V22 机械配件、构件 标准查询与下载

DLA MS51996 REV A (1)-2002 标准尺寸高强度环形锁定嵌块及柱头螺栓打孔

This amendment forms a part of MS51996A, dated 11 MARCH 1985, and is approved for use by all Departments and Agencies of the Department of Defense.

HOLE-PREPARATION-RING LOCKED INSERTS AND STUDS, HIGH STRENGTH, STANDARD DIMENSIONS FOR

DLA MS51498 VALID NOTICE 1-2002 特大代替物锯齿状高强度线形锁定螺杆嵌件

MS51498, Amendment 1, dated 6 August 1997, has been reviewed and determined to be valid for use in acquisition.

INSERT, SCREW THREAD-LOCKED IN, RING LOCKED, SERRATED, HIGH STRENGTH, OVERSIZE REPLACER

SAE ARP5483/8-2002 滚动轴承动力径向荷载测试

This test method outlines the recommended machine function, fixtures and procedures used to test airframe rolling element bearings for dynamic performance under steady unidirectional radial load and oscillatory motion. Bearings covered by this test method shall be ball, roller and needle type in either annular or rod end configuration, used in airframe control applications.

Rolling Bearing Dynamic Radial Load Test

BS EN 2130:2001 航空航天系列.仪器和设备用耐蚀钢制轴承和精密滚珠.技术规范

This standard specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for precision ball bearings, in corrosion resisting steel, with a nominal bore diameter ≤ 8 mm, used for aerospace instruments and equipment. It is applicable whenever referenced.

Aerospace Series - Bearings, precision ball in corrosion resisting steel for instruments and equipment - Technical specification

BS EN 2585:2001 航空航天系列.带有自润滑衬垫的球面耐蚀钢轴承.环境温度下的高负荷.负荷和尺寸规格

This standard specifies the characteristics of spherical plain bearings in corrosion resisting steel, with self-lubricating liner, narrow series, for elevated load at ambient temperature, with or without swaging groove, intended for use in the fixed or moving parts of the aircraft structure and control mechanisms. They shall be used in the temperature range - 55℃ to + 163℃.

Aerospace series - Bearings, spherical plain in corrosion-resisting steel with self-lubricating liner - Elevated load at ambient temperature - Dimensions and loads

DLA A-A-50213 A VALID NOTICE 1-2001 法国铁路和轮船机械工程师用规则和不规则绘图曲线板装置规则和不规则绘图曲线板

A-A-50213A, dated 18 May 1988, has been reviewed and determined to be valid for use in acquistion.

CURVES, DRAFTING, REGULAR AND IRREGULAR: CURVE SETS, DRAFTING, REGULAR AND IRREGULAR; FRENCH, MECHANICAL ENGINEERS, RAILROAD, AND SHIPS

DLA A-A-50201A VALID NOTICE 1-2001 带盒笔和铅笔支点弹簧绘图圆规

The General Services Administration has authorized the use of this commercial item description as a replacement for Military Specifications MIL-V-16720E and MIL-V-16721D which are cancelled.

COMPASS, DRAFTING, PIVOT, DROP SPRING BOW, PEN& PENCIL, WITH CASE

DLA MS9915 VALID NOTICE 3-2001 AMS 6322型镉板的0.250-28 UNJF-3A压力杆双重六边垫圈顶部加长锚杆机

MS9915, dated 22 September 1994, remains inactive for new design; however, the document is valid for acquisition when needed.

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD PD SHANK, STEEL, AMS 6322, CADMIUM PLATED, 250-28 UNJF-3A

DLA MS9896 VALID NOTICE 3-2001 AMS 5616型 0.3125-24 UNJF-3A钻孔双重六边垫圈顶部加长锚杆机

MS9896, dated 22 September 1994, remains inactive for new design; however, the document is valid for acquisition when needed.

BOLT, MACHINE, DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, AMS 5616, .3125-24 UNJF-3A

DLA MS51837 VALID NOTICE 2-2001 牙形孔尺寸安装螺纹嵌件

MS51837, dated 5 May 1988, has been reviewed and determined to be valid for use in acquistion.

INSERT, SCREW THREAD - THREAD FORMING HOLE DIMENSIONS FOR AND INSTALLATION OF

DLA MS51998 VALID NOTICE 2-2001 设计及使用限制锯齿环形锁定螺纹螺杆嵌块

MS51998, dated 10 May 1988, has been reviewed and determined to be valid for use in acquistion.

INSERT, SCREW THREAD-LOCKED IN, RING LOCKED, SERRATED, DESIGN AND USAGE LIMITATIONS FOR

DLA MS51994 REV A VALID NOTICE 1-2001 标准尺寸环形锁定嵌块及柱头螺栓打孔

MS51994A, dated 12 February 1988, has been reviewed and determined to be valid for use in acquistion.

HOLE PREPARATION-RING LOCKED INSERTS AND STUDS, STANDARD DIMENSIONS FOR

AIA/NAS NASM91524-2001 FSC 5355型金属和塑料旋钮控制短横条

Knob, Control, Short Bar, Metal and Plastic FSC 5355

Knob, Control, Short Bar, Metal and Plastic

SAE ARP5606-2001 合成蜂巢式部件的NDI参考标准

This recommended practice establishes generic reference standards that will accommodate nondestructive inspections (NDI) on a broad range of non-metallic composite honeycomb structures found on aircraft. The purpose of this Aerospace Recommended Practice (ARP) is to describe the design and production of composite honeycomb calibration standards to be used in ultrasonic, resonant, and tap test NDI equipment calibration for accomplishment of damage assessment and post-repair inspection of aircraft composites. These standards may also be appropriate for other NDT methods but will need to be assessed as appropriate prior to their use. The standards are representative of damage found in the field and include typical flaw scenarios such as disbonds and delaminations. It is intended that these standards be adopted by aircraft Original Equipment Manufacturers within procedures contained contained in their Nondestructive Testing Manuals. Depending on the nature of the inspection, it may be necessary to compensate for variations in material properties through the use of correction factors or by adjusting for these differences on the part or structure being inspected. In certain instances, it may be desirable or necessary to design a new reference standard to accommodate a specific inspection application. Currently, the recognized number of composite honeycomb construction variables makes the resulting number of specimens very large and unmanageable. Inspection characterizations and equipment responses have been used to determine the important variables needed in a composite reference standard thus eliminating unnecessary standard configurations. This ARP describes a workable number of reference specimens that can meet the needs of a broad range of honeycomb structures found on aircraft.

Composite Honeycomb NDI Reference Standards

SAE AIR5426-2001 配件和配件总成的选择,安装,检验和维护

This SAE Aerospace Information Report (AIR) includes the selection, installation, inspection, and maintenance of tube fittings and tube fitting assemblies used in aerospace plumbing applications. The user must determine the suitability of selected designs to meet the performance requirements of the system for which it is intended to be installed. Only fittings for which industry or government standards have been published are described. A variety of these tube fittings are shown in SAE AIR 310. Illustrations of some non-published proprietary designs are shown.

Fitting and Fitting Assembly Selection, Installation, Inspection and Maintenance of

NAVY QPL-AS23899-1-2001 听觉保护器

This list has been prepared for use by or for the Government in the acquisition of products covered by the subject non-government standard, and such listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense. All products listed herein have been qualified under the requirements for the product as specified in the latest adopted issue of the applicable non-government standard. This list is subject to change without notice; revision or amendment of this list will be issued as necessary. The listing of a product does not release or otherwise affect the obligation of the manufacturer to comply with the non-government standard requirements.

AURAL PROTECTOR, SOUND [Superseded: NAVY QPL-23899 -10 CANC NOTICE 1, NAVY QPL-23899 -10, NAVY QPL-23899 -9, NAVY QPL-23899 -8, NAVY QPL-23899 -7, NAVY QPL-23899 -6, NAVY QPL-23899 -5, NAVY QPL-23899 -4, NAVY QPL-23899 -3, NAVY QPL-23899 -2, N

SAE AIR1489B-2001 航空起落架系统术语

This report has been compiled by the Landing Gear Systems Terminology panel of SAE Committee A-5 (Aerospace Landing Gear Systems). It represents an effort to gather together those terms commonly used within the discipline.

Aerospace Landing Gear Systems Terminology

AECMA EN 3280/PRA1-2001 航空航天系列轴承，机身滚动刚性或自动调心技术规范第 1 版； EN 3280:1994 修正草案 A1

Aerospace Series Bearings, Airframe Rolling Rigid or Self-Aligning Technical Specification Edition 1; Draft Amendment A1 to EN 3280:1994

BS ISO 9760:2001 航空航天.航空器滚动轴承操纵钢丝绳上的锻制耐腐蚀钢制叉形端.尺寸规格及载荷

This International Standard specifies the characteristics of fork-ends for rolling bearings in corrosion-resistant steel swaged on aircraft control wire rope.

Aerospace - Fork-ends, in corrosion-resistant steel, swaged on aircraft control wire rope, for rolling bearings - Dimensions and loads

SAE AS4052A-2001 密封装置设计:铲运机起落架装置安装

This SAE Aerospace Standard (AS) covers an alternate gland design for the installation of scraper/wiper rings in the lower end of landing gear shock struts for the purpose of contaminant exclusion. The defined scraper gland covered by this document, as shown, is a variant of MIL-G-5514, the accepted gland standard for MS28775. Piston diameters, gland internal diameters, and the groove sidewall angles and surface finish are defined by MIL-G-5514, but the gland outer retaining wall diameter is changed. AS4088 is similar to this document, but was developed by SAE A-6 for flight control and general purpose cylinders. It differs from this document primarily by the clearance between the rod (piston) and outer gland wall. Since landing gears are more susceptible to dirt contamination, the additional clearance provides a larger path to allow excessive dirt accumulation to exit the gland.

Gland Design: Scraper, Landing Gear, Installation