| Manufacturer |
Fairchild-Dornier |
Bombardier |
| 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 |
2000-04-01 |
2004-01-08 |
| Launch Customer |
Atlantic Coast Jet |
|
| Designer |
|
Bombardier |
| Type |
|
Business jet |
| Length (m) |
21.284 |
20.9184 |
| Height (m) |
7.234 |
6.096 |
| Cockpit Crew |
2 |
|
| Max Seating |
34 |
19 |
| One Class Typical Seating |
32 |
|
| Cargo Volume (m³) |
6.4 |
|
| Max Speed (km/h) |
0.66 |
883.4032 |
| Cruise Speed (km/h) |
0.61 |
850.0673 |
| 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) |
20.976 |
19.2024 |
| Flat Wing Area (m²) |
40 |
48.5883 |
| 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 |
|