International Aircraft Directory

1996’€“ Present

2004’€“ Present

1999’€“ Present

1980’€“90

1988’€“Present

1952’€“1972

STANDARD DATA: Gross weight: 1,178 lbs.; Empty weight: 739 lbs.; Fuel capacity: 20 gals.; Wingspan: 19 ft. 7 in.; Length: 17 ft. 6 in.; Engine: 100–200 hp. PERFORMANCE: Top speed: 180 mph; Cruise speed: 130 mph; Stall speed: 50 mph; Climb rate: 3,500 fpm; Service ceiling: 14,000 ft.; Takeoff run: 350 ft.; Landing roll: 800 […]

STANDARD DATA: Gross weight: 1,520 lbs.; Empty weight: 875 lbs.; Fuel capacity: 25 gals.; Wingspan: 21 ft. 8 in.; Length: 18 ft. 11 in.; Engine: 180 hp Lycoming. PERFORMANCE: Cruise speed: 123 mph; Range: 400 nm. The Acro II, a two-place larger version of the single-place Acro-Sport, can be constructed for little more than its […]

STANDARD DATA: Gross weight: 1,350 lbs. Empty weight: 884 lbs.; Fuel capacity: 20 gals.; Wingspan: 19 ft. 7 in.; Length: 17 ft. 6 in.; Engine: 200 hp Lycoming. PERFORMANCE: Top speed: 156 mph; Cruise speed: 135 mph; Stall speed: 50 mph; Climb rate: 3,700 fpm; Service ceiling: 15,000 ft.; Takeoff run: 1,025 ft.; Landing roll: […]

STANDARD DATA: Gross weight: 1,023 lbs.; Emptyweight: 640 lbs.; Fuel capacity: 12 gals.; Wingspan: 20 ft.; Length: 17 ft. PERFORMANCE: Top speed: 125 mph; Cruise speed: 110 mph; Stall speed: 55 mph; Climb rate: 1,000 fpm; Takeoff run: 500 ft.; Landing roll: 550 ft.; Range: 200 nm. The EAA decided in 1955 to develop a […]