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


Certified Crew

2

Typical / Maximum Cabin Passenger Capacity

7/10

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

3937

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

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

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.



$
hrs


If you are further along in the aircraft buying process, our comprehensive aircraft operating cost reports are the perfect companion in your decision making process. View a sample or buy a report and have it available in minutes.




Range Map

The Bombardier Learjet 25D 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.


Legend