Embraer EMB145 - Page 922

FLIGHT PLANNING
EMB-145 A1 and A1P LB
AIRPLANE
OPERATIONS
MANUAL
1-05-50
Page
12
Code
02
REVISION 38
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 % 72.4 73.1 73.9 74.7 75.5 76.3 77.0 77.6 79.0
F FLOW LB/H/ENG 782 775 771 767 764 762 760 758 759
IAS KT 197 196 195 193 192 192 191 191 190
30000 TAS KT 307 310 314 318 321 326 331 336 342
INDICATED MACH 0.523 0.530 0.538 0.547 0.556 0.567 0.578 0.590 0.601
BUFFET MARGIN G 2.52 2.46 2.40 2.35 2.29 2.25 2.20 2.15 2.09
SR NM/LB 0.197 0.200 0.204 0.207 0.210 0.214 0.218 0.222 0.226
N1 % 70.8 71.5 72.2 73.0 73.8 74.6 75.4 76.2 77.6
F FLOW LB/H/ENG 731 725 721 717 713 711 707 705 706
IAS KT 192 191 190 189 188 187 186 185 185
28000 TAS KT 299 303 306 310 314 318 322 327 333
INDICATED MACH 0.510 0.518 0.526 0.535 0.543 0.553 0.562 0.574 0.585
BUFFET MARGIN G 2.56 2.54 2.49 2.44 2.38 2.33 2.27 2.22 2.17
SR NM/LB 0.205 0.209 0.212 0.216 0.220 0.224 0.228 0.232 0.236
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.