FAA-H-8083-25C · Source PDF page 459

Appendix A

Challenger 605 Time and Fuel Versus Distance · PHAK page A-7

Original FAA PHAK page A-7
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0.240 0.230 0.220 0.210 0.200 0.190 0.180 0.170 0.160 Conditions: 40,000 lb mid-cruise weight, zero wind, ISA 0.150 420 430 440 450 460 470 480 490 Speed (KTAS) A-7 )bl/MN( egnaR cificepS Challenger 605 Time and Fuel Versus Distance CHALLENGER 605 SPECIFIC RANGE FL 390 FL 370 M 0.74 FL 350 Cruise Speed FL 330 M 0.80 Cruise Speed FL 310 M 0.82 Cruise Speed Plotting of constant FL lines M0.82 M0.80 M0.74 Flight Level 290 Speed Spc Range 310 Speed 481 469 434 Spc Range 0.165 0.178 0.199 330 Speed 477 465 430 Spc Range 0.174 0.188 0.208 350 Speed 473 461 427 Spc Range 0.181 0.197 0.216 370 Speed 470 459 424 Spc Range 0.185 0.204 0.222 390 Speed 459 424 Spc Range 0.205 0.223 Plotting of Long Range Cruise and High Speed Cruise lines FL290 FL310 FL330 FL350 FL370 FL390 M0.74 "X" 434 430 427 424 424 M0.74 "Y" 0.199 0.208 0.216 0.222 0.223 M0.80 "X" 469 465 461 459 459 M0.80 "Y" 0.178 0.188 0.197 0.204 0.205 M0.82 "X" 481 477 473 470 M0.82 "Y" 0.165 0.174 0.181 0.185 Note: Based on 40,000 lb mid-cruise weight, ISA Conditions, zero wind Note: All Challenger 605 performance data are for discussion purposes only. By this document, Bombardier Inc., does not intend to make, and is not making, any offer, commitment, representation or warranty of any kind whatsoever. All data are subject to change without prior notice.