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 Characteristics


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

General Information


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

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 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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