Embraer EMB145 - Page 915

AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
REVISION 38
1-05-50
Page
5
Code
02
AOM-145/1114
LONG RANGE CRUISE - ALL ENGINES OPERATING
AE3007A1 and AE3007A1P ENGINES
ALTITUDE: 5000 FT TO 18000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ANTI ICE: ON (Engine or all)
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
5000 10000 11000 12000 13000 14000 15000 16000 17000 18000
N1 % 64.1 66.9 67.5 68.1 68.6 69.1 69.7 70.2 70.8 71.4
F FLOW LB/H/ENG 1294 1207 1192 1178 1164 1152 1139 1128 1117 1107
IAS KT 247 241 239 238 237 236 235 233 232 231
40000 TAS KT 265 278 280 283 286 289 292 295 298 301
INDICATED MACH 0.409 0.436 0.442 0.448 0.454 0.460 0.467 0.473 0.480 0.487
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 0.102 0.115 0.117 0.120 0.123 0.125 0.128 0.131 0.133 0.136
N1 % 62.9 65.9 66.5 67.1 67.6 68.1 68.6 69.2 69.7 70.3
F FLOW LB/H/ENG 1248 1163 1148 1134 1117 1104 1092 1080 1069 1058
IAS KT 243 237 236 235 233 232 231 229 228 227
38000 TAS KT 260 273 276 279 281 284 286 289 292 295
INDICATED MACH 0.402 0.429 0.435 0.441 0.446 0.453 0.459 0.466 0.472 0.479
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 0.104 0.117 0.120 0.123 0.126 0.128 0.131 0.134 0.137 0.140
N1 % 61.7 64.7 65.3 65.9 66.5 67.1 67.6 68.1 68.6 69.2
F FLOW LB/H/ENG 1203 1116 1101 1087 1073 1060 1045 1033 1021 1011
IAS KT 239 233 232 230 229 228 226 225 224 223
36000 TAS KT 256 268 270 273 276 279 281 284 287 290
INDICATED MACH 0.395 0.421 0.427 0.433 0.439 0.445 0.451 0.457 0.464 0.470
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 0.106 0.120 0.123 0.126 0.129 0.132 0.135 0.138 0.141 0.143
N1 % 60.6 63.5 64.1 64.7 65.3 65.8 66.4 67.0 67.5 68.0
F FLOW LB/H/ENG 1160 1070 1055 1040 1026 1013 1000 988 976 964
IAS KT 235 228 227 226 225 224 222 221 220 219
34000 TAS KT 251 263 265 268 270 273 276 279 282 284
INDICATED MACH 0.389 0.414 0.419 0.425 0.431 0.437 0.443 0.449 0.456 0.462
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 0.123 0.126 0.129 0.132 0.135 0.138 0.141 0.144 0.147
N1 % 59.3 62.3 62.8 63.4 64.0 64.6 65.2 65.7 66.3 66.9
F FLOW LB/H/ENG 1115 1028 1010 995 980 967 954 941 929 918
IAS KT 231 224 223 221 220 219 218 217 215 214
32000 TAS KT 246 258 260 262 265 267 270 273 276 278
INDICATED MACH 0.382 0.407 0.411 0.416 0.422 0.428 0.434 0.440 0.446 0.453
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 0.111 0.125 0.129 0.132 0.135 0.138 0.142 0.145 0.148 0.152
INCREASE/DECREASE N1% BY 1.1% PER 5°C ABOVE/BELOW ISA CONDITION.
INCREASE/DECREASE FUEL FLOW BY 1.2% PER 5°C ABOVE/BELOW ISA CONDITION.
INCREASE/DECREASE TAS BY 4 KT PER 5°C ABOVE/BELOW ISA CONDITION.