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时间:2011-03-20 15:25来源:蓝天飞行翻译 作者:admin
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* 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
o,®_
ABNORMAL PROCEDURES
REV 32
2.03


SEQ 210
The "SPEED SPEED SPEED" synthetic voice is triggered every 5 seconds whenever the aircraft energy goes below a threshold under which thrust shall be increased to recover a positive flight path angle.
- THR LEVERS   PUSH
Increase the thrust until the warning disappears.

A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 36
2.04


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 36
2.03


SEQ 350
The "SPEED SPEED SPEED" synthetic voice is triggered every 5 seconds, whenever the aircraft energy goes below a threshold under which thrust shall be increased to recover a positive flight path angle.
* THR LEVERS   PUSH
Increase the thrust until the warning disappears.
 This procedure should be applied, if the Cockpit Door Locking System (CDLS) fails. This failure is indicated when the FAULT light on the center pedestal's CKPT DOOR panel comes on.
* CKPT DOOR CONT PANEL   CHECK
This panel is located on the overhead panel. It is used to identify the faulty CDLS item, and to verify the status of the pressure sensors and the three electrical latches (referred to as strikes).
* If two or more electrical latches (strikes) are faulty :
The cockpit door is not intrusion-proof.
* If two pressure sensors are faulty :
Automatic latch release is unavailable, in case of cockpit decompression.
* If no LED on the CKPT DOOR CONT panel is on :
The CDLS control unit is faulty ; therefore, the cockpit door might unlock automatically. If it does not consider using the mechanical override system to unlock the door.
 
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