Embraer EMB145, Operation Manual

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FLIGHT PLANNING
EMB-145 A1 and A1P LB
AIRPLANE
OPERATIONS
MANUAL
1-05-50
Page
14
Code
02 REVISION 38
A
O
M-145/1
114
MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING
AE3007A1 and AE3007A1P ENGINES
ALTITUDE: 5000 FT TO 18000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ANTI ICE: ON (Engine or all)
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
5000 10000 11000 12000 13000 14000 15000 16000 17000 18000
N1 % 64.1 76.4 77.1 77.9 78.7 79.4 80.2 81.0 81.9 82.7
F FLOW LB/H/ENG 1310 1855 1853 1852 1853 1854 1857 1861 1866 1872
IAS KT 250 320 320 320 320 320 320 320 320 320
40000 TAS KT 268 367 372 377 383 388 394 400 406 412
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
SPECIFIC RANGENM/LB0.1020.099 0.100 0.102 0.103 0.105 0.106 0.107 0.109 0.110
N1 % 63.5 76.0 76.7 77.5 78.3 79.0 79.8 80.6 81.4 82.3
F FLOW LB/H/ENG 1289 1832 1829 1828 1827 1828 1830 1833 1838 1843
IAS KT 250 320 320 320 320 320 320 320 320 320
38000 TAS KT 267 366 371 377 382 388 394 399 405 411
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
SPECIFIC RANGENM/LB0.1040.100 0.102 0.103 0.105 0.106 0.107 0.109 0.110 0.112
N1 % 62.9 75.6 76.4 77.1 77.9 78.6 79.4 80.2 81.0 81.9
F FLOW LB/H/ENG 1270 1809 1805 1803 1803 1803 1804 1807 1810 1815
IAS KT 250 320 320 320 320 320 320 320 320 320
36000 TAS KT 267 366 371 376 382 387 393 399 405 411
INDICATED MACH 0.413 0.576 0.587 0.598 0.608 0.620 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
SPECIFIC RANGENM/LB0.1050.101 0.103 0.104 0.106 0.107 0.109 0.110 0.112 0.113
N1 % 62.4 75.3 76.0 76.7 77.5 78.2 79.0 79.7 80.6 81.4
F FLOW LB/H/ENG 1251 1786 1782 1780 1778 1778 1779 1781 1784 1788
IAS KT 250 320 320 320 320 320 320 320 320 320
34000 TAS KT 267 365 370 376 381 387 392 398 404 410
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
SPECIFIC RANGENM/LB0.1070.102 0.104 0.105 0.107 0.109 0.110 0.112 0.113 0.115
N1 % 61.9 75.0 75.6 76.4 77.1 77.8 78.6 79.3 80.1 81.0
F FLOW LB/H/ENG 1232 1764 1759 1756 1754 1753 1754 1755 1757 1761
IAS KT 250 320 320 320 320 320 320 320 320 320
32000 TAS KT 266 365 370 375 381 386 392 398 403 409
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
SPECIFIC RANGENM/LB0.1080.103 0.105 0.107 0.108 0.110 0.112 0.113 0.115 0.116
INCREASE/DECREASE N1% BY 1.1% PER 5°C ABOVE/BELOW ISA CONDITION.
INCREASE/DECREASE FUEL FLOW BY 1.2% PER 5°C ABOVE/BELOW ISA CONDITION.
INCREASE/DECREASE TAS BY 4 KT PER 5°C ABOVE/BELOW ISA CONDITION.