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“INCREASE CLIMB” is
triggered on final approach:
Note: Resolution Advisories (RA) are inhibited below 900 ft.
UNRELIABLE SPEED INDICATION/ADR CHECK PROC - MEMORY
ITEMS
�� If the safe conduct of the flight is impacted:
MEMORY ITEMS
AP/FD..............................................................................................................................
................ OFF
A/THR.............................................................................................................................
.................OFF
�� PITCH/THRUST:
Below THRUST RED
ALT................................................................................................ 15°/TOGA
Above THRUST RED ALT and Below FL
100.....................................................................10°/CLB
Above THRUST RED ALT and Above FL
100...................................................................... 5°/CLB
FLAPS............................................................................................................. Maintain
current CONFIG
SPEEDBRAKES..............................................................................................................
Check retracted
L/G..................................................................................................................................
................... UP
�� When at, or above MSA or Circuit Altitude:
‐ Level off for troubleshooting
GPS
ALTITUDE..................................................................................................................
Display on MCDU
To be continued on next page
ABN-34
8/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
UNRELIABLE SPEED INDICATION/ADR CHECK PROC - MEMORY
ITEMS (Cont'd)
WHEN FLIGHT PATH IS STABILIZED
PROBE/WINDOW
HEAT........................................................................................................................ ON
TECHNICAL RECOMMENDATIONS:
‐ Respect Stall Warning
‐ To monitor speed, refer to IRS Ground Speed, or GPS Ground Speed variations
�� If remaining altitude indication is unreliable:
‐ Do not use FPV and/or V/S, which are affected.
‐ ATC altitude is affected. Notify the ATC.
‐ Refer to GPS altitude: altitude variations may be used to control level flight, and is
an altitude
cue.Refer to Radio Altimeter. ‐
CAUTION If the failure is due to radome destruction, the drag will increase and
therefore N1
must be increased by 5 %. Fuel flow will increase by about 27 %.
AFFECTED ADR IDENTIFICATION:
Crosscheck all speed indications and Refer to FPE-SPD Speeds
�� If at least one ADR is reliable:
Faulty
ADR(s).............................................................................................................................
OFF
REMAINING AIR
DATA.................................................................................................... CONFIRM
Alternate sources may be used to evaluate the air data:
‐ GPS altitude
‐ GPS and IRS Ground Speeds, taking into account altitude and wind effect.
�� If affected ADR(s) cannot be identified or all ADRs are affected:
ONE
ADR..........................................................................................................................
KEEP ON
Keep one ADR ON to maintain the STALL WARNING protection.
TWO
ADRs...............................................................................................................................
OFF
This prevents the flight control laws from using two coherent but unreliable ADR
data.
LDG CONF...................................................................................................................
USE FLAP 3
APP
SPD............................................................................................................................
VLS +10
LDG DIST
PROC...................................................................................................................
APPLY
Refer to ABN-80-B LDG CONF/APPR SPD/LDG DIST On Dry Runways Following
Failures - 34 -
NAV
�� To return to departure airport:
Keep takeoff configuration preferably.
Refer to ABN-34-C UNRELIABLE SPEED INDICATION/ADR CHECK PROC -
Approaches
(Pitch & Thrust Tables)
�� To accelerate and clean up after takeoff:
Accelerate and clean up the aircraft in level flight:
THRUST.........................................................................................................................
　
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