Continuous vibration monitoring of engines in-flight has become routine since the introduction of FAR 25.1305 (d) (3) in 1974 not only on civil aircraft, but also increasingly with military aircraft. Although early AVM systems were often unreliable; modern systems are not only reliable and credible, but also cost-effective. This paper will discuss briefly the principal technical components of AVM systems, then describe 'th current state of the art' and the use and effectiveness of AVM.
An overview of airborne vibration monitoring (AVM) systems
Ein Ueberblick ueber Schwingungsanzeigesysteme fuer Flugzeuge
SAE-Papers ; Oct ; 1-10
1987
10 Seiten, 9 Bilder, 14 Quellen
Aufsatz (Konferenz)
Englisch
An Overview of Airborne Vibration Monitoring (AVM) Systems
SAE Technical Papers | 1987
|Condition Monitoring for Helicopters: 3303 Airborne Vibration Monitoring System
SAE Technical Papers | 1993
|Airborne engine vibration pickup
TIBKAT | 1963
|Airborne engine vibration monitor
TIBKAT | 1964
|