Cessna Cardinal Specs

Cessna produced the Cardinal 177 to replace the 172.

The Cessna 177 Cardinal was introduced in 1967 to replace the Cessna 172 series, a light, general aviation airplane. Several generations of the 177 were produced between 1968 and 1978. Although out of production, it remains a popular touring aircraft.

Background

The Cessna 177 Cardinal incorporated a cantilevered wing with laminar flow airfoil. Early models were underpowered at 150 horsepower (hp). Engines for final versions of the 177 were boosted to 200 hp.

Aircraft Specifications

A Lycoming engine powers the 177. Early top speed of 125 knots later reached 157 knots. The first 177s cruised at 117 knots, final versions at 149. Stall speeds averaged 50 knots for all aircraft. Fuel capacity for all models averages 50 gallons. Flight ranges average 500 nautical miles.

Takeoff Performance

The first 177s required 845 feet of runway for a standard takeoff and 1,575 feet to clear a 50-foot obstacle. Final versions required 890 feet of runway and 1,585 to clear a 50-foot obstacle. Flight ceiling increased from 12,700 feet to 17,100 feet.

Landing Performance

Early models required 400 feet on a runway with no approach obstructions; 1,135 feet were required to clear a 50-foot approach obstacle. Final models needed 730 feet of runway without obstructions and 1,350 feet when clearing a 50-foot obstacle.

References

• Aircraft Guru: Cessna 177 Cardinal
• Pilot Friend: Cessna 177 Cardinal history, performance and specifications
• Cardinal Flyers: Cardinal 177 RG Aircraft Performance Specifications

Resources

• Serving History: Cessna 177: Specifications (Cessna 177B)