Embraer EMB145 - Page 842

FLIGHT PLANNING
EMB-145 A1 and A1P LB
FAA
AIRPLANE
OPERATIONS
MANUAL
1-05-30
Page
2
Code
03
REVISION 40
AOM-145/1114
LONG RANGE CRUISE - ONE ENGINE INOPERATIVE
AE3007A1 AND AE3007A1P ENGINES
ALTITUDE: 5000 FT TO 14000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
5000 7000 9000 10000 11000 12000 13000 14000
N1 % 83.7 85.1 86.4 87.3 88.1 88.7 88.3 88.2
F FLOW LB/H/ENG 2382 2377 2373 2376 2378 2364 2294 2233
IAS KT 249 247 245 245 244 242 234 227
49000 TAS KT 268 274 280 283 287 288 284 280
INDICATED MACH 0.411 0.423 0.436 0.443 0.450 0.454 0.449 0.444
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.53 2.38 2.24
SR NM/LB 0.112 0.115 0.118 0.119 0.121 0.122 0.123 0.124
N1 % 81.9 83.4 84.7 85.6 86.3 87.1 87.9 88.6
F FLOW LB/H/ENG 2231 2223 2215 2216 2215 2216 2219 2224
IAS KT 243 241 239 239 238 237 236 236
46000 TAS KT 261 267 273 276 280 283 286 290
INDICATED MACH 0.401 0.413 0.425 0.432 0.439 0.445 0.452 0.460
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.54
SR NM/LB 0.117 0.120 0.123 0.125 0.126 0.128 0.129 0.130
N1 % 80.6 82.2 83.6 84.4 85.1 85.8 86.6 87.5
F FLOW LB/H/ENG 2133 2120 2114 2111 2108 2111 2113 2114
IAS KT 239 237 236 235 234 233 232 232
44000 TAS KT 257 262 269 272 275 278 281 285
INDICATED MACH 0.394 0.406 0.419 0.425 0.431 0.438 0.445 0.452
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.120 0.124 0.127 0.129 0.130 0.132 0.133 0.135
N1 % 79.3 80.8 82.4 83.2 83.9 84.6 85.3 86.1
F FLOW LB/H/ENG 2038 2022 2012 2007 2008 2006 2004 2005
IAS KT 235 233 231 230 230 229 228 227
42000 TAS KT 252 258 264 266 270 273 276 279
INDICATED MACH 0.388 0.399 0.411 0.417 0.424 0.431 0.437 0.444
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.124 0.127 0.131 0.133 0.134 0.136 0.138 0.139
N1 % 77.9 79.4 81.0 81.9 82.6 83.3 84.0 84.8
F FLOW LB/H/ENG 1942 1927 1912 1909 1906 1901 1901 1902
IAS KT 230 229 227 226 226 225 224 223
40000 TAS KT 247 253 258 262 265 268 271 274
INDICATED MACH 0.381 0.392 0.404 0.410 0.417 0.423 0.429 0.437
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.127 0.131 0.135 0.137 0.139 0.141 0.142 0.144
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%.