SEQ 002
- LANDING CONF CONF 3
* Repeat the following until landing configuration is reached :
* SPEED SEL VFE NEXT - 5 KT
Decelerate towards VFE NEXT — 5 KT, but not below VLS. If turbulence, the pilot may decide to decelerate to a lower speed (not below VLS) to avoid VFE exceedance.
NOTE : . Autopilot may be used down to 500 feet AGL. As it is not tuned for abnormal
configurations, its behavior can be less than optimum and must be monitored.
Approach with selected speed is recommended.
A/THR is recommended, except in the case of a G+B SYS LO PR warning. OVERSPEED warning and VLS, displayed on the PFD, are computed according to the actual flaps/slats position.
VFE and VFE NEXT are displayed on the PFD according to the FLAPS' lever position. If not displayed, use the placard speeds.
If VLS is greater than VFE NEXT (overweight landing), FLAPS lever can be set to the next required position while speed is reduced to follow VLS reduction, as
surfaces extend. The VFE warning threshold should not be triggered.
In this case, disconnect the A/THR. A/THR can be re-engaged when landing configuration is established.
As speed reduces through VFE NEXT :
* FLAPS LEVER ONE STEP DOWN
* When landing configuration is established :
* DECELERATE TO CALCULATED APPROACH SPEED IN FINAL APPROACH
FOR GO AROUND
The table on page 2.05 provides the MAX SPEEDS for abnormal configurations.
* IF SLATS FAULT
* FOR CIRCUIT
* MAINTAIN SLAT/FLAP CONFIGURATION
* Recommended speed : MAX SPEED - 10 KT
* FOR DIVERSION
* SELECT CLEAN CONFIGURATION
Recommended speed for flaps retraction is between MAX SPEED - 10 KT and MAX SPEED.
* Recommended speed : MAX SPEED - 10 KT
* IF FLAPS FAULT
* FOR CIRCUIT
* MAINTAIN SLAT/FLAP CONFIGURATION
* Recommended speed : MAX SPEED - 10 KT
* FOR DIVERSION
* If Flaps jammed at 0
* SELECT CLEAN CONFIGURATION
NOTE : Recommended speed for slats retraction is between MAX SPEED - 10 knots and max speed of actual slat/flap position.
* NORMAL OPERATING SPEEDS
* If Flaps jammed > 0
* MAINTAIN SLAT/FLAP CONFIGURATION
* Recommended speed : MAX SPEED - 10 KT
NOTE : . In case of go-around with CONF FULL selected, the VG NOT DOWN warning is triggered at landing gear retraction.
. In some cases, MAX SPEED - 10KT may be a few knots higher than the VFE. In this situation, pilots may follow the VFE.
A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 32
2.055
SEQ 001
MAX SPEED
Flaps
Slats
F = 0
0 <F1
1<F...2
2 <F...3
F>3
S = 0
NO LIMITATION
215 kt
200 kt
185 kt
177 kt
(Not allowed)
0 < S 51
230 kt
1 < S .-.. 3
200kt
200kt
185 kt
177 kt
S > 3
177 kt
177 kt
177 kt
177 kt
CAUTION
—
For flight with SLATS or FLAPS extended, fuel consumption is increased. Refer to fuel flow indication.
As a guideline, determine the fuel consumption in clean configuration at same altitude without airspeed limitation (e.g. from ALTERNATE FLIGHT PLANNING tables) and multiply this result by 1.6 (SLATS EXTENDED) or 1.8 (FLAPS EXTENDED) or 2 (SLATS and FLAPS EXTENDED) to give the fuel consumption required to reach the destination in the current configuration.
A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 34
2.06
SEQ 001
A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 34
2.07
SEQ 001
The system may not detect a stabilizer jam when the pitch trim wheel is jammed. The flight control normal law remains active in this case and there is no ECAM warning.
* AP OFF
* MAN PITCH TRIM CHECK
The pitch trim wheel may not be fully jammed, the force needed may be higher than usual.
* IF MAN TRIM AVAIL : - TRIM FOR NEUTRAL ELEV
If man pitch trim is available, trim to maintain the elevator at the zero position (indications on ECAM F/CTL page).
APPR PROC
* IF MAN TRIM NOT AVAIL :
* FOR LDG USE FLAP 3
Do not select configuration full, so as not to degrade handling qualities.
* GPWS LDG FLAP 3 ON
CAT 1 ONLY
A319/A320/A321
o,®_
ABNORMAL PROCEDURES
REV 36
2.08
SEQ 100
— ENG MODE SEL IGN
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