Bombardier Learjet 24F

Overview

When development of the improved model 24 was undertaken, the decision was made to forgo single-pilot operation in favor of higher operating weights. Thus the Learjet 24, which accomplished its first flight in February 1966, was certificated under the FAR Part 25 transport category with a maximum takeoff weight of 13,500 lbs. It was powered by the same General Electric CJ610-4 turbojets that had been used on the model 23. Seating for five passengers consists of a bench seat across the aft cabin, two forward-facing seats ahead of that, and a single side-facing seat backed against the starboard sidewall. The refreshment center is diminutive and baggage space is limited to a rear compartment behind the fold-down bench seat, accessible only from inside the cabin.


Aircraft Specifications


Certified Crew

2

Typical / Maximum Cabin Passenger Capacity

6/6

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

3297

Length (FT)

43.3

Wingspan (FT)

35.6

Height (FT)

12.3

Cabin Height (FT)

4.3

Cabin Width (FT)

4.9

Cabin Length (FT)

9

Baggage Capacity Internal / External (CFT)

0/0

Powerplant

2 GE CJ610-8A

Years Aircraft Manufactured

1976-1979

Estimated Retail Price Low

175,000

Estimated Retail Price High

265,000

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 Learjet 24F has a range of 1,014 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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