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Maximum permissible takeoff weight...........................................................................................78.3
Associated speed,
V1 = 147 kt – 1 × 15/10 = 145 kt
VR = 154 kt – 1 × 15/10 = 153 kt
V2 = 156 kt – 1 × 15/10 = 155 kt
Check that the speeds are higher than minimum speeds from the chart and from VMU table. (It is
reminded that if the speed checks are not fulfilled, the corrections must be recalculated using those
provided on lines 3 and 4).
Since the speed check is fulfilled :
Max permissible takeoff weight = 78.3 (1 000 kg)
V1 = 145 kt, VR = 153 kt, V2 = 155 kt.
Takeoff Configuration : 1+F
TOW V1 VR V2
TOW (RTOW) 82.2
FCOM correction(s) -2.2
Intermediate value 80.0 155 156 158
WET Correction -0.7 -8 -2 -2
Intermediate value 79.3 147 154 156
QNH Correction -1 -2 -1 -1
Final value 78.3 145 153 155
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - MTOW CALCULATION (WEIGHT ENTRY)
Intentionally left blank
A318/A319/A320/A321 FLEET PER-TOF-TOC-18-10 P 26/26
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - MTOW CALCULATION (WEIGHT ENTRY)
A318/A319/A320/A321 FLEET PER-TOF-TOC-18-15 P 1/2
FCOM 19 AUG 10
LANDING INFORMATION
LANDING INFORMATION
Applicable to: ALL
TGA is the maximum temperature at which the approach climb gradient condition can be satisfied
as a function of weight. The chart presents two TGAs (associated with two different flap settings) in
order to allow the pilot to choose the more appropriate one in view of the scheduled landing weight
and temperature. The configurations 2 and 3 specified under TGA are the configurations in which
the required gradient of 2.1 % is satisfied when one engine failed. The single-engine approach is
normally performed with the flaps one step further down until the pilot decides to overshoot, whereas
the two-engine approach is performed with the flaps set up to two steps (if applicable) beyond the
indicated flap position. In both cases, the pilot retracts one step of flaps when electing to go around.
The aircraft establishes the required gradient of 2.1 % at the airport reference altitude. The thrust
setting is TOGA with the air conditioning ON. The speed is 1.23 VS for the specified configuration.
The TGA temperature is also published for weights higher than the maximum landing weight in order
to cover the overweight landing condition.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - MTOW CALCULATION (WEIGHT ENTRY)
Intentionally left blank
A318/A319/A320/A321 FLEET PER-TOF-TOC-18-15 P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - MTOW CALCULATION (WEIGHT ENTRY)
A318/A319/A320/A321 FLEET PER-TOF-TOC-18-20 P 1/2
FCOM 19 AUG 10
EXTRAPOLATION
EXTRAPOLATION
Applicable to: ALL
For OAT lower than the lowest temperature value of a wind column, it is possible to obtain a higher
maximum permissible takeoff weight by using Grad 1/Grad 2 values. Refer to PER-TOF-TOC-18-10
MTOW DETERMINATION for more details.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - MTOW CALCULATION (WEIGHT ENTRY)
Intentionally left blank
A318/A319/A320/A321 FLEET PER-TOF-TOC-18-20 P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - MTOW CALCULATION (WEIGHT ENTRY)
A318/A319/A320/A321 FLEET PER-TOF-TOC-18-30 P 1/2
FCOM 19 AUG 10
MAXIMUM STRUCTURAL TAKEOFF WEIGHT
MAXIMUM STRUCTURAL TAKEOFF WEIGHT
Applicable to: ALL
The maximum structural takeoff weight is a weight limitation depending on the aircraft. This limitation
is provided in the Flight Manual and in the chapter limitation of the FCOM.
Compare the maximum structural takeoff weight to the maximum permissible takeoff weight
computed for given conditions and retain the lower of the two values.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - MTOW CALCULATION (WEIGHT ENTRY)
Intentionally left blank
A318/A319/A320/A321 FLEET PER-TOF-TOC-18-30 P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - MTOW CALCULATION (WEIGHT ENTRY)
A318/A319/A320/A321 FLEET PER-TOF-TOC-18-40 P 1/2
FCOM 19 AUG 10
SUMMARY
SUMMARY
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 7(66)
