FLIGHT PLANNING
EMB-145 A1 and A1P LB
FAA
AIRPLANE
OPERATIONS
MANUAL
1-05-30
Page
14
Code
03
REVISION 40
AOM-145/1114
HOLDING - ONE ENGINE INOPERATIVE
AE3007A1 AND AE3007A1P ENGINES
CRUISE CONFIGURATION
BLEED: OPEN
ANTI-ICE: ON (WITH ICE ACCRETION)
STANDARD ATMOSPHERE
WEIGHT ALTITUDE (FT)
(LB)
0 5000 10000 15000 20000 25000 30000 35000 37000
IAS KT 200 200 200 200 - - - - -
TAS KT 200.3 215.3 231.9 250.4 - - - - -
49000 Mach 0.302 0.331 0.363 0.399 - - - - -
N1 % 74.9 78.9 83.3 87.6 - - - - -
FF LB/H/ENG 2130 2110 2118 2159 - - - - -
FC LB/H 2130 2110 2118 2159 - - - - -
IAS KT 200 200 200 200 - - - - -
TAS KT 200 215 231.6 250 - - - - -
46000 Mach 0.302 0.331 0.363 0.399 - - - - -
N1 % 73.6 77.3 81.7 86.2 - - - - -
FF LB/H/ENG 2028 2003 2003 2033 - - - - -
FC LB/H 2028 2003 2003 2033 - - - - -
IAS KT 200 200 200 200 - - - - -
TAS KT 199.8 214.8 231.4 249.8 - - - - -
44000 Mach 0.302 0.331 0.363 0.399 - - - - -
N1 % 72.6 76.3 80.7 85.2 - - - - -
FF LB/H/ENG 1963 1935 1930 1954 - - - - -
FC LB/H 1963 1935 1930 1954 - - - - -
IAS KT 200 200 200 200 200 - - - -
TAS KT 199.6 214.6 231.1 249.6 270 - - - -
42000 Mach 0.302 0.331 0.363 0.399 0.44 - - - -
N1 % 71.7 75.3 79.7 84.1 88.3 - - - -
FF LB/H/ENG 1902 1870 1861 1879 1931 - - - -
FC LB/H 1902 1870 1861 1879 1931 - - - -
IAS KT 200 200 200 200 200 - - - -
TAS KT 199.4 214.4 230.9 249.3 269.8 - - - -
40000 Mach 0.302 0.331 0.363 0.399 0.44 - - - -
N1 % 70.8 74.4 78.6 83.1 87.3 - - - -
FF LB/H/ENG 1843 1809 1796 1808 1852 - - - -
FC LB/H 1843 1809 1796 1808 1852 - - - -
IAS KT 200 200 200 200 200 - - - -
TAS KT 199.2 214.2 230.7 249.1 269.5 - - - -
38000 Mach 0.302 0.331 0.363 0.399 0.44 - - - -
N1 % 69.9 73.5 77.6 82 86.3 - - - -
FF LB/H/ENG 1788 1750 1733 1741 1778 - - - -
FC LB/H 1788 1750 1733 1741 1778 - - - -
NOTE: MACH setting and FF KG/H/ENG remain constant, regardless
of the temperature change.
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