Embraer EMB145 - Page 776

FLIGHT PLANNING
EMB-145 A1 and A1P LB
AIRPLANE
OPERATIONS
MANUAL
1-05-05
Page
10
Code
02
REVISION 40
AOM-145/1114
CRUISE - ALTITUDE CAPABILITY TABLE
The table below permits quick determination of the altitude capability,
based on the initial cruise weight. The table data are presented for
various ISA conditions, all engines operating and Maximum Speed
Cruise schedule.
The estabilished associated conditions are:
- Flaps .................................... UP
- Gears ................................... UP
- Bleeds.................................. OPEN
CRUISE ALTITUDE CAPABILITY
ALL ENGINES OPERATING
AE3007A1 AND AE3007A1P ENGINES
MAX SPEED CRUISE, CRUISE THRUST LIMITED
ISA + ºC
Weight (lb) -10 -5 0 5 10 15 20 25 30 35
50000 370 370 370 370 370 360 340 320 390 280
48000 370 370 370 370 370 370 360 340 310 290
46000 370 370 370 370 370 370 370 360 340 300
44000 370 370 370 370 370 370 370 370 360 330
42000 370 370 370 370 370 370 370 370 370 360
40000 370 370 370 370 370 370 370 370 370 360
38000 370 370 370 370 370 370 370 370 370 370
36000 370 370 370 370 370 370 370 370 370 370
34000 370 370 370 370 370 370 370 370 370 370
32000 370 370 370 370 370 370 370 370 370 370
30000 370 370 370 370 370 370 370 370 370 370
28000 370 370 370 370 370 370 370 370 370 370
NOTE: The weight values refers to the initial cruise weight.