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BOMBARDIER BD-500 CSeries CS300
From SKYbrary Wiki
BCS3
| Aircraft | ||||
|---|---|---|---|---|
| Name | BD-500 CSeries CS300 | |||
| Manufacturer | BOMBARDIER | |||
| Body | Narrow | |||
| Wing | Fixed Wing | |||
| Position | Low wing (winglets) | |||
| Tail | Regular tail (Dihedral) | |||
| WTC | Medium | |||
| APC | C | |||
| Type code | L2J | |||
| Engine | Jet | |||
| Engine count | Multi | |||
| Position | Underwing mounted | |||
| Landing gear | Tricycle retractable | |||
| Mass group | 4 | |||
|
| ||||
BOMBARDIER BD-500 CSeries CS300
Description
Narrow-body, twin-engine, medium-range jet airliners originally designed by Canadian manufacturer Bombardier Aerospace able to carry between 130 and 160 passengers. First delivery in 2016. The Bombardier CSeries aircraft contains a high proportion of composite materials and features larger windows.
Technical Data
| Wing span | 35.1 m115.157 ft |
|---|---|
| Length | 38.7 m126.969 ft |
| Height | 11.5 m37.73 ft |
| Powerplant | 2 x Pratt & Whitney PurePower PW1500G Engines (93.4 kN) |
| Engine model | Pratt & Whitney PW1000G |
Performance Data
| Take-Off | Initial Climb (to 5000 ft) |
Initial Climb (to FL150) |
Initial Climb (to FL240) |
MACH Climb | Cruise | Initial Descent (to FL240) |
Descent (to FL100) |
Descent (FL100 & below) |
Approach | ||||||||||
| V2 (IAS) | kts | IAS | kts | IAS | kts | IAS | kts | MACH | TAS | kts | MACH | IAS | kts | IAS | kts | Vapp (IAS) | kts | ||
| Distance | 1890 m | ROC | ft/min | ROC | ft/min | ROC | ft/min | ROC | ft/min | MACH | 0.78 | ROD | ft/min | ROD | ft/min | MCS | kts | Distance | 1509 m |
| MTOW | 6758567,585 kg 67.585 tonnes kg |
Ceiling | FL410 | ROD | ft/min | APC | C | ||||||||||||
| WTC | M | Range | 33003,300 nm 6,111,600 m 6,111.6 km 20,051,181.117 ft NM |
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Accidents & Serious Incidents involving BCS3
None on SKYbrary