Single-Engine Aircraft

The single-engine aircraft has remained throughout the history of aviation as the preeminent platform for airframe design. In the beginning, one engine was the logical choice for weight considerations. Also, engine technology was not advanced to the point of providing decent power-to-weight ratios that were attractive for the flying machines of that time. As engine power technology continued to develop, manned, powered flight and the single-engine aircraft were a natural combination as an economical and practical mode of personal transportation. For the sportsman aviator in today’s world, it has remained the logical choice.

DIAMOND AIRCRAFT DA-40 DIAMOND STAR

STANDARD DATA: (DA-40) Seats 4. Gross wt. 2,535 lbs. Empty wt. 1,641 lbs. Fuel capacity 41 gallons. Engine 180-hp Lycoming IO-360-M1A. PERFORMANCE: Cruise 145 kts. Stall 49 kts. Initial climb rate 1,070 fpm. Takeoff distance (50′) 1,150′. Landing distance (50′) 1,190′. Building on the success of the Katana C1, Diamond began development of the four […]

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