Bombardier Challenger 601-1A

Overview

The Challenger 601-1A represents a considerable advancement over the original Challenger 600. When the first Challenger 601 was certificated in March 1983, the most notable improvement was the replacement of the 600's troublesome Lycoming ALF 502 engines with the far more reliable GE CF34 series engines. The 601 benefited from drag-reducing winglets and additional fuel capacity, which along with the new GE engines increased the aircraft's range to over 3,000 nm. The Challenger 601-1A is typically configured for eight to twelve passengers with a deluxe galley and full lavatory, but the aircraft can accommodate as many as nineteen in a high-density configuration.


Aircraft Specifications


Certified Crew

2

Typical / Maximum Cabin Passenger Capacity

9/19

Balanced Field Length [SL/ISA TMP] (FT)

5400

Length (FT)

68.4

Wingspan (FT)

64.3

Height (FT)

20.7

Cabin Height (FT)

6.1

Cabin Width (FT)

8.2

Cabin Length (FT)

28.3

Baggage Capacity Internal / External (CFT)

115/0

Powerplant

2 GE CF34-1A

Years Aircraft Manufactured

1983-1987

Estimated Retail Price Low

1,100,000

Estimated Retail Price High

1,600,000

Aircraft Category

JET > 20,000 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 Bombardier Challenger 601-1A has a range of 3,440 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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