Embraer EMB145 - Page 912

FLIGHT PLANNING
EMB-145 A1 and A1P LB
AIRPLANE
OPERATIONS
MANUAL
1-05-50
Page
2
Code
02
REVISION 38
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. This table must be used only when the airplane is
dispatched with the Engine Anti Ice Valve Locked Open in agreement
with MEL and DDPM.
The established associated conditions are:
- Flaps .................................... UP
- Gears ................................... UP
- Bleeds.................................. OPEN
- Anti Ice………………………..ON (Engine or all)
CRUISE ALTITUDE CAPABILITY
ENGINE ANTI ICE VALVE LOCKED OPEN
ALL ENGINES OPERATING
AE3007A1 AND A1P ENGINES, MAX SPEED CRUISE, CRUISE THRUST
LIMITED
ISA + °C
Weight (lb)
-10 -5 0 5 10 15 20 25 30 35
50000 330 350 350 320 300 280 260 220 220 200
48000 330 360 360 330 310 290 270 240 230 220
46000 330 370 360 360 330 300 280 260 240 240
44000 330 370 370 370 350 320 290 270 250 250
42000 330 370 370 370 360 350 300 280 270 260
40000 330 370 370 370 370 360 330 290 280 270
38000 330 370 370 370 370 370 360 310 290 270
36000 330 370 370 370 370 370 360 340 300 290
34000 330 370 370 370 370 370 370 360 330 300
32000 330 370 370 370 370 370 370 370 360 320
30000 330 370 370 370 370 370 370 370 370 350
28000 330 370 370 370 370 370 370 370 370 360
NOTE: The weight values refer to the initial cruise weight.