V56 机场地面服务系统及设备 标准查询与下载

BS EN 14737-1:2004 航天工程.地面系统和操作.原理和要求

Within the frame of the overall engineering standards for space missions, this European Standard contains the basic rules, principles and requirements to be applied to the engineering of the ground segment and mission operations, which form an integral part of the overall system implementing a space mission. This European Standard includes development of ground segment, operations preparation activities, mission planning activities, mission evaluation activities, the conduct of operations proper, and all post-operational activities. The ground segment comprises the ground systems (i.e. all ground facilities, hardware and software) and all operational aspects such as personnel and related data repositories required on ground to perform mission operations. For reasons of recognized commonality, ground segment within the meaning of this European Standard includes those elements and facilities required for the purpose of implementing the mission and fulfilling the missions requirements while the relevant space segments are in-orbit. It covers ground elements used for purposes of assembly, integration and verification of the space segment, to the extent needed for ground segment end-to-end verification activities. It also covers elements integrated into the ground segment after completion of space segment AIT; space segment AIT proper being considered outside the scope of this Standard. It does not however cover the spacecraft activities and facilities interfacing the launch service segment. Furthermore, while this European Standard is applicable to all classes of missions it does not consider aspects that are specific to manned space missions. This European Standard is structured as follows: — identification of the ground systems and operations domain; — overview of ground segment engineering processes in relation to the project life cycle; — detailed description of specific aspects of the ground segment elements and engineering tasks. When viewed from the perspective of a specific project context, the requirements defined in this European Standard should be tailored to match the genuine requirements of a particular profile and circumstances of a project. NOTE Tailoring is a process by which individual requirements of specifications, standards and related documents are evaluated, and made applicable to a specific project by selection, and in some exceptional cases, modification of existing or addition of new requirements.

Space engineering - Ground systems and operations - Principles and requirements

SAE ARP5916-2004 回程和/或维护牵引用区域性航空器无牵引杆牵引车辆的设计规范

The tow vehicle should be designed for towbarless push-back and/or maintenance towing of regional type aircraft as specified in 1.3. The design will ensure that the unit will safely secure the aircraft nose landing gear within the coupling system for any operational mode. The purpose of this towing procedure is to achieve a safer and faster operation than is possible with conventional towing equipment.

Design Specification for Regional Aircraft Towbarless Tow Vehicle for Pushback and/or Maintenance Towing Operations

MH 7011-2003 民用航空微剂量X射线安全检查设备

本标准规定了民用航空微剂量X射线安全检查设备的技术要求、试验方法、包装、标志、贮存和运输。 本标准适用于民用机场、航空公司安全检查部门所使用的安检设备的选型、验收和使用。

Micro-does X-ray security inspection system for civil aviation

BS EN 61821:2003 机场照明和航路信标指示用电气设备.地面导航照明用恒流串联电路的检修

This International Standard applies to the maintenance of AGL constant current series circuits. This International Standard · covers constant current series circuits for AGL installed at aerodromes and heliports; · concentrates on providing the safety requirements for the maintenance of an AGL constant current series circuit. It is recognised that AGL constant current series circuits of different design characteristics and parameters are in existence; · is mainly concerned with safety to persons by specifying the rules and fundamental principles for the maintenance of AGL constant current series circuits; · is not intended to apply to AGL primary series circuits supplied directly from a mains constant voltage source; · is not intended to be used for public street lighting, roadway lighting or any other installation requiring the use of constant current series circuits.

Electrical installation for lighting and beaconing of aerodromes - Maintenance of aeronautical ground lighting constant current series circuits

MH/T 6031-2003 飞机充氧车

本标准规定了飞机充氧车的技术要求、试验方法、检验规则及包装、标志、贮存。 本标准适用于灌充飞机氧气瓶、地面氧气瓶、气瓶组氧气的相互灌充，地面气瓶向气瓶组补气灌充等作业功能的自行式或车载式飞机充氧车(以下简称充氧车)，也适用于拖挂式充氧机组。

Aircarft oxygen filling vehicles

BS EN 12312-3:2003+A1:2009 航空器地勤支援设备.专门要求.第3部分:输送带车

This European Standard specifies the technical requirements to minimise the hazards listed in clause 4 which can arise during the commissioning, operation and maintenance of conveyor belt vehicles when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some requirements recognised as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies. This standard applies to: -self-propelled conveyor belt vehicles with or without driver's accommodation; -self-propelled conveyor belt vehicles equipped with a van body; -towed conveyor belt vehicles, Intended to be used for manual loading/unloading of aircraft. Examples of typical designs of conveyor belt vehicles are given in annex A. This standard does not apply to pneumatic systems and to cableless remote controls. This standard does not establish requirements for hazards caused by noise and vibration. This Part of EN 12312 is not applicable to conveyor belt vehicles which are manufactured before the date of publication of this standard by CEN. This part of EN 12312 is intended to be used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 (for vehicles) and EN 1915-4.

Aircraft ground support equipment - Specific requirements - Part 3:Conveyor belt vehicles

SAE ARP5015A-2003 地面设备.400Hz地面电源性能要求

This SAE Aerospace Recommended Practice (ARP) covers the requirements for ground power equipment that supplies 115/200 V, 3-phase, 400 Hz output capable of powering aircraft type loads requiring MIL-STD-704E/DFS-400 quality power. All forms of ground power including mobile and fixed systems are addressed by this document. High voltage (270 V DC) systems are not included in this specification.

Ground Equipment - 400 Hertz Ground Power Performance Requirements

SAE AS4831A-2003 地基监控系统用的软件接口

To establish a specification for software input and output interfaces for condition monitoring and performance programs used to monitor equipment from multiple manufacturers. The purpose of standardizing these interfaces is to improve operational flexibility and efficiency of monitoring systems as an aid to cost effectiveness (e.g., easier implementation).

Software Interfaces for Ground-Based Monitoring Systems

BS EN 12312-2:2002 飞行器地面支持设备.特殊要求.餐饮车

This European Standard specifies the technical requirements to minimise the hazards listed in clause 4 which can arise during the commissioning, the operation and the maintenance of catering vehicles when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some requirements recognised as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies. This standard applies to self-propelled catering vehicles, with seated driver, equipped with a liftable van body. Examples of catering vehicles are shown in annex A. Vehicles of a similar design within the load limits of this standard used as GSE for other purposes e.g. cleaning equipment, exchange of aircraft seats, are also covered by this European Standard. This standard does not apply to pneumatic systems. This standard does not establish requirements for hazards caused by noise and vibration. This Part of EN 12312 is not applicable to catering vehicles which are manufactured before the date of publication of this standard by CEN.

Aircraft ground support equipment - Specific requirements - Catering vehicles

BS EN 12312-12:2002+A1:2009 航空器地勤支援设备.具体要求.饮用水服务设备

This European Standard specifies the technical requirements to minimise the hazards listed in clause 4 which can arise during the commissioning, operation and maintenance of potable water service equipment when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some requirements recognised as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies. This standard applies to: -self-propelled potable water vehicles; -towable potable water vehicles; -moveable parts of ramp integrated systems, designed for servicing aircraft and intended to be used under the conditions given in clause 1 of EN 1915-1:2001 (Examples see annex A). This standard does not establish requirements for hazards caused by noise and vibration. This Part of EN 12312 is not applicable to potable water service equipment which is manufactured before the date of publication of this standard by CEN. This part of EN 12312 is intended to be used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 (for vehicles) and EN 1915-4.

Aircraft ground support equipment - Specific requirements - Part 12:Potable water service equipment

BS EN 12312-12:2002 飞行器地面支持设备.特殊要求.饮用水服务设备

This European Standard specifies the technical requirements to minimise the hazards listed in clause 4 which can arise during the commissioning, operation and maintenance of potable water service equipment when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some requirements recognised as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies. This standard applies to: — self-propelled potable water vehicles; — towable potable water vehicles; — moveable parts of ramp integrated systems, designed for servicing aircraft and intended to be used under the conditions given in clause 1 of EN 1915-1:2001 (Examples see annex A). This standard does not establish requirements for hazards caused by noise and vibration. This Part of EN 12312 is not applicable to potable water service equipment which is manufactured before the date of publication of this standard by CEN.

Aircraft ground support equipment - Specific requirements - Potable water service equipment

BS EN 12312-13:2002+A1:2009 航空器地勤支援设备.专门要求.洗浴室服务设备

Aircraft ground support equipment - Specific requirements - Lavatory service equipment

BS EN 12312-13:2002 飞行器地面支持设备.特定要求.卫生间服务设施

This European Standard specifies the technical requirements to minimise the hazards listed in clause 4 which can arise during the commissioning, operation and maintenance of lavatory service equipment when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some requirements recognised as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies. This standard applies to: — self-propelled lavatory vehicles; — towable lavatory vehicles; — moveable parts of ramp integrated systems, designed for servicing aircraft and intended to be used under the conditions given in clause 1 of EN 1915-1:2001 (examples see annex A). This standard does not establish requirements for hazards caused by noise and vibration. This Part of EN 12312 is not applicable to lavatory service equipment which is manufactured before the date of publication of this standard by CEN.

Aircraft ground support equipment - Specific requirements - Lavatory service equipment

DLA MS24489 REV D (1)-2002 机场着陆照明玻璃标记滤波器

This amendment forms a part of MS24489D dated 15 February 1960 and is approved for use by all Departments and Agencies of the Department of Defense.

FILTER, MARKER LIGHT, AIRPORT APPROACH, GLASS

DLA MS24502 REV E (1)-2002 机场进场照明玻璃标记滤波器

This amendment forms a part of MS24502E dated 15 February 1960 and is approved for use by all Departments and Agencies of the Department of Defense.

FILTER, MARKER LIGHT, AIRPORT RUNWAY, GLASS

DLA MS17814 REV C (1)-2002 航空地面灯易碎耦合

This amendment forms a part of MS17814C dated 9 March 1972 and is approved for use by all Departments and Agencies of the Department of Defense.

COUPLING, FRANGIBLE, AVIATION GROUND LIGHTS

SAE ARP5910-2002 匝道标线

This SAE Aerospace Recommended Practice (ARP) outlines recommended ramp pavement marking standards for proper guidance and positioning of GSE on commercial transport aircraft parking and handling stands (gates), in line with International Civil Aviation (ICAO) recommendations applicable to airport aprons. Throughout this document, the minimum essential criteria are identified by use of the key word shall. Recommended criteria are identified by use of the key word should and, while not mandatory, are considered to be of primary importance in providing safety effective ramp markings. Deviation from recommended criteria should only occur after careful consideration and thorough service evaluation have shown alternate methods to provide an equivalent level of safety. Experience has demonstrated that ramp safety, both as to prevention of GSE accidents and injury to ramp workers and as to prevention of accidental damage to aircraft, closely depends on GSE operators adherence to safe driving and positioning practices, which in turn are greatly enhanced by the existence of recognized standard ramp markings in order to permanently materialize the variety of driving rules to be met. The purpose of this Aerospace Recommended Practice is to accordingly provide airlines and airport operators with: the definition of standardized ramp markings; the corresponding driving and operating rules, to be taught in ramp staff training.

Ramp Markings

BS EN 1915-1:2001 飞行器地面保障设备.一般要求.基本安全要求

This part of EN 1915 applies to GSE when used in civil air transport as intended by the manufacturer and contains safety requirements relating to the equipment in general. This part of EN 1915 deals with the technical requirements to minimize the hazards listed in clause 4 which can arise during operation and maintenance of GSE as intended by the manufacturer or his authorized representative. This part of EN 1915 should be used together with the specific standard of the EN 12312 series for the specific type of GSE (see also Foreword). This part of EN 1915 does not apply to unmodified automotive parts when used on GSE for the purpose for which they are designed. This part of EN 1915 does not establish additional requirements for the following: - operation elsewhere than in an airport environment; - operation in severe conditions, e.g. ambient temperature below -20 ℃ or over 50 ℃, tropical or saturated salty atmospheric environment, strong magnetic or radiation field; - operation subject to special rules, e.g. potentially explosive atmosphere except as regards operation in the vicinity of an aircraft fuel tank during fuelling operation; - hazards caused by power supply other than from electrical networks; - hazards occuring during construction, transportation, commissioning and decommissioning of the GSE; - hazards caused by wind velocity in excess of the figures given in this European Standard; - direct contact with foodstuffs; - earthquake, flood, landslide, lightning and more generally any natural catastrophe; - electromagnetic compatibility (EMC); - cableless remote control; - hazards caused by noise and vibration; - hazards caused by errors in the software. This part of EN 1915 is not applicable to GSE which are manufactured before the date of publication by CEN of this standard.

Aircraft ground support equipment - General requirements - Basic safety requirements

BS EN 1915-2:2001+A1:2009 地勤支援设备.一般要求.第2部分:稳定性和强度要求,计算和试验方法

This Part of EN 1915 specifies the conditions to be taken into consideration when calculating the strength and the stability of GSE according to !EN 1915-1" and the EN 12312 series under intended use conditions. It also specifies general test methods. NOTE The methods given in this standard demonstrate one way of achieving an acceptable safety level. Methods that produce comparable results may be used. This Part of EN 1915 does not establish additional requirements for the following:  operation elsewhere than in an airport environment; operation in severe conditions, e.g. ambient temperature below -20 °C or over 50 °C, tropical or saturated salty atmospheric environment;  hazards caused by wind velocity in excess of the figures given in this European Standard;  earthquake, flood, landslide, lightning and more generally any natural catastrophe. This Part of EN 1915 is not applicable to GSE which are manufactured before the date of publication by CEN of this Standard.

Aircraft ground support equipment — General requirements — Part 2: Stability and strength requirements, calculations and test methods

BS EN 1915-1:2001+A1:2009 航空器地勤支援设备.一般要求.第1部分:基本安全性要求

This Part of EN 1915 applies to GSE when used in civil air transport as intended by the manufacturer and contains safety requirements relating to the equipment in general. This Part of EN 1915 deals with the technical requirements to minimize the hazards listed in clause 4 which can arise during operation and maintenance of GSE as intended by the manufacturer or his authorised representative. !This European Standard is intended to be used in conjunction with EN 1915-2, EN 1915-3 (for vehicles) and EN 1915-4, and with the relevant part of EN 12312." This Part of EN 1915 does not apply to unmodified automotive parts when used on GSE for the purpose for which they are designed. This Part of EN 1915 does not establish additional requirements for the following: ? operation elsewhere than in an airport environment; ? operation in severe conditions, e.g. ambient temperature below -20 °C or over 50 °C, tropical or saturated salty atmospheric environment, strong magnetic or radiation field; ? operation subject to special rules, e.g. potentially explosive atmosphere except as regards operation in the vicinity of an aircraft fuel tank during fuelling operation; ? hazards caused by power supply other than from electrical networks; ? hazards occurring during construction, transportation, commissioning and decommissioning of the GSE; ? hazards caused by wind velocity in excess of the figures given in this European Standard; ? direct contact with food stuffs; ? earthquake, flood, landslide, lightning and more generally any natural catastrophe; ? electromagnetic compatibility (EMC); ? cableless remote control; ? hazards caused by noise and vibration, see EN 1915-3 and EN 1915-4; ? hazards caused by errors in the software. This Part of EN 1915 is not applicable to GSE which are manufactured before the date of publication by CEN of this Standard.

Aircraft ground support equipment — General requirements — Part 1: Basic safety requirements