AeroShell Turbine Oil 2
2 mm²/s mineral turbine oil for jet engines
NATO Code O-133
| Property | Typical value | Limit |
|---|---|---|
| Oil type | Ester sintetic | Ester sintetic |
| Kinematic viscosity la 100°C | 5.24 | 4.90 to 5.40 |
| Kinematic viscosity la 40°C | 26.71 | 23.0 min |
| Kinematic viscosity la -40°C | 9351 | 13000 max |
| Flash point (COC)°C | 268 | 246 min |
| Pour point°C | -60 | -54 max |
| Total aciditymgKOH/g | 0.20 | 1 max |
| Pierderi prin Evaporation 6.5 hours @204°C | 2.0 | 10.0 max |
| Spumare | trece | trebuie sa treaca |
| Standard umflare Rubber sintetic - SAE-AMS 3217/4, 72 hours la 204°Cumflare % | 12.9 | 5 la 25 |
| Compatibilitate elastomer, schimbare de greutate dupa 24/120 hours: Fluorocarbon la 200°C | 7.5/9.0 | 10/15 max. |
| LCS Fluorocarbon la 200°C | 6.5/8.5 max. | 10/20 max. |
| Nitril la 130°C | 6.5/6.0 | Report |
| Silicon la 175°C | 14.5/13.5 | Report |
| Perfluoroelastomer la 200°C | 0.5/0.5 | |
| Stabilitate termica / Corozivitate 96 hours - schimbare greutate metal la 274°Cmg/cm2 | 0.23 | 4 max |
| Stabilitate termica / Corozivitate 96 hours - schimbare viscozitate la 37.8°C% | 0.3 | 5 max |
| Stabilitate termica / Corozivitate 96 hours - schimbare TANmgKOH/g | 1.5 | 6 max |
| Corrosion stability si Oxidation 72 hours la 175°C | trece | trebuie sa treaca |
| Corrosion stability si Oxidation 72 hours la 204°C | trece | trebuie sa treaca |
| Corrosion stability si Oxidation 72 hours @218°C | trece | trebuie sa treaca |
| Test Pasager de viteze, evaluare relativa Hercolube A% | 112 | 102 |
| Bearing test rig (100 hours), conditii tip 1 1/2 - evaluare generala depuneri | 21 | 80 max |
| Bearing test rig (100 hours), conditii tip 1 1/2 - schimbare viscozitate la 40°C | 24 | -5 la +30 |
| Bearing test rig (100 hours), conditii tip 1 1/2 - schimbare TAN | 0.81 | 2.0 max |
| Bearing test rig (200 hours), conditii tip 1 1/2 - depozite filtrug | 0.55 | 3 max |
| Stabilitate sonica la forfecare - schimbare viscozitate la 40°C% | 0.3 | 4 max |
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AeroShell Turbine Oil 560 is a third-generation, high-performance, low-coking 5 mm2/s synthetic ester oil incorporating a carefully selected and finely balanced combination of additives to improve thermal and oxidation stability.
NATO Code O-154 — aviation turbine oil
A NATO supply code identifying an aviation gas-turbine engine oil.
Allison gas-turbine engine oil specification (EMS-53, obsolete)
Allison's (now Rolls-Royce) obsolete specification for gas-turbine engine oil, historically used to qualify oils for Allison/Rolls-Royce turboprop and turboshaft engines such as the Model 250 series.Source
Synthetic ester aviation turbine oil, standard grade
UK MOD Joint Service Designation code for a 5 mm²/s synthetic ester aviation turbine oil, equivalent to MIL-PRF-23699 grade STD and DEF STAN 91-101 grade OX-27.Source
DEF STAN 91-101 — aviation turbine oil
The UK Defence Standard for a synthetic 5 cSt aviation gas-turbine engine oil, matching NATO Code O-156.Source
MIL-PRF-23699 — aviation turbine engine oil
The US military specification for synthetic aviation gas-turbine (jet) engine oils; STD, HTS and CI are its sub-classes by thermal stability/corrosion-inhibition level.