Embraer EMB145 - Page 811

AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
REVISION 40
1-05-15
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
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
5000 10000 11000 12000 13000 14000 15000 16000 17000 18000
N1 % 64.6 67.8 68.4 69 69.4 69.9 70.4 70.9 71.5 72.1
F FLOW LB/H/ENG 1196 1133 1122 1112 1102 1093 1084 1076 1068 1061
IAS KT 250 245 243 242 241 240 239 238 237 236
42000 TAS KT 268 283 285 289 292 295 298 301 305 308
INDICATED MACH 0.413 0.443 0.449 0.455 0.462 0.469 0.476 0.483 0.49 0.498
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 0.112 0.125 0.127 0.13 0.132 0.135 0.138 0.14 0.143 0.145
N1 % 63.7 66.7 67.3 67.9 68.5 69 69.4 70 70.5 71.1
F FLOW LB/H/ENG 1158 1090 1078 1066 1056 1046 1037 1029 1021 1013
IAS KT 247 241 239 238 237 236 235 234 233 232
40000 TAS KT 265 278 281 283 286 289 293 296 299 303
INDICATED MACH 0.408 0.436 0.442 0.448 0.454 0.461 0.468 0.475 0.482 0.489
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 0.114 0.127 0.13 0.133 0.136 0.138 0.141 0.144 0.147 0.149
N1 % 62.5 65.6 66.2 66.8 67.4 68 68.5 69 69.5 70
F FLOW LB/H/ENG 1116 1046 1035 1023 1012 1002 992 983 974 967
IAS KT 243 237 235 234 233 232 231 230 229 228
38000 TAS KT 260 273 276 279 281 284 287 290 294 297
INDICATED MACH 0.401 0.428 0.434 0.44 0.447 0.453 0.459 0.466 0.473 0.48
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 0.117 0.13 0.133 0.136 0.139 0.142 0.145 0.148 0.151 0.154
N1 % 61.4 64.4 65 65.6 66.2 66.9 67.5 68.1 68.5 69
F FLOW LB/H/ENG 1075 1002 990 978 968 957 947 938 930 921
IAS KT 239 232 231 230 229 228 227 226 225 223
36000 TAS KT 256 268 270 273 276 279 282 285 288 291
INDICATED MACH 0.395 0.42 0.426 0.432 0.438 0.445 0.451 0.458 0.465 0.472
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 0.119 0.134 0.137 0.14 0.143 0.146 0.149 0.152 0.155 0.158
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%.