Beechcraft King Air A100

Overview

In 1969, Beech introduced the Model 100 King Air. It featured a 4.2ft. stretch of the -90's fuselage to allow high density seating for 15 persons, a new wing with reduced span derived from the wing of the Model 99 Airliner, and enlarged rudder surfaces. In October 1972 Beech began deliveries of the A100 incorporating a series of detail refinements, including four-bladed propellers which significantly decreased cabin noise levels. The King Air A100 is powered by a pair of Pratt & Whitney Canada PT6A-28 turboprop engines each rated at 680shp, driving four-bladed Hartzell full-feathering, reversible, constant-speed propellers. Inspection interval on the engines is 3,600 hours.


Aircraft Characteristics


Certified Crew
1
Typical / Maximum Cabin Passenger Capacity
8/10
Balanced Field Length [SL/ISA TMP] (FT)
3200
Length (FT)
39.9
Wingspan (FT)
45.9
Height (FT)
15.4
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-28

General Information


Years Aircraft Manufactured
1972-1979
Estimated Retail Price Low
262,000
Estimated Retail Price High
400,000
Aircraft Category
ME TP < 12,500 LBS

Operating Cost Overview

Welcome to PlaneFastFacts©. Aircraft variable and fixed costs are important to determine before making a purchase decisions or planning annual budgets. Our interactive graphs demonstrate the relationships between fuel cost and annual flight hour utilization.


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Range Map

The Beechcraft King Air A100 has a range of 1,117 nautical miles. Type in your city or airport identifier for a visual representation of the NBAA IFR Range (NM) for this aircraft.


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