Embraer EMB145, Operation Manual

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FLIGHT PLANNING
EMB-145 A1 and A1P LB AIRPLANE
OPERATIONS
MANUAL
1-05-15
Page
10
Code
02 REVISION 40 A
O
M-145/1
114
LONG RANGE CRUISE - ALL ENGINES OPERATING
AE3007A1 AND AE3007A1P ENGINES
ALTITUDE : 29000 FT TO 37000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
29000 30000 31000 32000 33000 34000 35000 36000 37000
N1 % 84.9 85.6 86.3 87.1 88.2 89.3 90.2 90.7 91.2
F FLOW LB/H/ENG 1251 1255 1261 1268 1275 1284 1293 1314 1214
IAS KT 249 250 250 251 252 253 255 258 237
50000 TAS KT 387 394 401 409 417 426 435 448 424
INDICATED MACH 0.652 0.667 0.683 0.699 0.716 0.734 0.754 0.779 0.738
BUFFET MARGIN G 1.98 1.92 1.85 1.78 1.70 1.61 1.51 1.39 1.39
SR NM/LB 0.155 0.157 0.159 0.161 0.164 0.166 0.168 0.170 0.174
N1 % 83.9 84.6 85.3 86.1 86.9 88.0 89.1 90.0 91.0
F FLOW LB/H/ENG 1194 1197 1202 1207 1212 1221 1229 1238 1233
IAS KT 244 245 245 246 246 248 249 250 248
48000 TAS KT 379 386 393 401 408 417 426 435 440
INDICATED MACH 0.641 0.655 0.670 0.685 0.701 0.720 0.738 0.757 0.767
BUFFET MARGIN G 2.04 1.98 1.91 1.84 1.77 1.68 1.59 1.49 1.41
SR NM/LB 0.159 0.161 0.164 0.166 0.168 0.171 0.173 0.176 0.178
N1 % 82.7 83.4 84.2 84.8 85.4 86.2 87.1 88.5 90.1
F FLOW LB/H/ENG 1137 1139 1143 1148 1152 1158 1165 1174 1188
IAS KT 239 239 239 240 240 241 242 243 245
46000 TAS KT 371 378 385 392 399 407 416 424 436
INDICATED MACH 0.627 0.64 0.655 0.67 0.685 0.702 0.72 0.738 0.759
BUFFET MARGIN G 2.09 2.03 1.97 1.91 1.84 1.76 1.68 1.58 1.48
SR NM/LB 0.163 0.166 0.168 0.171 0.173 0.176 0.178 0.181 0.183
N1 % 81.6 82.3 83.1 83.8 84.5 85.1 85.9 86.9 88.6
F FLOW LB/H/ENG 1082 1084 1086 1088 1092 1097 1103 1111 1124
IAS KT 234 234 234 234 235 235 236 237 239
44000 TAS KT 364 370 377 383 391 398 406 415 425
INDICATED MACH 0.614 0.628 0.641 0.656 0.671 0.687 0.704 0.722 0.741
BUFFET MARGIN G 2.14 2.09 2.03 1.97 1.9 1.83 1.76 1.67 1.58
SR NM/LB 0.168 0.171 0.173 0.176 0.179 0.181 0.184 0.187 0.189
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%.