Embraer EMB145 - Page 845

AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
FAA
REVISION 40
1-05-30
Page
5
Code
03
AOM-145/1114
LONG RANGE CRUISE - ONE ENGINE INOPERATIVE
AE3007A1 AND AE3007A1P ENGINES
ALTITUDE: 15000 FT TO 22000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
15000 16000 17000 18000 19000 20000 21000 22000
N1 % 84.1 84.9 85.7 86.6 87.2 88.0 88.9 90.0
F FLOW LB/H/ENG 1796 1797 1797 1805 1805 1811 1820 1831
IAS KT 218 217 217 216 215 215 214 214
38000 TAS KT 272 275 278 283 286 289 293 298
INDICATED MACH 0.435 0.442 0.449 0.457 0.464 0.472 0.480 0.489
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.53 2.50 2.48 2.45
SR NM/LB 0.151 0.153 0.155 0.157 0.158 0.160 0.161 0.163
N1 % 82.8 83.5 84.2 85.0 85.9 86.6 87.3 88.2
F FLOW LB/H/ENG 1696 1695 1695 1693 1698 1699 1704 1711
IAS KT 214 213 212 211 211 210 209 209
36000 TAS KT 266 270 273 276 280 283 287 291
INDICATED MACH 0.427 0.433 0.440 0.447 0.455 0.462 0.470 0.478
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.54 2.51 2.48
SR NM/LB 0.157 0.159 0.161 0.163 0.165 0.167 0.168 0.170
N1 % 81.3 82.0 82.7 83.5 84.3 85.1 86.0 86.6
F FLOW LB/H/ENG 1594 1590 1589 1592 1590 1593 1599 1599
IAS KT 209 208 207 207 206 206 205 204
34000 TAS KT 260 263 266 270 273 277 281 284
INDICATED MACH 0.417 0.423 0.430 0.438 0.444 0.452 0.461 0.467
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.52
SR NM/LB 0.163 0.165 0.168 0.170 0.172 0.174 0.176 0.177
N1 % 79.7 80.5 81.3 81.9 82.7 83.4 84.3 85.2
F FLOW LB/H/ENG 1496 1493 1492 1489 1488 1488 1489 1494
IAS KT 204 204 203 202 201 201 200 200
32000 TAS KT 254 257 261 263 267 270 273 278
INDICATED MACH 0.407 0.414 0.421 0.427 0.435 0.442 0.449 0.458
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.170 0.172 0.175 0.177 0.179 0.181 0.184 0.186
N1 % 77.9 78.8 79.6 80.3 81.1 81.8 82.6 83.4
F FLOW LB/H/ENG 1403 1399 1394 1389 1389 1387 1389 1386
IAS KT 200 199 198 197 196 196 195 194
30000 TAS KT 248 251 254 257 260 263 267 270
INDICATED MACH 0.398 0.405 0.411 0.417 0.424 0.431 0.439 0.446
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.177 0.179 0.182 0.185 0.187 0.190 0.192 0.195
N1 % 76.0 76.8 77.7 78.6 79.3 80.1 80.8 81.6
F FLOW LB/H/ENG 1310 1302 1297 1296 1290 1290 1285 1287
IAS KT 194 193 193 192 191 191 190 189
28000 TAS KT 241 244 247 250 253 257 259 263
INDICATED MACH 0.388 0.394 0.400 0.407 0.413 0.421 0.427 0.434
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.184 0.187 0.190 0.193 0.196 0.199 0.202 0.204
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%.