Embraer EMB145 - Page 843

AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
FAA
REVISION 40
1-05-30
Page
3
Code
03
AOM-145/1114
LONG RANGE CRUISE - ONE ENGINE INOPERATIVE
AE3007A1 AND AE3007A1P ENGINES
ALTITUDE: 5000 FT TO 14000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
5000 7000 9000 10000 11000 12000 13000 14000
N1 % 76.5 78.0 79.6 80.5 81.2 82.0 82.8 83.4
F FLOW LB/H/ENG 1849 1830 1815 1812 1804 1801 1801 1796
IAS KT 226 224 223 222 221 220 220 219
38000 TAS KT 243 248 253 257 259 262 266 268
INDICATED MACH 0.374 0.385 0.396 0.403 0.408 0.415 0.422 0.428
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.131 0.135 0.140 0.142 0.144 0.146 0.148 0.149
N1 % 75.2 76.5 78.0 78.9 79.7 80.6 81.3 82.1
F FLOW LB/H/ENG 1758 1738 1721 1715 1707 1705 1698 1695
IAS KT 222 220 218 218 217 216 215 214
36000 TAS KT 238 243 248 251 254 257 260 263
INDICATED MACH 0.367 0.377 0.389 0.395 0.400 0.407 0.413 0.419
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.135 0.140 0.144 0.146 0.149 0.151 0.153 0.155
N1 % 73.8 75.1 76.5 77.3 78.1 79.0 79.8 80.6
F FLOW LB/H/ENG 1668 1647 1629 1619 1613 1608 1600 1599
IAS KT 217 216 214 213 212 212 210 210
34000 TAS KT 233 238 243 245 248 251 254 257
INDICATED MACH 0.359 0.370 0.381 0.386 0.392 0.398 0.404 0.411
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.139 0.144 0.149 0.152 0.154 0.156 0.159 0.161
N1 % 72.5 73.6 74.9 75.6 76.5 77.2 78.1 78.9
F FLOW LB/H/ENG 1578 1556 1536 1526 1522 1512 1508 1501
IAS KT 213 211 209 208 208 207 206 205
32000 TAS KT 227 232 237 240 243 245 248 251
INDICATED MACH 0.351 0.362 0.372 0.377 0.384 0.389 0.395 0.401
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.144 0.149 0.154 0.157 0.160 0.162 0.165 0.167
N1 % 71.1 72.1 73.3 74.0 74.7 75.5 76.3 77.0
F FLOW LB/H/ENG 1492 1467 1445 1438 1429 1421 1415 1406
IAS KT 208 206 204 203 203 202 201 200
30000 TAS KT 222 226 231 234 237 239 242 245
INDICATED MACH 0.344 0.353 0.363 0.369 0.375 0.380 0.386 0.391
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.149 0.154 0.160 0.163 0.166 0.169 0.171 0.174
N1 % 69.8 70.7 71.8 72.5 73.0 73.7 74.4 75.2
F FLOW LB/H/ENG 1407 1381 1358 1351 1338 1332 1321 1316
IAS KT 203 201 199 199 197 197 196 195
28000 TAS KT 217 221 226 228 230 233 236 239
INDICATED MACH 0.335 0.345 0.354 0.360 0.365 0.371 0.376 0.382
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.154 0.160 0.166 0.169 0.172 0.175 0.178 0.181
INCREASE / DECREASE N1% BY 1 % PER 5°C ABOVE / BELOW ISA CONDITIONS.
INCREASE / DECREASE FUEL FLOW 1 % PER 5°C ABOVE / BELOW ISA CONDITIONS.
INCREASE / DECREASE TAS BY 3 KT PER 5°C ABOVE / BELOW ISA CONDITIONS.
FOR ANTI-ICE ON:
INCREASE N1 BY 0.7 % AND FUEL FLOW BY 8%.
DECREASE SR BY 7%.