Single Engine Light Utility Aircraft
The Seagull -300 is a single-engine light utility aircraft with a high-wing configuration and pusher propeller. It has a maximum range of 1,300 km and a service ceiling of 4,500 m.
Technical Specifications
General Overview
Versatile Light Utility Aircraft
This high-performance single-engine aircraft is engineered for multi-terrain utility, offering exceptional flexibility for both land and water operations. With a robust 310 hp engine and a high-wing configuration, it delivers reliable short-field performance and stable flight characteristics. It is an ideal solution for operators requiring a durable, efficient, and versatile light utility platform for varied missions.
Physical Dimensions
8.94 m
Length
12.3 m
Wingspan
3.05 m
Height
Weight and Capacity
Weight Data
| Metric | Value |
|---|---|
| Maximum Takeoff Weight | 1,680 |
| Normal Takeoff Weight | 1,470 |
| Maximum Landing Weight | 1,580 |
| Empty Weight | 1,060 |
| Maximum Useful Load | 620 |
Engine and Propulsion
Propulsion System
- Engine Model: Lycoming TIO-540-AJ1A
- Power Output: 310 hp
- Engine Speed: 2500 rev/min
- Propeller Diameter: 1.98 m
Performance
Performance Metrics
250 km/h
Max Speed
4.5 m/s
Climb Rate
4,500 m
Service Ceiling
7 hours
Endurance
Operational Capabilities
Takeoff and Landing Requirements
| Condition | Takeoff (m) | Landing (m) |
|---|---|---|
| Land | 398 | 238 |
| Water | 475 | 260 |
