Overview: This document provides specifications and performance data for
aircraft equipped with different powerplant options: ROTAX 582E, VERNER 133M, and ROTAX 912 ULS. The data includes weight, speed, climb rate, and other critical performance metrics.
Specifications and Performance:
- ROTAX 582E:
- Empty Weight: 565 lbs
- Useful Load: 635 lbs
- Gross Weight: 1200 lbs
- Cruise Speed: 75 mph
- VNE (Never Exceed Speed): 120 mph
- Glide Ratio: 8 to 1
- Stall Speed: 40 mph (Solo), 45 mph (Dual)
- Rate of Climb: 800 fpm (Solo), 500 fpm (Dual)
- Takeoff Roll: 100 ft (Solo), 350 ft (Dual)
- Engine Horsepower: 65 hp
- Service Ceiling: 10,000 ft (Solo), 8,000 ft (Dual)
- VERNER 133M:
- Empty Weight: 700 lbs
- Useful Load: 620 lbs
- Gross Weight: 1320 lbs
- Cruise Speed: 80 mph
- VNE (Never Exceed Speed): 120 mph
- Glide Ratio: 8 to 1
- Stall Speed: 41 mph (Solo), 47 mph (Dual)
- Rate of Climb: 1100 fpm (Solo), 500 fpm (Dual)
- Takeoff Roll: 200 ft (Solo), 400 ft (Dual)
- Engine Horsepower: 81 hp
- Service Ceiling: 10,000 ft (Solo), 8,000 ft (Dual)
- ROTAX 912 ULS:
- Empty Weight: 720 lbs
- Useful Load: 600 lbs
- Gross Weight: 1320 lbs
- Cruise Speed: 90 mph
- VNE (Never Exceed Speed): 120 mph
- Glide Ratio: 8 to 1
- Stall Speed: 41 mph (Solo), 47 mph (Dual)
- Rate of Climb: 1200 fpm (Solo), 800 fpm (Dual)
- Takeoff Roll: 200 ft (Solo), 350 ft (Dual)
- Engine Horsepower: 100 hp
- Service Ceiling: 12,000 ft (Solo), 10,000 ft (Dual)
Additional Notes: All performance data is based on sea level conditions on a standard day. The gross weight for the LSA version is 1320 lbs, while the experimental version allows for a gross weight of 1400 lbs.
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