Embraer EMB145 - Page 821

AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
REVISION 40
1-05-15
Page
15
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 CONDITIONS
WEIGHT ALTITUDE (FT)
(LB)
5000 10000 11000 12000 13000 14000 15000 16000 17000 18000
N1 % 62.5 75.3 76.0 76.7 77.4 78.2 79.0 79.8 80.7 81.5
F FLOW LB/H/ENG 1119 1610 1606 1604 1602 1600 1599 1599 1600 1601
IAS KT 250 320 320 320 320 320 320 320 320 320
34000 TAS KT 267 366 371 376 382 387 393 399 405 411
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 0.119 0.114 0.116 0.117 0.119 0.121 0.123 0.125 0.126 0.128
N1 % 61.8 74.8 75.4 76.1 76.8 77.6 78.4 79.2 80.0 80.8
F FLOW LB/H/ENG 1093 1578 1574 1571 1568 1566 1564 1563 1563 1563
IAS KT 250 320 320 320 320 320 320 320 320 320
31000 TAS KT 267 365 370 375 381 386 392 398 404 410
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 0.122 0.116 0.118 0.120 0.121 0.123 0.125 0.127 0.129 0.131
N1 % 61.0 74.3 74.9 75.6 76.3 77.0 77.7 78.5 79.3 80.2
F FLOW LB/H/ENG 1068 1547 1542 1538 1535 1532 1530 1528 1527 1526
IAS KT 250 320 320 320 320 320 320 320 320 320
28000 TAS KT 266 364 369 375 380 386 391 397 403 409
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 0.125 0.118 0.120 0.122 0.124 0.126 0.128 0.130 0.132 0.134
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.