Embraer EMB145 - Page 810

FLIGHT PLANNING
EMB-145 A1 and A1P LB
AIRPLANE
OPERATIONS
MANUAL
1-05-15
Page
4
Code
02
REVISION 40
AOM-145/1114
LONG RANGE CRUISE - ALL ENGINES OPERATING
AE3007A1 AND AE3007A1P ENGINES
ALTITUDE : 5000 FT TO 18000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
5000 10000 11000 12000 13000 14000 15000 16000 17000 18000
N1 % 66.7 71.6 72.2 72.8 73.5 74.1 74.7 75.4 76.1 76.9
Fuel Flow LB/H/ENG 1285 1317 1308 1299 1291 1281 1274 1268 1263 1258
IAS KT 250 261 260 259 258 256 255 254 253 252
50000 TAS KT 269 301 305 308 311 314 318 321 325 329
INDICATED MACH 0.414 0.471 0.478 0.485 0.492 0.499 0.506 0.514 0.522 0.530
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.52
SR NM/LB 0.105 0.114 0.116 0.118 0.120 0.123 0.125 0.127 0.129 0.131
N1 % 66.1 70.7 71.3 71.9 72.5 73.1 73.8 74.5 75.2 75.9
Fuel Flow LB/H/ENG 1259 1270 1259 1250 1242 1234 1226 1220 1215 1208
IAS KT 250 257 256 255 254 253 252 251 250 248
48000 TAS KT 269 296 300 303 306 310 313 317 321 324
INDICATED MACH 0.413 0.464 0.471 0.478 0.485 0.492 0.500 0.507 0.515 0.523
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.107 0.117 0.119 0.121 0.123 0.126 0.128 0.130 0.132 0.134
N1 % 65.3 69.7 70.1 70.6 71.1 71.7 72.3 72.9 73.6 74.3
F FLOW LB/H/ENG 1232 1224 1213 1203 1194 1186 1178 1171 1165 1159
IAS KT 248 252 251 250 249 248 247 246 245 244
46000 TAS KT 267 292 295 298 301 305 308 312 315 319
INDICATED MACH 0.41 0.457 0.463 0.47 0.477 0.484 0.491 0.499 0.506 0.514
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.108 0.119 0.122 0.124 0.126 0.129 0.131 0.133 0.135 0.138
N1 % 64.9 68.8 69.4 69.8 70.2 70.7 71.3 71.9 72.5 73.2
F FLOW LB/H/ENG 1214 1180 1169 1158 1147 1138 1130 1122 1115 1109
IAS KT 249 249 248 246 245 244 243 242 241 240
44000 TAS KT 268 288 291 294 297 300 303 306 310 314
INDICATED MACH 0.411 0.45 0.457 0.463 0.469 0.476 0.483 0.49 0.498 0.506
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.11 0.122 0.124 0.127 0.129 0.132 0.134 0.137 0.139 0.141
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 5 KT PER 5°C ABOVE / BELOW ISA CONDITIONS.
FOR ANTI-ICE ON:
INCREASE N1 BY 0.6 % AND FUEL FLOW BY 8%.
DECREASE SR BY 9%.