Bombardier Challenger 601-3A

Overview

The CL-601-3A, with the newer -3A variant of the GE CF34 turbofan engine, made its first flight in September 1986 and was certificated in April 1987 with 134 aircraft delivered through 1993. The Challenger 601-3A has a maximum occupancy of 19, but typical configurations accommodate 10-12 passengers with a deluxe galley and lavatory, and amenities appropriate for the relatively long leg times expected for an aircraft of this class. The GE CF34-3A two-spool, high-bypass ratio turbofans rated at 8,650 lbs. of thrust each at takeoff. Automatic power reserve rating is 9,140 lbs. thrust each. Inspection interval on the engines is 6,000 hours.


Aircraft Specifications


Certified Crew

2

Typical / Maximum Cabin Passenger Capacity

11/19

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 CF34-3A

Years Aircraft Manufactured

1987-1993

Estimated Retail Price Low

1,670,000

Estimated Retail Price High

2,400,000

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 601-3A has a range of 3,291 nautical miles. Type in your city or airport identifier for a visual representation of the NBAA IFR Range (NM) for this aircraft.


Legend