Embraer EMB145 - Page 823

AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
REVISION 40
1-05-15
Page
17
Code
02
AOM-145/1114
MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING
AE3007A1 AND AE3007A1P ENGINES
PRESSURE ALTITUDE: 19000 FT TO 28000 FT
CRUISE CONFIGURATION
BLEED: OPEN
WEIGHT ALTITUDE (FT)
(LB)
19000 20000 21000 22000 23000 24000 25000 26000 27000 28000
N1 % 83.8 84.4 85.1 85.8 86.5 87.3 87.6 87.9 87.9 87.8
F FLOW LB/H/ENG 1710 1715 1720 1727 1734 1741 1717 1695 1641 1589
IAS KT 320 320 320 320 320 320 317 313 309 303
42000 TAS KT 419 425 432 438 445 452 454 456 457 456
INDICATED MACH 0.680 0.692 0.706 0.719 0.733 0.747 0.754 0.761 0.765 0.767
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.44
SR NM/LB 0.123 0.124 0.126 0.127 0.128 0.13 0.132 0.135 0.1390.143
N1 % 83.5 84.1 84.7 85.4 86.1 86.9 87.6 87.9 87.8 87.8
F FLOW LB/H/ENG 1682 1686 1691 1697 1703 1710 1717 1698 1643 1590
IAS KT 320 320 320 320 320 320 320 317 311 305
40000 TAS KT 419 425 431 438 444 451 458 460 459 458
INDICATED MACH 0.68 0.692 0.706 0.719 0.733 0.747 0.761 0.769 0.770 0.772
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.55
SR NM/LB 0.124 0.126 0.127 0.129 0.13 0.132 0.133 0.135 0.14 0.144
N1 % 83.1 83.7 84.3 85 85.7 86.4 87.2 87.8 87.8 87.8
F FLOW LB/H/ENG 1655 1658 1663 1668 1673 1679 1686 1693 1646 1592
IAS KT 320 320 320 320 320 320 320 320 314 307
38000 TAS KT 418 424 431 437 444 450 457 464 463 461
INDICATED MACH 0.68 0.692 0.706 0.719 0.733 0.747 0.761 0.776 0.778 0.777
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 0.126 0.128 0.129 0.131 0.133 0.134 0.136 0.137 0.141 0.145
N1 % 82.7 83.4 84 84.6 85.2 86 86.7 87.4 87.5 87.5
F FLOW LB/ /ENG 1628 1631 1635 1639 1644 1649 1655 1662 1621 1565
IAS KT 320 320 320 320 320 320 320 320 315 309
36000 TAS KT 417 424 430 436 443 450 456 463 464 462
INDICATED MACH 0.68 0.692 0.706 0.719 0.733 0.747 0.761 0.776 0.78 0.78
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 0.128 0.13 0.131 0.133 0.135 0.136 0.138 0.139 0.143 0.148
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.