Bombardier Learjet 25D

Overview

The Learjet 25 was originally powered by a pair of General Electric CJ610-4 turbojets engines rated at 2,850lbs of thrust each. Later variants included the 25D and 25G, powered by the CJ610-8A engine rated at 2,950lbs. of thrust each. Inspection interval on the -8A engines is 5,000 hours. The Learjet 25D is normally configured for six passengers in a seating arrangement consisting of four individual forward facing seats, and a full-width bench seat aft of these.


Aircraft Specifications

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Aircraft Characteristics


Certified Crew
2
Typical / Maximum Cabin Passenger Capacity
7/10
Take Off Ground Roll (FT)
0
Landing Ground Roll (FT)
0
Balanced Field Length [SL/ISA TMP] (FT)
3,937
Maximum Fuel (GL)
0
Length (FT)
47.6
Wingspan (FT)
35.6
Height (FT)
12.3
Cabin Height (FT)
4.3
Cabin Width (FT)
4.9
Cabin Length (FT)
12.1
Baggage Capacity Internal / External (CFT)
0/0
Powerplant
2 GE CJ610-8A

General Information


Years Aircraft Manufactured
1971-1976
Estimated Retail Price Low
115,000
Estimated Retail Price High
185,000
Aircraft Category
JET < 20,000 LBS

Operating Cost Overview

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Range Map

The Bombardier Learjet 25D has a range of 1,014 nautical miles. You can use the map below to visual this range from a particular airport...


Legend


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