NAVISTAR ESP F-1 421-NPP-2015 VOID - Tooth Lock Washers - Non-Preferred Parts (Noun Code 9720).pdf

上传人:Iclinic170 文档编号:962475 上传时间:2019-03-10 格式:PDF 页数:1 大小:92.67KB
下载 相关 举报
NAVISTAR ESP F-1 421-NPP-2015 VOID - Tooth Lock Washers - Non-Preferred Parts (Noun Code 9720).pdf_第1页
第1页 / 共1页
亲,该文档总共1页,全部预览完了,如果喜欢就下载吧!
资源描述

1、This document is restricted and may not be sent outside Navistar, Inc. or reproduced without permission from Corporate Technical Standards. Suppliers are required to assume all patent liability. 2015 by Navistar, Inc. July 2015 Page 1 of 1 NAVISTAR, INC. Engineering Standard Parts NUMBER ESP-F-1.421

2、NPP TITLE: Tooth Lock Washers Non-Preferred Parts (Noun Code 9720) CURRENT ISSUE DATE: July 2015 WRITTEN/REVIEWED BY: Corporate Technical Standards APPROVED BY: Corporate Technical Standards SUPERSEDES ISSUE OF: August 2014 PRINTED COPIES OF THIS DOCUMENT MUST BE VERIFIED FOR CURRENT REVISION Change Notice: Made VOID. This specification is VOID, and is replaced by MPAPS S-F-1.301-GS/PL. For questions, contact MaterialsEngineeringN VOID

展开阅读全文
相关资源
猜你喜欢
  • NASA NACA-TN-1851-1949 Critical shear stress of infinitely long simply supported plate with transverse stiffeners《带有横向增强板且无限长的简支板的临界剪切应力》.pdf NASA NACA-TN-1851-1949 Critical shear stress of infinitely long simply supported plate with transverse stiffeners《带有横向增强板且无限长的简支板的临界剪切应力》.pdf
  • NASA NACA-TN-1872-1949 High-lift and lateral control characteristics of an NACA 652-215 semispan wing equipped with plug and retractable ailerons and a full-span slotted flap《装配有插头.pdf NASA NACA-TN-1872-1949 High-lift and lateral control characteristics of an NACA 652-215 semispan wing equipped with plug and retractable ailerons and a full-span slotted flap《装配有插头.pdf
  • NASA NACA-TN-1977-1949 Summary of the theoretical lift damping-in-roll and center-of-pressure characteristics of various wing plan forms at supersonic speeds《在超音速下 多个机翼平面升力 滚转阻尼和压力.pdf NASA NACA-TN-1977-1949 Summary of the theoretical lift damping-in-roll and center-of-pressure characteristics of various wing plan forms at supersonic speeds《在超音速下 多个机翼平面升力 滚转阻尼和压力.pdf
  • NASA NACA-TN-2001-1956 Aerodynamic characteristics of damping screens《阻尼屏幕的空气动力特性》.pdf NASA NACA-TN-2001-1956 Aerodynamic characteristics of damping screens《阻尼屏幕的空气动力特性》.pdf
  • NASA NACA-TN-2010-1950 Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces《水平尾翼对带有45后掠翼和尾翼面.pdf NASA NACA-TN-2010-1950 Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces《水平尾翼对带有45后掠翼和尾翼面.pdf
  • NASA NACA-TN-2069-1950 Cylinder-head temperatures and coolant heat rejection of a multicylinder liquid-cooled engine of 1650-cubic-inch displacement《1 650 in3位移且多汽缸的液体冷却发动机的汽缸头温度和冷.pdf NASA NACA-TN-2069-1950 Cylinder-head temperatures and coolant heat rejection of a multicylinder liquid-cooled engine of 1650-cubic-inch displacement《1 650 in3位移且多汽缸的液体冷却发动机的汽缸头温度和冷.pdf
  • NASA NACA-TN-2080-1950 Wind-tunnel investigation at low speed of an unswept untapered semispan wing of aspect ratio 3 13 equipped with various 25-percent-chord plain flaps《装配有多个25%.pdf NASA NACA-TN-2080-1950 Wind-tunnel investigation at low speed of an unswept untapered semispan wing of aspect ratio 3 13 equipped with various 25-percent-chord plain flaps《装配有多个25%.pdf
  • NASA NACA-TN-2114-1950 Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds supersonic leading and trailing edges《在超音速下 带有任意掠角和锥形薄.pdf NASA NACA-TN-2114-1950 Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds supersonic leading and trailing edges《在超音速下 带有任意掠角和锥形薄.pdf
  • NASA NACA-TN-2146-1950 On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream《关于亚音速机翼后缘对在超音速流下薄后掠翼滚动和倾斜阻尼的影响》.pdf NASA NACA-TN-2146-1950 On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream《关于亚音速机翼后缘对在超音速流下薄后掠翼滚动和倾斜阻尼的影响》.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