| Boeing 737-900ER: model by xsaint/Syd Adams/etcetera, version circa February 2010 (1) | |||||
|---|---|---|---|---|---|
| Cruise Altitude | Fuel to Cruise (2) | Downrange nm | KIAS at Cruise | Groundspeed | Fuel Flow (lbs/hr)(3) |
| FL340 | 5,770 | 99.1 | 273 | 430 | 11,520 |
| FL320 | 5,400 | 88.9 | 285 | 434 | 12,480 |
| FL300 | 5,091 | 81.1 | 297 | 438 | 13,620 |
| FL280 | 4,796 | 73.9 | 310 | 442 | 14,520 |
| FL260 | 4,520 | 67.6 | 323 | 444 | 15,780 |
| FL240 | 4,243 | 61.8 | 337 | 449 | 17,220 |
| FL220 | 3,981 | 56.5 | 350 | 453 | 18,660 |
| FL200 | 3,722 | 51.7 | 365 | 468 | 19,620 |
| FL180 | 3,450 | 46.5 | 300 | 378 | 12,780 |
| 15,000 | 3,036 | 39.6 | 300 | 362 | 12,720 |
| 10,000 | 2,185 | 27.8 | 300 | 336 | 12,480 |
| 5,000 | 1,320 | 13.7 | 250 | 263 | 8,940 |
| 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 (187,700 lbs) and climbing at autopilot-managed climb rate; maintaining 250 KIAS until 10,000, then at full-throttle, where airspeed stabilized at M0.6. | |||||
| (3) Estimated using weight differential over a one-minute cruise. | |||||