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