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1.1 This practice covers the minimum requirements for an in-line, non-intrusive, through-flow oil debris monitoring system that monitors ferromagnetic and non-ferromagnetic metallic wear debris from both industrial aero-derivative and aircraft gas turbine engine bearings. Gas turbine engines are rotating machines fitted with high-speed ball and roller bearings that can be the cause of failure modes with high secondary damage potential. (1)2
| Author | ASTM |
|---|---|
| Editor | ASTM |
| Document type | Standard |
| Format | File |
| Confirmation date | 2016-10-01 |
| ICS | 49.050 : Aerospace engines and propulsion systems
|
| Number of pages | 16 |
| Replace | ASTM D7685-11 |
| Set | ASTMVOL0504 |
| Year | 2011 |
| Document history | ASTM D7685-11 |
| Country | USA |
| Keyword | ASTM 7685;ASTM D7685;ASTM D7685;10.1520/D7685-11R16 |