V44 生命保障系统与设备 标准查询与下载

HB 7278.2-1996 民用航空器应急撤离滑梯轻便梯及滑梯/救生筏组合装置最低性能要求 充气式应急撤离滑梯/救生筏组合装置

本标准第二部分规定了充气式应急撤离滑梯/救生筏组合装置的最低安全性能要求。注：CCAR25所含关于充气式应急撤离和漂浮装置安装置安装于航空器时的附加要求，应与本标准的要求一并加以考虑。 　　本标准适用于充气式应急撤离滑梯/救生筏组合装置，也适用于可作救生筏使用的撤离滑梯。

Civil aircraft emergency evacuation slide portable ladder and slide/life raft combination device minimum performance requirements inflatable emergency evacuation slide/life raft combination device

NAVY MS3398 NOTICE 1-1996 通过颜色对比的湿度指示卡

This notice should be filed in front of MS3398, dated 15 July 1969.

CARD - HUMIDITY - INDICATING COLOR COMPARISON

NAVY MIL-S-7877 B NOTICE 1-1996 机舱折叠乘客席

MIL-S-7877B is inactive for new design and is no longer used, except for replacement purposes.

SEATS; PASSENGER, CABIN FOLDING

NAVY MIL-S-85018 A NOTICE 1-1996 AN/ASN-116二阶姿态参考系统(跃上)

This notice should be filed in front of MIL-S-85018A, dated 5 May 1978.

SECOND ORDER ATTITUDE REFERENCE SYSTEM (SOARS) AN/ASN-116

ARINC 644A ITEM 5.0-1996 选择性能

Optional Capabilities

Optional Capabilities

SAE AIR822A-1996 通用航空氧气系统R(2001)

This specification has been declared "NONCURRENT" as of June 2006. It is recommended, therefore, that this document not be specified for new designs. This SAE Aerospace Information Report (AIR) provides a general overview of oxygen systems for general aviation use. Included are a brief review of the factors and effects of hypoxia, system descriptions and mission explanations for system or component selection, and techniques for safe handling of oxygen distribution systems.

Oxygen Systems for General Aviation R(2001)

SAE AS916B-1996 氧流量指标

This SAE Aerospace Standard (AS) defines the overall requirements applicable to oxygen flow indicating devices intended to operate in conjunction with an oxygen regulator and mask system. Flow indicators covered by this document are for use with pressure demand, diluter-demand and continuous flow oxygen systems.

Oxygen Flow Indicators

SAE AS8026A-1996 运输类飞机乘务人员用氧气面罩

This standard covers oxygen masks and breathing valves used with both panel mounted and mask mounted demand and pressure-demand oxygen regulators. Mask mounted oxygen regulators are covered under other standards, but when the mask mounted regulator incorporates an integral exhalation valve, the performance of this valve shall meet the requirements of this standard. This standard establishes the minimum performance standards for the manufacturer of demand type crewmember oxygen masks to be used with straight demand, diluter-demand and pressure-demand oxygen systems.

Crewmember Demand Oxygen Mask for Transport Category Aircraft

SAE ARP1532A-1996 飞机氧气系统线路的制造,测试和安装

This ARP covers procedures or methods to be used for fabricating, handling, testing, and installation of oxygen lines in an aircraft oxygen system. The purpose of this recommended practice is to establish and/or outline the methods for fabricating, handling, and testing of oxygen lines and their installation into an aircraft oxygen system. Compliance with this practice should enhance satisfactory operation of the oxygen system.

Aircraft Oxygen System Lines, Fabrication, Test and Installation

SAE AS1303A-1996 便携式化学氧气

This SAE Aerospace Standard (AS) applies to a portable chemical oxygen generator assembly intended for the following uses: a. First aid treatment of aircraft occupants after an emergency descent following a decompression or other emergency condition; and b. use by cabin attendants to maintain their mobility after a decompression.

Portable Chemical Oxygen

SAE AS1304A-1996 持续气流化学氧生成器

This SAE Aerospace Standard (AS) applies to performance and testing of solid chemical oxygen generators which produce oxygen at essentiall ambient pressure for use aboard aircraft whose cabin pressure altitude does not exceed 40,000 ft (about 12,200 m). Portable chemical oxygen devices are covered by AS1303.

Continuous Flow Chemical Oxygen Generators

HB 7171-1995 飞机热力防冰系统通用规范

本标准规定了飞机热力防冰系统的设计、制造、试验和验收的一般要求。 　　本标准适用于军用飞机的防冰，不适用于发动机进气系统和雷达罩的防冰。 　　本标准是飞机热力防冰系统设计、制造和验收的依据。对于给定用途的任何预设计，若偏离本标准会改善系统的性能、降低寿命周期费用及研制经费，或者按本标准会降低系统工作性能时，设计单位应将需改进的细节提出论证，经订购方同意，方可在设计中进行更改。

General specification for aircraft thermal anti-icing system

HB 7263-1995 民用飞机座椅垫燃烧试验方法

本标准规定了民用飞机客舱内部座椅垫燃烧试验的试验设备、试验程序及试样等。 　　本标准适用于民用飞机客舱内部座椅垫的适航鉴定及产品检验。

Civil Aircraft Seat Cushion Burning Test Method

BS G 247-2:1995 航空用定位灯.救生船照明灯规范

This Part of BS G 247 specifies the design, performance, testing and quality requirements for survivor locator lights for fitting to liferafts used in airborne applications.

Locator lights for airborne applications - Specification for liferaft lights

AC-25.1191-1-1995 1301 固定灭火瓶的批准

1301 Approval of Fixed Extinguisher Bottles

NF L17-914:1995 航空航天系列.降落伞织物.带和窄幅织物的试验.曲率的测定

Aerospace series. Parachute fabric. Testing of straps and tapes. Determination of curvature.

NF L17-915:1995 航空航天系列.降落伞织物.带和窄幅织物的试验.扭结的测定

Aerospace series. Parachute fabric. Testing of tapes and straps. Determination of kinking.

SAE AIR1168/14-1995 太空船生命支撑系统

A life support system (LSS) is usually defined as a system that provides elements necessary for maintaining human life and health in the state required for performing a prescribed mission. The LSS, depending upon specific design requirements, will provide pressure, temperature, and composition of local atmosphere, food and water. It may or may not collect, dispose, or reprocess wastes such as carbon dioxide, water vapor, urine, and feces. It can be seen from the preceding definition that LSS requirements may differ widely, depending on the mission specified, such as operation in Earth orbit or lunar mission. In all cases the time of operation is an important design factor. An Lss is sometimes briefly defined as a system providing atmospheric control and water, waste, and thermal management. The major subsystems required to accomplish the general functions mentioned above are: 1. breathing and pressurization gas storage system, 2. temperature and humidity control system, 3. carbon dioxide control system, 4. trace contaminant control system, 5. water management system, and 6. waste management system.

Spacecraft Life Support Systems

JIS W 1920:1995 飞行器.辅助传动装置和安装缓冲垫

この規格は，運用中の航空機のエンジン/ギアボックスから補機を取り外せるようにしたインボリュートスプライン駆動軸付さ迅速着脱式結合の設計基準について規定する。

Aircraft -- Accessory drives and mounting pads

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