The SILA 450 C embodies the perfect blend of elegance, reliability, and performance in a lightweight, all-metallic aircraft. Designed under JAR VLA standards, this high-wing aircraft weighs in at just 472.5 kg MTOW, yet it delivers a level of comfort and stability that sets it apart from the competition. Certified in Germany to meet stringent LTF-UL standards, the SILA 450 C is as attractive as it is functional.
Crafted by Aero-East-Europe, the SILA 450 C offers impressive range and endurance, making it ideal for long-range cruising with the capacity to carry 50-75 kg of luggage. Its cabin is spacious and vibration-free, ensuring a smooth, precise, and comfortable flight experience, even in turbulent conditions. With STOL capabilities, this aircraft excels in short takeoffs and landings, embodying Aero-East-Europe's commitment to safety and pilot-friendly design.
The SILA 450 C is powered by a reliable four-stroke engine, with a semi-monocoque fuselage and wings constructed from high-quality aeronautical aluminum. The aircraft's traditional flight controls are designed for precision, with a mix of mechanical and automatic systems for optimal performance.
In essence, the SILA 450 C is not just an aircraft—it's a testament to Aero-East-Europe's dedication to creating top-tier, pilot-friendly planes that combine style, comfort, and superior flying dynamics. Whether you're looking for an aircraft that meets the highest standards or one that offers a luxurious and stable flight, the SILA 450 C is your ultimate choice.
Basic equipment of Sila 450 “C” is next:
| 1. Airspeed indicator |
| 2. Altimeter |
| 3. Magnetic compass |
| 4. Bank & Yaw indicator (ball) |
| 5. Tachometer |
| 6. Hourmeter |
| 7. Fuel quanity indicator |
| 8. Cylinder head temperature indicator |
| 9. Oil pressure indicator |
| 10. Oil temperature indicator |
| 11. Pitot static system |
| 12. Seat belts for each occupant (2 harnesses) |
| 13. VHF Radio – dual watch |
General Information
| Type | SILA |
| Model | 450 C |
| Manufacturer | AERO – EAST – EUROPE d.o.o. Dimitrija Tucovica 2. L 4/5 36000 Kraljevo Serbia |
Characteristics
| Construction | Metallic – Aluminum, CrMo steel |
| Wing assembly | High wing airplane with struts |
| Tail assebly | Behind the wings |
| Empennage form | Cross – shaped form |
| Wing Profile - Airfoil | NACA 5417 |
| Landing gear | Tricycle |
| Seats | 2 Side by Side |
| Engine | Rotax 912/914 |
| Propeller | 2/3 Bl. Fix or Variable p.p. |
| Powerplant assembly | Tractor |
| Fuel Tanks Nr. 3 | 45+45+10Litres |
| Multifuel | 100LL avgas, automotive 94/95/98 |
| Average Fuel Consumption | 16lit/hr |
| Empty weight | 292,5Kg |
| MTOW | Meet the LTF-UL German Requirements of 472,5Kg |
Dimensions
| Wing span | 9,46m |
| Wing Chord | 1,27m |
| Wing area | 11,94m2 |
| Horizontal Tail | 0,75m x 2,9m |
| Length | 6,47m |
| Height | 2,40m |
| Cabin Height | 1,15m |
| Cabin Width | 1,15m |
| Baggage Comp. | 1,13m x 0,6m x 0,77m |
| Landing Gear Width | 1,80m |
Performances (Rotax 912 100Hp)
| Vne (never exceed speed) | 223Km/h |
| Max Speed(at max continuous power) | 205Km/h |
| Cruising Speed 75% | 185Km/h |
| Vs0 | 64Km/h |
| Maximum speed with deployed flaps | 106Km/h |
| Vs1 | 83Km/h |
| Va (maneuvering speed) | 165Km/h |
| Maximum speed in rough air | 183Km/h |
| Vc | 183-223Km/h |
| Vno | 83-183Km/h |
| Xss Wind Component | 28calculated - 45demostrated Km/h |
| Tail Wind Component | 15calculated – 28demonstrated Km/h |
| Rate of Climb | 5,6m/sec |
| Endurance/Range | 6Hrs/1080Km |
| Service Ceiling | 3.658m/12.000ft |
| Lift to Drag | 15 |
| Take off Run | 90m |
| Landing Run | 140m |