T/CSAA 13-2021 Active Group standards

T/CSAA 13-2021 Guidelines for Safety Analysis of High Pressure Compressor in Civil Blended Wing Body Turbofan Engines

T/CSAA 13-2021 Guidelines for Safety Analysis of High Pressure Compressor in Civil Blended Wing Body Turbofan Engines

Publish Date: 2021-02-09 Implement Date: 2021-05-01 For services related to genuine standard inquiry, procurement, translation, and other related services in China, please Contact Us
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Basic Information

Standard Code: T/CSAA 13-2021
Standard Type: Group standards
Standard Status: Active
is_force_gb: no
CCS Name: -
ICS Name: Terminology (principles and coordination and cooperation)
Publish Date: 2021-02-09
Implement Date: 2021-05-01

Scope

Scope: This document provides guidance on work inputs for the safety analysis of high-pressure compressor components of civil large-bypass turbofan engines, the safety analysis process, preliminary fault tree analysis, fault tree analysis (FTA), failure mode, effect and hazard analysis (FMECA), and analysis reports. This document is applicable to the safety analysis of high-pressure compressor components of civil large-bypass turbofan engines. Main technical content: 4 Work inputs 5 Safety analysis process 6 Preliminary fault tree analysis 7 Fault tree analysis (FTA) 7.1 Fault tree analysis (FTA) process 7.2 Establishing a fault tree 7.3 Quantitative analysis of the fault tree 7.4 Preparing a fault tree analysis report 8 Failure mode, effect and hazard analysis (FMECA) 8.1 Composition 8.2 Failure mode and effect analysis (FMEA) 8.3 Hazard analysis (CA) 8.4 FMECA work process 8.5 Defining the object of analysis 8.6 Determining failure modes 8.7 Determining failure causes 8.8 Determining failure effects 8.9 Determining severity levels 8.10 Determining detection methods, using compensatory measures, and designing assurance measures 8.11 Failure mode and effect analysis (FMEA) 8.12 Hazard analysis (CA) method 8.13 FMECA analysis report 9 Analysis reports Appendix A (informative) CCAR-33-R2 Airworthiness provisions related to high-pressure compressors of civil aeroengines Appendix B (informative) Typical failure modes of components Appendix C (informative) Whole-machine failure modes and severity levels Appendix D (informative) FMECA report technical requirements

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