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General| Engine | Lycoming O-360-A4M |
|---|---|
| Horsepower | 180 hp |
| Height | 7 ft 3 in (2.21 m) |
| Maximum Takeoff Weight | 2, 550 lb (1, 157 kg) |
| Fuel Capacity | 50 US gal (189 l) |
| Seats | 4 |
| Length | 24 ft |
| Cruise Speed | 128 knots |
| Range | 522 nm (601 mi, 967 km) |
| Rate of Climb | 720 ft/min (3.7 m/s) |
| Stall Speed (Flaps Down) | 49 knots |
Specifications and details of the aircraft's engine.
Specifies critical airspeeds for safe aircraft operation.
Defines the forward and rearward CG limits for normal and utility categories.
Details limitations and requirements for the G1000 avionics system.
Provides checklists for various emergency procedures.
Outlines procedures for handling alternator and complete electrical failures.
Detailed steps for preflight inspection of the aircraft.
Procedures for normal and short field takeoff techniques.
Outlines how to calculate loaded weight and CG for flight.
Overview of the Garmin G1000 integrated avionics system components.
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