Embraer EMB145, Operation Manual

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AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
FAA
REVISION 40
1-05-30
Page
7
Code
03
AOM
-145/
111
4
LONG RANGE CRUISE - ONE ENGINE INOPERATIVE
AE3007A1 AND AE3007A1P ENGINES
ALTITUDE: 23000 FT TO 30000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
23000 24000 25000 26000 27000 28000 29000 30000
N1 % 89.7 90.7 90.9 91.3 - - - -
F FLOW LB/H/ENG 1756 1711 1646 1577 - - - -
IAS KT 205 198 187 170 - - - -
38000 TAS KT 290 285 274 254 - - - -
INDICATED MACH 0.479 0.472 0.456 0.425 - - - -
BUFFET MARGIN G 2.26 2.11 1.90 1.60 - - - -
SR NM/LB 0.164 0.166 0.166 0.161 - - - -
N1 % 89.3 90.3 90.0 91.1 91.3 - - -
F FLOW LB/H/ENG 1721 1713 1643 1603 1543 - - -
IAS KT 209 206 197 190 179 - - -
36000 TAS KT 295 296 288 283 271 - - -
INDICATED MACH 0.487 0.492 0.481 0.474 0.456 - - -
BUFFET MARGIN G 2.45 2.39 2.20 2.05 1.83 - - -
SR NM/LB 0.171 0.173 0.174 0.177 0.176 - - -
N1 % 87.4 88.4 89.7 90.7 90.5 91.5 91.7 -
F FLOW LB/H/ENG 1605 1611 1619 1607 1547 1509 1454 -
IAS KT 203 203 202 199 191 184 173 -
34000 TAS KT 288 291 295 296 289 284 272 -
INDICATED MACH 0.476 0.484 0.493 0.496 0.486 0.479 0.462 -
BUFFET MARGIN G 2.49 2.46 2.43 2.35 2.17 2.02 1.81 -
SR NM/LB 0.179 0.181 0.182 0.184 0.185 0.188 0.187 -
N1 % 85.9 86.6 87.5 88.7 90.2 91.1 90.9 91.9
F FLOW LB/H/ENG 1497 1500 1505 1513 1521 1511 1459 1431
IAS KT 199 198 197 197 196 194 186 180
32000 TAS KT 281 284 288 292 296 297 291 287
INDICATED MACH 0.465 0.473 0.481 0.490 0.499 0.503 0.494 0.489
BUFFET MARGIN G 2.54 2.50 2.47 2.44 2.40 2.33 2.16 2.03
SR NM/LB 0.188 0.190 0.192 0.193 0.195 0.196 0.198 0.200
N1 % 84.2 85.0 85.7 86.5 87.6 89.0 90.5 91.7
F FLOW LB/H/ENG 1389 1393 1397 1400 1406 1414 1424 1434
IAS KT 194 193 192 192 191 191 190 190
30000 TAS KT 274 278 281 285 289 293 297 301
INDICATED MACH 0.454 0.462 0.470 0.478 0.486 0.495 0.505 0.515
BUFFET MARGIN G 2.56 2.56 2.52 2.49 2.45 2.42 2.39 2.35
SR NM/LB 0.197 0.199 0.201 0.203 0.205 0.207 0.209 0.210
N1 % 82.4 83.2 84.1 84.8 85.5 86.5 87.6 89.2
F FLOW LB/H/ENG 1287 1286 1290 1293 1297 1301 1308 1315
IAS KT 189 188 187 187 186 185 185 184
28000 TAS KT 266 270 273 277 281 285 289 293
INDICATED MACH 0.442 0.449 0.457 0.465 0.474 0.482 0.491 0.500
BUFFET MARGIN G 2.56 2.56 2.56 2.54 2.51 2.47 2.44 2.41
SR NM/LB 0.207 0.210 0.212 0.214 0.217 0.219 0.221 0.223
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%.