The Cessna 152 is a high wing, single-engine, two seat, tricycle gear airplane based on the design of the popular Cessna 150. The 152 boats a number of design changes over the 150 and has a more powerful engine and is generally a more stable platform for instrument flight.
| *SPEED: | ||
| Maximum at Sea Level | 109 KNOTS | |
| Cruise, 75% Power at 8500 Ft | 106 KNOTS | |
| engine start, taxi, takeoff, climb and 45 minutes | ||
| reserve. | ||
| 75% Power at 8500 Ft | Range | 315 NM |
| 24.5 Gallons Usable Fuel | Time | 3.0 HRS |
| 37.5 Gallons Usable Fuel | Time | 5.2 HRS |
| Maximum Range at 10,000 Ft | Range | 370 NM |
| 24.5 Gallons Usable Fuel | Time | 4.1 HRS |
| Maximum Range at 10,000 Ft | Range | 625 NM |
| 37.5 Gallons Usable Fuel | Time | 6.9 HRS |
| RATE OF CLIMB AT SEA LEVEL | 715 FPM | |
| SERVICE CEILING | 14,700 FT | |
| TAKEOFF PERFORMANCE: | ||
| Ground Roll | 725 FT | |
| Total Distance Over 50-Ft Obstacle | 1340 FT | |
| LANDING PERFORMANCE: | ||
| Ground Roll | 475 FT | |
| Total Distance Over 50-Ft Obstacle | 1200 FT | |
| STALL SPEED (CAS): | ||
| Flaps Up, Power Off | 48 KNOTS | |
| Flaps Down, Power Off | 43 KNOTS | |
| MAXIMUM WEIGHT: | ||
| Ramp | 1675 LBS | |
| Takeoff or Landing | 1670 LBS | |
| STANDARD EMPTY WEIGHT: | ||
| 152 | 1104 LBS | |
| 152 II | 1136 LBS | |
| MAXIMUM USEFUL LOAD: | ||
| 152 | 571 LBS | |
| 152 II | 539 LBS | |
| BAGGAGE ALLOWANCE | 120 LBS | |
| WING LOADING: Pounds/Sq Ft | 10.5 | |
| POWER LOADING: Pounds/HP | 15.5 | |
| FUEL CAPACITY: Total | ||
| Standard Tanks | 26 GAL. | |
| Long Range Tanks | 39 GAL. | |
| OIL CAPACITY | 7 QTS | |
| ENGINE: Avco Lycoming | O-235-L2C | |
| 108 BHP at 2550 RPM | ||
| PROPELLER: Fixed Pitch, Diameter | 69 IN. |
Rates are subject to change.
