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		 =     Raytheon Beechcraft     =
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		 =     King Air  Model 350     =
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		 =  Version 3  - 19 June 1998  =
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 Designed by: Barry Blaisdell (barrywb@compuserve.com)
	
 Visit my web site at: http://www.propanels.simflight.com/bwbfiles

 NOTAM: This aircraft is in FS98 Format.

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 Aircraft Data:

 The Super King Air 350 is powered by 2 P&W Canada
 PT6A-60A Turbo Shaft Engines rated at 1,050 shp,
 each driving Hartzell 4 blade constant speed, fully
 feathering, pitch reverseible metal propellers,
 landing lights and polished spinners.

 Wing span....................58 ft.
 Length overall...............47 ft.
 Overall Height...............15 ft.
 Max cruise speed.............311 kts 
 Normal Cruise speed..........290 kts 
 Service Ceiling..............21,500 ft.
 Rate of Climb @ MTOW.........800 fpm
 Runway length T/O............3,300 ft
 Runway length Landing........2,630 ft.
 Clean stall..................99 kts.
 Dirty stall (flaps & gear)...81 kts.
 Max. Take Off Wt (MTOW)......15,000 lbs.          
 Max. Range...................1067 nm
 Range with full load.........1,252 nm
 Total Usable Fuel............540 US Gallons
        

 Typical Cruise Data: Altitude 9,100 ft.
 (for reference only)

 CRUISE	 KIAS   FF-PPH  Torque
 Economy  197     400    66%
 Normal   218     520    72%
 High     246     700    80%


 Additional aerodynamic tuning by Steve Hallquist
 N618BD <SteveH44@ix.netcom.com> and Bill Walch
 <wwce@snet.net> by permission of author. 8 July 98.