AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
REVISION 40
1-05-15
Page
9
Code
02
AOM-145/1114
LONG RANGE CRUISE - ALL ENGINES OPERATING
AE3007A1 AND AE3007A1P ENGINES
ALTITUDE : 19000 FT TO 28000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
19000 20000 21000 22000 23000 24000 25000 26000 27000 28000
N1 % 68.4 69 69.5 70.1 70.8 71.5 72.2 73 73.8 74.7
F FLOW LB/H/ENG 868 860 854 848 842 838 833 830 825 822
IAS KT 218 217 216 215 214 213 212 211 210 209
34000 TAS KT 288 292 295 298 302 306 310 313 317 321
INDICATED MACH 0.469 0.476 0.484 0.492 0.500 0.508 0.516 0.525 0.533 0.542
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.52 2.47
SR NM/LB 0.166 0.169 0.173 0.176 0.179 0.183 0.186 0.189 0.192 0.195
N1 % 66.8 67.3 67.8 68.3 68.9 69.5 70.1 70.8 71.5 72.3
F FLOW LB/H/ENG 801 793 786 780 773 768 763 758 752 748
IAS KT 211 210 209 208 207 206 205 204 203 202
31000 TAS KT 279 282 285 289 292 296 299 303 306 310
INDICATED MACH 0.454 0.461 0.469 0.476 0.484 0.492 0.500 0.508 0.515 0.524
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.174 0.178 0.181 0.185 0.189 0.192 0.196 0.200 0.203 0.207
N1 % 64.6 65.3 66 66.5 67 67.5 68.1 68.6 69.2 69.9
F FLOW LB/H/ENG 737 729 721 713 706 700 694 688 682 677
IAS KT 203 202 202 200 199 199 198 197 195 194
28000 TAS KT 269 272 275 278 281 285 288 291 294 298
INDICATED MACH 0.439 0.446 0.453 0.46 0.467 0.474 0.482 0.489 0.497 0.505
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.183 0.187 0.191 0.195 0.199 0.203 0.208 0.212 0.216 0.220
INCREASE / DECREASE N1% BY 1 % PER 5°C ABOVE / BELOW ISA CONDITIONS.
INCREASE / DECREASE FUEL FLOW 1 % PER 5°C ABOVE / BELOW ISA CONDITIONS.
INCREASE / DECREASE TAS BY 5 KT PER 5°C ABOVE / BELOW ISA CONDITIONS.
FOR ANTI-ICE ON:
INCREASE N1 BY 0.6 % AND FUEL FLOW BY 8%.
DECREASE SR BY 9%.