Beechcraft King Air 300LW

Overview

The 300LW model was developed as a “Light Weight” version in this long running and successful line of corporate and utility transports. The max weight was reduced for the 300LW, intended to minimize the effects of weight based airways user fees, particularly in Europe. The King Air 300LW is powered by a pair of Pratt & Whitney Canada PT6A-60A turboprop engines rated at 1,050 shp each, driving four blade, full feathering, reversible constant speed propellers. Engine inspection interval is 3,600 hours.


Aircraft Specifications

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Aircraft Characteristics


Certified Crew
1
Typical / Maximum Cabin Passenger Capacity
7/10
Take Off Ground Roll (FT)
0
Landing Ground Roll (FT)
0
Balanced Field Length [SL/ISA TMP] (FT)
1,686
Maximum Fuel (GL)
0
Length (FT)
43.8
Wingspan (FT)
54.5
Height (FT)
14.3
Cabin Height (FT)
4.8
Cabin Width (FT)
4.5
Cabin Length (FT)
16.7
Baggage Capacity Internal / External (CFT)
55/0
Powerplant
2 P&WC PT6A-60A

General Information


Years Aircraft Manufactured
1991-1994
Estimated Retail Price Low
643,000
Estimated Retail Price High
1,300,000
Aircraft Category
ME TP < 12,500 LBS

Operating Cost Overview

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hrs

Range Map

The Beechcraft King Air 300LW has a range of 977 nautical miles. You can use the map below to visual this range from a particular airport...


Legend


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