| Bombardier CRJ-200 LR: model by Joshua Wilson, version circa Fall 2009 (1) | |||||
|---|---|---|---|---|---|
| Cruise Altitude | Fuel to Cruise (2) | Downrange nm | KIAS at Cruise | Groundspeed | Fuel Flow (lbs/hr)(4) |
| FL360 (3) | 1,162 | 99.2 | 246 | 402 | 2220 |
| FL340 (3) | 1,118 | 93.4 | 258 | 406 | 2306 |
| FL320 | 1,072 | 87.4 | 270 | 420 | 2416 |
| FL300 | 1,023 | 81.4 | 281 | 431 | 2520 |
| FL280 | 969 | 74.9 | 294 | 427 | 2680 |
| FL260 | 912 | 68.4 | 300 | 428 | 2740 |
| FL240 | 850 | 61.6 | 300 | 411 | 2712 |
| FL220 | 784 | 55.2 | 300 | 399 | 2684 |
| FL200 | 718 | 49.0 | 300 | 382 | 2660 |
| FL180 | 651 | 42.7 | 300 | 402 | 2636 |
| 15,000 | 549 | 33.9 | 300 | 402 | 2606 |
| 10,000 | 374 | 20.8 | 300 | 333 | 2562 |
| 5,000 | 225 | 9.9 | 250 | 257 | 1936 |
| NOTES: | (1) ALL PERFORMANCE FIGURES ARE ESTIMATES and can vary by atmospheric conditions or other factors. | ||||
| (2) All tests performed starting at max takeoff weight (53000 lbs) and climbing at 250 KIAS until 10,000, then 300 KIAS, at autopilot-managed climb rate. | |||||
| (3) Autopilot-managed climb straight to levels above FL320 not recommended at max takeoff weight. Beyond that point, airspeed started to decay significantly. | |||||
| (4) Chart figures are total. On-board gauge represents a per-engine figure, equal to half the amount shown here. | |||||