T-182 Q II Turbo Skylane |
| CESSNA AIRCRAFT CORPORATION |
| General Information |
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|---|---|---|---|
| Engine Type: | Piston | ||
| Engine Make: | Lycoming 235hp | ||
| Power (HP or Lbs Thrust): | 235 | ||
| Engine TBO: | 2000 | ||
| S P E E D S | MPH | KTS | KPH | ||||
|---|---|---|---|---|---|---|---|
| Maximum Cruising Speed | 193 | 167 | 309 | ||||
| Recommended Cruising Speed | 181 | 157 | 290 | ||||
| Stalling Speed | 56 | 48 | 88 | ||||
| F U E L C A P A C I T Y | Lbs | US Gals | Litres | ||||
|---|---|---|---|---|---|---|---|
| Standard Fuel | 607 | 92 | 348 | ||||
| Long Range Version | 0 | 0 | 0 | ||||
| W E I G H T S | US Lbs | Kilos | |||||
|---|---|---|---|---|---|---|---|
| Gross Weight | 3100 | 1405 | |||||
| Empty Weight | 1781 | 807 | |||||
| Max Useful Load | 1319 | 598 | |||||
| Max Useful w/Full Fuel | 712 | 322 | |||||
| R A N G E | SM | NM | KM | Hrs | |||||
|---|---|---|---|---|---|---|---|---|---|
| Max Range - Std Cruise | 855 | 742 | 1374 | 4.72 | |||||
| C E I L I N G S | Feet | Meters | |||
|---|---|---|---|---|---|
| Max Service Ceiling | 20000 | 6095 | |||
| 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 | 965 | 294 | |||
| 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 | 790 | 240 | |||
| TakeOff Over 50ft/15meter Obstacle, Sea Level, Gross Weight | 1475 | 449 | |||
| Landing Ground Roll, Sea Level, Gross Weight | 590 | 179 | |||
| Landing Over 50ft/15meter Obstacle, Sea Level, Gross Weight | 1350 | 411 | |||
| A I R C R A F T D I M E N S I O N S | Feet | Meters | |||||
|---|---|---|---|---|---|---|---|
| Fuselage Length (approx.) | 28.5 | 8.69 | |||||
| Fuselage (usually tail section) Height (approx.) | 9.3 | 2.83 | |||||
| Total Wingspan (approx.) | 35.1 | 10.7 | |||||