| Manufacturer |
Bombardier |
Fairchild-Dornier |
| Family |
|
Do328 |
| Description |
The Bombardier Challenger 300 is a range super mid-sized business jet designed and produced by the Canadian aircraft manufacturer Bombardier Aviation. |
|
| ICAO Code |
CL30 |
|
| EASA TCDSN |
|
EASA.A.096 |
| Program Launch |
|
1999-09-30 |
| First Flight |
2001-08-14 |
|
| Entry Into service |
2004-01-08 |
2000-04-01 |
| Launch Customer |
|
Atlantic Coast Jet |
| Designer |
Bombardier |
|
| Type |
Business jet |
|
| Length (m) |
20.9184 |
21.284 |
| Height (m) |
6.096 |
7.234 |
| Cockpit Crew |
|
2 |
| Max Seating |
19 |
34 |
| One Class Typical Seating |
|
32 |
| Cargo Volume (m³) |
|
6.4 |
| Max Speed (km/h) |
883.4032 |
0.66 |
| Cruise Speed (km/h) |
850.0673 |
0.61 |
| Max Ceiling (m) |
13716 |
|
| Capacity Description |
Max 19 occupants (including the crew and no more than 16 passengers). Typically 8 or 9 max passenger seating capacity with standard cabin layout options. |
|
| National Origin |
Canada |
|
| Number Built |
450 |
|
| Primary Users |
Flexjet, XOJET, NetJets, VistaJet |
|
| Status |
In production |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Bombardier_Challenger_300 |
|
| Flat Wing Span (m) |
19.2024 |
20.976 |
| Flat Wing Area (m²) |
48.5883 |
40 |
| Flat Wing Aspect Ratio |
|
11 |
| Wing Sweepback (°) |
|
7.1 |
| Fuselage Diameter (m) |
|
2.41 |
| Cabin Diameter (m) |
|
2.18 |
| Wake Category |
M |
M |
| Aircraft Engine |
|
PW306B |
| Number of Engines |
2 |
2 |
| Lateral Noise Level (EPNdB) |
|
89.8 |
| Flyover Noise Level (EPNdB) |
|
76.5 |
| Approac hNoise Level (EPNdB) |
|
92.1 |