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 Specifications


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

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

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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