Embraer EMB145 - Page 820

FLIGHT PLANNING
EMB-145 A1 and A1P LB
AIRPLANE
OPERATIONS
MANUAL
1-05-15
Page
14
Code
02
REVISION 40
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 CONDITIONS
WEIGHT ALTITUDE (FT)
(LB)
5000 10000 11000 12000 13000 14000 15000 16000 17000 18000
N1 % 64.6 76.7 77.4 78.2 79 79.8 80.7 82.4 82.4 83.1
F FLOW LB/H/ENG 1197 1699 1697 1696 1696 1696 1697 1716 1702 1706
IAS KT 250 320 320 320 320 320 320 320 320 320
42000 TAS KT 268 368 373 379 384 390 395 405 407 413
INDICATED MACH 0.413 0.576 0.587 0.598 0.608 0.620 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 0.112 0.108 0.110 0.112 0.113 0.115 0.116 0.118 0.120 0.121
N1 % 64.1 76.3 77 77.8 78.6 79.4 80.3 81.9 81.9 82.7
F FLOW LB/H/ENG 1177 1675 1673 1672 1671 1671 1672 1689 1675 1678
IAS KT 250 320 320 320 320 320 320 320 320 320
40000 TAS KT 268 367 373 378 384 389 395 404 406 412
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 0.114 0.110 0.111 0.113 0.115 0.116 0.118 0.12 0.121 0.123
N1 % 63.6 76.0 76.7 77.4 78.2 79.0 79.8 80.7 81.5 82.3
F FLOW LB/H/ENG 1157 1653 1650 1648 1647 1647 1647 1648 1650 1652
IAS KT 250 320 320 320 320 320 320 320 320 320
38000 TAS KT 268 367 372 377 383 389 394 400 406 412
INDICATED MACH 0.413 0.576 0.587 0.598 0.608 0.620 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 0.116 0.111 0.113 0.115 0.116 0.118 0.120 0.121 0.123 0.125
N1 % 63.1 75.6 76.3 77.0 77.8 78.6 79.4 80.3 81.1 81.9
F FLOW LB/H/ENG 1138 1631 1628 1626 1624 1623 1623 1623 1624 1626
IAS KT 250 320 320 320 320 320 320 320 320 320
36000 TAS KT 268 366 372 377 382 388 394 399 405 411
INDICATED MACH 0.413 0.576 0.587 0.598 0.608 0.620 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 0.118 0.112 0.114 0.116 0.118 0.120 0.121 0.123 0.125 0.126
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.