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Expanded Profile

Bombardier Challenger 300

Overview

The Bombardier Challenger 300 is a business aviation aircraft manufactured by Bombardier, with the profile centered on its executive transport role. It first flew in 2001-08-14 and entered service in 2004-01-08. Production is recorded as ending in 2014. The listed configuration provides for a crew of 2 and passenger capacity of 9. Power is provided by 2 Honeywell HTF7000 engines. Recorded dimensions include length 68 ft 8 in, wingspan 63 ft 10 in, height 20 ft 4 in. Maximum takeoff weight is listed as 38850. Listed performance includes cruise speed 470 kt, range 3065 nautical miles, service ceiling 41000 ft. Its ICAO type designator is CL30. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.

Quick Facts

First Flight Aug 14, 2001
Crew 2
Passengers 9
Range 3065 nm
Cruise Speed 470 kt

Specifications

ICAO Type CodeCL30
First FlightAug 14, 2001
Introduction DateJan 8, 2004
Crew2
Passenger Capacity9
Length68 ft 8 in
Wingspan / Rotor Diameter63 ft 10 in
Height20 ft 4 in
Max Takeoff Weight38850 lb
Cruise Speed470 kt
Range3065 nm
Service Ceiling41000 ft
Engine ManufacturerHoneywell
Engine ModelHTF7000
Engine Count2

Data verification status: Partially Verified

Source: AOPA - Quick Look: Bombardier Challenger 300