49.120 货运设备 标准查询与下载

SAE ARP4769B-2013 主甲板或下甲板用船员休息舱

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 by the Aerospace Materials Division, SAE, as of January 2007. It is recommended, therefore, that this specification not be specified for new designs.

Crew Rest Container for Main Deck or Lower Deck

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

SAE AIR825D-2012 飞机用氧气设备

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 report provides information on the design and use of aircraft oxygen systems. It explains the physiological oxygen requirements of the human body in both a normal environment and in an hypoxic environment. It includes an overview of the continuous flow, demand and pressure demand, and liquid oxygen systems. A basic understanding of how each system operates is then specifically addressed in its own titled section. The ch

Oxygen Equipment for Aircraft

SAE AS8905A-2012 飞机地板系紧接头和运货环

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 establishes requirements for two types of aircraft floor fittings for tiedown of cargo and seats, and two types of cargo tiedown rings.

Fittings and Cargo Rings, Tie-Down, Aircraft Floor

SAE ARP36103A-2012 空运货物单位负荷装置.重心控制方法

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 Recommended Practice (ARP) provides the industry agreed methods to keep the center of gravity (C.G.) location of loaded air cargo Unit Load Devices (ULDs) within the maximum horizontal and vertical limits allowed by their airworthiness approval.

Air Cargo Unit Load Devices - Center of Gravity Control Methods

SAE AIR1223B-2012 民航机内液压氧系统的安装

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 March 1999. It is recommended, therefore, that this document not be specified for new designs. Liquid supply systems for breathing oxygen for the crew and/or passengers of transport aircraft require design and installation considerations, which are detailed herein. AIR 825, Oxygen Equipment for Aircraft, contains general information on determination of breathing oxygen

Installation of Liquid Oxygen Systems in Civil Aircraft

SAE AIR4165A-2012 飞机货运系统中动力驱动单元(PDUs)通用要求

This Aerospace Information Report (AIR) is intended to assist the user (aircraft manufacturer/airline) in the following areas: a. In the decision of whether or not to plan for the installation of a powered drive system in the cargo loading system (CLS) during the definition of the aircraft on-board cargo loading system; b. If a powered drive system is decided upong, to provide general requirements to be considered during the preparation of component specifications for the powered drive units (PDUs) to be used. This provides a selection of criteria in order to obtain an optimum component PDU the application considered.

General Requirements for Powered Drive Units (PDUs) in Aircraft Cargo Systems

SAE ARP4101/4A-2012 飞行甲板环境

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 document is intended to specify the environmental conditions for transport aircraft necessary to permit the crew to perform their duties and functions in comfort, with minimum fatigue and no distraction. Environment conditions should cause no short or long-term effects deleterious to health or physical well-being, nor significantly impair ability to perform normal or abnormal crew functions.

Flight Deck Environment

SAE ARP5285B-2012 无牵引杆牵引车的操作规程

This document describes: the minimum requirements for the operation of towbarless towing vehicles equipped with aircraft nose landing gear pick up/release and associated safety systems. What procedure should be used in case of an alert given by the Towbarless Towing Vehicle System System(s). Training of Towbarless Towing vehicle operators. Approvals and auditing of third party handlers.

Towbarless Towing Vehicle Operating Procedure

SAE AIR512E-2012 机舱照明

This document covers the general recommendations for cabin lighting in order to provide satisfactory illumination for, but not limites to:provides the aircraft designer, architect, industrial designer and electrical engineer with design criteria to properly illuminate aircraft cabin interiors: 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 ARP5596B-2012 货物支撑指南

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) specifies guidelines for calculating and performing shoring (load spreading) required on board civil transport aircraft whenever a piece of cargo to be carried exceeds the aircraft's maximum allowable limits in area load, running load, or both. It provides both the engineering methods needed to properly design a shoring arrangement, and the main practical dos and donts known from experience to ensure its effectiveness in protecting the aircraft's structure against overload. This document aims at providing recognized industry standard methods to achieve the best attainable level of aircraft structural protection when designing and performing a shoring arrangement, taking into account the general requirements expressed in the aircraft manufacturers Weight and Balance Manuals, the requirements to be met as a result of the air cargo pallets airworthiness certification requisites, as well as the various potential areas of concern identified based on experience. This document, therefore, provides recommended practical means of compliance with flight safety objectives, intended to be available as a common base for carriers as well as their airport handling agents when establishing their own in-house procedures, publications and staff training programs. This document, however, is primarily intended for use by qualified structural engineers to be responsible for calculating and implementing cargo shoring arrangements where the size and weight of the piece of cargo require. It is not intended as a guide for more common simpler shoring requirements, identified thereafter: ARP5486, Air Cargo Pallets - Utilization Guidelines, Section 5 addresses such relatively simple cases. This document shall not, under any circumstance, supersede the requirements of applicable airworthiness regulations (see FAR Part 25) or the aircraft manufacturer's Weight and Balance Manual. In addition, any aircraft manufacturers specific cargo shoring instructions shall be strictly complied with. Since in several instances they contain proprietary data, such data should be used only by authorized companies and persons with proper understanding thereof.

Cargo Shoring Guidelines

SAE AIR36107A-2011 AS36100背景和发展记录

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 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, intended as a technical reference for airworthiness approval of air cargo unit load devices (pallets, nets and containers) to be loaded with either baggage 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 C90c). AS36100 was developed over a 5 year period (1999-2004) by a Panel of SAE AGE-2A designated as "NAS 3610 Oversight Panel" (OSP), based on a worldwide industry consensus that NAS 3610, used since 1969 as technical reference for TSO C90c, 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 2000) to ISO 8097 (based on NAS 3610), and to entrust SAE AGE-2A, on behalf of the industry, with identification of the needs for a replacement document. AGE-2A in 1999 created the OSP, which undertook a systematic review of the air cargo industry's actual requirements and the step by step development and discussion of AS36100. 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.

AS36100 Background and Development Record

SAE ARP5595A-2011 货物约束带.使用指南

This Aerospace Recommended Practice aims at providing general utilization guidelines 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, main deck or upper deck cargo systems meeting the requirements of air cargo pallets approved in accordance with NAS 3610 or AS36100A, or b. additional tie-down on aircraft structure when necessitated by pallet maximum gross mass or CG, or c. individual pieces of cargo, or pieces of cargo placed onto an unrestrained ("floating") pallet into either lower deck or 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 ARP aims at providing industry recognized means of complying with Airworthiness Authorities general regulations applicable to load securing on board civil transport aircraft (see 14 CFR Parts 25 and 121, in 2.1, Applicable Documents), and aircraft manufacturers Authority approved Weight and Balance Manuals for each aircraft type as specified therein. It is not the intent of this ARP to specify when restraint straps should be used, but how they should be used. It shall not, under any circumstance, supersede the requirements of any of these documents, which shall take precedence at all times. This ARP therefore provides recommended practical means of compliance with flight safety objectives, intended to be available as a common base for carriers as well as their airport handling agents when establishing their own in-house publications and staff training programs. This ARP document is not intended to apply to cargo restraint on board military transport aircraft, and does not take into account any specific criteria for military aircraft. Nothing, however, precludes it being used for guidelines in this case, it pertaining to the military operator to identify and implement any additional applicable criteria.

Cargo Restraint Straps - Utilization Guidelines

SAE AS36101A-2011 空运货物成组载荷装置.载荷分配模型

This Aerospace Standard (AS) defines an industry agreed reference model for load distribution on air cargo unit load device (ULD) bases, to reflect maximum allowable center of gravity (CG) eccentricity and ensure the maximum allowable area load is not exceeded.

Air Cargo Unit Load Devices - Load Distribution Model

SAE ARP1372C-2011 针对空运货物成组装运设备地面装卸和运输系统的最低要求

The requirements of this SAE Aerospace Recommended Practice (ARP) are applicable to ground handling and transport systems equipment which is designated to accommodate main deck unitized cargo in the form of intermodal containers and other compatible unitized load devices. Intermodality in the context of this document concerns primarily air and land modes but does not exclude the marine mode. Equipment with compatibility features for other than main deck cargo is likewise not excluded. It is not the intent of this document to specify equipment design but rather to ensure interface compatibility of the various elements which might make up a total ground handling and transport system developed within a number of different operational schemes. It is the intent of this document to specify minimum ULD handling and restraint features to ensure future interchange capability. This document specifies minimum performance and compatibility requirements for air cargo unit load device (ULD) ground handling and transport systems equipment employed to service wide-body freighter aircraft operations.

Minimum Requirements for Air Cargo Unit Load Device, Ground Handling and Transport Systems

SAE AS4914C-2011 飞机荧光灯镇流器/固定装置的安全标准

The purpose of this standard is to recommend minimum performance requirements to assist the specification writer in establishing a failsafe airplane interior Fluorescent light assembly design. This standard relates to the design of lamp ballasts, lampholders, fixtures, and installation of the same.

Aircraft Fluorescent Lighting Ballast/Fixture Safety Standard

SAE AIR1168/7A-2011 航天压力输送系统设备

The requirements for cabin pressure for all types of aircraft have been established for the Armed Services in military specifications, by the Federal Aviation Authority and by the SAE in recommendations. These requirements limit the cabin altitude to 8000 ft in transport and long range military aircraft. In the fighter aircraft, when the pilot uses oxygen and the mission duration is relatively brief, cabin altitudes up to 25,000 ft are allowed. Supersonic transports, which operate at high speed and high altitude, have short flight durations and high rates of descent. To avoid an uncomfortable rate of change of cabin pressure when descending from high altitudes, a maximum cabin altitude of 6000 ft is recommended. The pressurization system design considerations presented in this AIR deal with human physiological requirements, characteristics of pressurization air sources, methods of controlling cabin pressure, cabin leakage control, leakage calculation methods, and methods of emergency cabin pressure release.

Aerospace Pressurization System Design

SAE AS6554-2011 货物阻塞装置

The purpose of this SAE Aerospace Standard (AS) is to standardize the basic design, performance and testing requirements for "Cargo Stoppers" cargo tie-down accessories to be used in conjunction with approved tie-down straps meeting AS5385C (TSO C-172) requirements. The lack of an agreed industry standard resulted in uncertainties about their operational capabilities, so that it was deemed advisable to specify the applicable design, minimum performance and testing requirements, since Cargo Stoppers are used as part of cargo tie-down arrangements that must meet regulatory airworthiness requirements.

Cargo Stopper Devices

SAE AS1065A-2011 充有飞行员呼吸氧气的航天器气缸总成的质量和适用性要求

Quality and Serviceability Requirements for Aircraft Cylinder Assemblies Charged with Aviators Breathing Oxygen

MH/T 1032-2010 航空集装板的货物组装规范

本标准规定了货物在航空货运集装板(以下简称集装板)上组装的一般要求,特殊货物组装和集装板附属组件的要求。 本标准适用于集装板的使用和管理。

Specification of cargo assembling on air cargo pallet