Embraer EMB145 - Page 818

FLIGHT PLANNING
EMB-145 A1 and A1P LB
AIRPLANE
OPERATIONS
MANUAL
1-05-15
Page
12
Code
02
REVISION 40
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 % 75.6 76.4 77.2 78 78.6 79.3 80 80.8 81.9
F FLOW LB/H/ENG 820 819 816 815 814 815 815 817 823
IAS KT 209 208 207 207 207 207 207 207 208
34000 TAS KT 325 329 334 339 345 351 358 364 372
INDICATED MACH 0.552 0.561 0.571 0.583 0.596 0.609 0.623 0.637 0.652
BUFFET MARGIN G 2.42 2.37 2.31 2.27 2.22 2.17 2.12 2.06 2.00
SR NM/LB 0.198 0.201 0.205 0.208 0.212 0.216 0.219 0.223 0.226
N1 % 73.1 74 74.9 75.8 76.6 77.4 78 78.7 79.7
F FLOW LB/H/ENG 745 743 741 740 738 737 737 738 742
IAS KT 201 200 200 199 198 198 198 198 199
31000 TAS KT 314 318 322 327 331 337 343 349 357
INDICATED MACH 0.533 0.542 0.552 0.562 0.573 0.585 0.598 0.612 0.626
BUFFET MARGIN G 2.52 2.47 2.42 2.37 2.32 2.27 2.22 2.17 2.12
SR NM/LB 0.21 0.214 0.217 0.221 0.224 0.229 0.233 0.237 0.241
N1 % 70.7 71.4 72.3 73.2 74.1 75 75.8 76.5 77.5
F FLOW LB/H/ENG 673 670 668 666 665 664 661 660 662
IAS KT 194 193 192 191 191 190 189 189 189
28000 TAS KT 302 306 310 314 319 323 327 333 340
INDICATED MACH 0.513 0.522 0.532 0.541 0.552 0.562 0.572 0.584 0.597
BUFFET MARGIN G 2.56 2.56 2.53 2.48 2.43 2.38 2.33 2.28 2.23
SR NM/LB 0.224 0.228 0.232 0.236 0.24 0.243 0.248 0.252 0.257
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%.