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‐ increase the approach and landing speeds by 5 kt and multiply landing distance by
1.1.
3. In the following tables corrections for anti ice are only valid for OAT of 10 °C, or below.
PROCEDURE
Applicable to: ,
According to airport pressure altitude and temperature determine if the slats/flaps setting must be
restricted as a function of the landing weight, in order to meet the go around gradient requirement of
2.1 %.
Establish the final approach configuration with one more step of flaps. If the approach is interrupted,
retract the flaps by one step during the go-around.
In case of category II approach, JAR-OPS requires a regulatory approach climb gradient of 2.5 % to
be maintained.
Use the tables for CAT II approach to determine the maximum approach climb limiting weight
according to airport pressure altitude and temperature.
Note: 1. If circumstances dictate, landing may be made at a weight corresponding to the
maximum structural takeoff weight. (Refer to 99 Duref Cible FCOM).
2. When icing conditions are predicted during the flight and TAT is 10 °C or below and there
is evidence of significant ice accretion, to take into account ice formation on the non
heated structure :
‐ decrease the approach climb limiting weight by 5 %
‐ increase the approach and landing speeds by 5 kt and multiply landing distance by
1.1.
3. In the following tables corrections for anti ice are only valid for OAT of 10 °C, or below.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
GO AROUND
APPROACH CLIMB LIMITING WEIGHT - NORMAL
A330/A340 FLEET PER-GOA-ACG-NOR P 1/4
FCOM 19 AUG 10
CONF 2
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
GO AROUND
APPROACH CLIMB LIMITING WEIGHT - NORMAL
A330/A340 FLEET PER-GOA-ACG-NOR P 2/4
FCOM 19 AUG 10
CONF 2
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
GO AROUND
APPROACH CLIMB LIMITING WEIGHT - NORMAL
A330/A340 FLEET PER-GOA-ACG-NOR P 3/4
FCOM 19 AUG 10
CONF 3
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
GO AROUND
APPROACH CLIMB LIMITING WEIGHT - NORMAL
A330/A340 FLEET PER-GOA-ACG-NOR P 4/4
FCOM 19 AUG 10
CONF 3
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
GO AROUND
APPROACH CLIMB LIMITING WEIGHT - CATII
A330/A340 FLEET PER-GOA-ACG-CAT P 1/2
FCOM 19 AUG 10
CAT II CONF 2
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
GO AROUND
APPROACH CLIMB LIMITING WEIGHT - CATII
A330/A340 FLEET PER-GOA-ACG-CAT P 2/2
FCOM 19 AUG 10
CAT II CONF 3
Applicable to: ,
PERFORMANCE
HOLDING
Intentionally left blank
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
HOLDING
PRELIMINARY PAGES - TABLE OF CONTENTS
A330/A340 FLEET PER-HOL-PLP-TOC P 1/2
FCOM 19 AUG 10
PER-HOL-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
PER-HOL-GEN GENERAL
GENERAL............................................................................................................................................................1/2
PER-HOL-AEO ALL ENGINES OPERATIVE
CONF 0 - GD SPEED........................................................................................................................................ 1/8
CONF 0 - 240 KT............................................................................................................................................... 3/8
CONF 0 - 210 KT............................................................................................................................................... 4/8
CONF 1 - S SPEED........................................................................................................................................... 5/8
CONF 1 - 210 KT............................................................................................................................................... 7/8
CONF 1 - 170 KT............................................................................................................................................... 8/8
PER-HOL-OEI ONE ENGINE INOPERATIVE
HOLDING............................................................................................................................................................ 1/2
PER-HOL-TEI TWO ENGINES INOPERATIVE
HOLDING............................................................................................................................................................ 1/2
　
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