| Boeing 737-300: model by David Culp/Innis Cunningham/Heiko Shultz, version CVS April 2010 (1) | |||||
|---|---|---|---|---|---|
| Cruise Altitude | Fuel to Cruise (2) | Downrange nm | KIAS at Cruise | Groundspeed | Fuel Flow (lbs/hr)(3) |
| FL340 | 4,350 | 119.8 | 255 | 437 | 6,000 |
| FL320 | 4,177 | 111.5 | 267 | 441 | 6,180 |
| FL300 | 4,010 | 103.5 | 279 | 445 | 6,840 |
| FL280 | 3,830 | 95.3 | 292 | 449 | 7,200 |
| FL260 | 3,645 | 87.7 | 304 | 453 | 7,740 |
| FL240 | 3,442 | 79.6 | 317 | 445 | 8,580 |
| FL220 | 3,230 | 71.9 | 330 | 449 | 9,180 |
| FL200 | 3,015 | 64.6 | 340 | 448 | 10,140 |
| FL180 | 2,790 | 57.4 | 300 | 386 | 8,580 |
| 15,000 | 2,447 | 47.1 | 300 | 369 | 8,880 |
| 10,000 | 1,640 | 25.1 | 300 | 343 | 9,240 |
| 5,000 | 1,020 | 11.7 | 250 | 265 | 8,580 |
| 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 300 KIAS until M0.74, then M0.74 until cruise. | |||||
| (3) Estimated using weight differential over a one-minute cruise. | |||||