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Manufacturer | Daher |
---|---|
Engine | Pratt & Whitney Canada PT6A-34 |
Service Ceiling | 25, 000 feet |
Seating Capacity | 10 |
Crew | 1-2 |
Range | 1, 132 nautical miles |
Type | Utility aircraft |
Length | 34 feet 2 inches |
Wingspan | 45 feet |
Max takeoff weight | 7, 255 pounds |
Power Output | 750 shp |
Cabin Width | 4 feet 6 inches |
Defines operational speed limits for Vfe, Vmo, and Vo, crucial for flight safety.
Lists maximum ramp, takeoff, landing, zero fuel, and minimum flying weights.
Details forward and aft CG limits, including MAC and datum reference for safe loading.
Lists critical airspeeds for various emergency scenarios like engine failures and landings.
Provides immediate action items for various emergencies like engine failures and fires.
Provides responses for abnormal engine, electrical, trim, flap, and nav system issues.
Addresses ITT, Ng Overspeed, NP Overspeed, Torque, and Dry Motoring Run.
Procedures for landing with flat tires or abnormal environmental system conditions.
A comprehensive checklist covering preflight, engine start, taxi, takeoff, and shutdown procedures.
Detailed checks of cabin, exterior surfaces, and systems before flight.
Procedures for battery and external power engine starts, including critical temperature monitoring.
Procedures for normal and short field takeoffs, including flap settings and rotation speeds.
Procedures for normal, short field, and balked landings, including flap settings and touchdown techniques.
Lists stall speeds based on weight, bank angle, flaps, and CG, with and without ice.
Specifies maximum takeoff weights based on outside air temperature and pressure altitude.
Procedures for calculating total weight, moment, and CG for flight.
Outlines using W&B forms, fuel data, and occupant/cargo weights for calculations.
Illustrates the airplane's center of gravity envelope for safe loading.
Describes primary and standby flight instruments like airspeed, altimeter, and HSI.
Provides descriptions of the PT6A-34 powerplant, controls, instruments, and lubrication system.
Covers the entire fuel system from tanks to engine, including pumps and filters.
Covers engine oil specifications and fuel on-loading procedures.
Procedures for fuel on-loading and manual blending of anti-icing additives.
Outlines operational limits for autopilot and yaw damper, including altitude and speed restrictions.
Procedures for handling autopilot and yaw damper malfunctions, including runaway conditions.