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General| Category | Aircraft |
|---|---|
| Manufacturer | Piper Aircraft |
| Model | PA-44-180 Seminole |
| Year | 1979 |
| Number of Engines | 2 |
| Horsepower | 180 hp each |
| Seating Capacity | 4 |
| Max Takeoff Weight | 3, 800 lbs |
| Height | 8 ft 6 in |
| Stall Speed | 60 knots |
| Service Ceiling | 15, 000 ft |
| Length | 27 ft 7 in |
| Rate of Climb | 1, 200 ft/min |
Details engine specifications: manufacturer, model, horsepower, RPM, bore, stroke, displacement, and type.
Specifies fuel capacity, usable fuel, minimum grade, and alternate fuel requirements.
Details maximum takeoff, ramp, landing, and baggage compartment weights.
Specifies critical airspeeds like Maneuvering Speed (VA) at different weights.
Lists limitations for engines, including operating limits, pressures, temperatures, and fuel grades.
Specifies maximum takeoff, ramp, landing weights, and baggage compartment limits.
Provides forward and rearward CG limits based on weight.
States that intentional acrobatic maneuvers are prohibited.
Specifies total fuel capacity, unusable fuel, and usable fuel volumes.
Includes airspeeds for safe operations and engine inoperative procedures.
Details procedures for detecting dead engines and engine securing (feathering).
Covers procedures for engine fires on the ground and in flight.
Provides procedures for managing electrical failures, including ammeter issues and alternator problems.
Lists significant airspeeds for safe operation, including climb and approach speeds.
Provides a checklist for preparation, preflight checks inside and outside the cabin.
Describes normal and short field takeoff procedures, including flap settings and rotation speeds.
Provides recommended climb speeds and power settings for best rate and angle of climb.
Details procedures for traffic pattern, approach speeds, gear and flap settings, and landing techniques.
Lists figures and graphs related to airspeed calibration, stall speeds, takeoff distances, and climb performance.
Outlines steps to determine loaded airplane weight, moment, and CG location for flight.
Details the Lycoming four-cylinder engines, including cooling, oil systems, and counter-rotation.
Describes the hydraulically operated, fully retractable tricycle landing gear system.
Covers fuel storage, grade requirements, pumps, and fuel management controls.
Offers specific safety advice on takeoff, gear retraction, circuit breakers, and fuel management.
