V05 可靠性 标准查询与下载

GB/T 38918-2020 民用飞机起落架结构设计与仿真

本标准规定了民用飞机起落架结构设计的基本要求、详细要求和仿真要求。 本标准适用于民用飞机起落架（以下简称起落架）结构设计及仿真，其他飞机可参考使用。

Civil airplane landing gear structure design and simulation

GB/T 29075-2012 航天器概率风险评估程序

本标准规定了航天器概率风险评估(PRA)的一般要求、总体流程和实施程序、本标准适用于定量评估航天器的系统、分系统及设备的安全风险或任务风险、

Probabilistic risk assessment procedure for spacecrafts

MH/T 9004-2013 飞机燃油系统及部件的结冰试验

本标准规定了飞机燃油系统和部件结冰试验用的设备和材料、燃油的选择及试验方法。本标准适用于使用喷气式发动机的固定翼飞机在其运行环境条件下的飞机燃油系统和部件的结冰试验。

Aircraft fuel system and component icing test

IEC 107/161/DTS:2011 IEC/TS 62239-1(第一版):航空电子设备工艺管理.管理方案.第1部分:电子部件管理计划的制备和维护

IEC/TS 62239-1, Ed. 1: Process management for avionics - Management plan - Part 1: Preparation and maintenance of an electronic components management plan

SAE AS6029-2011 用于飞行安全性的激光控制措施性能标准

This document provides guidance for laser operators and aviation authorities to determine the performance criteria that laser hazard control measures shall meet for the operation of an outdoor laser system in navigable airspace. The document does not cover systems intended to deliberately aim and or track lasers at aircraft except for FAA approved purposes, such as visual warning systems, search and rescue, etc. Aircraft operations to be protected include all types that can be reasonably expected to operate in the affected area, which are traveling at speeds and altitudes defined in the Performance/Functional Requirements section. This document does not address all possible aircraft operations, (e.g. the operation of stealth, high-speed (> Mach 1), unmanned aircraft systems, aircraft above 60 000 feet MSL, etc.), including aircraft operating under a waiver from FAA regulations. Depending on the laser system's location and operational characteristics, the proponent may be required to coordinate with local military facilities and with the USAF Space Command. The military may request additional requirements (such as limitations on lasing hours or locations), or they may take actions to avoid the laser location. The purpose of this document is to specify performance criteria standards for control measures to ensure the safe incorporation of lasers propagated into the navigable airspace.

Performance Criteria for Laser Control Measures Used for Aviation Safety

AECMA TR 3198-2005 航空航天系列.制造商鉴定组合标记EN航空产品鉴定

This Technical Report lists the monograms and marks which identify manufacturers of EN aerospace products.

Luft- Und Raumfahrt Herstellerkennzeichen Und -Markierungen Fur EN-Erzeugnisse Der Luft- Und Raumfahrt Aerospace Series Manufacturers' Identification Monograms and Marks for EN Aerospace Products Serie Aerospatiale Monogrammes Et Marques D'Identification

AECMA PREN 9162-2005 航空航天系列.操作自我查证.P1版

The focus of Operator Self-Verification is on traditional manufacturing operations, and applications can be made wherever traditional inspection is employed. The practices recommended in this document are intended to identify the basic elements and provide a “guideline” for structuring Operator Self-Verification programs within the aerospace industry; applicable to producers of commercial and military aircraft and weapons platforms, space vehicles, and all related hardware, software, electronics, engines and composite components. Operator Self-Verification programs are applied to improve the overall efficiency and product quality of processes considered mature, as judged by the implementing organization. Operator Self- Verification programs are not stand-alone processes, but augment existing quality management systems. The identified program elements are for voluntary implementation by the organization, and are not intended for contractual flow-down unless otherwise stipulated through contractual agreement.

Aerospace Series Operator Self-Verification Programs Edition P 1

SAE ARP5580-2001 针对非汽车应用推荐的失效模式及影响分析(FMEA)实践

Recommended Failure Modes and Effects Analysis (FMEA) Practices for Non-Automobile Applications describes the basic procedures for performing a Failure Modes and Effects Analysis (FMEA). It encompasses functional, interface, and detailed FMEA, as well as certain pre-analysis activities (FMEA planning and functional requirements analysis), post-analysis activities (failure latency analysis, FMEA verification, and documentation), and applications to hardware, software, and process design. It is intended for use by organizations whose product development processes use FMEA as a tool for assessing the safety and reliability of system elements, or as part of their product improvement processes. A separate, Surface Vehicle Recommended Practice, J1739, is intended for use in automobile applications. Purpose: In developing this procedure the subcommittee has endeavored to develop a procedure that reflects the best current commercial practices. This procedure was developed in recognition of todays intense and competitive market demands for high reliability, affordability, and speed to market. The subcommittee had several objectives in defining the FMEA process: 1. Define a basic methodology to include functional, interface, and detailed FMEA. This will facilitate performing the analysis throughout the design process, from early in the conceptual stage to implementation and production. 2. Extend the methodology to include both product and process FMEAs. The methodology can be applied to the many technologies (e.g., mechanical, electrical, software, etc.) used in the development of a product. This helps to facilitate communications between all the parties involved in the development of a system and is useful in a concurrent engineering environment. 1. Provide simple techniques for ranking failure modes for corrective actions and for identifying fault equivalencies. 2. Define the types of information needed for the FMEA in electronic databases, thus facilitating semi-automation of the analysis. 3. Provide procedures for managing the FMEA and for getting the most benefit from the analysis.

Recommended Failure Modes and Effects Analysis (FMEA) Practices for Non-Automobile Applications

ARINC 628P1-3 ITEM 12.0-2001 可靠性

Reliability

Reliability

AECMA TR 3198-2000 航空航天系列.制造商鉴定组合标记EN航空产品鉴定

This Technical Report was drawn up by the AECMA-STAN Standardization Committee. The reason which led to the publication of the document as a Technical Report is explained in the foreword.

Luft- Und Raumfahrt Herstellerkennzeichen Und -Markierungen Fur EN-Erzeugnisse Der Luft- Und Raumfahrt Aerospace Series Manufacturers' Identification Monograms and Marks for EN Aerospace Products Serie Aerospatiale Monogrammes Et Marques D'Identification

HB 7592-1998 飞机非电子系统可靠性增长的试验方法

本标准规定了新研飞机（含直升机，下同）非电子系统（以下简称系统）利用试验进行可靠性增长的方法和要求。 　　本标准主要适用于新研飞机在研制阶段系统的可靠性增长，在役飞机系统的可靠性增长也可参照执行。

Test method for reliability growth of aircraft non-electronic systems

HB 7501-1997 机载导弹发射装置可靠性设计准则

本标准规定了机载导弹发射装置（以下简称发射装置）可靠性设计的一般要求和详细要求。 　　本标准适用于机载导弹发射装置的可靠性设计，是控制型号可靠性设计准则的主要依据。具体型号的可靠性设计准则可根据需要对本标准进行适当剪裁。

Reliability Design Criteria for Airborne Missile Launcher

HB 7500-1997 空空导弹可靠性设计准则

本标准规定了空空导弹可靠性设计准则的一般要求和详细要求。 　　本标准适用于空空导弹（以下简称导弹）的可靠性设计，是制定型号可靠性设计准则的主要依据。具体型号可靠性设计准则可根据需要对本标准进行适当剪裁。

Air-to-Air Missile Reliability Design Criteria

BS M 89:1996 飞机地面支持设备 装载和维修设备的稳定性要求

1 This International Standard specifies: a) the criteria to be used to determine stability of aircraft loading and servicing equipment, including wind loads; b) the classification of systems recommended to achieve stability; c) the formula to be used for calculating steady-state wind stability; d) the recommended test methods applicable to equipment. 2 The intent of this International Standard is not to specify equipment design, but rather to define uni-form criteria, calculation and testing methods in order to provide a safe work environment under all predict-able circumstances for the users of aircraft loading and servicing equipment. 3 This International Standard specifies the world-wide requirements recognized by aircraft and equip-ment manufacturers as well as airlines and handling agencies. In addition, it shall be applied with due reference to national governmental regulations of the country where the equipment is to be operated. 4 This International Standard applies to aircraft loading and servicing equipment, typically but not exclusively defined as follows: — container and pallet loaders (see ISO 6967 and ISO 6968); — catering trucks (see ISO 10841); — passenger stairs (see ISO 12056); — maintenance and fueling access platforms, when operated in a static position on an aircraft. 5 This International Standard does not apply to: — forklifts; — aircraft de-icers; — any equipment with rotating booms, and more generally any equipment the normal mode of operation of which includes moving in the elevated position.

Aircraft ground support equipment. Stability requirements for loading and servicing equipment

SAE AIR5022-1996 可靠性和安全性过程整合

This SAE Aerospace Information Report (AIR) describes several of the commonly performed Reliability and Safety (R&S) analysis tasks, with emphasis on their inter-relationships and common data elements. This document also describes how the R&S process can be integrated, reducing duplicate work effort and providing more accurate, comprehensive, and standardized analysis results. To illustrate how this integration can be accomplished, several specific reliability and safety tasks are performed on a subsystem of an example product.

Reliability and Safety Process Integration

AECMA TR 3198-1996 航空航天系列.制造商鉴定组合标记EN航空产品鉴定

This Technical Report was drawn up by the AECMA Standardization Committee. The reason which led to the publication of the document as a Technical Report is explained in the foreword.

Luft- Und Raumfahrt Herstellerkennzeichen Und -Markierungen Fur EN-Erzeugnisse Der Luft- Und Raumfahrt Aerospace Series Manufacturers' Identification Monograms and Marks for EN Aerospace Products Serie Aerospatiale Monogrammes Et Marques D'Identification

HB 7232-1995 军用飞机可靠性设计准则

本标准规定了战斗机主要系统（机体结构除外）在研制阶段进行可靠性设计的要求。 　　本标准适用于战斗机（歼击机），亦适用于歼击轰炸机、强击机和教练机的可靠性设计，可作为可靠性设计、评审的依据。根据型号具体特点允许对本准则进行剪裁。

Reliability Design Criteria for Military Aircraft

HB 7254-1995 直升机可靠性设计准则

本标准规定了直升机机体结构、旋翼尾桨及各系统可靠性设计的通用准则，它是直升机可靠性设计的依据之一。 　　本标准适用于各类新研直升机的可靠性设计，也适用于改型直升机的改动部分。在应用本标准时，应根据型号特点及有关文件的规定对本标准进行合理裁剪。

Helicopter Reliability Design Criteria

HB 7177-1995 军用飞机可靠性维修性外场验证

本标准规定了军用飞机可靠性、维修性外场验证的基本要求，提出了军用飞机可靠性、维修性外场验证的程序和方法。 　　本标准适用于所有有可靠性、维修性指标要求的军用战术飞机（含武装直升机）整机、系统、发动机以及由于受条件限制不能在试验室进行验证试验的机载设备，在研制阶段结束时，可靠性、维修性指标的外场验证。

Field verification of reliability and maintainability of military aircraft

HB/Z 230-1993 运输机系统可靠性设计准则

本标准规定了运输机系统、分系统、设备等可靠性设计的一般要求和详细要求。 　　本标准适用于民用运输机和军用运输机系统、分系统、设备等的可靠性设计。（不适用于水上飞机和直升飞机）根据运输机型号的具体需要，可对本标准进行剪裁。

Reliability Design Criteria for Transport Aircraft Systems