172 K, L |
| CESSNA AIRCRAFT CORPORATION | Float Plane configuration. |
| General Information |
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|---|---|---|---|
| Engine Type: | Piston | ||
| Engine Make: | Lycoming 150hp | ||
| Power (HP or Lbs Thrust): | 150 | ||
| Engine TBO: | 2000 | ||
| S P E E D S | MPH | KTS | KPH | ||||
|---|---|---|---|---|---|---|---|
| Maximum Cruising Speed | 108 | 93 | 172 | ||||
| Recommended Cruising Speed | 106 | 92 | 170 | ||||
| Stalling Speed | 52 | 45 | 83 | ||||
| F U E L C A P A C I T Y | Lbs | US Gals | Litres | ||||
|---|---|---|---|---|---|---|---|
| Standard Fuel | 277 | 42 | 159 | ||||
| Long Range Version | 343 | 52 | 196 | ||||
| W E I G H T S | US Lbs | Kilos | |||||
|---|---|---|---|---|---|---|---|
| Gross Weight | 2220 | 1006 | |||||
| Empty Weight | 1405 | 637 | |||||
| Max Useful Load | 815 | 369 | |||||
| Max Useful w/Full Fuel | 538 | 243 | |||||
| R A N G E | SM | NM | KM | Hrs | |||||
|---|---|---|---|---|---|---|---|---|---|
| Max Range - Std Cruise | 481 | 417 | 772 | 4.54 | |||||
| C E I L I N G S | Feet | Meters | |||
|---|---|---|---|---|---|
| Max Service Ceiling | 12000 | 3657 | |||
| Max Engine Out Ceiling | 0 | 0 | |||
| C L I M B R A T E S | Feet P/Min | Meters P/Min | |||
|---|---|---|---|---|---|
| Max Climb, Sea Level, Gross Weight | 580 | 176 | |||
| Max Climb, Engine Out, Sea Level, Gross Weight | 0 | 0 | |||
| T A K E O F F & L A N D I N G D I S T A N C E S | Feet | Meters | |||
|---|---|---|---|---|---|
| TakeOff Ground Roll, Sea Level, Gross Weight | 1620 | 493 | |||
| TakeOff Over 50ft/15meter Obstacle, Sea Level, Gross Weight | 2390 | 728 | |||
| Landing Ground Roll, Sea Level, Gross Weight | 590 | 179 | |||
| Landing Over 50ft/15meter Obstacle, Sea Level, Gross Weight | 1345 | 409 | |||
| A I R C R A F T D I M E N S I O N S | Feet | Meters | |||||
|---|---|---|---|---|---|---|---|
| Fuselage Length (approx.) | 26.7 | 8.14 | |||||
| Fuselage (usually tail section) Height (approx.) | 10 | 3.05 | |||||
| Total Wingspan (approx.) | 35.9 | 10.94 | |||||