SAE ARP6461
Guidelines for Implementation of Structural Health Monitoring on Fixed Wing Aircraft.
Standard:
AKA:
- ARP6461
- 2013-09-19
- G-11shm, Structural Health Monitoring And Mgmt (Aisc)
This document is applicable to civil aerospace airframe structural applications where stakeholders are seeking guidance on the definition, development and certification of Structural Health Monitoring (SHM) technologies for aircraft health management applications.For the purpose of this document, SHM is defined as “the process of acquiring and analyzing data from on-board sensors to evaluate the health of a structure.” The suite of on-board sensors could include any presently installed aircraft sensors as well as new sensors to be defined in the future.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| ARP6461 | 2013-09-19 | Latest |
- SAE ARP 6461
- Aerospace
- Aircraft Structures
- Analysis methodologies
- Failure modes and effects analysis
- Sensors and Actuators
- Aircraft Operations
- Diagnostics
- Fleet Management
- Maintenance, Repair and Service Operations
- Prognostics
- Reliability Maintainability Supportability
- Safety
- Tests and Testing
- Aircraft certification