49.120 货运设备 标准查询与下载

ISO 21100:2020 空运货物装载装置 - 性能要求和试验参数

This document specifies the minimum requirements for airworthiness approval of air cargo pallets, nets and containers, generally designated as air cargo unit load devices (ULD). This document is intended to provide a uniform technical reference for air cargo unit load devices approval. As a prerequisite, it is presupposed that the applicable general civil aviation requirements and the aircraft manufacturer’s approved Weight and Balance Manual are followed. This document 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). This document applies to airworthiness approved air cargo unit load devices intended for carriage on board civil transport category airplanes type certificated under EASA CS-25 or 14 CFR Part 25, or equivalent. This document exclusively applies to unit load devices airworthiness approval and testing parameters. It does not apply to aircraft design or aircraft operating requirements, which are provided by the approved Weight and Balance Manual for each aircraft type. Other aspects that do not directly pertain to air cargo unit load devices airworthiness approval and testing are not covered by this document and are defined in other International Standards (see Bibliography), 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 CG (centre for gravity) location control means, — ULD pressure equalization methods, — ULD utilization guidelines. Air cargo unit load devices qualified prior to publication of this document were approved in accordance with the requirements of ISO 8097:2001. This document is intended as a TSO approval reference for all new models of unit load devices in the sizes and types it covers, in replacement of ISO 8097. For air cargo unit load devices the size or type of which is not covered in this document, see the requirements NOTE 1 ISO 8097 is based on USA National Aerospace Standard NAS 3610 revision 10:1990, Specification for Cargo Unit Load Devices.  NOTE 2 The requirements for cargo covers are not defined in this document, except insofar as net restraint is incorporated therein.

Air cargo unit load devices — Performance requirements and test parameters

ISO 21785:2020 空运货物装载装置 - 载荷分布模型

This document defines the industry agreed model for load distribution on air cargo unit load devices (ULD) bases to apply the maximum allowable centre of gravity (C.G.) eccentricity. Its purpose is to establish a common reference load distribution algorithm for: a) comparable and repeatable ULD testing methods, or equivalent numeric simulations; b) aircraft structure and cargo systems design assumptions, consistent with existing airframers practices; and c) definition of operators unit load devices utilization rules and cargo build-up training programs. It applies to all types of unit load devices intended for use on board civil transport aircraft and airworthiness approved in accordance with the performance requirements and testing parameters of either ISO 21100 or, as applicable, ISO 8097. It also applies to non-airworthiness approved (non-certified) containers as defined in ISO 4118, the utilisation of which is controlled by the provisions of the aircraft type's Weight and Balance Manual and other airframe manufacturer's documents.

Air cargo unit load devices — Load distribution model

ISO 16049-1:2020 空运设备 - 约束带 - 第1部分:设计标准和测试方法

This document specifies the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22250 N (5000 lbf) rated ultimate tension load capability, as used by the airline industry. These restraint straps are used in civil transport aircraft during flight for: a) cargo loaded and tied down onto airworthiness approved air cargo pallets, themselves restrained into aircraft lower deck, main deck or upper deck cargo systems and meeting the requirements of b) non unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained ("floating") pallet into either lower deck, main deck or upper deck containerized cargo compartments of an aircraft, c) the same restraint strap assemblies can also be used in other applications such as: 1) non containerized (bulk loaded) baggage and cargo compartments; 2) to ensure cargo restraint inside an airworthiness approved air cargo container. NOTE The ultimate loads allowable on the attachment points available in most aircraft bulk compartments and inside many air cargo containers are significantly lower than 22250 N (5000 lbf). This results in the restraint arrangements ultimate load capability being dictated by the weakest element, i.e. the attachment points: typical 22250 N ultimate load restraint straps will therefore be in excess of the requirements for such applications. Compliance with this document provides one means of cargo restraint straps airworthiness approval by Civil Aviation Authorities under TSO/ETSO-C172a, in addition to the other requirements therein.

Air cargo equipment — Restraint straps — Part 1: Design criteria and testing methods

ISO 16049-2:2020 航空货运设备.约束带.第2部分:使用要求和建议及捆扎计算

This document aims at providing general utilization requirements and recommendations and calculation methods adequate to guarantee the effectiveness and ultimate load strength of tie-down/ lashing arrangements performed to restrain cargo on board civil transport aircraft during flight: a) cargo loaded and tied down onto airworthiness approved air cargo pallets, themselves restrained into aircraft lower deck or main deck or upper deck cargo systems meeting the restraint requirements of air cargo pallets approved in accordance with ISO 8097 (NAS3610) or ISO 21100, or b) additional tie-down on aircraft structure when necessitated by pallet maximum gross mass or centre of gravity limits, or c) non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained (“floating”) pallet into either lower deck, main deck or upper deck containerized cargo compartments of an aircraft, or d) individual pieces of load loaded in non-containerized (bulk loaded) baggage or cargo compartments. This document applies to cargo tie-down/lashing arrangements using exclusively air cargo restraint straps conforming to ISO 16049-1. Its general recommendations may also be used for tie-down arrangements using other means (e.g. steel cables, rope, other types of straps), but under the user’s responsibility as to their adequacy and the strength calculations required. NOTE 1 Where tie-down is performed onto aircraft structure as per b) or c) above, additional restrictions can be stated in the aircraft's Authority approved Weight and Balance Manual. NOTE 2 The use of chains, rods, or other rigid devices for tie-down onto civil transport aircraft floor tracks, which can generate excessive stress in the aircraft structure, is not part of the scope of this document. . This document aims at providing industry recognized means of complying with Airworthiness Authorities general requirements applicable to load securing on board civil transport aircraft (see CCAR-25, JAS Part 3, 14 CFR Part 25 and EASA CS-25), and aircraft manufacturers Authority approved Weight and Balance Manuals for each aircraft type as specified therein. It is not the intent of this document to specify when restraint straps should be used, but how they should be used. Meeting the methods requirements of this document is not alone sufficient to ensure flight safety: this document is based on the assumption that cargo tie-down will be designed, performed, and checked prior to aircraft departure in accordance with appropriate operating instructions conforming to the Weight and Balance Manual of the aircraft concerned, by competent, suitably trained, personnel as defined for example in ISO 9001:2015, 6.2.2 (see Clause 8).

Air cargo equipment — Restraint straps — Part 2: Utilization requirements and recommendations and lashing calculations

ISO 9788:2017 航空货运.双螺柱固定接头.设计和试验要求

Air cargo - Double stud tie-down fittings - Design and testing requirements

GSO ISO 7715:2016 航空货运设备 单元负载设备的地面处理和运输系统 最低要求

This International Standard specifies minimum performance and compatibility requirements for ground handling and transport systems equipment for air cargo unit load devices, used to service civil wide body freight aircraft. The purpose of this International Standard is not to specify equipment design, but rather to ensure interface compatibility of the various elements which might make up a complete ground handling and transport system, developed within a number of different operational schemes. This International Standard is applicable to ground handling and transport systems equipment, designed to deal with main deck unitized cargo in the form of intermodal containers and other compatible unitized load devices. In the context of this International Standard, intermodality concerns, primarily, air and land modes, but does not exclude sea mode. Likewise, compatible equipment, other than that used for main deck cargo, is not excluded.

Air cargo equipment -- Ground handling and transport systems for unit load devices -- Minimum requirements

GSO ISO 9031:2016 航空货运设备 成组负载装置（ULD）的处理系统 图示符号

This International Standard specifies symbols for the pictorial standardization of aircraft cargo-handling systems for unit load devices (ULDs). These symbols are applicable to all aircraft cargo-handling systems for underfloor as well as for main-deck systems. The conveyance, guidance, restraint, power drive unit and the degree of automation for the total cargo-handling system can be depicted using the symbols.

Air cargo equipment -- Handling systems for unit load devices (ULDs) -- Symbols for pictorial representation

GSO ISO/TR 8647:2016 航空货运约束设备中使用的纺织品的环境降解

The intent of this Technical Report is to make available information concerning the environmental degradation of textiles as used in unit load device (ULD) equipment common to the air cargo community. Since the ULD device containing textiles should have a predictable service life, there should be data available from which the predictions can be made. This Technical Report compiles available information on textiles of the types used in air cargo ULD devices and reviews the degradation characteristics of each. Textiles are used primarily in cargo restraint nets on air cargo pallets and non structural containers, restraint nets installed in cargo aircraft, and similar applications.

Environmental degradation of textiles used in air cargo restraint equipment

GSO ISO 9788:2016 航空货运设备 负载能力为22 250 N（5 000 lbf）的双螺柱配件组件铸造部件 用于飞机货物约束装置

1.1 This International Standard specifies the geometry and requirements for the cast components of a double stud fitting assembly, having a load capacity of 22 250 N (5 000 lbf), when installed in rail conforming to ISO 7166. 1.2 Other materials than those specified in 4.2 may alternatively be used, provided the performance and testing requirements of this International Standard are complied with.

Air cargo equipment -- Cast components of double stud fitting assembly with a load capacity of 22 250 N (5 000 lbf), for aircraft cargo restraint

GSO ISO 8268:2015 航空货运设备 汽车运输设备 基本要求

  Scope is not provided for this standard

Air cargo equipment -- Automobile transport devices -- Basic requirements

SAE AS452B-2014 氧气面罩组件，需求和压力呼吸，船员

The purpose of this standard is to establish optimum standards for crew demand and pressure-breathing oxygen mask assemblies for use by crew members in civil aircraft. This standard covers both general type and quick-donning type mask assemblies in the following classes: a. Class A, oronasal, demand b. Class B, oronasal, pressure-demand c. Class C, full face, demand d. Class D, full face, pressure-demand

Oxygen Mask Assembly, Demand and Pressure Breathing, Crew

SAE AIR1673B-2014 地面支持设备接口的飞机货舱门开口/门槛细节

Manufacturers/designers of all aircraft equipped with a pallet/container capability have provided a means of linking the ground loaders/elevators with the aircraft sill for the smoother transfer of pallets and containers into or out of the aircraft holds. Use of the aircraft attachment points may be used as a means of averting damage to the aircraft door frames and other important parts. Latch-on guarantees fore and aft and vertical alignment of the loader bed with the aircraft doorway, when used in conjunction with the appropriate ground equipment. This SAE Aerospace Information Report (AIR) has been prepared by SAE Subcommittee AGE-2A to present a review of the current range of aircraft attachment points on wide body aircraft and those narrow body aircraft with a ULD cargo capability. Airline operators, who utilized these facilities, have been faced with a growing number of adaptor bars necessary to suit each type of aircraft and door position. There is also a stowage problem on the elevator compounded by the increasing number of bars necessary to suit each aircraft. Some measure of standardization is obviously desirable. The adapter bars which have to be fitted to the forward face of the elevators to suit each different type of sill attachment are very heavy and present some handling problems to operators. Where the same elevator services different aircraft types, these bars may have to be changed many times each day on the ramp. Alternatively, elevators have to be restricted to servicing specific aircraft types or to those aircraft where a common attachment point already exists.

Aircraft Cargo Door Opening/Sill Details for Ground Support Equipment Interface

SAE AIR822C-2014 一般航空用氧气系统

This SAE Aerospace Information Report (AIR) provides a general overview of oxygen systems for general aviation use. Included are a brief review of the factors and effects of hypoxia, system descriptions, and mission explanations for system or component selection, and techniques for safe handling of oxygen distribution systems.

Oxygen Systems for General Aviation

SAE AS1304B-2014 持续气流化学氧生成器

This SAE Aerospace Standard (AS) applies to performance and testing of solid chemical oxygen generators which produce oxygen at essentiall ambient pressure for use aboard aircraft whose cabin pressure altitude does not exceed 40,000 ft (about 12,200 m). Portable chemical oxygen devices are covered by AS1303.

Continuous Flow Chemical Oxygen Generators

HB 8445-2014 民用飞机货运系统通用要求

本标准规定了民用飞机货运系统功能、性能、货运设备、货运环境等设计与验证的通用技术要求。 本标准适用于民用运输类飞机，其他飞机可参照使用。

General requirements of the freight systems for the civil airplane

SAE ARP1283B-2014 货物运输类飞机和旋翼机的车厢照明

This SAE Aerospace Recommended Practice (ARP) establishes design guidance and photometric values for adequate cargo compartment and cargo access lighting systems for ground handling. The adoption of a standard set of illuminance values, found appropriate for the performance of the task in specified areas should expedite ground handling.

Cargo Compartment Lighting for Transport Category Aircraft and Rotorcraft

SAE AS1825C-2014 航空货运货物体积的计算方法

The scope of this SAE Aerospace Standard (AS) shall cover the methodology of defining and determining the ""internal volumes"" of both the main deck and lower deck aircraft cargo compartments. The minimum required clearance between the compartment envelope and the unit load devices (ULDs) shall also be stated in order to provide the maximum ULD external contour and the methodology to define the ULD internal volumes.

Methodology of Calculating Aircraft Cargo Volumes

SAE AIR4899A-2014 货舱最大包装件尺寸计算方法

The methodology for maximum package size loading is bsed on a mathematical method allowing the calculation of maximum package size tables. This method does not in principal differentiate between bulk loading and cargo system loading. However, some restrictions have to be considered: - Some cargo systems generate pre-determined pallet trajectories. Envelope curves depending on the pallet size and the possible trajectories have to be determined first. - Door geometric limitations (with or without cargo loading system) - Turning limitations due to weight, load geometry and conveyance capability - Securing requirements This document is not intended for airline

Cargo Compartments Maximum Package Size Calculation Methodology

SAE ARP1523C-2014 空气隔绝容器.热有效性要求

This SAE Aerospace Recommended Practice (ARP) delineates the minimum operational requirements that will ensure that perishable cargoes in insulated standard airborne containers are kept in prime condition during the ground handling and air transportation cycle for a maximum period of 36 h.

Air Mode Insulated Containers - Thermal Efficiency Requirements

SAE ARP5140A-2014 行动不便的乘客登上门槛≤144 in的飞机时使用的升降装置设计标准

This SAE Aerospace Recommended Practice (ARP) outlines the design and functional requirements for aircraft passenger lifts, operated manually and self-propelled. The primary function of the lift described in this document is to act as an elevator between ground level and aircraft doorsills to a maximum of 144 in.

Design Criteria for Lifts Used to Board Passengers with Mobility Impairments onto Aircraft with Doorsill Heights of 144 in or Less