Bombardier CRJ Second Gen: Difference between revisions
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{{Infobox Aircraft Type | {{Infobox Aircraft Type | ||
| | |Role=[[:Category:Regional Jets|Regional jet]] | ||
| | |Country of Origin=Canada | ||
| | |Manufacturer= Bombardier Aerospace | ||
| | |Status=In production | ||
| | |Number Built= 56 | ||
| | |Unit Cost= 33.000.000v$ | ||
| | |Updateday= 17 | ||
| | |Updatemonth= 4 | ||
| | |Updateyear= 2009 | ||
|picture= yes | |picture= yes | ||
}} | }} | ||
| Line 26: | Line 26: | ||
| colspan=4 | 4 (2 pilots + flight attendants) | | colspan=4 | 4 (2 pilots + flight attendants) | ||
|- | |- | ||
! | ! Seating capacity | ||
| 70 | | 70 | ||
| 75 | | 75 | ||
| Line 73: | Line 73: | ||
| Mach .85 max or 330 kts indicated | | Mach .85 max or 330 kts indicated | ||
|- | |- | ||
! | ! Service ceiling | ||
| colspan=4 | 12,496 m (41,000 ft) | | colspan=4 | 12,496 m (41,000 ft) | ||
|- | |- | ||
| Line 92: | Line 92: | ||
| 4th Quarter 2009 | | 4th Quarter 2009 | ||
|} | |} | ||
[[Category:Regional Jets]] | |||
Revision as of 22:13, 17 April 2009
| Bombardier CRJ Second Gen at a Glance | |
|---|---|
| Role | {{{type}}} |
| Country of Origin | {{{country}}} |
| Manufacturer | {{{manufacturer}}} |
| Status | In Production |
| Number Built | {{{number built}}} |
| Unit Cost | {{{unit cost}}} |
| |
The Bombardier CRJ 900 is a regional airliner that was developed from the Bombardier CRJ 200.
Specifications
| Variant | CRJ700 |
CRJ705 | CRJ900 | CRJ1000 |
|---|---|---|---|---|
| Crew | 4 (2 pilots + flight attendants) | |||
| Seating capacity | 70 | 75 | 86-90* | 100-104 |
| Length Wing span Height |
32.51 m (106 ft 8 in) 23.24 m (76 ft 3 in) 7.57 m (24 ft 10 in) |
36.40 m (119 ft 4 in) 24.85 m (81 ft 6 in) 7.51 m (24 ft 7 in) |
39.13 m (128 ft 4.7 in) 26.18 m (85 ft 10.6 in) 7.13 m (23 ft 4.8 in) | |
| Wing area | 70.61 m² (760 ft²) | 70.61 m² (760 ft²) | ||
| Fuselage max diameter | 2.69 m (8 ft 10 in) | |||
| Engines (2x) Takeoff thrust (2x) Thrust APR (2x) |
GE CF34-8C1 56.4 kN (12,670 lbf) 61.3 kN (13,790 lbf) |
GE CF34-8C5 58.4 kN (13,123 lbf) 63.4 kN (14,255 lbf) |
GE CF34-8C5A1
60.63kN (13,630 lbf) | |
| Max Zero Fuel Weight (ZFW) | 28,801 kg (63,495 lb) | 31,751 kg (70,000 lb) | 35,154 kg (77,500 lb) | |
| Max payload weight | 8,527 kg (18,800 lb) | 10,319 kg (22,750 lb) | 12,156 kg (26,800 lb) | |
| Maximum range | 3,121 km (1,939 mi) ER: 3,676 km (2,284 mi) |
3,591 km (2,231 mi) ER/LR: 3,773 km (2,344 mi) |
2,956 km (1,837 mi) ER: 3,408 km (2,117 mi) LR: 3,660 km (2,274 mi) |
2,761 km (1,491 mi) ER: 3,131 km (1,691 mi) |
| Basic cruising speed | Mach 0.79 (810 km/h, 503 mph) | Mach .80 (838 km/h, 521 mph) | Mach .82 (877 km/h, 545 mph) | Mach .85 max or 330 kts indicated |
| Service ceiling | 12,496 m (41,000 ft) | |||
| Turning circle | 22.86 m (75 ft) | |||
| Number of Orders | 253 | 168* | 38 23 Options | |
| Certification Date | Dec 2000 | Sept 2002 | 4th Quarter 2009 | |