49.120 货运设备 标准查询与下载

BS M 85:1995 航空货运设备 具有 22250 N（5000lbf）或以上全向额定负载能力的双螺柱系紧配件的标识

This International Standard specifies an identification scheme for double-stud tie-down fittings having an omnidirectional rated load capacity of 22 250 N (5 000 Ibf) or above in a rail conforming to ISO 7166. It is applicable to all cargo tie-down fittings equipped with a moveable plunger, regardless of material or method of fabrication, that satisfy national regulatory airworthiness requirements with regard to the ad-ditional special factors appropriate to the method of fabrication of the assembly or component parts thereof. The requirements specified in this International Stan-dard are intended to facilitate identification of such tie-down fittings by non-technical ramp and cargo personnel.

Air cargo equipment. Identification of double-stud tie-down fittings having an omnidirectional rated load capacity of 22 250 N (5 000 lbf) or above

SAE AIR4771-1995 推荐的支撑位置

This SAE Aerospace Information Report (AIR) contains information that can be used by the air transportation industry to provide passengers in forward facing seats, using lap belt restraints only, with consistent brace for impact positions. This information is intended to reduce the potential confusion passengers may experience upon being presented with different brace for impact positions as they travel on different aircraft or on different carriers. This document does not address child restraint, situations where adult passengers are seated behind fixed tables, or who are using upper-torso restraint, or where passengers are not seated in forward facing seats.

Recommended Brace Positions

ISO 12118:1995 航空货运设备 全向额定承载能力等于或高于22250N(50001bf)的双螺柱系留接头的识别标志

Specifies an identification scheme for double-stud tie-down fittings having an omnidirectional rated load capacity of 22 250 N (5 000 lbf) or above in a rail conforming to ISO 7166. Applicable to all cargo tie-down fittings equipped with a movable plunger, regardless of material or method of fabrication.

Air cargo equipment - Identification of double-stud tie-down fittings having an omnidirectional rated load capacity of 22250 N (5000 lbf) or above

SAE AS8027-1995 乘务员氧气调节器需求

This SAE Aerospace Standard (AS) is intended to apply to those oxygen regulators which supply gaseous oxygen at breathing pressures to meet physiological requirements of aircraft flight crew members. It defines the minimum performance requirements and testing for aircraft demand type breathing oxygen regulators.

Crew Member Oxygen Regulators, Demand

SAE AS4492-1995 幸存者定位灯

This document covers steady type lights (Type I) and flashing-type lights (Type II). This document provides minimum performance and design standards to be applied to battery-powered emergency lights intended to be fitting to individual and multiplace flotation devices to mark the location and aid in the marshalling of aviation accident survivors in bodies of water.

Survivor Locator Lights

SAE ARP89D-1995 飞机座舱自动温度控制系统

The recommendations of this SAE Aerospace Recommended Practice (ARP) for aircraft compartment automatic temperature control systems are primarily intended to be applicable to occupied or unoccupied compartments of civil and military aircraft. The purpose of this ARP is to outline the design considerations and criteria for automatic temperature control systems, for use as a guide in the aircraft industry. In most environmental control systems (ECS), temperature control is accomplished by an ECS controller; several of the control schemes discussed are based on these controllers. These recommendations are representative of present engineering practices, and necessarily subject to revision from time to time due to rapid development of the industry.

Aircraft Compartment Automatic Temperature Control Systems

SAE AIR1168/6-1994 设备部件的特性,设备冷却系统的设计和温度控制系统的设计

This section relates the engineering fundamentals and thermophysical property material of the previous sections to the airborne equipment for which thermodynamic considerations apply. For each generic classification of equipment, information is presented for the types of equipment included in these categories, and the thermodynamic design considerations with respect to performance, sizing, and selection of this equipment.

Characteristics of Equipment Components, Equipment Cooling System Design, and Temperature Control System Design

SAE ARD50034-1993 乘客防护呼吸设备

This Aerospace Resource Document (ARD) accepts, subject to the expectations noted, the use of EUROCAE ED-65 as an international specification for passenger protective breathing equipment (PPB-E), designed for carriage and use abroad transport aircraft.

Passenger Protective Breathing Equipment

SAE AIR4740-1993 安全考虑.在运输类飞机盥洗室内吸烟

This SAE Aerospace Information Report (AIR) discusses the question of smokers and their opinions and intentions toward smoking in lavatories of transport aircraft during flight. The study has implications for instructions and warnings given to passengers.

Safety Considerations - Smoking in Lavatories of Transport Aircraft

SAE AIR4165-1992(R2008) 航空货运系统电力传动装置的一般要求

This Aerospace Information Report (AIR) serves a dual purpose. It enables the user (aircraft manufacturer/airline) to do the following:a. To make a positive decision for the installation of a powered drive system in the cargo loading system during the definition of the aircraft on-board cargo loading system to be develop/procured.b. To provide the user with general requirement to be taken into consideration during the preparation of component specification for powered drive units (PDUs) to be used in a aircraft cargo systems. This is to provide the author of such a component specifiction with a selection of criteria in order to obtain an optimum component suitable for the users' applications.

General requirements for powered drive units in aircraft cargo systems

SAE ARP4712-1992 手提式机舱灭火器运输机

This SAE Aerospace Recommended Practice (ARP) specifies minimum requirements of hand-held portable fire extinguishers, as identified below, for use on fires which may occur in the passenger cabin of air carrier transport aircraft. The types of fires for which these extinguishers are intended are further specified in this standard.

Hand-Held Cabin Fire Extinguishers Transport Aircraft

SAE AS8015B-1992 降落伞组件,部件和人员的最低性能标准

This document defines the minimum performance standards for personnel parachute assemblies to be carried in aircraft or worn by passengers, crew, or parachutists for emergency use. This document covers three types of personnel carrying parachute assemblies and the operating limitations for each.

Minimum Performance Standards for Parachute Assemblies and Components, Personnel

SAE ARP4101/3-1992 乘员组的休息设施

This document recommends criteria for the design and installation of flight crew rest facilities on commercial transport aircraft capable of ultra long-range operations with augmented/enlarged crew complement.

Crew Rest Facilities

SAE AIR4496-1992 个人轮椅的安放位置

This SAE Aerospace Information Report (AIR) provides guidance criteria for the storage of personal wheelchairs in the passenger compartment of transport category aircraft, which have not been provided by the air carrier and are designated for the sole use of the passenger requiring such assistance.

Cabin Stowage of Personal Wheelchairs

SAE ARP1283A-1992 货物运输类飞机和旋翼机的车厢照明

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

Cargo Compartment Lighting for Transport Category Aircraft and Rotorcraft

SAE AIR1168/7-1991 航空增压系统的设计

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 ARP1320A-1991 固体化学氧气发生器的氧中氯气的测定

This ARP covers a procedure to be used in the determination of 0.05 to 0.3 ppm of chlorine in oxygen from any type of generator used for emergency or other life-support systems. The methyl orange method described can be considered as a referee technique. Instrumental analysis is also given. This ARP describes a method for rapid and reliable measurement of chlorine in oxygen from a solid chemical oxygen generator. The method of sampling and analysis used in this procedure is adequate to encompass the range of interest relevant to the 0.3 ppm limit set for chlorine in oxygen. The test is sufficiently flexible to make the determination during a part of or for the first 60 s after activation, since this is the usual time during which chlorine may be found in the oxygen being generated.

Determination of Chlorine in Oxygen from Solid Chemical Oxygen Generators

NAVY MIL-C-85123 VALID NOTICE 1-1991 CNU-159/E型导弹运输和组装容器

MIL-C-85123(AS), dated 17 February 1978, has been reviewed and determined to be valid for use in acquisition

CONTAINER, SHIPPING AND STORAGE GUIDED MISSILE CNU-159/E

NAVY MIL-C-85124 VALID NOTICE 1-1991 CNU-163/E型导弹运输和组装容器

MILITARY SPECIFICATION CONTAINER, SHIPPING AND STORAGE GUIDED MISSILE CNU-l63

CONTAINER, SHIPPING AND STORAGE GUIDED MISSILE CNU-163/E

ISO 9788:1990 航空货运设备 固定航空货物用承载能力为22250N(5000lbf)双螺柱接头的铸件

Deals with the geometry and requirements for assemblies, when installed in rail conforming to ISO 7166. Other materials than those specified in 4.2 may alternatively be used, provided the performance and testing requirements of this standard are complied with. Includes definitions, certification and testing, designation and identification.

Air cargo equipment; cast components of double stud fitting assembly with a load capacity of 22250 N (5000 lbf), for aircraft cargo restraint