Embraer EMB145 - Page 817

AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
REVISION 40
1-05-15
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
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
29000 30000 31000 32000 33000 34000 35000 36000 37000
N1 % 80.5 81.2 82 82.8 83.5 84.1 84.8 85.6 86.9
F FLOW LB/H/ENG 1027 1029 1031 1032 1035 1039 1044 1050 1061
IAS KT 229 229 229 229 229 230 231 232 232
42000 TAS KT 356 362 369 375 382 389 397 405 415
INDICATED MACH 0.602 0.615 0.628 0.642 0.657 0.672 0.688 0.706 0.724
BUFFET MARGIN G 2.19 2.14 2.09 2.03 1.97 1.9 1.83 1.75 1.67
SR NM/LB 0.173 0.176 0.179 0.182 0.185 0.187 0.19 0.193 0.196
N1 % 79.5 80.2 80.8 81.6 82.4 83.1 83.7 84.4 85.5
F FLOW LB/H/ENG 975 975 976 977 979 982 986 991 1000
IAS KT 223 224 224 224 224 225 225 226 226
40000 TAS KT 348 354 360 367 373 380 388 395 405
INDICATED MACH 0.589 0.602 0.615 0.628 0.642 0.657 0.673 0.689 0.706
BUFFET MARGIN G 2.25 2.2 2.15 2.09 2.04 1.97 1.91 1.83 1.75
SR NM/LB 0.179 0.182 0.185 0.188 0.191 0.194 0.197 0.199 0.202
N1 % 78.4 79.1 79.7 80.4 81.1 81.9 82.7 83.3 84.3
F FLOW LB/H/ENG 923 922 922 922 923 925 928 931 939
IAS KT 218 218 218 218 218 219 219 219 220
38000 TAS KT 341 346 352 358 364 371 378 385 394
INDICATED MACH 0.576 0.588 0.601 0.614 0.627 0.641 0.656 0.672 0.688
BUFFET MARGIN G 2.30 2.25 2.2 2.15 2.1 2.04 1.98 1.91 1.84
SR NM/LB 0.184 0.188 0.191 0.194 0.197 0.200 0.204 0.207 0.21
N1 % 77 77.8 78.5 79.2 79.8 80.6 81.4 82.1 83.1
F FLOW LB/H/ENG 870 869 868 867 868 869 871 873 880
IAS KT 213 213 213 213 213 213 213 213 214
36000 TAS KT 332 337 343 349 355 361 368 374 383
INDICATED MACH 0.562 0.574 0.586 0.598 0.611 0.625 0.639 0.654 0.67
BUFFET MARGIN G 2.35 2.3 2.26 2.21 2.16 2.11 2.05 1.99 1.92
SR NM/LB 0.191 0.194 0.198 0.201 0.204 0.208 0.211 0.214 0.218
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%.