Bombardier Challenger 604
Overview
The Bombardier Challenger 604 is a business aviation aircraft manufactured by Bombardier, with the profile centered on its executive transport role. It first flew in 2016-10-08 and entered service in 1995. Production is recorded as ending in 2005. The listed configuration provides for a crew of 2 and passenger capacity of 9-12. Power is provided by 2 Honeywell HTF7700L engines. Recorded dimensions include length 73 ft 10 in, wingspan 68 ft 5 in, height 20.7 ft. Maximum takeoff weight is listed as 47600 lb. Listed performance includes cruise speed Mach 0.80 kt, range ~3500 nm nautical miles, service ceiling 41000 ft. Its ICAO type designator is CL60. 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 | CL60 |
|---|---|
| First Flight | Oct 8, 2016 |
| Introduction Date | 1995 |
| Crew | 2 |
| Passenger Capacity | 9-12 |
| Length | 73 ft 10 in |
| Wingspan / Rotor Diameter | 68 ft 5 in |
| Height | 20.7 ft |
| Max Takeoff Weight | 47600 lb |
| Cruise Speed | Mach 0.80 |
| Range | ~3500 nm |
| Service Ceiling | 41000 ft |
| Engine Manufacturer | Honeywell |
| Engine Model | HTF7700L |
| Engine Count | 2 |
Data verification status: Partially Verified