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Bombardier Learjet 25 (25/25B/25C), exterior
Light JetOut of production

Gates Learjet

Passengers
8

01 · Basic info

Bombardier Learjet 25 (25/25B/25C)

Stretched development of the Learjet 24 with a fuselage 1.27 m longer, allowing up to eight passengers, powered by two General Electric CJ610 turbojets. The Model 25 first flew on 12 August 1966 and was first delivered in November 1967; the improved 25B and 25C (the latter with greater fuel capacity) were certified on 4 September 1970. This record covers these early versions; the later Learjet 25D is listed separately.

Manufacturer
Gates Learjet
Class
Light Jet
Production
Out of production
First delivery
1967
Engines
2 × General Electric CJ610-6
Bombardier Learjet 25 (25/25B/25C), exterior

Photo: Aeroprints.com · Wikimedia Commons · CC BY-SA 3.0

02 · Specifications

Technical data

Capacity

Flight crew
2
Seats (maximum)
8

External dimensions

Length
47.58 ft
Height
12.25 ft
Wingspan
35.58 ft

Powerplant

Engines
2 × General Electric CJ610-6
Thrust (each)
2,950 lbf

Manufacturer-published or publicly documented type data, for orientation only. Figures vary with configuration, serial number, modifications and operating conditions. Not for flight planning. Values not publicly documented are omitted.

03 · Cabin layout

Cabin plan & cross-section

Cross-section data not published

Cabin width

–

Cabin height

–

Cabin length 21.41 ft
Passenger cabinGalley / lavatoryBaggageEntrySchematic · indicative layout · not to scale
  • Club seating
  • Seating
  • Lavatory
  • Baggage

04 · Range map

Where the Learjet 25 (25/25B/25C) can fly nonstop

Range data has not been published for this model.

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