AIR1872A: Guide to Life Usage Monitoring and Parts Management for Aircraft Gas Turbine Engines

Features

Issuing Committee: E-32 Aerospace Propulsion Systems Health Management

Scope

Content

The effectiveness of Engine Life Usage Monitoring and Parts Management systems is largely determined by the aircraft-specific requirements. This document addresses the following areas:

a
Safety
b
Life-limiting criteria
c
Life usage algorithm development
d
Data acquisition and management
e
Parts life tracking
f
Design feedback
g
Cost effectiveness

It primarily examines the requirements and techniques currently in use, and considers the potential impact of new technology to the following areas:

a
Parts classification and control requirements
b
Failure causes of life-limited parts
c
Engine life prediction and usage measurement techniques
d
Method validation
e
Parts life usage data management
f
Lessons learned
g
Life usage tracking benefits

Meta Tags

Topics: Aircraft propulsion systems
Vehicle health management (VHM)
Military aircraft
Engine components
Failure modes and effects analysis
Fatigue
Life cycle analysis
Data management
Cost analysis

Details

DOI: https://doi.org/10.4271/AIR1872A

Pages: 1

Citation: SAE International Information Report, Guide to Life Usage Monitoring and Parts Management for Aircraft Gas Turbine Engines, SAE Standard AIR1872A, Revised May 1998, Issued February 1988, https://doi.org/10.4271/AIR1872A.

Additional Details