Embraer EMB145 - Page 925

AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
REVISION 38
1-05-50
Page
15
Code
02
AOM-145/1114
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 % 61.4 74.7 75.3 76.0 76.7 77.4 78.2 78.9 79.7 80.5
F FLOW LB/H/ENG 1214 1741 1737 1733 1730 1729 1728 1729 1731 1733
IAS KT 250 320 320 320 320 320 320 320 320 320
30000 TAS KT 266 364 369 374 380 385 391 397 403 409
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
SPECIFIC RANGENM/LB0.1100.104 0.106 0.108 0.110 0.112 0.113 0.115 0.116 0.118
N1 % 60.9 74.3 75.0 75.6 76.3 77.0 77.7 78.5 79.2 80.0
F FLOW LB/H/ENG 1197 1719 1714 1710 1707 1705 1704 1704 1705 1707
IAS KT 250 320 320 320 320 320 320 320 320 320
28000 TAS KT 266 363 369 374 379 385 390 396 402 408
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/LB0.1110.106 0.107 0.109 0.111 0.113 0.115 0.116 0.118 0.119
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.