49.100 地面服务和维修设备 标准查询与下载

MH/T 6017-2017 飞机牵引车

本标准规定了飞机牵引车的术语和定义、技术要求、试验方法、检验规则、标牌、标识、使用说明书、包装、运输和贮存。 本标准适用于在机场范围内使用拖把牵引或顶推飞机的飞机牵引车(以下简称牵引车)。

Aircraft tow tractor

MH/T 6016-2017 航空食品车

本标准规定了航空食品车的术语和定义、技术要求、试验方法、检验规则、标牌、标识、使用说明书、包装、运输和贮存。 本标准适用于在民用机场内使用的航空食品车(以下简称食品车)。

Aviation catering vehicle

ISO 16004:2017 航空地勤设备. 旅客登机桥或客梯车. 飞机舱门接口要求

Aircraft ground equipment - Passenger boarding bridge or transfer vehicle - Interface requirements with aircraft doors

GOST R 18.12.02-2017 航空加油技术. 航空燃油供应典型方案的安装. 通用技术要求

Technology of the aviation fueling. Installation of the aviation fuel supply typical schemes.General technical requirements

BS ISO 7718-2:2016 航空器.乘客登机桥或机场摆渡车连接用客舱门接口要求.上层舱门

Aircraft. Passenger doors interface requirements for connection of passenger boarding bridge or passenger transfer vehicle. Upper deck doors

BS ISO 7718-1:2016 航空器.乘客登机桥或机场摆渡车连接用客舱门接口要求.主舱门

Aircraft. Passenger doors interface requirements for connection of passenger boarding bridge or passenger transfer vehicle. Main deck doors

GSO ISO 7716:2016 航空货运设备 单元负载装置运输车辆（UTV） 功能要求

This International Standard specifies minimum functional requirements for type 3, class A, air cargo unit load device (ULD) chassis in accordance with the terminology defined in ISO 7715. This International Standard outlines the functional requirements for a ULD transport vehicle, capable of carrying unit load devices over airport and public roads and transferring them to/from rollerized ULD handling equipment.

Air cargo equipment -- Unit load devices transport vehicle (UTV) -- Functional requirements

GSO ISO 9678:2016 飞机 自走式饮水机

This International Standard specifies the functional requirements for a self-propelled potable-water vehicle capable of servicing all aircraft commonly in service in civil air transport. It is not intended to specify equipment design but rather to highlight certain criteria that are known to be essential for efficient operation in the civil airline environment. In all cases this International Standard should be applied with due reference to national regulations on sanitation that may be applicable in the area in which it is proposed that the vehicle will be used. To avoid any accidental contamination, the unit should only be used to supply aircraft with potable water.

Aircraft -- Self-propelled potable-water vehicle

GSO ISO 8267-1:2016 飞机 牵引杆附件接口要求 第1部分：干线飞机

This part of ISO 8267 specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) in conventional tricycle type landing gears of commercial civil transport passenger and freight aircraft. Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft mass category (which determines tow bar forces) in order to ensure that a single type of tow bar with a standard connection can be used for all aircraft types within or near that mass category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used. This part of ISO 8267 is applicable to all new models of main line aircraft within the specified maximum ramp mass range, entering service or designed after its date of publication. This part of ISO 8267 is applicable to main line commercial transport aircraft of airworthiness certified under FAR/JAR Parts 25 with a maximum ramp mass of > 50 000 kg (110 000 lb). It does not apply to aircraft of airworthiness certified under FAR/JAR Parts 25 but with a maximum ramp mass of ≤ 50 000 kg (110 000 lb), which are covered by ISO 8267-2. Where a family of existing or contemplated aircraft types bridges two mass categories, use a single tow bar attachment fitting interface for all of them, and consider the use of the standard dimensions for the higher mass category throughout the family. NOTE As far as practical, this part of ISO 8267 was defined in order to be compatible with as many existing aircraft types as possible in the mass category concerned.

Aircraft -- Tow bar attachment fittings interface requirements -- Part 1: Main line aircraft

GSO ISO 6966-2:2016 飞机地面设备 基本要求 第2部分：安全要求

This part of ISO 6966 specifies the minimum design requirements applicable to all aircraft ground support equipment (GSE), as defined in 3.1 hereafter, in order to ensure a) safety of staff operating or maintaining the equipment or in its vicinity, and b) protection of aircraft against interference or damage. An informative list of the most commonly used pieces of ground equipment is provided in Annex A hereafter. Nevertheless, the requirements of this part of ISO 6966 apply to any piece of aircraft ground support equipment, as defined, used on airports. This part of ISO 6966 does not intend to provide all the design requirements applicable for aircraft ground support equipment. Other requirements apply, and can be found in separate International Standards: — ISO 6966-1 specifies the general, other than safety-related, requirements applicable to all aircraft ground support equipment; — ISO 4116 specifies the additional requirements applicable for conveying surfaces of those pieces of aircraft ground support equipment intended for handling and loading of baggage and cargo unit load devices; — specific International Standards, listed in the Bibliography, define the functional and performance requirements for certain types of aircraft ground support equipment. In most countries, standing Government Health and Safety laws and regulations apply to machinery, implicitly or explicitly, including aircraft ground support equipment. Nothing in this part of ISO 6966, however, shall be deemed or otherwise used to supersede any locally applicable law or regulation, unless a specific exemption has been obtained for this purpose from the appropriate Authority. This part of ISO 6966 does not apply to automotive vehicles or parts thereof approved for public vehicles, when used on aircraft ground support equipment for the purpose for which they are designed.

Aircraft ground equipment -- Basic requirements -- Part 2: Safety requirements

GSO ISO 21100:2016 航空货运单元负载装置性能要求和试验参数

1.1 The purpose of this International Standard is to establish the minimum requirements for airworthiness approval of air cargo pallets, nets and containers, generally designated as air cargo unit load devices. NOTE In all countries, standing Government regulations apply to air cargo unit load devices airworthiness approval. This International Standard is intended to provide a uniform technical reference for air cargo unit load devices approval, but does not, under any circumstance, supersede the requirements of applicable regulations or the aircraft manufacturer’s Authority approved Weight and Balance Manual. 1.2 This International Standard defines the minimum performance requirements and test parameters for air cargo unit load devices requiring approval of airworthiness for installation in an approved aircraft cargo compartment and restraint system that complies with the cargo restraint and occupant protection requirements of EASA CS-25 or 14 CFR Part 25, except for the 9,0 g forward ultimate inertia force of § 25.561(b) (3) (ii). 1.3 This International Standard applies to airworthiness approved air cargo unit load devices intended for carriage on board civil transport category airplanes type certificated under EASA CS-25, “Certification Specifications for Large Aeroplanes” or 14 CFR Part 25, “Airworthiness Standards - Transport Category Airplanes”, or equivalent regulations. 1.4 It exclusively applies to unit load devices airworthiness approval and testing parameters. It does not apply to either aircraft design or aircraft operating requirements, which are provided by the approved Weight and Balance Manual for each aircraft type. 1.5 Other aspects that do not directly pertain to air cargo unit load devices airworthiness approval and testing, e.g.: — ULD design specifications, — ULD in service damage limits, — ULD restraint malfunction limitations, — ULD test methods, — ULD load distribution models, — ULD maximum allowable contours, — ULD C.G. location control means, — ULD pressure equalization methods, — ULD utilization guidelines, are defined in other International Standards (see 2.2, Normative References and Bibliography). 1.6 Air cargo unit load devices qualified prior to publication of this specification were TSO (Technical Standard Order) approved in accordance with the requirements of International Standard ISO 8097:2001. This International Standard is intended as a TSO approval reference for all new models of unit load devices in the sizes or types it covers, in replacement of previously used ISO 8097. NOTE ISO 8097 is based on USA National Aerospace Standard NAS 3610 revision 10:1990, Specification for Cargo Unit Load Devices. 1.7 Air cargo unit load devices the size or type of which is not covered in this specification are to keep being airworthiness approved in accordance with the requirements of ISO 8097:2011, if their size or type is contained therein, or in accordance with other equivalent criteria, if not. NOTE the requirements for cargo covers are not defined in this International Standard, except insofar as net restraint is incorporated therein.

Air cargo unit load devices -- Performance requirements and test parameters

GSO ISO 9667:2016 飞机地面支持设备 牵引杆

This International Standard specifies dimensional and physical requirements of tow bar connections to tractor and aircraft (see figure 1). It is applicable to any new type of commercial transport category aircraft tow bar designed or built after publication of this standard. The purpose of this International Standard is to standardize tow bar attachments to airplane and tractor according to the mass category of the towed aircraft, so that one tow bar head with different shear levels can be used for all aircraft that are within the same mass category and are manufactured in compliance with ISO 8267.

Aircraft ground support equipment -- Tow bars

GSO ISO 7717:2016 飞机 四轮驱动牵引车 设计的性能要求因素

This International Standard identifies and summarizes the various factors that shall be considered and evaluated by the design or specifying engineer in establishing performance requirements for four-wheel-drive aircraft tow tractors. The International Standard provides a summary of design factors that shall be considered in establishing performance requirements, as well as various tabulated design data and explanatory examples. It is not within the scope of this International Standard to specify a comprehensive set of design criteria for aircraft tractors, but only those relating to performance requirements.

Aircraft -- Four-wheel-drive tow tractors -- Performance requirements factors for design

GSO ISO 6966-1:2016 飞机地面设备 基本要求 第1部分：总体设计要求

This part of ISO 6966 specifies the minimum general design requirements applicable to aircraft ground support equipment, as defined in 3.1, in order to ensure a) definition of aircraft ground support equipment general requirements for designers; b) effective operation of aircraft ground support equipment. The requirements of this part of ISO 6966 apply to any piece of aircraft ground support equipment, as defined in 3.1, used on airports. NOTE An informative list of the most commonly used pieces of ground equipment is provided in Annex B. This part of ISO 6966 does not provide all the design requirements applicable for aircraft ground support equipment. Other requirements apply, and can be found in separate standards: — ISO 6966-2 specifies the safety-related requirements applicable to all aircraft ground support equipment; — ISO 4116 specifies the additional requirements applicable for conveying surfaces of those pieces of aircraft ground support equipment intended for handling and loading of baggage and cargo unit load devices (ULDs); NOTE In addition, guidelines for efficiency of conveying surfaces of ground support equipment used to handle air cargo ULDs are provided in Annex A. — specific standards, listed in the Bibliography, define the functional and performance requirements for certain types of aircraft ground support equipment. This part of ISO 6966 does not apply to unmodified general-use transportation vehicles such as automobiles, vans, buses and flat-bed trucks when used on airports.

Aircraft ground equipment -- Basic requirements -- Part 1: General design requirements

KS W 8311-2016(2021) 航空地面灯和表面标记颜色

Aeronautical ground light and surface marking colours

KS W 8311-2016 航空地面灯和表面标记颜色

Aeronautical ground light and surface marking colours

JIS W 8301:2016 航空用地面信号灯和色标

Aeronautical ground light and surface marking colours

ISO 7718-1:2016 航空器. 旅客登机桥或旅客客梯车连接的乘客门接口要求. 第1部分: 主舱门

Aircraft - Passenger doors interface requirements for connection of passenger boarding bridge or passenger transfer vehicle - Part 1: Main deck doors

ISO 7718-2:2016 航空器. 旅客登机桥或旅客客梯车连接的乘客门接口要求. 第2部分: 上舱门

Aircraft - Passenger doors interface requirements for connection of passenger boarding bridge or passenger transfer vehicle - Part 2: Upper deck doors

BS ISO 43:2016 航空器千斤顶基座

Aircraft. Jacking pads