49.120 货运设备 标准查询与下载

SAE AIR1609A-2005 飞机加湿

This SAE Aerospace Information Report (AIR) covers the design parameters for various methods of humidification applicable to aircraft, the physiological aspects of low humidities, the possible benefits of controlling cabin humidity, the penalties associated with humidification, and the problems which must be solved for practical aircraft humidification systems. The design information is applicable to commercial and military aircraft. The physiological aspects cover all aircraft environmental control applications. The purpose of this (AIR) is to provide guidelines for the design of aircraft humidification systems. Physiological effects of humidity levels on crew and passengers are reviewed. Various techniques used for cabin humidification are discussed and evaluated. Various potential problems and penalties associated with humidification systems are also described.

(R) Aircraft Humidification

SAE AS36102-2005 空运成组装运设备.试验方法

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

ISO 16049-2:2005 航空货运设备.紧固带.第2部分:使用导则及绳套计算

This part of ISO 16049 specifies utilization guidelines and principles to be used in strength calculation methods adequate to guarantee the effectiveness and ultimate load strength of tie-down/lashing arrangements used to restrain cargo on board civil transport aircraft during flight for either: 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 ISO 8097; b) additional tie down on aircraft structure when necessitated by pallet maximum gross mass or centre of gravity limits; c) 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; or d) individual pieces of load loaded in non containerized (bulk loaded) baggage or cargo compartments. This part of ISO 16049 is applicable to cargo tie-down/lashing arrangements using exclusively air cargo restraint straps conforming to ISO 16049-1. Its general recommendations may be used for tie-down arrangements using other means (e.g. steel cables, rope, chains, other types of straps), but under the user's responsibility as to their adequacy and the strength calculations required. This part of ISO 16049 is not applicable to the use of chains or other rigid devices for tie-down onto civil transport aircraft floor tracks. These devices are generally not recommended for use due to the possibility of generating excessive stresses in the aircraft structure, except where explicitly approved in the manufacturer's Authority approved Weight and Balance Manual. This part of ISO 16049 is intended to provide industry recognized means of complying with Airworthiness Authorities general regulations applicable to load-securing on board civil transport aircraft (see FAR/JAR Parts 25), and aircraft manufacturers Authority approved Weight and Balance Manuals for each aircraft type as specified therein. It is not the intent of this part of ISO 16049 to specify when restraint straps should be used, but how they should be used. It does not, under any circumstance, supersede the requirements of any of the above documents that take precedence at all times.

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

SAE AS8049B-2005 民用旋翼飞行器、运输飞行器和一般航空飞行器座位的性能标准

This SAE Aerospace Standard (AS) defines minimum performance standards, qualification requirements, and minimum documentation requirements for passenger and crew seats in civil rotorcraft, transport aircraft, and general aviation aircraft. The goal is to achieve comfort, durability, and occupant protection under normal operational loads and to define test and evaluation criteria to demonstrate occupant protection when a seat/occupant/restraint system is subjected to statically applied ultimate loads and to dynamic impact test conditions set forth in the applicable Federal Aviation Regulations 14 CFR 23, 25, 27, or 29. Guidance for test procedures, measurements, equipment, and interpretation of results is presented to promote uniform techniques and to achieve acceptable data. While this document addresses system performance, responsibility for the seating system is divided between the seat supplier and the installation applicant. The seat suppliers 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 ultimate system responsibility in assuring that all requirements for safe seat installation have been met.

Performance Standard for Seats in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft

SAE ARP1804A-2005 电动货物牵引车

This SAE Aerospace Recommended Practice (ARP) outlines the desing and performance requirements for a battery-powered electric tow tractor for the handling of baggage or cargo trailers in airline service. The use of shall in this document indicates a mandatory requirement. The use of should indicates a recommendation or that which is advised but not required.

(R) Electric Baggage/Cargo Tractor

SAE ARP712B-2004 空厨照明

This SAE Aerospace Recommended Practice (ARP) provides minimum standards and environmental design requirement recommendations for lighting and control in galley areas. It also addresses electrical shock hazard in galley areas. The purpose of this recommended practice is to provide minimum standards for the illumination of galleys (buffets) and for the location of lighting controls within the galley area of passenger transport aircraft.

Galley Lighting

SAE AS36101-2004 空运货物单位装载用具.荷载分布模型

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 ARP583H-2004 飞机维修人员工作站

This SAE Aerospace Recommended Practice (ARP) provides guideance for the design and location of flight attendant stations, including emergency equipment installations at or near such stations, so as to enable the flight attendant to function effectively in an emergency situations, including emergency evacuations. Recommendations regarding the design of flight attendant stations shall apply to all stations; such recommendations relative to location shall apply to those stations located near or adjacent to floor level exits.

Flight Attendant Stations

SAE ARP5596-2003 货物撑垫指南

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 aircrafts 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 aircrafts 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 manufacturers 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 AS1825B-2003 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. The purpose of this document is to establish a uniform methodology for defining and determining the usable internal volume of aircraft cargo compartments and usable external envelope for ULDs which can be accommodated within these compartments. This will provide the aircraft industry with a set of standard terminology which when specified, can be utilized by the airlines when comparing similar type aircraft. The minimum essential criteria are defined by the key word shall. Recommended criteria are identified by the key word should and while not mandatory, are considered to be primary importance.

Methodology of Calculating Aircraft Cargo Volumes

SAE ARP5595-2003 货物固定带.使用指南

This SAE Aerospace Recommended Practice (ARP) 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 certified air cargo pallets, themselves restrained into aircraft lower deck, main deck or upper deck cargo systems meeting the requirements of NAS 3610, or b. additional tie-down on aircraft structure when necessitated by pallet maximum gross mass or CG, or c. 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, or d. individual pieces of load loaded in non-containerized (bulk loaded) baggage or cargo compartments. This document aims at providing industry recognized means of complying with Airworthiness Authorities general regulations applicable to load securing on board civil transport aircraft (see FAR 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 document 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 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 publications and staff training programs. This 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 AIR910B-2003 (R)高空飞机中的臭氧问题

The purpose of this report is to provide information on ozone, its effects, generally accepted ozone exposure limits (aviation and non-aviation), and methods of its control in high altitude aircraft. Sources of information are listed and referenced in the text.

(R) Ozone Problems in High Altitude Aircraft

SAE ARP731C-2003 (R)飞机蒸汽循环制冷系统应用的一般要求

The purpose of this SAE Aerospace Recommended Practice (ARP) is to establish recommendations for the design, installation and testing of aircraft vapor cycle refrigeration systems. These recommendations are representative of the present state-of-the-art.

(R) General Requirements for Application of Vapor Cycle Refrigeration Systems for Aircraft

SAE ARP1384C-2003 (R)乘客安全信息发布会卡和视频简报

These recommendations are to aid the international air transport industry by identifying a standard, minimum amount of safety instructions that shall ben given in passenger safety information briefing cards and, if available passenger safety video briefings. Aircraft operators are encounraged to customize the passenger safety information briefing cards and safety videos for their own operations. The purpose of this ARP is to assist airlines, as well as corporate and private operators, in producing safety information briefing cards and videos which will reinforce and expand passenger knowledge of the safety equipment and procedures designed for passenger use.

(R) Passenger Safety Information Briefing Cards and Video Briefings

SAE AIR1673A-2002 地面支持设备接口用飞机货舱门洞口/闸槛的详细资料

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 to the aircraft door frames and other important parts.Latch-on guarantees fore and aft and vertical alignment of the loaders 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 still attachment are very heavy and present handing 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 serving 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 AS1066B-2002 (R)手动操作式气缸关闭高压氧阀门的最低标准

This standard covers all types of manually operated high pressure oxygen, cylinder shut off valves for use in commercial type aircraft. It is intended that the valve shall be attached to a pressure cylinder storing oxygen under pressure of 1800 to 2100 psi at 70 F. Upon opening the valve, oxygen will be permitted to discharge from the storage cylinder to the valve outlet and thence to other components of the oxygen system. It shall also be possible to recharge the cylinder through the valve. The purpose of this standard is to define general minimum standards for the design, fabrication, test and packaging of manually operated, high pressure breathing oxygen cylinder shut off valves. Applicable is AS 861, MINIMUM GENERAL STANDARDS FOR OXYGEN SYSTEMS.

(R) Minimum Standards for Valve, High Pressure Oxygen, Cylinder Shut Off, Manually Operated

SAE AIR1069A-2002 最高海拔 45,000 英尺的船员氧气需求

Crew Oxygen Requirements Up to a Maximum Altitude of 45,000 Feet

SAE ARP1161A-2002 商务机乘务员站照明

This SAE Aerospace Recommended Practice covers the recommended requirements for the lighting and characteristics of instruments; information plates and displays, emergency, cautionary, advisory and stuatus displays; circuit breaker and toggle switch positions; and the recommended requirements for the utility lighting system. The purpose of this document is to present a practical set of requirements for the lighting systems which provide illumination for crew station areas and displays for the characteristics of displays which affect their readability. It is intended that it be used as a guide by those involved with the design, use, or procurement of lighting systems for commercial and non-military aircraft or aerospace vehicles.

Crew Station Lighting - Commercial Aircraft

SAE AS33601-2001 运输货物的飞行器用导向装置和螺柱配件.标准尺寸

Track and Stud Fitting for Cargo Transport Aircraft, Standard Dimensions for FSC 1560THE REQUIREMENTS FOR ACQUIRING THE PRODUCT(S) DESCRIBED HEREIN SHALL CONSIST OF THISSPECIFICATION SHEET AND THE ISSUE OF THE FOLLOWING SPECIFICATION LISTED IN THAT ISSUE OF THEDODISS SPECIFIED IN THE SOLICITATION: NONE.THIS SPECIFICATION SHEET DEPICTS THE CONFIGURATIONS AND DIMENSIONS OF TRACKS AND STUDS FORSEAT ATTACHMENTS FOR SEATS AND OTHER EQUIPMENT IN CARGO/TRANSPORT AIRCRAFT.THIS NOTE WAS DELETED AS IT DID NOT PERTAIN TO THE CONVERTED SAE DOCUMENT.DIMENSIONS ARE IN INCHES.

Track and Stud Fitting for Cargo Transport Aircraft, Standard Dimensions for FSC 1560

SAE AIR825/1-2001 飞机氧气设备介绍

This is the first document of a set of fourteen related documents. The fourteen-document set is written at an introductory level, suitable for anyone who would like to understand the basics of oxygen systems in aircraft, and specifically for the engineer who has just recently been assigned to aircraft oxygen systems.

Introduction to Oxygen Equipment for Aircraft