V56 机场地面服务系统及设备 标准查询与下载

SAE AIR1336B-2013 地面支持设备电气系统

This SAE Aerospace Information Report (AIR) considers the following major areas: 1. major components and their ratings, 2. selection criteria for optimum design balance for electrical systems, 3. effects of operating conditions and environment on both maintenance and life of components, and 4. trouble signals--their diagnosis and cure. Electrical Systems Engineering is the modern concept of integrating load requirements with generator/alternator and battery capacity and regarding this electrical equipment as a complete system rather than a collection of independent units. The old adage ""a chain is not stronger than its weakest link"" is particularly valid

Ground Support Equipment Electrical Systems

MH/T 6076-2013 民用航空燃料设施设备浸润冲洗质量控制

本标准规定了民用航空燃料设施设备（以下简称设施设备）浸润冲洗的基本要求，设施设备检查，浸润，冲洗和记录档案的要求。本标准适用于各类民用航空燃料新建，改建，扩建或新购置的设施设备的浸润冲洗。

Quality control for soaking and flushing of civil aviation fuel facilities and equipment

SAE AS6480B-2013 C-2型飞机货物系紧装置

This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification has been declared ""NONCURRENT"" as of June 2007. It is recommended, therefore, that this document not be specified for new designs. This specification covers one type of aircraft cargo tie down, designated Type C-2.

Tie Down, Cargo, Aircraft, Type C-2

BS EN 12312-1:2013 航空器地勤支援设备.具体要求.客梯

Aircraft ground support equipment. Specific requirements. Passenger stairs

BS EN 12312-9:2013 航空器地面支持设备.详细要求.集装箱/托盘装箱机

Aircraft ground support equipment. Specific requirements. Container/Pallet loaders

BS EN 1915-1:2013 航空器地勤支援设备. 一般要求. 基本安全性要求

Aircraft ground support equipment. General requirements Basic safety requirements

SAE ARP4853C-2013 无杆牵引拖车用设计规范

The tow vehicle should be designed for towbarless movement of aircraft on the ground. The design will ensure that the unit will safely secure the aircraft nose landing gear within the coupling system for any operational mode.

Design Specification for Towbarless Tow Vehicles

ASTM D4306-13 受痕量杂质影响的试验用航空燃料采样容器标准操作规程

3.1 General descriptions for the manual sampling of petroleum products are given in Practice D4057. However, a number of aviation fuel properties are established or affected by trace levels of polar or other compounds. Measurement significance therefore requires that the sample containers not add or adsorb any materials. This practice presents types and preparations of sampling containers found satisfactory for the determination of water separation, copper corrosion, electrical conductivity, thermal stability, lubricity, and trace metal content. An approval procedure for new containers is also given. 3.2 Two properties, particulate contamination and free water content, involve materials easily removed by any sampling container. These properties should be determined by placing the sample directly into the measuring apparatus and not using containers to transport the sample to the measuring equipment. 3.3 Recommendations in this practice provide guidance for immediate use and for storage of samples. Immediate use involves sample storage for periods less than 24 h. 1.1 This practice2 covers the types of and preparation of containers found most suitable for the handling of aviation fuel samples for the determination of critical properties affected by trace contamination. 1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. For specific warning statements, see 5.1, 5.2, 5.3, 5.4, and 5.6.

Standard Practice for Aviation Fuel Sample Containers for Tests Affected by Trace Contamination

BS ISO 11076:2012 航空器.地面液体除冰和防冰法

Aircraft. De-icing/anti-icing methods on the ground

SAE ARP4852C-2012 无杆推回牵引车辆的设计规范

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This SAE Aerospace Recommended Practice (ARP) describes the dimensions, design, layout, performance, and capability of a towbarless tow vehicle (TLTV), mainly used for push-back operation on the nose gear. This tow vehicle will basically be used for aircraft listed in 1.3. Overall design of the unit is to allo operations under climatic conditions as stated under 5.1 and safe operations during day and nigh conditions on airpo

Design Specification for Towbarless Push-Back Tow Vehicles

SAE AIR1353C-2012 减震牵引装置试验

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. The main purpose of this test was to determine the application advantages of cushion tow hitches in comparison to the commonly used rigid tow hitch type fitted on heavy aircraft towing tractors. As diverse opinions emerged about its suitability since the introduction on the market of this new tow hitch type, it was intended to physically measure and evaluate the damping capability of this cushioned tow link when applied in p

Cushion Tow Hitches Test

SAE AS4262B-2012 飞机地面空调服务连接

This SAE Aerospace Standard (AS) defines interface configurations for the ground air conditioning service connection on commercial transport aircraft. In addition, it defines the clearances required to accommodate the connection of ground air conditioning hose couplings. Two types of service connections are included. The Type A connection is a slotted ring with integral locking pads and is comparable to the MS33562 connection. The Type B connection is a flanged tube with external locking lugs. The Type B connection has the same interface dimensional requirements as the Type A connection. The purpose of this document is to establish uniform interface configu

Aircraft Ground Air Conditioning Service Connection

SAE AS36102A-2012 空运成组装运设备.试验方法

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This SAE Aerospace Standard (AS) provides requirements on how to test air cargo Unit Load Devices (ULD). The purpose of this Aerospace Standard is to establish acceptable ULD test methods and load distributions used to prove compliance with minimum performance requirements as established in AS36100.

Air Cargo unit Load Devices - Testing Methods

ISO 11532:2012 飞机地面设备.图形符号

Aircraft ground equipment - Graphical symbols

ISO 11076:2012 航空器.地面液体除冰和防冰法

Aircraft - De-icing/anti-icing methods on the ground

SAE ARP5911A-2012 支线分机无杆牵引车辆.试验要求

The present Aerospace Recommended Practice specifies for airplane operator and tow vehicle manufacturers the basic testing requirements for towbarless tow vehicles to be used on the nose gear of conventional tricycle type landing gears of commercial civil transport aircraft with maximum ramp weight between 8600 kg (19 000 lb) and 50 000 kg (110 000 lb), commonly designated as "regional aircraft". Its purpose is to achieve testing results, or equivalent computer modeling, demonstrating that the loads induced by the tow vehicle will not exceed the design loads of the airplane's nose landing gear and associated structure, reduce the certified safe life limit of the nose landing gear, or otherwise compromise the airplane's structural integrity and airworthiness certification. This document is intended to be applicable to all towbarless tow vehicles to be used for push-back and maintenance towing of commercial airplanes in the specified range. See Section 3 hereafter. It is not intended to apply to tow vehicles used for airplane operational (dispatch) towing.

Regional Aircraft Towbarless Tow Vehicle - Test Requirements

DIN EN 61821:2012 机场照明和航路信标电气设备.航空用地面照明恒流串联电路的维修(IEC 61821-2011).德文版本EN 61821-2011

Electrical installations for lighting and beaconing of aerodromes - Maintenance of aeronautical ground lighting constant current series circuits (IEC 61821:2011); German version EN 61821:2011

SAE AIR1361A-2012 传输联动装置

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. The following recommendations and suggestions are made for consideration for procurement of new equipment, or modification to existing equipment where practical. Excluded from this AIR is mobile ground equipment, such as fork lift trucks and from end loaders, that have a functional requirement for simultaneous vehicle motion and accessory operation .

Transmission Interlocks

BS ISO 27471:2012 航空地勤支援设备.上层甲板装载机.功能要求

Aircraft ground equipment. Upper deck loader. Functional requirements

ISO 27471:2012 航空地勤支援设备.上层甲板装载机.功能要求

This International Standard specifies the functional and performance requirements for a self-propelled container/pallet loader capable of raising air cargo unit load devices (ULDs) to the upper deck of very large capacity freighter (VLCF) aircraft and also to the main deck of any main-line freighter aircraft. This International Standard does not intend to provide all the design requirements applicable for aircraft upperdeck loaders. Other requirements can be found in separate standards which are also applicable: — equipment intended for handling and loading of baggage and cargo ULDs; — to all aircraft ground support equipment. The requirements of this International Standard were determined based on generally recognized assumptions as to: a) the normally intended use of aircraft ground support equipment, when used on the ramp of international civil airports in order to handle, service or maintain civil transport aircraft; b) the environmental (surface, slope, weather, lighting, operating rules, traffic infrastructure, staff qualification, etc.) conditions prevailing on the ramp area of the majority of international civil airports. It is assumed that the manufacturers of aircraft upper-deck loaders define in the relevant documentation the specifically intended conditions of use and environment for each model, and that the purchasers systematically review their own specific conditions of use and environment in order to determine whether those stated are adequate, or negotiate with the manufacturer appropriate modifications to ensure they are. This International Standard does not specify requirements applicable to: — any adapters or ancillary/supplemental equipment additions to in-service main-deck loaders in order to allow their occasional upper-deck use; — any main-deck loaders fitted with optional access to upper-deck height of the front platform only

Aircraft ground equipment - Upper deck loader - Functional requirements