曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
‐ Select and pull the predetermined target speed on the FCU.
Note: The speed selection on the FCU must be made when above 150 ft RA.
‐ This action disengages the SRS mode and reverts to OPEN CLB.
‐ Accelerate to the new target speed following FD bars.
‐ When the target speed is reached resume climb to the GA altitude following the FD bars.
NAV or HDG mode........................................................................................................ SELECT
‐ Reselect NAV or HDG, as required.
At go-around thrust reduction altitude (CLB or LVR CLB flashing on FMA)
THRUST LEVERS................................................................................................................... CL
At go-around thrust acceleration altitude :
FCU SPEED................................................................................................... PUSH or SELECT
‐ Push to select managed speed or select appropriate speed to accelerate.
‐ Retract flaps on schedule.
Note: Consider the next step :
‐ Engage NAV mode, to follow the published missed approach procedure, or
‐ Prepare for a second approach by selecting the ACTIVATE APP PHASE, and
CONFIRM on the PERF page.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
HIGH ALTITUDE OPERATIONS AT BANGDA AIRPORT
A318/A319/A320/A321 FLEET PRO-SPO-32 P 4/8
FCOM 19 AUG 10
LANDING CONFIGURATION DETERMINATION
Applicable to:
LANDING CONFIGURATION DETERMINATION
During the approach briefing, determine the landing configuration.
FULL is preferred for ‐ shorter landing distance and reduced VLS.
‐ Check if the aircraft weight is below the maximum weight given in the table below. If so, retain
CONF FULL as landing configuration and CONF 3 as go-around configuration.
‐ If the aircraft weight is above the maximum weight given in the table below use FLAP 3
for landing. In all cases, if landing configuration is different from FLAP FULL, use 1+F for
go-around.
A go-around target speed increase may be necessary for the landing weight (Refer to
PRO-SPO-32 GO-AROUND TARGET SPEED DETERMINATION ). Verify also that the landing
weight is not higher than the maximum allowed (corresponding to 1.41 Vs1g).
MAXIMUM WEIGHT FOR GO AROUND IN CONF 3 (1 000 kg)
OAT °C PRESSURE ALTITUDE (FT)
0 2 000 4 000 6 000 8 000 10 000 12 000 14 500
< 10 73 71 69 67 64 62 59 55
15 73 71 69 67 64 62 59 55
20 73 71 69 67 64 61 59 53
25 73 71 69 67 64 61 56 51
30 73 71 69 67 63 58 53
35 73 71 68 65 60 55
40 72 71 67 62
45 72 68 64
50 69 65
55 66
GO-AROUND TARGET SPEED DETERMINATION
Applicable to:
GO-AROUND TARGET SPEED DETERMINATION
Use the table of the following page to determine the increase in the go-around speed as a function
of the landing weight, the altitude and the OAT.
The values provided in the table are, for each cell :
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
HIGH ALTITUDE OPERATIONS AT BANGDA AIRPORT
A318/A319/A320/A321 FLEET PRO-SPO-32 P 5/8
FCOM 19 AUG 10
M1 = Maximum go-around weight for 1.23 Vs1g
V1 = Go-around speed for 1.23 Vs1g
M2 = Maximum go around weight for 1.41 Vs1g
V2 = Go-around speed for 1.41 Vs1g
Method to use the table :
‐ Determine the corrected maximum go-around weight for 1.23 Vs1g (corrected M1) using
corrections at the bottom of following charts.
‐ If landing weight is less than the corrected maximum go-around weight for 1.23 Vs1g (corrected
M1), no target speed increment is necessary.
‐ Verify that the landing weight is not greater than the maximum allowed corresponding to 1.41
Vs1g (corrected M2), otherwise, the pilot should find a suitable diversion airport. If landing
weight is greater than the corrected maximum go-around weight for 1.23 Vs1g (corrected M1)
interpolate, within the current cell, to find the go-around target speed that corresponds to the
landing weight.
GO-AROUND – CONF 1+F – ONE ENGINE OUT
ONE ENG. AT GO-AROUND
THRUST APPROACH CLIMB LIMITING WEIGHT (1 000 kg) SPEEDS (KT)
HIGH AIR CONDITIONING for 1.23 Vs1g 1.23 Vs1g
ANTI ICE OFF for 1.41 Vs1g 1.41 Vs1g
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
HIGH ALTITUDE OPERATIONS AT BANGDA AIRPORT
A318/A319/A320/A321 FLEET PRO-SPO-32 P 6/8
FCOM 19 AUG 10
GO-AROUND – CONF 1+F – ONE ENGINE OUT
ONE ENG. AT GO-AROUND
THRUST APPROACH CLIMB LIMITING WEIGHT (1 000 kg) SPEEDS (KT)
HIGH AIR CONDITIONING for 1.23 Vs1g 1.23 Vs1g
ANTI ICE OFF for 1.41 Vs1g 1.41 Vs1g
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
A320机组操作手册FLIGHT CREW OPERATING MANUAL 14(26)
