Embraer EMB145 - Page 876

FLIGHT PLANNING
EMB-145 A1 and A1P LB
AIRPLANE
OPERATIONS
MANUAL
1-05-35
Page
20
Code
02
REVISION 39
AOM-145/1114
MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING
FLIGHT WITH LANDING GEAR DOWN
AE3007A1 and A1P ENGINES
ALTITUDE: 12000 FT TO 18000 FT
BLEED: OPEN
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
12000 13000 14000 15000 16000 17000 18000
N1 % 82.5 82.9 83.2 83.9 84.5 85.3 86.0
F FLOW LB/H/ENG 1829 1796 1763 1754 1746 1745 1747
IAS KT 211 208 206 204 203 202 201
50000 TAS KT 252 253 253 255 258 261 264
INDICATED MACH 0.398 0.400 0.402 0.406 0.413 0.419 0.426
BUFFET MARGIN G 1.93 1.87 1.82 1.79 1.77 1.75 1.73
SR NM/LB 0.069 0.070 0.072 0.073 0.074 0.075 0.076
N1 % 82.4 82.7 83.0 83.3 84.2 85.2 85.9
F FLOW LB/H/ENG 1825 1792 1758 1728 1745 1755 1746
IAS KT 216 213 210 208 209 209 208
46000 TAS KT 258 259 259 260 265 269 272
INDICATED MACH 0.407 0.409 0.411 0.415 0.425 0.433 0.439
BUFFET MARGIN G 2.19 2.13 2.06 2.02 2.03 2.02 1.99
SR NM/LB 0.071 0.072 0.074 0.075 0.076 0.077 0.078
N1 % 82.4 82.7 83 83.3 84.2 85.2 85.9
F FLOW LB/H/ENG 1828 1795 1761 1731 1748 1759 1751
IAS KT 221 218 216 213 214 215 214
42000 TAS KT 264 264 266 266 271 277 279
INDICATED MACH 0.416 0.418 0.422 0.424 0.434 0.445 0.451
BUFFET MARGIN G 2.50 2.42 2.37 2.30 2.31 2.32 2.28
SR NM/LB 0.072 0.074 0.075 0.077 0.078 0.079 0.080
N1 % 82.4 82.7 83.0 83.3 84.2 85.2 85.9
F FLOW LB/H/ENG 1830 1798 1764 1735 1752 1763 1755
IAS KT 225 223 220 218 219 220 219
38000 TAS KT 268 269 270 271 277 282 285
INDICATED MACH 0.423 0.427 0.430 0.434 0.444 0.455 0.461
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.073 0.075 0.076 0.078 0.079 0.080 0.081
N1 % 82.4 82.7 83.0 83.3 84.2 85.1 85.9
F FLOW LB/H/ENG 1833 1801 1767 1737 1756 1766 1758
IAS KT 229 227 225 222 224 223 222
34000 TAS KT 272 273 275 275 282 286 290
INDICATED MACH 0.430 0.435 0.439 0.442 0.454 0.463 0.469
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.56
SR NM/LB 0.074 0.076 0.078 0.079 0.080 0.081 0.082