Embraer EMB145 - Page 931

AIRPLANE
OPERATIONS
MANUAL
FLIGHT PLANNING
EMB-145 A1 and A1P LB
REVISION 38
1-05-50
Page
21
Code
02
AOM-145/1114
MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING
AE3007A1 and AE3007A1P ENGINES
ALTITUDE: 29000 FT TO 37000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ANTI ICE: ON (Engine or all)
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
29000 30000 31000 32000 33000 34000 35000 36000 37000
N1 % 85.5 85.5 85.4 85.3 85.6 85.4 85.2 85.1 85.7
F FLOW LB/H/ENG 1582 1532 1478 1419 1396 1337 1280 1226 1180
IAS KT 298 293 286 280 277 271 264 258 252
30000 TAS KT 452 452 450 447 450 448 446 444 444
INDICATED MACH 0.771 0.774 0.773 0.773 0.780 0.780 0.780 0.780 0.780
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.50 2.38 2.27 2.16
SR NM/LB 0.143 0.147 0.152 0.158 0.161 0.168 0.174 0.181 0.188
N1 % 85.3 85.2 85.1 85.1 85.0 85.0 84.9 84.7 85.3
F FLOW LB/H/ENG 1583 1523 1467 1413 1361 1311 1262 1207 1160
IAS KT 302 296 289 283 277 271 264 258 252
28000 TAS KT 457 455 453 451 449 447 445 443 443
INDICATED MACH 0.780 0.780 0.780 0.780 0.780 0.780 0.780 0.780 0.780
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.54 2.43 2.31
SR NM/LB 0.144 0.149 0.154 0.160 0.165 0.171 0.176 0.184 0.191
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.