Embraer EMB145 - Page 822

FLIGHT PLANNING
EMB-145 A1 and A1P LB
AIRPLANE
OPERATIONS
MANUAL
1-05-15
Page
16
Code
02
REVISION 40
AOM-145/1114
MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING
AE3007A1 AND AE3007A1P ENGINES
PRESSURE ALTITUDE: 19000 FT TO 28000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ISA CONDITIONS
WEIGHT ALTITUDE (FT)
(LB)
19000 20000 21000 22000 23000 24000 25000 26000 27000 28000
N1 % 85.2 85.9 86.5 86.8 87.1 87.4 87.6 87.9 87.9 87.9
F FLOW LB/H/ENG 1806 1813 1816 1789 1762 1733 1709 1685 1632 1579
IAS KT 318 318 317 314 312 309 307 305 299 293
50000 TAS KT 419 425 430 433 436 439 442 446 445 444
INDICATED MACH 0.676 0.689 0.700 0.707 0.716 0.723 0.732 0.742 0.743 0.745
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.44 2.32 2.21 2.11
SR NM/LB 0.116 0.117 0.118 0.121 0.124 0.127 0.129 0.132 0.136 0.141
N1 % 84.9 85.6 86.2 86.8 87.1 87.3 87.6 87.9 87.9 87.9
F FLOW LB/H/ENG 1780 1787 1795 1794 1763 1735 1711 1688 1635 1581
IAS KT 319 319 319 318 314 312 309 307 302 296
48000 TAS KT 419 425 432 437 438 441 445 449 449 447
INDICATED MACH 0.677 0.690 0.703 0.715 0.719 0.728 0.738 0.747 0.751 0.750
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.53 2.40 2.29 2.19
SR NM/LB 0.118 0.119 0.120 0.122 0.124 0.127 0.130 0.133 0.137 0.141
N1 % 84.5 85.2 85.9 86.6 87 87.3 87.6 87.9 87.9 87.9
F FLOW LB/H/ENG 1768 1774 1781 1789 1765 1738 1714 1691 1638 1585
IAS KT 320 320 320 320 317 314 311 309 304 299
46000 TAS KT 421 427 433 440 442 444 448 452 452 451
INDICATED MACH 0.68 0.692 0.706 0.719 0.726 0.733 0.742 0.752 0.755 0.757
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.48 2.36 2.25
SR NM/LB 0.119 0.120 0.122 0.123 0.125 0.128 0.131 0.134 0.138 0.142
N1 % 84.2 84.8 85.5 86.2 87 87.3 87.6 87.9 87.9 87.9
F FLOW LB/H/ENG 1738 1744 1750 1757 1765 1740 1715 1693 1640 1587
IAS KT 320 320 320 320 320 317 314 311 306 301
44000 TAS KT 420 426 432 439 445 448 450 454 454 454
INDICATED MACH 0.680 0.692 0.706 0.719 0.733 0.740 0.747 0.756 0.760 0.762
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.46 2.35
SR NM/LB 0.121 0.122 0.124 0.125 0.126 0.129 0.131 0.134 0.139 0.143
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.