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General| Manufacturer | Piper Aircraft |
|---|---|
| Model | Cherokee Cruiser PA-28-140 |
| Engine Type | Lycoming O-320-E2A |
| Horsepower | 150 hp |
| Maximum Takeoff Weight | 2, 150 lb (975 kg) |
| Seating Capacity | 4 |
| Wing Span | 30 ft 0 in |
| Length | 23 ft 3 in |
| Height | 7 ft 3 in |
| Maximum Speed | 123 knots |
| Cruise Speed | 108 knots (124 mph, 200 km/h) |
| Service Ceiling | 14, 300 ft |
| Fuel Capacity | 50 US gallons (189 liters) |
| Rate of Climb | 660 ft/min (3.35 m/s) |
Critical operating limitations for the aircraft.
Normal operating procedures for the aircraft.
Performance data for the aircraft under various conditions.
Actions to take if engine power is lost during takeoff.
Steps to restore engine power or prepare for landing if power is lost in flight.
Procedures for landing the aircraft without engine power.
Procedures for identifying and dealing with fire sources in the aircraft.
Actions to take in case of partial or complete loss of oil pressure.
Steps to take when alternator output is lost.
Detailed information and procedures for determining aircraft weight and CG.
Instructions for using graphs to determine CG range and loading requirements.
Procedures and speeds for normal, short field, and soft field takeoffs.
Recommended airspeeds for best rate and best angle of climb.
Stall characteristics, warning indications, and speeds.
Factors affecting cruising speed and mixture control usage.
Landing checklist, approach speeds, and landing techniques.
Chart showing takeoff distance vs. density altitude.
Chart showing rate of climb vs. density altitude.
Chart showing engine RPM vs. density altitude for different power settings.
Chart showing true airspeed at different altitudes and power settings.
Chart showing stall speed at different gross weights.
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