AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
REVISION 38
1-05-50
Page
11
Code
02
AOM-145/1114
LONG RANGE CRUISE - ALL ENGINES OPERATING
AE3007A1 and AE3007A1P ENGINES
ALTITUDE: 29000 FT TO 37000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ANTI ICE: ON (Engine or all)
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
29000 30000 31000 32000 33000 34000 35000 36000 37000
N1 % 79.2 79.9 80.5 81.2 81.9 82.6 83.3 84.0 85.4
F FLOW LB/H/ENG 1039 1037 1036 1035 1036 1040 1045 1048 1058
IAS KT 219 218 218 218 217 217 218 217 218
40000 TAS KT 341 346 351 356 362 368 375 381 390
INDICATED MACH 0.578 0.588 0.600 0.612 0.624 0.638 0.652 0.666 0.681
BUFFET MARGIN G 2.19 2.14 2.09 2.04 1.98 1.93 1.87 1.81 1.74
SR NM/LB 0.164 0.167 0.170 0.172 0.175 0.177 0.179 0.182 0.184
N1 % 78.1 78.7 79.4 80.1 80.8 81.4 82.1 82.8 84.2
F FLOW LB/H/ENG 985 982 981 980 979 980 982 987 995
IAS KT 214 214 213 213 213 212 212 212 212
38000 TAS KT 334 338 344 349 354 360 366 373 381
INDICATED MACH 0.566 0.576 0.588 0.600 0.611 0.623 0.637 0.651 0.666
BUFFET MARGIN G 2.24 2.19 2.15 2.10 2.04 1.99 1.93 1.87 1.81
SR NM/LB 0.169 0.172 0.175 0.178 0.181 0.184 0.186 0.189 0.191
N1 % 76.7 77.5 78.3 78.9 79.6 80.2 80.9 81.6 83.0
F FLOW LB/H/ENG 932 929 928 926 924 923 923 925 932
IAS KT 209 209 209 208 208 207 207 207 207
36000 TAS KT 326 331 336 342 347 352 357 363 371
INDICATED MACH 0.554 0.564 0.576 0.587 0.598 0.610 0.622 0.635 0.649
BUFFET MARGIN G 2.29 2.25 2.21 2.16 2.11 2.05 2.00 1.94 1.88
SR NM/LB 0.175 0.178 0.181 0.184 0.188 0.191 0.193 0.196 0.199
N1 % 75.4 76.1 76.9 77.7 78.3 79.0 79.7 80.3 81.8
F FLOW LB/H/ENG 881 878 875 873 870 868 867 867 874
IAS KT 206 205 204 203 203 202 202 202 202
34000 TAS KT 320 324 329 334 338 343 349 354 362
INDICATED MACH 0.544 0.553 0.563 0.574 0.585 0.596 0.608 0.620 0.634
BUFFET MARGIN G 2.37 2.31 2.27 2.22 2.17 2.12 2.06 2.01 1.95
SR NM/LB 0.182 0.185 0.188 0.191 0.195 0.198 0.201 0.204 0.207
N1 % 73.9 74.7 75.5 76.2 77.0 77.7 78.4 79.0 80.4
F FLOW LB/H/ENG 831 828 823 819 817 814 813 812 815
IAS KT 202 201 199 198 198 197 197 196 196
32000 TAS KT 314 318 321 325 330 335 340 345 352
INDICATED MACH 0.534 0.543 0.551 0.560 0.571 0.582 0.594 0.606 0.618
BUFFET MARGIN G 2.44 2.39 2.33 2.28 2.23 2.18 2.13 2.08 2.02
SR NM/LB 0.189 0.192 0.195 0.199 0.202 0.206 0.209 0.213 0.216
INCREASE/DECREASE N1% BY 1.1% PER 5°C ABOVE/BELOW ISA CONDITION.
INCREASE/DECREASE FUEL FLOW BY 1.2% PER 5°C ABOVE/BELOW ISA CONDITION.
INCREASE/DECREASE TAS BY 4 KT PER 5°C ABOVE/BELOW ISA CONDITION.