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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 74/163 74/163 70/154 70/154
330/370 69/152 71/156 67/147 67/147 63/138 63/138
350/390 62/136 62/136 59/130 59/130 56/123 56/123
BLEED CORRECTIONS
ENGINE ANTI ICE TOTAL ANTI ICE
ISA OMpatx AAltlt.. :: -N 2o0 c0o frtr. OMpatx AAltlt.. :: -N 4o0 c0o frtr.
ISA +10 OMpatx AAltlt.. :: -N1o 2 c0o0r rf.t OMpatx AAltlt.. :: -N2o 3 c0o0r rf.t
ISA +15 OMpatx AAltlt.. :: -N1o 4 c0o0r rf.t OMpatx .A Alt.lt. :: --1300 fftt
ISA +20 OMpatx AAltlt.. :: --2300 fftt OMpatx AAltlt.. :: --5700 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 15/16
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
Intentionally left blank
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 16/16
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-20 P 1/10
FCOM 19 AUG 10
WIND ALTITUDE TRADE FOR CONSTANT SPECIFIC RANGE
WIND ALTITUDE TRADE FOR CONSTANT SPECIFIC RANGE
Applicable to:
GIVEN : Weight : 60 000 kg (132 300 lb)
Wind at FL 350 : 10 kt head
FIND : Minimum wind difference to descend to FL 310 : (57 - 14) = 43 kt
RESULTS : Descent to FL 310 may be considered provided the tail wind at this altitude is more
than (43 - 10) = 33 kt.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-20 P 2/10
FCOM 19 AUG 10
WIND ALTITUDE TRADE FOR CONSTANT SPECIFIC RANGE
Applicable to: MSN,
GIVEN : Weight : 75 000 kg (165 300 lb)
Wind at FL 350 : 10 kt head
FIND : Minimum wind difference to descend to FL 310 : (27 - 2) = 25 kt
RESULTS : Descent to FL 310 may be considered provided the tail wind at this altitude is more
than (25 - 10) = 15 kt.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-20 P 3/10
FCOM 19 AUG 10
WIND ALTITUDE TRADE FOR CONSTANT SPECIFIC RANGE
Applicable to: MSN,
GIVEN : Weight : 62 000 kg (136 700 lb)
Wind at FL 350 : 10 kt head
FIND : Minimum wind difference to descend to FL 330 : (27 - 7) = 20 kt
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-20 P 4/10
FCOM 19 AUG 10
RESULTS : Descent to FL 330 may be considered provided the tail wind at this altitude is more
than (20 - 10) = 10 kt.
WIND ALTITUDE TRADE FOR CONSTANT SPECIFIC RANGE
Applicable to:
GIVEN : Weight : 65 000 kg (143 300 lb)
Wind at FL 370 : 10 kt head
FIND : Minimum wind difference to descend to FL 330 : (18 + 2) = 20 kt
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-20 P 5/10
FCOM 19 AUG 10
RESULTS : Descent to FL 330 may be considered provided the tail wind at this altitude is more
than (20 - 10) = 10 kt.
WIND ALTITUDE TRADE FOR CONSTANT SPECIFIC RANGE
Applicable to:
GIVEN : Weight : 65 000 kg (143 300 lb)
Wind at FL 350 : 10 kt head
FIND : Minimum wind difference to descend to FL 310 : (40 - 4) = 36 kt
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-20 P 6/10
FCOM 19 AUG 10
RESULTS : Descent to FL 310 may be considered provided the tail wind at this altitude is more
than (36 - 10) = 26 kt.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-20 P 7/10
FCOM 19 AUG 10
WIND ALTITUDE TRADE FOR CONSTANT SPECIFIC RANGE
Applicable to:
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-20 P 8/10
FCOM 19 AUG 10
GIVEN : Weight : 65 000 kg (143 300 lb)
Wind at FL 370 : 10 kt head
FIND : Minimum wind difference to descend to FL 330 : (17 - 2) = 15 kt
RESULTS : Descent to FL 330 may be considered provided the tail wind at this altitude is more
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 5(106)
