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N2132W - C172SP
The Skyhawk SP aircraft is an all-metal, single-engine piston, high-wing monoplane with a four-person seating capacity including a crew of one or two. Suitable allowance for luggage is provided.
All information herein applies to the Skyhawk SP (Model 172S).
The Model 172S is certified to the requirements of U.S. FAA Federal Aviation Regulation Part 23 through amendment 23-6, including day, night, VFR and IFR.
Performance
All estimated performance data are based on airplane weights at 2,550 pounds; standard atmospheric conditions; level, hard-surface, dry runways; and no wind. They are calculated values derived from flight tests conducted by Cessna Aircraft Company under carefully documented conditions and will vary with individual airplanes, pilots, and numerous factors affecting flight performance.
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English |
Metric |
| Cruise (45% power @ 10000') |
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| range |
638nm |
1182km |
| duration |
6.72hr |
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| Cruise (75% power @8500') |
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| range |
518nm |
959km |
| duration |
4.26hr |
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| Engine: Textron Lycoming IO-360-L2A |
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| 180 BHP @ 2700 RPM |
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| Propeller: 2 blade fixed pitch diameter: |
76in. |
1.93m |
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| Rate of climb (sea level): |
730ft/min |
223m/min |
| Service Ceiling: |
14000' |
4267m |
| Speed |
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| Max at sea level |
126kts. |
233kph |
| Cruise (75% power @ 8500') |
124kts |
230kph |
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| Stall Speed, CAS |
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| Flaps Up, power off |
53kts |
98kph |
| Flaps Down, power off |
48kts |
89kph |
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| Takeoff Performance |
960ft |
293m |
| Total distance over 50' obstacle |
1630ft |
497m |
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| Landing Performance |
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| Ground Roll |
575' |
175m |
| Total distance over 50' obstacle |
1335' |
407m |
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| Wing Loading |
14.7lb/sq. ft. |
71.8kgm/sq. m. |
| Power Loading |
14.2lb/hp |
6.4kg/hp |
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