Aviation Turbine Fuel
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Jet Fuel A-1 is a high-quality aviation turbine fuel designed for use in commercial and military aircraft with turbine engines. It is a kerosene-type aviation turbine fuel with a maximum freezing point of −47 °C and a maximum aromatics content of 25% (v/v), meeting the requirements of international standards (ASTM D1655 / Def Stan 91-091) and ensuring optimal engine performance, safety and reliability.
Produced and supplied through certified refineries and a quality-assured supply chain.
Meets stringent international standards ensuring safety in every flight.
Excellent cold flow properties with a maximum freezing point of −47 °C.
| Property | Unit | Limit (Jet A-1) | Test Method |
|---|---|---|---|
| Appearance | - | Clear and bright | Visual |
| Density at 15 °C | kg/m³ | 775.0 – 840.0 | ASTM D4052 |
| Freezing Point (max.) | °C | −47 | ASTM D2386 |
| Flash Point (min.) | °C | 38 | ASTM D56 |
| Kinematic Viscosity at −20 °C (max.) | mm²/s | 8.0 | ASTM D445 |
| Kinematic Viscosity at 40 °C | mm²/s | Report | ASTM D445 |
| Net Heat of Combustion (min.) | MJ/kg | 42.8 | ASTM D3338 |
| Smoke Point (min.) | mm | 25 | ASTM D1322 |
| Aromatics Content (max.) | % (v/v) | 25 | ASTM D1319 |
| Sulfur Content (max.) | mg/kg | 3000 (0.30% mass) | ASTM D2622 |
| Total Acid Number (max.) | mg KOH/g | 0.10 | ASTM D3242 |
| Copper Strip Corrosion (2 h at 100 °C) | Rating | Max 1 | ASTM D130 |
| Water Reaction | - | Max rating 1 | ASTM D1094 |
| Conductivity (at point of issue) | pS/m | 50 – 600 | ASTM D2624 |
| Thermal Stability (JFTOT) | - | See Note 1 | ASTM D3241 |
| Color | - | Report | ASTM D1500 |
