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KING AIR C90
Supplement manual
Beechcraft KING AIR C90 Supplement Manual
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Table Of Contents
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Contents
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Table of Contents
Table of Divisions
Propellers
Power Plant Limitations
Engine Operating Limits
Propeller Data
Propeller Rotational Speed Limits
Airspeed Limitations
Emergency Procedures
Engine Failure During Take-Off
Electrothermal Propeller De-Ice
Simulating Engine Failures
After Starting Engines
Icing Flight
Noise Characteristics
Section V Normal Procedures
Performance
Descent and Langing Data
Stall Speeds - Zero Thrust
Minimum Take-Off Power at 2200 RPM
Take-Off Climb Gradient - One Engine Inoperative
Maximum Take-Off Weight - Flaps up
Take-Off Distance - 0% Flaps - Two Engines
Accelerate-Stop Distance
Accelerate-Go Distance
Climb - Two Engines - Flaps up
Climb - One Engine Inoperative - Flaps up
Service Ceiling - One Engine Inoperative
Time, Fuel & Distance to Cruise Climb
Normal Cruise Power Settings at 1750 RPM
Normal Cruise Speeds 1750 RPM Weight 8500 LBS
Fuel Flow at Normal Cruise Power 1750 RPM
Range Profile - Normal Cruise Power - 1750 RPM
Endurance Profile - Normal Cruise Power - 1750 RPM
Maximum Cruise Power Settings at 1750 RPM
Maximum Cruise Speeds - 1750 RPM
Fuel Flow at Maximum Cruise Power - 1750 RPM
Range Profile - Maximum Cruise Power
Endurance Profile - Maximum Cruise Power
Descent and Landing Data
Holding Time
Time, Fuel and Distance to Descend
Climb - Balked Landing
Landing Distance Without Propeller Reversing - Flaps 100%
Weight and Balance
Empty Weight Changes
Center-Of-Gravity Limits
System Description
Optional 1600 RPM Minimum Cruise
Dual Aft Body Strakes
Ice Protection Systems
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Table of Divisions
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Propellers
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Power Plant Limitations
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Engine Operating Limits
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Performance
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King air c90a
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