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General| Manufacturer | Piper Aircraft |
|---|---|
| Model | Cherokee 140 |
| Engine | Lycoming O-320-E2A |
| Horsepower | 150 hp |
| Service Ceiling | 14, 300 ft (4, 400 m) |
| Empty Weight | 1, 201 lb (545 kg) |
| Gross Weight | 2, 150 lb (975 kg) |
| Maximum Takeoff Weight | 2, 150 lb (975 kg) |
| Useful Load | 949 lb (430 kg) |
| Rate of Climb | 660 ft/min (3.4 m/s) |
| Seating | 4 |
| Wingspan | 30 ft |
| Length | 23 ft 3 in |
| Height | 7 ft 3 in |
| Range | 455 nautical miles |
| Fuel Capacity | 50 gallons |
| Cruise Speed | 115 knots |
Key aircraft operating parameters, speeds, and climb rates at different weights and altitudes.
Details on gross weight, empty weight, and useful load for standard and AutoFlight configurations.
Essential visual inspection steps to perform before each flight for safety.
Step-by-step instructions for safely starting the aircraft engine in various conditions.
Procedures for warming up the engine and checking oil pressure post-start.
Checks to be performed while the aircraft is on the ground before take-off.
Guidance on conventional and short/soft field take-off procedures.
Techniques for approach speed, flap usage, and landing.
Charts showing take-off distance required based on density altitude and gross weight.
Charts illustrating the rate of climb as a function of density altitude.
Graphs showing true airspeed at different power settings and density altitudes.
Charts to estimate the aircraft's range based on altitude and fuel load.
Charts detailing landing distance requirements under various conditions.
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