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TTN160-1E7a

TTN160-1E7a

TTN160-1E7a

Product catalog summary
Technical Data Sheet: Turbonycoil 160
Description: Turbonycoil 160 is a synthetic oil with a viscosity of 3 cSt at 100°C, composed of neopolyol esters and additives for enhanced anti-oxidant, anti-corrosion, and extreme-pressure properties. It is suitable for high-temperature military jet engines and remains fluid at temperatures as low as -54°C.
Main Applications:
  • Fighter engine turbines (e.g., F-15, F-16)
  • Civil engine turbines in temperatures below -40°C
  • Helicopter turbine and tail rotor gearboxes in cold weather
  • APU of civil aircraft for easy in-flight restart
  • Trimmable Horizontal Stabilizer (THS) of civil aircraft
Specifications:
  • Appearance: Limpid
  • Density at 20°C: 0.957 kg/dm³
  • Kinematic Viscosity: 3.20 mm²/s at 100°C, 12.8 mm²/s at 40°C, 9600 mm²/s at -51°C after 35 min, 9620 mm²/s at -51°C after 3 h
  • Acid Number: 0.19 mg KOH/g
  • Flash Point: 228°C
  • Evaporation Loss: 20.2% at 205°C
  • Static Foam Test: 20 cm³ foam volume
  • Lead Corrosion: -0.8 g/m²
Oxidation & Corrosiveness Stability:
  • Acid Number Increase: 2.0 mg KOH/g
  • Viscosity Change: +14%
  • Insoluble Matter: None
  • Metal Weight Change: 0.0 mg/cm² for Aluminium, Silver, Steel M/50, Iron, Titanium, Brass, Magnesium
Contamination and Compatibility:
  • Solid Particle Contamination: 0.3 mg/dm³
  • Trace Metal Content: 0.0 mg/kg for Ag, Al, Cr, Cu, Fe, Mg, Mo, Ni, Pb, Si, Sn, Ti, Zn
  • Compatibility with Elastomers: SAE-AMS 3217/1 (NBR), SAE-AMS 3217/4 (FKM), SAE-AMS 3217/5 (FS)
  • Corrosion Test: 0.0 g/m² weight change for Brass and Silver
Note: The values provided are typical and do not constitute a contractual commitment. Sales specifications are available upon request.
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Catalog excerpts

TTN160-1E7a-1

AERONAUTICS & DEFENCE TECHNICAL DATA SHEET NATO CODE O-148 - MIL-PRF-7808 L Grade 3 - OX 9 DESCRIPTION Turbonycoil 160 is a 3 cSt oil at 100°C and is made of neopolyol esters containing additives to improve its anti-oxidant, anticorrosion and extreme-pressure properties. It is designed to withstand the high temperature experienced by the military engines of combat jet aircraft and retain fluidity at very low temperature (operation down to - 54°C). MAIN APPLICATIONS • Turbine oil of fighter engines (McDonnel Douglas F-15, Lockheed Martin F-16, ...) • Turbine oil of civil engines below -40°C ambient temperature • Turbine and tail rotor gearbox of helicopter in cold weather • APU of civil aircraft for easy in-flight restart • Trimmable Horizontal Stabilizer (THS) of civil aircraft Characteristic Typical Result MIL-PRF-7808 Limit Test method Appearance visual examination - Density at 20°C - Kinematic viscosity at 100°C at 40°C at -51°C after 35 min. at -51°C after 3 h - Acid number - Flash point - Static foam test at 80°C Foam volume / Collapse cm3 / s 20 / 0 max. 100 / FTM-S-791- NYCO - 66 avenue des Champs Elysees BP 414 - 75366 PARIS CEDEX 8 France | Tel. : +33 145 615 000 | Fax : +33 145 615 013 | E.mail : [email protected]: [email protected] | www.nyco.fr

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TTN160-1E7a-2

AERONAUTICS & DEFENCE TECHNICAL DATA SHEET Typical Result Test method - Oxidation & corrosiveness stability, 96 h at 200°C Acid number increase Viscosity change Insoluble matter Metal weight change Aluminium Silver Steel M/50 Iron Titanium Brass Magnesium - Solid particle contamination - T race metal content Ag, Al, Cr, Cu, Fe, Mg, Mo, Ni, Pb, Si, Sn, Ti, Zn, mg/kg Coupled Plasma Spectroscopy - Compatibility with standard elastomer SAE-AMS 3217/1 (NBR), 168 h at 70°C % volume Swelling - Compatibility with standard elastomer SAE-AMS 3217/4 (FKM), 72 h at 175°C Swelling % volume...

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*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.