MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING
PRESSURE ALTITUDE: 29000 FT TO 37000 FT
CRUISE CONFIGURATION
BLEED: OPEN
WEIGHT
(LB)
N1
F FLOW LB/H/ENG
IAS
34000
TAS
INDICATED MACH
BUFFET MARGIN G
SR
N1
F FLOW LB/H/ENG
IAS
31000
TAS
INDICATED MACH
BUFFET MARGIN G
SR
N1
F FLOW LB/H/ENG
IAS
28000
TAS
INDICATED MACH
BUFFET MARGIN G
SR
INCREASE / DECREASE N1% BY 1 % PER 5°C ABOVE / BELOW ISA CONDITIONS.
INCREASE / DECREASE FUEL FLOW 1 % PER 5°C ABOVE / BELOW STD ISA CONDITIONS.
INCREASE / DECREASE TAS BY 5 KT PER 5°C ABOVE / BELOW STD ISA CONDITIONS.
REVISION 40
AIRPLANE
OPERATIONS
MANUAL
AE3007A1 AND AE3007A1P ENGINES
29000 30000 31000 32000 33000 34000 35000 36000 37000
%
87
86.9
1481 1431 1378 1320 1266 1215 1166 1121 1082
KT
302
296
KT
459
458
0.78
0.78
2.56
2.56
NM/LB
0.155
0.16 0.165 0.172 0.178 0.185 0.192 0.199 0.206
%
86.3
86.3
1435 1384 1335 1289 1240 1188 1138 1092 1052
KT
302
296
KT
458
457
0.78
0.78
2.56
2.56
NM/LB
0.16 0.165
%
85.6
85.6
1390 1339 1290 1243 1199 1156 1113 1066 1025
KT
302
296
KT
457
455
0.78
0.78
2.56
2.56
NM/LB
0.164
0.17 0.176 0.182 0.188 0.194
EMB-145 A1 and A1P LB
ALTITUDE (FT)
86.8
86.7
86.5
86.3
289
283
277
271
456
454
452
450
0.78
0.78
0.78
0.78
2.56
2.48
2.37
2.26
86.2
86.2
86.1
85.8
289
283
277
271
455
453
451
449
0.78
0.78
0.78
0.78
2.56
2.56
2.56
2.48
0.17 0.176 0.182 0.189 0.196 0.204 0.211
85.5
85.4
85.4
85.3
289
283
277
271
454
452
450
448
0.78
0.78
0.78
0.78
2.56
2.56
2.56
2.56
1-05-15
FLIGHT PLANNING
86.2
86.2
86.5
264
258
252
448
446
446
0.78
0.78
0.78
2.15
2.05
1.95
85.7
85.5
85.8
264
258
252
447
445
445
0.78
0.78
0.78
2.37
2.26
2.15
85.2
85
85.2
264
258
252
446
444
444
0.78
0.78
0.78
2.56
2.5
2.38
0.2 0.208 0.217
Page
Code
21
02
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