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BOMBARDIER BD-500 CSeries CS100
From SKYbrary Wiki
BCS1
| Aircraft | ||||
|---|---|---|---|---|
| Name | BD-500 CSeries CS100 | |||
| Manufacturer | BOMBARDIER | |||
| 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 CS100
Description
Narrow-body, twin-engine, medium-range jet airliners originally designed by Canadian manufacturer Bombardier Aerospace able to carry between 108 and 135 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 | 35 m114.829 ft |
| Height | 11.5 m37.73 ft |
| Powerplant | 2 x Pratt & Whitney PurePower PW1500G Engines (84.1 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 | 1463 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 | 1387 m |
| MTOW | 6078160,781 kg 60.781 tonnes kg |
Ceiling | FL410 | ROD | ft/min | APC | C | ||||||||||||
| WTC | M | Range | 31003,100 nm 5,741,200 m 5,741.2 km 18,835,958.019 ft NM |
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Accidents & Serious Incidents involving BCS1
None on SKYbrary