Engine Specifications
The Bombardier Rotax 912 S3 engine features 4 cylinders with a power output of 100 PS (73.5 KW). The Time Between Overhaul (TBO) is 2,000 hours or 15 years.

Propeller Specifications
The MT-Propeller MTV-21-A / 170-05 is a hydraulic 2-blade constant-speed propeller with a TBO of 2,000 hours or 6 years.

Dimensions
- Length: 7.40 m (24.28 ft)
- Height: 2.40 m (7.87 ft)
- Wingspan: 10.30 m (33.79 ft)
- Wing area: 10.50 m² (113.00 ft²)
- Cabin width: 1.20 m (3.97 ft)
- Baggage compartment capacity: 500 liters (17.70 ft³)

Weight and Capacities
- Empty weight: from 500 kg (1,102 lb)
- Maximum take-off weight: 750 kg (1,653 lb)
- Maximum load capacity: 250 kg (551 lb)
- Maximum baggage weight: 40 kg (88.2 lb)
- Seats: 2
- Fuel capacity: 2 x 60 liters (2 x 15.85 US GAL)
- Fuel grade: EN228 Super / Super Plus, AVGAS 100LL, AVGAS UL91

Performance
- VNE (Never exceed speed): 305 km/h (165 kts)
- VNO (Speed for normal operations): 240 km/h (130 kts)
- Maximum range (5,000 ft at 55% power): 1,150 km (620 NM)
- Climb rate (MSL): 3.56 m/s (700 ft/min)
- Service ceiling at MTOW: 4,420 m (14,500 ft)

Take-off and Landing Distances at MTOW
- Take-off ground roll distance: 250 m (820 ft)
- Take-off distance over 50 ft obstacle: 430 m (1,411 ft)
- Landing ground roll distance: 210 m (689 ft)
- Landing distance over 50 ft obstacle: 500 m (1,640 ft)

Technical Data
The document provides detailed specifications for the engine, propeller, dimensions, weight, capacities, performance, and take-off and landing distances.