
Gas Turbine Engine Test Facility Vibration Measurement
NORM herausgegeben am 1.12.2025
Designation standards: SAE ARP6068A
Publication date standards: 1.12.2025
Country: American technical standard
Kategorie: Technische Normen SAE
The test procedure per the applicable Engine Manual does require a vibration check for the low/intermediate and high speed rotor systems.
Release of an engine with high vibrations can result in:
On-wing vibration complaints, with subsequent troubleshooting
Rotor system failures
Premature engine removals
Limits are provided for transient conditions and steady state data points.
Troubleshooting recommendations are limited to verification of the proper signal input and tracking. This practice provides recommendations for:
Correct cable and transmitter installation and connections
Calibration
Recorded data interpretation and data analysis
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard