BEECHCRAFT King Air C90
Equipped With:
•
Swept Blade Turbofan Propellers
•
Dual Aft Body Strakes
•
Increased Gross Weight
•
PT6A-28 Engines
5-2
Revision IR: August 15, 2017
Document No. 16-206CGW-28
DESCENT AND LANDING DATA
Holding Time ....................................................................................................................................... 5-37
Descent ................................................................................................................................................ 5-38
Balked Landing Climb ......................................................................................................................... 5-39
Landing Distance Without Reversing ................................................................................................. 5-40
INTRODUCTION
The performance of all Beechcraft King Air C90 airplanes equipped with the Raisbeck Increased Gross
Weight System will perform to the graphs and charts in this section, up to a maximum takeoff gross weight of
10,500 lbs and a maximum landing weight of 9,700 lbs.
Federal Aviation Regulations for this class aircraft require only that the all-engines operating distance over a
50 foot height be presented for take-off distance. We include for your information accelerate-go, accelerate-
stop, climb-limited weight, net climb gradient, and other FAR 25 transport category information. For data not
shown in this section, refer to the Performance section of the Beechcraft POH.
Takeoff RPM has been reduced to 1900 RPM, with maximum torque increased to 1520 ft-lbs for all flight
conditions.
