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Welcomes the user and introduces the purpose of the supplement.
Details engine operating limits, torque, ITT, and RPM.
Lists maximum operating speed and minimum control speed.
Procedure for engine failure during takeoff with Magicam.
Information on propeller de-ice system operation and readings.
Procedures for propeller de-ice system during icing conditions.
Recommendations for minimizing noise impact near sensitive areas.
Overview of takeoff and climb performance parameters.
Chart showing stall speeds based on weight and bank angle.
Chart for accelerate-stop performance data.
Table of normal cruise power data for ISA -30°C.
Table of maximum cruise power data for ISA -30°C.
Chart for calculating holding time based on fuel and altitude.
Chart for landing distance without propeller reverse.
Graph showing CG limits for specific aircraft serial numbers.
Description of the propeller system.
Details the propeller electric de-ice system.
General| Manufacturer | Beechcraft |
|---|---|
| Model | KING AIR C90 |
| Crew | 1-2 |
| Wingspan | 50 ft 3 in (15.32 m) |
| Max Takeoff Weight | 10, 100 lb (4, 581 kg) |
| Powerplant Output | 550 shp (410 kW) each |
| Service Ceiling | 30, 000 ft (9, 144 m) |
| Category | Turboprop |
| Length | 35 ft 6 in (10.82 m) |
| Height | 14 ft 3 in (4.34 m) |
| Engines | 2 |
| Fuel Capacity | 384 US gallons |
| Range | 1, 321 nautical miles (1, 520 miles, 2, 447 km) |
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