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‐ ISA
‐ CG = 33 %
‐ Normal air conditioning
‐ Anti ice OFF
Note: 1. In the tables, the asterisk (*) means that a step climb of 4 000 ft must be flown to reach
the corresponding flight level.
2. The flight level shown on the top of each column is the final flight level.
3. For each degree Celsius above ISA temperature apply a fuel correction of 0.015
f.°B.ML(×ΔHR°B(×hqchrsmbdML(
nq//22ka.°B.ML(×ΔHR°B(×hqchrsmbdML(
GENERAL
Applicable to: ,
, MSN
The alternate planning tables allow the flight crew to determine the fuel consumption and time
required to cover a given air distance from go-around at destination airport to landing at alternate
airport.
These tables are established for :
‐ Go-around : 120 kg or 270 lb
‐ Climb profile : 250 kt/300 kt/M .78
‐ Long range cruise
‐ Descent profile : .M 78/300 kt/250 kt
‐ Approach and landing at alternate airport : 100 kg or 220 lb (4 min)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - ALTERNATE
A318/A319/A320/A321 FLEET PER-FPL-FLP-ALN-10 P 2/4
FCOM 19 AUG 10
‐ ISA
‐ CG = 33 %
‐ Normal air conditioning
‐ Anti ice OFF
Note: 1. In the tables, the asterisk (*) means that a step climb of 4 000 ft must be flown to reach
the corresponding flight level.
2. The flight level shown on the top of each column is the final flight level.
3. For each degree Celsius above ISA temperature apply a fuel correction of 0.015
f.°B.ML(×ΔHR°B(×hqchrsmbdML(
nq//22ka.°B.ML(×ΔHR°B(×hqchrsmbdML(
GENERAL
Applicable to:
The alternate planning tables allow the flight crew to determine the fuel consumption and time
required to cover a given air distance from go-around at destination airport to landing at alternate
airport.
These tables are established for :
‐ Go-around : 80 kg or 180 lb
‐ Climb profile : 250 kt/300 kt/M .78
‐ Long range cruise
‐ Descent profile : .M 78/300 kt/250 kt
‐ Approach and landing at alternate airport : 60 kg or 140 lb (4 min)
‐ ISA
‐ CG = 33 %
‐ Normal air conditioning
‐ Anti ice OFF
Note: 1. In the tables, the asterisk (*) means that a step climb of 4 000 ft must be flown to reach
the corresponding flight level.
2. The flight level shown on the top of each column is the final flight level.
3. For each degree Celsius above ISA temperature apply a fuel correction of 0.015
(kg.°B.ML(×ΔHR°B(×hqchrsmbdML(
nq//22ka.°B.ML(×ΔHR°B(×hqchrsmbdML(
CORRECTION FOR DEVIATION FROM REFERENCE WEIGHT
Applicable to: ALL
The alternate planning tables are based on a reference landing weight at alternate.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - ALTERNATE
A318/A319/A320/A321 FLEET PER-FPL-FLP-ALN-10 P 3/4
FCOM 19 AUG 10
The fuel consumption must be corrected when the actual weight is different from the reference
weight.
If it is lower (or greater) than the reference weight, subtract (or add) the value given in the correction
part of the table per 1 000 kg or 1 000 lb below (or above) the reference weight.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - ALTERNATE
Intentionally left blank
A318/A319/A320/A321 FLEET PER-FPL-FLP-ALN-10 P 4/4
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - ALTERNATE
A318/A319/A320/A321 FLEET PER-FPL-FLP-ALN-20 P 1/14
FCOM 19 AUG 10
ALL ENGINES OPERATIVE
ALTERNATE PLANNING ISA
Applicable to:
A318/A319/A320/A321 FLIGHT CREW
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 6(72)