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OPERATING MANUAL
LIMITATIONS
SPEED LIMITATIONS
A330/A340 FLEET LIM-13 P 3/12
FCOM 19 AUG 10
CAUTION Rapid and large alternating control inputs, especially in combination with large
changes in pitch, roll, or yaw (e.g. large sideslip angles) may result in structural
failures at any speed, even below VA.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
SPEED LIMITATIONS
A330/A340 FLEET LIM-13 P 4/12
FCOM 19 AUG 10
BUFFET ONSET
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
SPEED LIMITATIONS
A330/A340 FLEET LIM-13 P 5/12
FCOM 19 AUG 10
Examples :
1. Determine Maximum Bank Angle limited by buffet :
DATA : M = 0.6, FL = 350, CG = 40 %, WEIGHT = 180 000 kg
RESULT: load factor = 1.15 g or 30 ° bank
2. Determine low and high speed limited by buffet :
DATA : 52 ° bank or 1.63 g, WEIGHT = 200 000 kg, CG = 40 %, FL = 350
RESULT: M = 0.775 (low speed buffet) and M = 0.825 (high speed buffet).
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
SPEED LIMITATIONS
A330/A340 FLEET LIM-13 P 6/12
FCOM 19 AUG 10
BUFFET ONSET
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
SPEED LIMITATIONS
A330/A340 FLEET LIM-13 P 7/12
FCOM 19 AUG 10
Examples :
1. Determine Maximum Bank Angle limited by buffet :
DATA : M = 0.58, FL = 350, CG = 40 %, WEIGHT = 180 000 kg
RESULT: load factor = 1.15 g or 30 ° bank
2. Determine low and high speed limited by buffet :
DATA : 52 ° bank or 1.63 g, WEIGHT = 200 000 kg, CG = 40 %, FL = 350
RESULT: M = 0.775 (low speed buffet) and M = 0.85 (high speed buffet).
MINIMUM CONTROL SPEEDS
Applicable to:
VMCL = 125 kt (IAS) ; VMCL-2 = 157 kt (IAS).
Altitude (ft) VMCA (KT CAS) CONF 1 + F VMCCGO N(KFT 2 IAS) CONF 3
0
2 000
4 000
6 000
8 000
124
121
118
115
111.5
126.5
123.5
120
117
114
126.5
123.5
120
117
114
127
124
121
118
114.5
MINIMUM CONTROL SPEEDS
Applicable to:
VMCL = 118 kt (IAS)
Altitude (ft) VMCA (KT CAS) CONF 1 + F VMCCGO N(KFT 2 IAS) CONF 3
0
2 000
4 000
6 000
8 000
107
105
103.5
100.5
97
109.5
107.5
106
103
100
109.5
107.5
106.5
103.5
100
110
108
106.5
103.5
100.5
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
SPEED LIMITATIONS
A330/A340 FLEET LIM-13 P 8/12
FCOM 19 AUG 10
STALLING SPEEDS
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
SPEED LIMITATIONS
A330/A340 FLEET LIM-13 P 9/12
FCOM 19 AUG 10
EXAMPLE :
DATA : GW = 178 000 kg (392 419 lb), PRESSURE ALTITUDE 15 000 ft, CLEAN
CONFIGURATION
RESULT : VS1G = 158 kt CAS
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
SPEED LIMITATIONS
A330/A340 FLEET LIM-13 P 10/12
FCOM 19 AUG 10
STALLING SPEEDS
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
SPEED LIMITATIONS
A330/A340 FLEET LIM-13 P 11/12
FCOM 19 AUG 10
EXAMPLE :
DATA : GW = 160 000 kg (352 740 lb), PRESSURE ALTITUDE 15 000 ft, CLEAN
CONFIGURATION
RESULT : VS1G = 140 kt CAS
MAXIMUM FLAPS/SLATS SPEEDS
Applicable to:
Lever Position SLATS FLAPS AILERONS Ind. on ECAM MAX SPD FLIGHT PHASE
1 20 107 100 1 +1 F 221555 THAOKLEDOINFGF
2 2244 1227 1100 22(1) 120956 TAKEAOPFPFR/AOPAPCRHOACH
3 24 26 10 3 186 TAKEOFF/APPR/LDG
FULL 24 32 10 FULL 180 LANDING
(1) This slats/flaps position corresponds to CONF 1*
Maximum altitude with flaps/slats extended : 20 000 ft.
MAXIMUM FLAPS/SLATS SPEEDS
Applicable to: ,
Lever Position SLATS FLAPS AILERONS Ind. on ECAM MAX SPD FLIGHT PHASE
1 16 08 05 1 +1 F 221405 THAOKLEDOINFGF
2 2200 184 1100 22(1) 120956 TAKEAOPFPFR/AOPAPCRHOACH
3 23 22 10 3 186 TAKEOFF/APPR/LDG
FULL 23 32 10 FULL 180 LANDING
(1) This slats/flaps position corresponds to CONF 1*
Maximum altitude with flaps/slats extended : 20 000 ft.
GEAR DOWN SPEEDS
Applicable to:
Maximum speed with landing gear extended (VLE)...............................................................240 kt/.55
Maximum speed at which the landing gear may be operated (extension and retraction) (VLO).240 kt/.55
Maximum speed for gravity extension (VLE/VLO)....................................................................... 200 kt
　
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