49.120 货运设备 标准查询与下载

SAE AIR1059C-2010 氧气瓶质量,适用性,维修移动式充气和标记

This document provides guidance concerning the maintenance and serviceability of oxygen cylinders beginning with the quality of oxygen that is required, supplemental oxygen information, handling and cleaning procedures, transfilling and marking of serviced oxygen assemblies. This document attempts to outline in a logical sequence oxygen quality,serviceability and maintenance of oxygen cylinders.

Oxygen Cylinder Quality, Serviceability, Maintenance Transfiling and Marking

SAE AS8049/1-2010 旋翼飞机,运输飞机和通用航空飞机上单人侧向安置的座椅用性能标准

This Society of Automotive Engineers (SAE) Aerospace Standard (AS) Annex defines Minimum Performance Standards (MPS), qualification requirements, and minimum documentation requirements for side-facing seats in civil rotorcraft, transport aircraft, and general aviation aircraft. The goal is to define test and evaluation criteria to demonstrate occupant protection when a single-occupant side-facing seat/occupant/restraint system is subjected to statically applied ultimate loads and to dynamic test conditions set forth in the applicable 14, Code of Federal Regulations (CFR) Part 23, 25, 27 or 29. While this Annex addresses system performance, responsibility for the seating system is divided between the seat supplier and the installation applicant. The seat supplier's responsibility consists of meeting all the seat system performance requirements and obtaining and supplying to the installation applicant all the data prescribed by this document. The installation applicant has the final responsibility in assuring that all requirements for safe seat installation have been met. This document addresses the performance criteria for single occupant side-facing seat systems requiring dynamic testing to be used in civil rotorcraft, transport aircraft, and general aviation aircraft. This document covers passenger seats for use in aircraft type-certificated as defined in AS8049 section 1.3.

Performance Standards for Single-Occupant, Side-Facing Seats in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft

SAE AIR5742-2010 氧气设备的包装和运输

The scope of this document is related to the particular needs of oxygen equipment with regards to packaging and transportation. The document provides guidance for handling chemical, gaseous and liquid oxygen equipment. It summarizes national and international regulations to be taken into account for transportation on land, sea and air and provides information on classification of hazardous material. The aim of this document is to summarize information on packaging and transportation of oxygen equipment. Statements and references to regulations cited herein are for information only and should not be considered as interpretation of a law. Processes to maintain cleanliness of components and subassemblies during processing and assembly or storage of work-in-progress are outside the scope of this document.

Packaging and Transportation of Oxygen Equipment

SAE AIR1869C-2009 广体和标准体航空器下层货船ULD容量

This SAE Aerospace Information Report (AIR) covers information relative to ULDs (Unit Load Devices) container and pallet configurations, maximum usable container, pallet and bulk compartment volumes and tare weights for the lower deck of various wide-body aircraft. Bulk compartment volumes are also included for standard-body aircraft. This document brings together data concerning the lower deck capacity of wide-body and standard- body airplanes. The information includes airplanes manufactured by Airbus, Boeing, British Aerospace, British Aircraft, Fokker-VFW, Hawker Siddeley, Ilyushin, Lockheed and McDonnell- Douglas.

Wide-Body and Standard-Body Aircraft Lower Deck Cargo Compartment ULD Capacities

GOST R 53428-2009 空运货物和地面设备.术语和定义

Air cargo and ground equipment. Terms and definitions

KS W ISO 4116-2008(2018) 航空货运设备－与飞机单元负载装置兼容性的地面设备要求

Air cargo equipment－Ground equipment requirements for compatibility with aircraft unit load devices

KS W ISO 4116-2008(2023) 航空货运设备.地面设备与飞机单位载荷装置兼容性的要求

Air cargo equipment－Ground equipment requirements for compatibility with aircraft unit load devices

SAE ARP1836B-2008 电池驱动的航空货运设备

This SAE Aerospace Recommended Practice (ARP) outlines the functional and design requirements for a battery powered, self-propelled belt conveyor for handling baggage and cargo at aircraft bulk cargo holds. Additional considerations and requirements may legally apply in other countries. As an example, for operation in Europe (E.U. and E.F.T.A.), the applicable EN standards shall be complied with.

Aircraft Cargo Conveyor-Battery Powered

SAE AS8043B-2008 民航机用限制设备

This SAE Aerospace Standard (AS) specifies laboratory test procedures and minimal requirements for the manufacturer of restraint systems for use in civil aircraft. It is intended to establish a minimum level of quality which can be called upon by the designer of those systems. However, compliance with this standard alone may not assure adequate performance for the restraint system under normal and emergency conditions. Such performance requires consideration of factors beyond the scope of this standard, and must be demonstrated by a system evaluation procedure which includes the seat, the occupant, the specific restraint installation and the cabin interior configuration. This standard specifies the requirements for Type 1, Type 2 and Type 3 restraint systems.

Restraint Systems for Civil Aircraft

SAE AIR36106A-2008 空运货物成组装运设备.耐飞性参考文件的使用

1.1 Purpose1.1.1 This SAE Aerospace Information Report (AIR) provides instructions for intended proper use of Aerospace Standard AS36100A, published 2006-04 [TSO pending], as the technical reference for airworthiness approval of air cargo unit load devices (pallets, nets and containers) to be loaded on board civil transport aircraft. For consistency and cross-checking purposes, it also includes instructions for proper use of previous NAS 3610 [Revision 10, 1990, referenced in TSO C90c], as commonly understood by the industry.1.1.2 This AIR does not provide detailed background or rationale for the technical contents of AS36100A, which are separately provided in AIR36108, AS36100A background and development record.1.1.3 AS36100A exclusively defines the general geometric parameters (insofar as they affect restraint on board aircraft), minimum performance requirements and testing parameters of unit load devices. Additional areas as perAS36100A paragraph 1.1, such as continued airworthiness and maintenance requirements, design and testing methods, unit load devices design specifications and accessories, and rules for proper operation/utilization andoperating staff training also need to be considered for designing unit load devices, and are covered by other documents, listed in AIR36105A.1.2 Field of Application1.2.1 This AIR is intended to provide AS36100A users including Airworthiness Authorities, unit load devices designers, purchasers and operators as well as civil transport aircraft and aircraft cargo systems designers within the industry,with a single agreed method for using AS36100A to determine applicable airworthiness requirements.1.2.2 In the same way, it is intended to provide them with the commonly understood though more complex method for using NAS 3610 [Revision 10, 1990, referenced in TSO C90c], to determine the airworthiness requirements applicable to unit load devices approved or to be approved under TSO C90c (e.g., because their size or type arenot covered in AS36100A).

Air Cargo Unit Load Devices - Use of Airworthiness Reference Documents

SAE AIR36108-2008 AS36100背景和发展报告

1.1 Purpose1.1.1 This Aerospace Information Report (AIR) provides a record of the development by SAE AGE-2A Air Cargo Sub-Committee of Aerospace Standard AS36100, Air Cargo Unit Load Devices — Performance Requirements and Test Parameters, published 2005-02, and its revision A published 2006-04, intended as a technical reference for airworthiness approval of air cargo unit load devices (pallets, nets and containers) to be loaded with eitherbaggage or freight on board civil transport aircraft, and to partly supersede previously used NAS 3610, Cargo unit load devices - Specification for—[Revision 10, 1990, referenced in TSO C90(c)].1.1.2 AS36100 was developed over a 5 year period (1999-2004) by a Panel of SAE AGE-2A designated as “NAS 3610Oversight Panel“ (OSP), based on a worldwide industry consensus that NAS 3610, used since 1969 as technical reference for TSO C90(c), had become largely obsolescent, not properly understood by many of its users, and still contained errors while document sponsor AIA stated they were not going to update or revise this document.This consensus was initially reached at the International Standardization Organization (ISO) TC20/SC9 Air Cargo Sub-Committee meeting Nr 29 (1998, Memphis TN), which hence agreed to prepare a corrigendum (published 2001) to ISO 8097 (based on NAS 3610), and to entrust SAE AGE-2A, on behalf of the industry, with dentification of the needs for a replacement document. AGE-2A thus created in 1999 the OSP, which undertook a systematic review of the air cargo industry’s actual requirements and the step by step development and discussion of AS 36100.AS36100 Revision A (published 2006-04) was subsequently developed in 2005 by AGE-2A in order to obviate the first edition's identified shortcomings prior to expected TSO C90(d) publication.1.1.3 The scope of the OSP work, thus the present AIR, also included other documents - some of which existed, some of which were subsequently developed - associated with AS36100 or supplementing it, covering such other areas as continued airworthiness requirements, design and testing methods, unit load devices design specifications and accessories, and rules for their proper operation/utilization and operating staff training. A list of the identifiedareas is provided under 1.1 of AS36100. See 2.1.2 hereafter for other associated documents concerned.1.2 Field of Application1.2.1 The present AIR is intended to provide future users of AS36100, including Airworthiness Authorities, unit loaddevices designers, purchasers and operators as well as civil transport aircraft and aircraft cargo systems or ULD designers within the industry, with the background and rationales of the requirements and parameters retained therein, in order to achieve full understanding of the technical justifications for these requirements.1.2.2 In the same way, it is intended to provide AGE-2A members with means to re-examine provisions of AS36100 for any future revisions resulting from operational experience or the evolutions of industry needs, while keeping trackof the originally retained rationales.1.2.3 It is intended such revisions will be evaluated by the AGE-2A permanent Airworthiness Panel established to continuously monitor AS36100 and the associated documents, and the rationales for these revisions documented and recorded at that time.

AS36100 Background and Development Record

MH/T 1022-2008 货物航空运输垫板使用规范

本标准规定了货物航空运输垫板使用的基本要求、垫板尺寸的计算和垫板的铺设方法。 本标准适用于货物航空运输时垫板的使用。

The specification of shoring(dunnage) for air cargo

SAE AIR512D-2007 机舱照明

This document provides the aircraft designer, architect, industrial designer and electrical engineer with design criteria to properly illuminate aircraft cabin interiors. This document covers the general recommendations for cabin lighting in order to provide satisfactory illumination for, but not limited to: boarding and deplaning; movement about the cabin; reading; use of lavatories; use of work areas; exiting under emergency conditions; using stowage compartments, coat rooms and closets; and using interior stairways and elevators (lifts).

Aircraft Cabin Illumination

SAE ARP997C-2007 民用运输机客舱应急设备

The purpose of this SAE Aerospace Recommended Practice (ARP) is to establish criteria for the installation of emergency equipment that shall permit its efficient use and encourage standardization, thereby reducing reorientation of crewmembers to equipment accessibility while working on differing types, models, and series of transport-category aircraft. This does not preclude the requirement to pre-flight check all emergency equipment relative to its location, availability, and operational status.

(R) Installation and Stowage Provisions for Emergency Equipment in the Transport Aircraft Passenger Cabin

SAE AS5385C-2007 货物固定带.设计标准和测试方法

This Standard aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22 250 N (5,000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain on board civil transport aircraft during flight: a. cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main deck cargo systems meeting the requirements of NAS 3610 or AS 36100; or b. non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained (floating) pallet into either lower deck or main deck containerized cargo compartments of an aircraft.

(R) Cargo Restraint Straps - Design Criteria and Testing Methods

SAE ARP378C-2006 乘客阅读灯

The purpose of this SAE Aerospace Recommended Practice (ARP) is to recommend minimum design criteria which will lead to adequate performance standards for passenger reading lights in aircraft. This document presents criteria for design and location of passenger reading lights in commercial aircraft.

Passenger Reading Lights

SAE AS36100A-2006 空运成组装运设备.性能要求和试验参数

This SAE Aerospace Standard (AS) 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 Title 14 CFR Part 25, expect for the 9.0 g forward ultimate inertia force of 25.561 (b)(3)(ii).

Air Cargo Unit Load Devices - Performance Requirements and Test Parameters

SAE AIR36106-2006 空运成组装运设备.适航参考文献的使用

This Aerospace Information Report (AIR) provides instructions for intended proper use of Aerospace Standard AS36100 published 2005-02, as the technical reference for airworthiness approval of air cargo unit load devices (pallets, nets and containers) to be loaded on board civil transport aircraft. For consistency and cross-checking purposes, it also includes instructions for proper use of previous NAS 3610 (Revision 10, 1990, referenced in TSO C90c), as commonly understood by the industry. This AIR does not provide detailed background or rationale for the technical contents of AS36100, which are separately provided in AIR36107, AS36100 background and development record. AS36100 exclusively defines the general geometric parameters (insofar as they affect restraint on board aircraft), minimum performance requirements and testing parameters of unit load devices. Additional areas as per AS36100 paragraph 1.1, such as continued airworthiness and maintenance requirements, design and testing methods, unit load devices design specifications and accessories, and rules for proper operation/utilization and operating staff training also need to be considered for designing unit load devices, and are covered by other documents, listed in AIR36105.

Air Cargo Unit Load Devices - Use of Airworthiness Reference Documents

NF L91-131-2:2005 航空货运设备.紧固带.第2部分:使用导则及绳套计算

Air cargo equipment - Restraint straps - Part 2 : utilization guidelines and lashing calculations.

SAE AIR36105-2005 空运货物成组装运设备.参考标准

The present Aerospace Information Report (AIR) provides a list of the main government regulations, SAE and international standards, and standing industry recommendations applying to air cargo unit load devices (pallets, nets and containers) to be loaded with either baggage or freight on board civil transport aircraft. It is intended to provide unit load devices designers, purchasers and operators as well as civil transport aircraft and aircraft cargo systems designers within the industry with a list of the available document references to cover the other aspects that do not all directly pertain to airworthiness and testing, listed in clause 1.1, Purpose, of AS36100, Air Cargo Unit Load Devices - Performance Requirements and Test Parameters (TSO applied for, pending). The scope of the listed documents covers airworthiness and continued airworthiness requirements, design and testing methods, design specifications, unit load devices accessories, and the main published rules for their proper operation/utilization and operating staff training.

Air Cargo Unit Load Devices - Reference Standards