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altitude.
2. The n = 1.3 g (n = 1.4 g) curve indicates the buffet margin.
OPTIMUM WEIGHT FOR FEET STEP CLIMB
WEIGHT (1 000 kg/1 000 lb)
STEP CLIMB FROM/TO ≤ ISA +10 ISA +15 ISA +20
LR M .78 LR M .78 LR M .78
310/350 76/167 76/167 76/167 76/167 76/167 76/167
330/370 69/152 71/156 69/152 71/156 69/152 70/154
350/390 63/138 64/141 62/136 64/141 62/136 62/136
BLEED CORRECTIONS
ENGINE ANTI ICE TOTAL ANTI ICE
ISA OMpatx AAltlt.. :: -N 1o0 c0o frtr. OMpatx AAltlt.. :: -N 6o0 c0o frtr.
ISA +10 OMpatx AAltlt.. :: -N1o 6 c0o0r rf.t OMpatx AAltlt.. :: -N3o 3 c0o0r rft
ISA +15 OMpatx AAltlt.. :: -N1o 9 c0o0r rf.t OMpatx .A Alt.lt. :: -N3o 4 c0o0r rf.t
ISA +20 OMpatx AAltlt.. :: -N2o 5 c0o0r rf.t OMpatx AAltlt.. :: -- 65 0f tft
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 9/16
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 10/16
FCOM 19 AUG 10
CRUISE LEVEL CHARTS
Applicable to: ,
, MSN
These charts have been established for a center of gravity at 33 % MAC.
Maximum and optimum altitudes are given for different temperatures at long range speed and M .78.
Note: 1. Optimum and maximum altitudes curves do not cover for M .78 the whole weight range
because above a given weight these Mach numbers cannot be maintained, whatever the
altitude.
2. The n = 1.3 g (n = 1.4 g) curve indicates the buffet margin.
OPTIMUM WEIGHT FOR FEET STEP CLIMB
WEIGHT (1 000 kg/1 000 lb)
STEP CLIMB FROM/TO ≤ ISA +10 ISA +15 ISA +20
LR M .78 LR M .78 LR M .78
310/350 81/178 83/183 79/174 79/174 74/163 74/163
330/370 73/160 75/165 72/158 72/158 67/147 67/147
350/390 66/145 68/149 64/141 64/141 60/132 58/127
BLEED CORRECTIONS
ENGINE ANTI ICE TOTAL ANTI ICE
ISA OMpatx AAltlt.. :: --00 fftt OMpatx AAltlt.. :: -- 12 0f tft
ISA +10 OMpatx AAltlt.. :: --1300 fftt OMpatx AAltlt.. :: --2500 fftt
ISA +15 OMpatx AAltlt.. :: --5500 fftt OMpatx .A Alt.lt. :: --7900 fftt
ISA +20 OMpatx AAltlt.. :: --8800 fftt OMpatx AAltlt.. :: --110000 fftt
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 11/16
FCOM 19 AUG 10
CRUISE LEVEL CHARTS
Applicable to:
These charts have been established for a center of gravity at 33 % MAC.
Maximum and optimum altitudes are given for different temperatures at long range speed and M .78.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 12/16
FCOM 19 AUG 10
Note: 1. Optimum and maximum altitudes curves do not cover for M .78 the whole weight range
because above a given weight these Mach numbers cannot be maintained, whatever the
altitude.
2. The n = 1.3 g (n = 1.4 g) curve indicates the buffet margin.
OPTIMUM WEIGHT FOR FEET STEP CLIMB
WEIGHT (1 000 kg/1 000 lb)
STEP CLIMB FROM/TO ≤ ISA +10 ISA +15 ISA +20
LR M .78 LR M .78 LR M .78
310/350 76/167 76/167 73/160 73/160 69/152 69/152
330/370 69/152 69/152 66/145 66/145 62/136 62/136
350/390 62/136 62/136 59/130 59/130 55/121 55/121
BLEED CORRECTIONS
ENGINE ANTI ICE TOTAL ANTI ICE
ISA OMpatx AAltlt.. :: --00 fftt OMpatx AAltlt.. :: --00 fftt
ISA +10 OMpatx AAltlt.. :: -- 14 0f tft OMpatx AAltlt.. :: --3400 fftt
ISA +15 OMpatx AAltlt.. :: --3300 fftt OMpatx .A Alt.lt. :: --4400 fftt
ISA +20 OMpatx AAltlt.. :: --3500 fftt OMpatx AAltlt.. :: --6600 fftt
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 13/16
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 14/16
FCOM 19 AUG 10
CRUISE LEVEL CHARTS
Applicable to:
These charts have been established for a center of gravity at 33 % MAC.
Maximum and optimum altitudes are given for different temperatures at long range speed and M .78.
Note: 1. Optimum and maximum altitudes curves do not cover for M .78 the whole weight range
because above a given weight these Mach numbers cannot be maintained, whatever the
altitude.
2. The n = 1.3 g (n = 1.4 g) curve indicates the buffet margin.
OPTIMUM WEIGHT FOR FEET STEP CLIMB
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 5(105)
