FAA-H-8083-25C · Source PDF page 459
Appendix A
Challenger 605 Time and Fuel Versus Distance · PHAK page A-7

Searchable transcription
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.