49.095 客运设备和座舱设备 标准查询与下载

HB 8393-2014 民用飞机驾驶舱座椅和约束系统规范

本规范规定了民用运输类飞机驾驶舱座椅和约束系统的设计、验证和交付要求。 本规范适用于民用运输类飞机驾驶舱座椅和约束系统的设计、验证和交付。其他飞机驾驶舱座椅和约束系统可参照执行。

Specification for the pilot seat and restraint system in civil aircraft

HB 8398-2014 民用飞机紧急撤离用滑梯、轻便梯和救生筏规范

本规范规定了民用运输类飞机应急撤离用滑梯、轻便梯、轻便梯/滑梯和滑梯/救生筏(以下简称滑梯装置)的设计、制造、验证及交货准备等要求。 本规范适用于民用运输类飞机滑梯装置的设计、制造和验收。

Specification for the emergency evacuation slides,ramps and rafts of civil aircraft

HB 8410-2014 民用飞机人体躯干约束系统要求

本标准规定了民用飞机人体躯干约束系统(以下简称约束系统)设计和验证要求。 本标准适用于民用飞机的人体躯干约束系统的设计和试验。

Requirements for restrain system of the human torso in civil aircraft

HB 7047-2012 民用运输类飞机旅客座椅通用要求

本标准规定了民用运输类飞机旅客座椅的设计，试验和验收的通用要求。适用于民用运输类飞机旅客座椅的研制。

General requirements for passenger seat in civil transport aircraft

SAE ARP1176A-2013 氧气系统与组件的清洁

This SAE Aerospace Recommended Practice (ARP) provides recommended practices for cleaning aircraft oxygen equipment such as tubing, pieces parts (including regulator and valve parts), cylinders and ground-based equipment that may be used to support aircraft oxygen systems. This revision introduces a cleanliness coding scheme that can be referenced as a requirements, and/or referenced to identify compliance to meeting such a requirements. These methods may apply to gaseous and liquid oxygen equipment. This document specifies work area details, methods to select suitable cleaning chemicals, cleaning methods, test methods to verify cleanliness level, and metho

Oxygen System and Component Cleaning

SAE AIR6036-2013 利用富氧气体混合物的乘客缺氧保护

Currently, existing civil aviation standards address the design and certification of oxygen dispensing devices that utilize oxygen sources supplying at least 99.5% oxygen. This Aerospace Information Report discusses issues relating to the use in the passenger cabin of oxygen enriched breathing gas mixtures having an oxygen content of less than 99.5% and describes one method of showing that passenger oxygen dispensing devices provide suitable hypoxia protection when used with such mixtures.

Passenger Hypoxia Protection Utilizing Oxygen Enriched Gas Mixtures

SAE AMS2678A-2013 真空环境中零部件的炉内钎焊

This specification covers the requirements and procedures for the brazing of parts in a very low pressure gas which referred to as ""vacuum"" herein.

Furnace Brazing of Parts in a Vacuum Atmosphere

ANSI/ASHRAE 161 Addendum g-2013 商用飞行器内部空气质量

Air Quality within Commercial Aircraft

ANSI/ASHRAE 161 Addendum f-2013 商用飞行器内部空气质量

Air Quality within Commercial Aircraft

ANSI/ASHRAE 161 Addendum c-2013 商用飞行器内部空气质量

Air Quality within Commercial Aircraft

ANSI/ASHRAE 161 Addendum d-2013 商用飞行器内部空气质量

Air Quality within Commercial Aircraft

SAE ARP5770-2012 机械控制设计指南

This SAE Aerospace Recommended Practice (ARP) provides guidelines for the configuration and design of mechanical control signal transmission systems and subsystems. It is focused on the recommended practices for designing cable and pulley, pushrod and bellcrank and push-pull flexible cable control systems. These systems are typically used in some combination to transmit pilot commands into primary, secondary and utility control system commands (mechanical or electrical) or aircraft surface commands. On mechanically controlled aircraft, most pilot control commands are initiated through cockpit mounted wheels, sticks, levers, pedals or cranks that are coupled

Mechanical Control Design Guide

SAE ARP85F-2012 亚音速飞机的空气调节系统

This SAE Aerospace Recommended Practice (ARP) contains guidelines and recommendations for subsonic airplane air conditioning systems an components, including requirements, design philosophy, testing and ambient conditions. The airplane air conditioning system comprises that arrangement of equipment, controls and indicators that supply and distribute air to the occupied compartments for ventilation, pressurization, and temperature and moisture control. The principal features of the system are: a. a supply of outside air with independent control valve(s); b. a means for heating; c. a means for cooling (air or vapor cycle units and heat exchangers); d. a means

Air Conditioning Systems for Subsonic Airplanes

DIN EN 4697:2012 航空航天系列.乘客座椅配件通用和安装要求.德文和英文版本EN 4697-2012

Aerospace series - General and installation requirements for passenger seat fittings; German and English version EN 4697:2012

SAE AS1356-2012 救生艇

This SAE Aerospace Standard (AS) establishes Minimum Performance Standards (MPS) for life rafts carried on board aircraft. This document is not intended to specify particular design methods, mechanisms, or equipment to be used to accomplish the objectives established herein. The purpose of this AS is to improve the performance of life rafts carried on transport aircraft, by ensuring that their design and function support rapid and effective use as group flotation aids after an emergency landing in water (ditching). ARP1356A has been converted to AS1356, at the request of the FAA, to support revision of Technical Standard Order C-70.

Life Rafts

SAE AS17852A-2012 氧气压力异径接头

This specification covers the requirements for two types of oxygen pressure reducers.

Reducers, Oxygen Pressure

SAE ARP1282B-2012 救生背包.救生艇和滑梯/救生艇

This SAE Aerospace Recommended Practice (ARP) applies to survival kits to be carries with life rafts or slide/rafts on transport category airplanes flying extended over water routes and equipped with approved satelite alerting devices (e.g. 406 MHz Emergency Locator Transmitter (ELT)), available for deployment after an emergency landing. The purpose of this document is to establish the minimum contents for survival kits so as to enhance health and survivability of airplane occupants after a planned or unplanned landing on open water or a remote land environment.

Survival Kit - Life Rafts and Slide/Rafts

SAE ARP6448-2012 与第AC21-49节第7.b条款一致的带集成电子座椅的单向开槽批准

This document provides an industry-recommended framework for establishing agreements to ensure that seats with integrated electronic components (e.g., actuation system, reading light, inflatable restraint, IFE, etc.) meet the seat TSO Minimum Performance Standard. These agreements will allow Seat Suppliers to build and ship completed, integrated and approved seat assemblies under TSOA with electronics included. The document presents the roles, responsibilities and accontibilities of the Electronics Manufacturer, the Seat Supplier, and the Seat Installer/Electronics Activator in the context of AC 21-49 Section 7.b ' Type Certification using TSO-approved seat with electronic components defined in TSO design'. This document applies to all FAA seat TSOs (C39(), C127()...etc). Only the TSO attributes of integrated electronic components that affect the seat TSO compliance (e.g., component strength and attachment under static and dynamic loading conditions, delethalization, flammability, HIC, and lumbar loads) are addressed. The approval for the integration of the electronics will fall, in part or in full, under the type design authority of the Seat Installer rather than the Seat Supplier shipping the integrated seat. The defined responsibilities, areas of authority and accountability of each party, as well as necessary communication protocols, must ensure configuration management, design control and quality control. These definitions, controls and protocols are agreed (thru normal commercial agreements and binding contracts) and adhered to by all parties ensuring all parts in the supply chain remain approved (e.g. certified and conformed). This document primarily focuses on the relationship between the Seat Supplier and the Electronics Manufacturer. Table A1 of Appendix A of this document contains information which details the key characteristics of electronic components derived from the Change Impact Analysis characteristics identified in AS9016 (see Reference), tailored to the specific needs of AC 21-49, that require review to ensure proper compliance with the TSO requirements per Table 1 of AC21-49. Additionally, Appendix B has been included to outline a typical data approval and change management process tailored specifically for ensuring proper communication links are established between all parties. There are many different ways to ensure design and quality control procedures are in place to meet AC21-49 Section 7.b requirements through the established process identified in this document. While the responsibility rests solely with the Seat Supplier to ensure all TSO attributes identified in Table 1 of AC21-49 are acceptable, Appendix C has been included to outline the process for authorization of Electronics Manufacturers to assess the impact of changes in their equipment on the TSO attributes. This authorization will allow the classification of the change and the appropriate handling of the implementation of the change.

Gaining Approval for Seats with Integrated Electronics in Accordance with AC21-49 Section 7.b

LST EN 4697-2012 航空航天系列乘客座椅配件通用和安装要求

Aerospace series - General and installation requirements for passenger seat fittings

DS/EN 4697:2012 航空航天系列乘客座椅配件通用和安装要求

This European Standard specifies the installation and removal requirements and the space envelopes for passenger seat fittings on aircraft. The purpose is to reduce the installation time and the tooling required for seat installation by standardizing the

Aerospace series - General and installation requirements for passenger seat fittings