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General| Manufacturer | Piper Aircraft |
|---|---|
| Model | AZTEC D PA-23-250 |
| Number of Engines | 2 |
| Rate of Climb | 1, 400 ft/min (7.1 m/s) |
| Maximum Takeoff Weight | 5, 200 lb (2, 359 kg) |
| Seating Capacity | 6 |
| Horsepower | 250 hp |
| Fuel Capacity | 144 US gallons (545 liters) |
| Cabin Width | 4.1 feet |
| Wingspan | 37.2 feet |
Detailed performance data including speeds, rates, and ceilings for the aircraft.
Essential safety checks and inspection procedures before flight operations.
Procedures for starting aircraft engines under cold, hot, and flooded conditions.
Steps for engine warm-up and system checks, including oil pressure verification.
Procedures and checklist items required for a safe aircraft take-off.
Procedures for safe approach and landing, including a landing checklist.
Steps to properly shut down aircraft engines after landing and parking.
Actions to take in case of in-flight emergencies, such as engine failure or feathering.
Chart for calculating take-off distance required to clear a 50-foot obstacle.
Chart showing the relationship between density altitude and take-off distance.
Chart for determining the distance required to accelerate and stop the aircraft.
Charts detailing climb performance data for multi-engine operations.
Charts detailing climb performance data for single-engine operations.
Chart illustrating the impact of aircraft weight on stall speed.
Chart illustrating the impact of bank angle on stall speed.
Chart for calculating landing distance required to clear a 50-foot obstacle.
Chart showing the relationship between density altitude and landing distance.
Chart detailing engine power output versus altitude, RPM, and manifold pressure.
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