们 - 网站声明 - 网站地图 - 资源地图 - 友情链接 - 网站客服 - 联系我们

    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 

    收起
    展开