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General| Manufacturer | Pacific Aerospace |
|---|---|
| Model | PAC 750XL |
| Type | Utility Aircraft |
| Crew | 1 |
| Max takeoff weight | 3, 402 kg (7, 500 lb) |
| Powerplant | 1 × Pratt & Whitney Canada PT6A-34 turboprop, 560 kW (750 shp) |
Details total, usable, and unusable fuel volumes across different tanks.
Lists approved aviation fuels with ice inhibitor notes.
Specifies maximum takeoff and landing weights for the aircraft.
Provides basic empty weight and maximum useful load figures.
Details standard engine, propeller, and fuel system components.
Covers fuselage, wings, fin, rudder, and horizontal stabilizer construction.
Explains standard flight controls and avionics equipment.
Lists optional avionics, communication, and navigation equipment.
Includes engine monitoring, skydiving config, and autopilot systems.
Details optional flight instruments and passenger seating.
Covers max altitude, stall speeds, maneuvering and flap speeds.
Details takeoff distances and landing distance over obstacle.
Specifies climb times, cruise speeds, range, and endurance.
Details best rate/angle of climb and maximum demonstrated crosswind.
Aircraft certified to FAR Part 23, lists max operating and maneuvering speeds.
Specifies flap deployment speeds and flight load factor limits.
Details the simple, robust, all-metal, riveted stressed skin construction.
Covers 24 months/500 hours, material/workmanship defects, and exclusions.
Warranty for parts not made by manufacturer depends on their manufacturer's warranty.
Modifications by authorities do not make parts defective; proper notice for defects required.
Purchaser must notify defects promptly and send parts for inspection at own cost.
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