Beechcraft King Air 300

Overview

The Super King Air 300 can be configured in a variety of seating arrangements, but is commonly configured for eight passengers in a combination of a club and individual or divan seating. The lavatory is located aft of the main seating, and a large baggage compartment occupies the aft cabin. The Super King Air 300 was granted FAA certification in January 1984, with deliveries beginning in April of the same year. After a production run of 225 aircraft, the King Air 300 was discontinued in 1993 in favor of the larger Super King Air 350. The Super King Air 300 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
7/15
Take Off Ground Roll (FT)
0
Landing Ground Roll (FT)
0
Balanced Field Length [SL/ISA TMP] (FT)
2,208
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
1984-1994
Estimated Retail Price Low
645,000
Estimated Retail Price High
1,300,000
Aircraft Category
ME TP > 12,500 LBS

Operating Cost Overview

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Range Map

The Beechcraft King Air 300 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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