AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
FAA
REVISION 40
1-05-30
Page
15
Code
03
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 200 200 200 200 200 - - - -
TAS KT 199.1 214 230.5 248.9 269.3 - - - -
36000 Mach 0.302 0.331 0.363 0.399 0.44 - - - -
N1 % 69 72.7 76.5 81 85.4 - - - -
FF LB/H/ENG 1735 1695 1675 1677 1708 - - - -
FC LB/H 1735 1695 1675 1677 1708 - - - -
IAS KT 200 200 200 200 200 - - - -
TAS KT 198.9 213.8 230.3 248.6 269.1 - - - -
34000 Mach 0.302 0.331 0.363 0.399 0.44 - - - -
N1 % 68.1 71.7 75.5 80.1 84.4 - - - -
FF LB/H/ENG 1685 1643 1619 1617 1642 - - - -
FC LB/H 1685 1643 1619 1617 1642 - - - -
IAS KT 200 200 200 200 200 - - - -
TAS KT 198.7 213.6 230.1 248.4 268.8 - - - -
32000 Mach 0.302 0.331 0.363 0.399 0.44 - - - -
N1 % 67.2 70.9 74.6 79.2 83.4 - - - -
FF LB/H/ENG 1637 1593 1567 1561 1580 - - - -
FC LB/H 1637 1593 1567 1561 1580 - - - -
IAS KT 200 200 200 200 200 200 - - -
TAS KT 198.5 213.4 229.9 248.2 268.6 291.3 - - -
30000 Mach 0.302 0.331 0.363 0.399 0.44 0.487 - - -
N1 % 66.3 70 73.7 78.2 82.4 86.7 - - -
FF LB/H/ENG 1593 1546 1517 1508 1521 1564 - - -
FC LB/H 1593 1546 1517 1508 1521 1564 - - -
IAS KT 200 200 200 200 200 200 - - -
TAS KT 198.3 213.2 229.7 248 268.3 291.1 - - -
28000 Mach 0.302 0.331 0.363 0.399 0.44 0.487 - - -
N1 % 65.5 69.2 72.9 77.1 81.4 85.8 - - -
FF LB/H/ENG 1551 1503 1471 1458 1467 1503 - - -
FC LB/H 1551 1503 1471 1458 1467 1503 - - -
IAS KT 200 200 200 200 200 200 - - -
TAS KT 198.2 213.1 229.5 247.8 268.2 290.9 - - -
26000 Mach 0.302 0.331 0.363 0.399 0.44 0.487 - - -
N1 % 62.7 68.4 72.1 76.1 80.5 84.8 - - -
FF LB/H/ENG 1427 1462 1428 1411 1416 1446 - - -
FC LB/H 1427 1462 1428 1411 1416 1446 - - -
NOTE: MACH setting and FF KG/H/ENG remain constant, regardless
of the temperature change.
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