Bombardier Learjet 25
Overview
The Bombardier Learjet 25 is a business aviation aircraft manufactured by Bombardier, with the profile centered on its business jet role. It first flew in 1966 and entered service in 1967. The current production-status field is listed as In Production. The listed configuration provides for a crew of 2 and passenger capacity of 8. Power is provided by 2 General Electric CJ610 engines. Recorded dimensions include length 47.6 ft, wingspan 35.6 ft, height 12.3 ft. Maximum takeoff weight is listed as 15,000 lb. Listed performance includes cruise speed 465 kt, range 1438 nautical miles, service ceiling 51000 ft. Its ICAO type designator is LJ25. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
Specifications
| ICAO Type Code | LJ25 |
|---|---|
| First Flight | 1966 |
| Introduction Date | 1967 |
| Crew | 2 |
| Passenger Capacity | 8 |
| Length | 47.6 ft |
| Wingspan / Rotor Diameter | 35.6 ft |
| Height | 12.3 ft |
| Empty Weight | 7640 lb |
| Max Takeoff Weight | 15,000 lb |
| Cruise Speed | 465 kt |
| Range | 1438 nm |
| Service Ceiling | 51000 ft |
| Engine Manufacturer | General Electric |
| Engine Model | CJ610 |
| Engine Count | 2 |
Data verification status: Partially Verified