FLIGHT PLANNING
EMB-145 A1 and A1P LB
FAA
AIRPLANE
OPERATIONS
MANUAL
1-05-30
Page
6
Code
03
REVISION 40
AOM-145/1114
LONG RANGE CRUISE - ONE ENGINE INOPERATIVE
AE3007A1 AND AE3007A1P ENGINES
ALTITUDE: 23000 FT TO 30000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
23000 24000 25000 26000 27000 28000 29000 30000
N1 % - - - - - - - -
F FLOW LB/H/ENG - - - - - - - -
IAS KT - - - - - - - -
49000 TAS KT - - - - - - - -
INDICATED MACH - - - - - - - -
BUFFET MARGIN G - - - - - - - -
SR NM/LB - - - - - - - -
N1 % - - - - - - - -
F FLOW LB/H/ENG - - - - - - - -
IAS KT - - - - - - - -
46000 TAS KT - - - - - - - -
INDICATED MACH - - - - - - - -
BUFFET MARGIN G - - - - - - - -
SR NM/LB - - - - - - - -
N1 % - - - - - - - -
F FLOW LB/H/ENG - - - - - - - -
IAS KT - - - - - - - -
44000 TAS KT - - - - - - - -
INDICATED MACH - - - - - - - -
BUFFET MARGIN G - - - - - - - -
SR NM/LB - - - - - - - -
N1 % - - - - - - - -
F FLOW LB/H/ENG - - - - - - - -
IAS KT - - - - - - - -
42000 TAS KT - - - - - - - -
INDICATED MACH - - - - - - - -
BUFFET MARGIN G - - - - - - - -
SR NM/LB - - - - - - - -
N1 % 90.5 90.8 - - - - - -
F FLOW LB/H/ENG 1761 1691 - - - - - -
IAS KT 196 183 - - - - - -
40000 TAS KT 279 264 - - - - - -
INDICATED MACH 0.460 0.438 - - - - - -
BUFFET MARGIN G 2.00 1.75 - - - - - -
SR NM/LB 0.158 0.156 - - - - - -
INCREASE / DECREASE N1% BY 1 % PER 5°C ABOVE / BELOW ISA CONDITIONS.
INCREASE / DECREASE FUEL FLOW 1 % PER 5°C ABOVE / BELOW ISA CONDITIONS.
INCREASE / DECREASE TAS BY 3 KT PER 5°C ABOVE / BELOW ISA CONDITIONS.
FOR ANTI-ICE ON:
INCREASE N1 BY 0.7 % AND FUEL FLOW BY 8%.
DECREASE SR BY 7%.
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