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General| Manufacturer | Piper Aircraft |
|---|---|
| Model | PA-28-180 |
| Engine | Lycoming O-360-A4A |
| Horsepower | 180 hp |
| Seating Capacity | 4 |
| Wingspan | 30 ft (9.1 m) |
| Height | 7 ft 3 in |
| Service Ceiling | 14, 300 ft |
| Maximum Takeoff Weight | 2, 400 lbs |
| Fuel Capacity | 50 US gal (190 L) |
| Rate of Climb | 720 ft/min |
| Cruise Speed | 140 mph |
Details aircraft performance metrics like takeoff, climb, speed, range, and fuel consumption.
Specifies aircraft weight parameters including gross, empty, and useful load.
Details the aircraft's engine specifications, including type, horsepower, and dimensions.
Outlines fuel and oil capacities and required fuel grade.
Provides a comprehensive checklist for pre-flight aircraft inspection.
Details the step-by-step procedure for starting the aircraft engine.
Covers essential checks of the engine and systems while on the ground.
Details the take-off technique and pre-takeoff checks.
Lists stall speeds for various bank angles and flap configurations.
Details the approach speed, flap usage, and landing technique.
Describes the correct procedure for shutting down the aircraft engine after landing.
Outlines procedures to follow in case of engine power loss.
Details actions to take in case of engine power loss during takeoff.
Provides procedures for engine power loss that occurs in flight.
Outlines the procedure for conducting a power-off landing.
Details procedures to follow in case of electrical or engine fires.
Explains procedures to follow when experiencing a loss of oil pressure.
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