Specifications
Gevers Aircraft, Inc. * GENESIS *

Unprecedented safety, utility, and performance.

• DIMENSIONS EXTERNAL:
• Wing span extended..............15.24 m (50 ft 0 in)
• Wing span retracted................7.87 m (26 ft 0 in)
• Wing chord at fixed root.........3.25 m (10 ft 8 in)
• at fixed tip.......................2.03 m (6 ft 8 in)
• at extension root..............1.12 m (3 ft 8 in)
• at extension tip................1.12 m (3 ft 8 in)
• Wing aspect ratio extended.....8.33
• Wing aspect ratio retracted.....3.1
• Length overall.......................11.58 m (38 ft 0 in)
• Height overall.........................3.75 m (12 ft 4 in)
• Tailplane span.........................4.44 m (14 ft 7 in)
• Wheel track.............................3.2 m (10 ft 6 in)
• Wheelbase...............................6.35 m (18 ft 6 in)
• Propeller diameter..................1.98 m (6 ft 6 in)
• Passenger door:
• Height.............................0.97 m (3 ft 2 in)
• Width..............................2.24 m (7 ft 4 in)
• DIMENSIONS INTERNAL:
• Cabin:
• Length.............................3.05 m (10 ft 0 in)
• Max width.......................1.21 m (3 ft 11-1/2 in)
• Max height......................1.07 m (3 ft 6 in)
• Volume...........................3.74 cu.m (132 cuft)
• Nose baggage.........................0.283 cu.m (10 cuft)
• Rear baggage..........................0.425 cu.m (15 cuft)
• AREAS:
• Wing extended, gross...........................28.60 sqm (308 sqft)
• Wing retracted, gross...........................20.40 sqm (220 sqft)
• Ailerons ret. (total)................................1.16 sqm (12.5 sqft)
• Ailerons ext. (total)...............................2.79 sqm (30 sqft)
• Trailing edge flaps (tot.)........................0.71 sqm (7.67 sqft)
• Vertical stabilizer (not incl. rudder)......4.16 sqm (44.8 sqft)
• Rudder, incl. tab.....................................1.39 sqm (15 sqft)
• Horizontal stabilizer...............................3.81 sqm (41 sqft)
• Elevator incl. tab....................................1.90 sqm (20.5 sqft)
• WEIGHTS:
• Empty weight.........................................1540 kg (3600 lb)
• Max T O weight.....................................2720 kg (6000 lb)
• Max wing loading ext..............................95.1 kg/sqm (19.5 lb/sqft)
• Max wing loading ret..............................133. kg/sqm (27.3 lb/sqft)
• Max power loading.................................5.61 kg/kW (9.23 lb/hp)
• PERFORMANCE:
• Max level speed at max weight of 2720 kg (6000 lb)......... 267 kt (496 km/h; 308 mph)
• Cruise speed at max weight of 2720 kg (6000 lb) at S/L,
• wings retracted
• 75% power..................................................................225 kt (450 km/h; 280 mph)
• 65% power..................................................................214 kt (435 km/h; 270 mph)
• one engine inop............................................................192 kt (386 km/h; 240 mph)
• Stall speed:
• flaps, gear, wings retracted...........................................95 kt (175 km/h; 109 mph)
• flaps, gear, wings extended...........................................55 kt (101 km/h; 63 mph)
• Rotation speed.......................................................................66 kt (122 km/h; 76 mph)
• Approach speed....................................................................71 kt (132 km/h; 82 mph)
• T O run:
• on hard surface............................................................220 m (720 ft)
• on water.......................................................................305 m (1000 ft)
• T O to 50 ft:
• on hard surface............................................................495 m (1625 ft)
• on water.......................................................................581 m (1905 ft)
• Landing from 50 ft:
• on hard surface............................................................600 m (1970 ft)
• on water........................................................................683 m (2240 ft)
• Landing run:
• on hard surface..............................................................70 m (230 ft)
• on water.......................................................................152 m (500 ft)
• Range with max fuel (200 gal)..........................................1,910 nm(3540 km; 2,200 miles)