FLIGHT PLANNING
EMB-145 A1 and A1P LB
FAA
AIRPLANE
OPERATIONS
MANUAL
1-05-30
Page
12
Code
03
REVISION 40
AOM-145/1114
HOLDING - ONE ENGINE INOPERATIVE
AE3007A1 AND AE3007A1P ENGINES
CRUISE CONFIGURATION
BLEED: OPEN
ANTI-ICE: OFF
MINIMUM FUEL CONSUMPTION SPEED
STANDARD ATMOSPHERE
WEIGHT ALTITUDE (FT)
(LB)
0 5000 10000 15000 20000 25000 30000 35000 37000
IAS KT 179 174 171 169 - - - - -
TAS KT 178.6 187 197.8 211.7 - - - - -
49000 Mach 0.27 0.288 0.311 0.339 - - - - -
N1 % 74.3 78.4 83.1 87.4 - - - - -
FF LB/H/ENG 1931 1925 1946 1995 - - - - -
FC LB/H 1931 1925 1946 1995 - - - - -
IAS KT 175 170 167 165 164 - - - -
TAS KT 174.9 182.6 192.6 205.5 222.2 - - - -
46000 Mach 0.265 0.282 0.303 0.329 0.363 - - - -
N1 % 72.6 76.4 81.1 85.6 90.9 - - - -
FF LB/H/ENG 1809 1796 1807 1845 1910 - - - -
FC LB/H 1809 1796 1807 1845 1910 - - - -
IAS KT 173 168 164 161 161 - - - -
TAS KT 172.3 179.6 189.1 201.3 217.1 - - - -
44000 Mach 0.261 0.277 0.298 0.323 0.355 - - - -
N1 % 71.3 75.1 79.7 84.3 89 - - - -
FF LB/H/ENG 1730 1711 1717 1747 1804 - - - -
FC LB/H 1730 1711 1717 1747 1804 - - - -
IAS KT 170 165 161 158 157 - - - -
TAS KT 169.7 176.7 185.6 197.1 212.1 - - - -
42000 Mach 0.258 0.273 0.292 0.316 0.347 - - - -
N1 % 70 73.8 78.2 82.8 87.3 - - - -
FF LB/H/ENG 1653 1629 1629 1652 1700 - - - -
FC LB/H 1653 1629 1629 1652 1700 - - - -
IAS KT 168 162 158 155 153 - - - -
TAS KT 167.2 173.7 182.1 193 207.1 - - - -
40000 Mach 0.254 0.269 0.287 0.31 0.339 - - - -
N1 % 68.6 72.5 76.6 81.4 85.8 - - - -
FF LB/H/ENG 1577 1548 1542 1559 1599 - - - -
FC LB/H 1577 1548 1542 1559 1599 - - - -
IAS KT 166 160 155 152 150 150 - - -
TAS KT 164.7 170.7 178.5 188.7 202 219.3 - - -
38000 Mach 0.25 0.264 0.282 0.304 0.331 0.367 - - -
N1 % 67.3 71.1 75 79.8 84.4 90.1 - - -
FF LB/H/ENG 1503 1469 1457 1468 1501 1558 - - -
FC LB/H 1503 1469 1457 1468 1501 1558 - - -
NOTE: MACH setting and FF KG/H/ENG remain constant, regardless
of the temperature change.
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