Aircraft Performance Specifications
This information is provided as a guide "at users risk" and is not intended for flight planning purposes! Please consult the relevant Pilots Operating Handbook prior to flight.
177 B Cardinal |
| CESSNA AIRCRAFT CORPORATION | Serial numbers 17701371 through 17702123 |
| General Information |
 1971 177B Owned by the Flying Pigs Partnership Pipestone, Minnesota. | ||
|---|---|---|---|
| Engine Make: | Lycoming 180hp | ||
| Engine Model: | O-360-A1F6 | ||
| Propeller Type: | McCauley Constant Speed | ||
| Power (HP or Lbs Thrust): | 180 | ||
| Engine TBO: | 2000 | ||
| S P E E D S | MPH | KTS | KPH | ||||
|---|---|---|---|---|---|---|---|
| Maximum Cruising Speed | 153 | 132 | 244 | ||||
| Recommended Cruising Speed | 142 | 123 | 227 | ||||
| Stalling Speed | 53 | 46 | 85 | ||||
| F U E L C A P A C I T Y | Lbs | US Gals | Litres | ||||
|---|---|---|---|---|---|---|---|
| Standard Fuel | 330 | 50 | 189 | ||||
| Long Range Version | 0 | 0 | 0 | ||||
| W E I G H T S | US Lbs | Kilos | |||||
|---|---|---|---|---|---|---|---|
| Gross Weight | 2500 | 1133 | |||||
| Empty Weight | 1485 | 673 | |||||
| Max Useful Load | 1015 | 460 | |||||
| Max Useful w/Full Fuel | 685 | 310 | |||||
| R A N G E (No Reserve) | SM | NM | KM | Hrs | |||||
|---|---|---|---|---|---|---|---|---|---|
| Max Range - Std Cruise | 850 | 733 | 1356 | 6 | |||||
| C E I L I N G S | Feet | Meters | |||
|---|---|---|---|---|---|
| Max Service Ceiling | 14600 | 4449 | |||
| 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 | 840 | 256 | |||
| 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 | 750 | 228 | |||
| TakeOff Over 50ft/15meter Obstacle, Sea Level, Gross Weight | 1400 | 426 | |||
| Landing Ground Roll, Sea Level, Gross Weight | 600 | 182 | |||
| Landing Over 50ft/15meter Obstacle, Sea Level, Gross Weight | 1220 | 371 | |||
| A I R C R A F T D I M E N S I O N S | Feet | Meters | |||||
|---|---|---|---|---|---|---|---|
| Fuselage Length: 1970-71 (approx.) | 27 | 8.0 | |||||
| Fuselage Length: 1972-74 (approx.) | 27.3 | 8.32 | |||||
| Fuselage: 1970-71 (usually tail section) Height (approx.) | 8.7 | 2.65 | |||||
| Fuselage: 1972-74 (usually tail section) Height (approx.) | 9.2 | 2.45 | |||||
| Total Wingspan (approx.) | 35.6 | 10.85 | |||||