Genesis Specifications

Product catalog summary

Overview: This document provides specifications and performance data for the Genesis aircraft with three different engine options: Verner 133M, Rotax 912 ULS, and Rotax 914. The specifications include weight, speed, climb rate, and other performance metrics.

1. Verner 133M Engine (Qualifies as LSA):

Empty Weight: 730 lbs
Useful Load: 590 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)
Service Ceiling: 10,000 ft (Solo), 8,000 ft (Dual)
Engine Horsepower: 84 hp

2. Rotax 912 ULS Engine (Qualifies as LSA):

Empty Weight: 750 lbs
Useful Load: 570 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)
Service Ceiling: 12,000 ft (Solo), 10,000 ft (Dual)
Engine Horsepower: 100 hp

3. Rotax 914 Engine (Does not qualify as LSA):

Empty Weight: 760 lbs
Useful Load: 560 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: 1300 fpm (Solo), 900 fpm (Dual)
Takeoff Roll: 200 ft (Solo), 300 ft (Dual)
Service Ceiling: 24,000 ft (Solo), 22,000 ft (Dual)
Engine Horsepower: 115 hp

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.

Catalog excerpts

(Other Power Plant Options) TYPICAL PERFORMANCE SPECIFICATIONS Empty weight Useful load Gross weight Overall height Wing span Chord Wing area Engine horsepower Cruise speed VNE (never exceed) Glide Ratio Stall speed Rate of climb Take off roll Service ceiling SPECIFICATIONS Empty weight Useful load Gross weight Overall height Wing span Chord Wing area Engine horsepower TYPICAL PERFORMANCE Cruise speed VNE (never exceed) Glide Ratio Stall speed Rate of climb Take off roll Service ceiling with ROTAX 914 (Does not qualify as LSA) 760 lbs 560 lbs 1320 lbsi 6’3-1/2” 30’8” 5’0” 154 sq ft 115 hp TYPICAL PERFORMANCE SPECIFICATIONS Empty weight Useful load Gross weight Overall height Wing span Chord Wing area Engine horsepower Cruise speed: VNE (never exceed) Glide ratio Stall Speed Rate of climb Take off roll Service ceiling *All performance data based at sea level on a standard day. Dual figures at gross. iLSA Version. Experimental Version:

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Genesis Specifications

Genesis Specifications

Catalog excerpts

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