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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 manual 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 the handling qualities.
GPWS LDG FLAP
3.........................................................................................................................ON
CAT 2 INOP
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AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
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ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
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LANDING WITH SLATS OR FLAPS JAMMED
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. In case of turbulence, to
avoid VFE
exceedance, the pilot may decide to decelerate to a lower speed, but not below VLS.
Note: • The autopilot may be used down to 500 ft 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 case), the FLAPS lever can
be set in
the required next position, while the 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 the 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 below provides the MAX SPEEDS for the abnormal configurations.
�� IF SLATS FAULT:
�� FOR CIRCUIT:
MAINTAIN SLATS/FLAPS CONFIGURATION
Recommended speed: MAX SPEED -10 kt
�� FOR DIVERSION
SELECT CLEAN CONFIGURATION
Recommended flaps retraction speed is between MAX SPEED -10 kt and MAX
SPEED.
Recommended diversion speed: MAX SPEED -10 kt.
�� IF FLAPS FAULT:
�� FOR CIRCUIT:
MAINTAIN SLATS/FLAPS 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 kt and
MAX
SPEED of actual slat/flap position.
Normal operating speeds
�� If FLAPS jammed > 0
MAINTAIN SLAT/FLAP CONFIGURATION
Recommended speed for diversion: MAX SPEED -10 kt
To be continued on next page
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ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
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LANDING WITH SLATS OR FLAPS JAMMED (Cont'd)
Note: ‐ In some cases, MAX SPEED -10 kt may be a few knots higher than the VFE.
In
this situation, pilot may follow the VFE.
‐ In case of a go-around with CONF FULL selected, the L/G NOT DOWN warning
is triggered at landing gear retraction.
　
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