Embraer EMB145 - Page 819

AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
REVISION 40
1-05-15
Page
13
Code
02
AOM-145/1114
MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING
AE3007A1 AND AE3007A1P ENGINES
PRESSURE ALTITUDE: 5000 FT TO 18000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
5000 10000 11000 12000 13000 14000 15000 16000 17000 18000
N1 % 66.7 78.1 78.9 79.8 80.5 81.3 82.2 83.0 83.7 84.4
F FLOW LB/H/ENG 1285 1776 1776 1777 1778 1781 1784 1788 1793 1799
IAS KT 250 318 318 318 318 318 318 318 318 318
50000 TAS KT 269 368 373 379 384 390 395 401 407 413
INDICATED MACH 0.414 0.574 0.584 0.595 0.606 0.617 0.628 0.640 0.652 0.664
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.105 0.104 0.105 0.106 0.108 0.109 0.111 0.112 0.114 0.115
N1 % 66.1 77.7 78.5 79.4 80.2 81.0 81.8 82.7 83.4 84.1
F FLOW LB/H/ENG 1259 1756 1755 1755 1757 1759 1761 1765 1769 1774
IAS KT 250 319 319 319 319 319 319 319 319 319
48000 TAS KT 269 368 373 379 384 390 395 401 407 413
INDICATED MACH 0.413 0.575 0.585 0.596 0.607 0.618 0.629 0.641 0.653 0.665
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.107 0.105 0.106 0.108 0.109 0.111 0.112 0.114 0.115 0.116
N1 % 65.7 77.4 78.2 79 79.8 80.7 81.6 83.3 83.2 83.9
F FLOW LB/H/ENG 1240 1747 1746 1746 1747 1748 1751 1771 1758 1762
IAS KT 250 320 320 320 320 320 320 320 320 320
46000 TAS KT 269 369 374 380 385 391 397 406 408 414
INDICATED MACH 0.413 0.576 0.587 0.598 0.608 0.62 0.631 0.643 0.655 0.667
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.108 0.106 0.107 0.109 0.11 0.112 0.113 0.115 0.116 0.118
N1 % 65.2 77 77.8 78.6 79.4 80.3 81.2 82.8 82.8 83.6
F FLOW LB/H/ENG 1218 1722 1721 1721 1721 1722 1724 1743 1730 1734
IAS KT 250 320 320 320 320 320 320 320 320 320
44000 TAS KT 269 369 374 379 385 390 396 406 408 414
INDICATED MACH 0.413 0.576 0.587 0.598 0.608 0.62 0.631 0.643 0.655 0.667
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.110 0.107 0.109 0.110 0.112 0.113 0.115 0.116 0.118 0.119
INCREASE / DECREASE N1% BY 1 % PER 5°C ABOVE / BELOW ISA CONDITIONS.
INCREASE / DECREASE FUEL FLOW 1 % PER 5°C ABOVE / BELOW STD ISA CONDITIONS.
INCREASE / DECREASE TAS BY 5 KT PER 5°C ABOVE / BELOW STD ISA CONDITIONS.