CESSNA SKYHAWK

1997’€“Present

Gemini Sparkle

Key Takeaways:

  • The article provides standard data and performance specifications for the Cessna Skyhawk 172R, a four-seat aircraft with a 160-hp engine, capable of a 122 kts cruise and a 720 fpm climb rate.
  • Cessna re-entered the single-engine piston market in the 1990s with the Skyhawk 172, making modest improvements to an established design.
  • Key modernizations to the Skyhawk 172 included features like leather seats, a quiet cockpit, modern avionics, an all-glass panel introduced in 2004, and optional pilot/copilot airbags from 2005.
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STANDARD DATA: (Model 172R) Seats 4. Gross wt. 2,450. Empty wt. 1,620. Fuel capacity 56 gallons. Engine 160-hp Textron Lycoming IO-360-L2A.
PERFORMANCE: Max Cruise 123 kts. Cruise 122 kts. Stall 47-51 kts. Rate of climb, sea level 720 fpm. Service ceiling 13,500′. Takeoff distance (50′) 1,685. Landing distance (50′) 1,295.

As the general aviation market regained momentum in the 1990s, Cessna re-entered the single engine piston aircraft with the Skyhawk 172. Changes to the new aircraft were modest as the manufacturer sought to improve upon a winning design. Leather seats, a quiet cockpit, and modern avionics led the Skyhawk into the 21st century. In 2004, Cessna introduced the “most popular airplane in the world” with an all glass panel. Optional equipment for 2005 included pilot and copilot airbags.

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