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AP/FD..............................................................................................................................
..................OFF
A/THR.............................................................................................................................
.................. OFF
Note: Check the actual slat/flap configuration on ECAM, since flap auto-retraction
may occur.
SLATS/FLAPS EXTENDED
Above 78 t 78 t-66 t Below 66 t
CONF Speed Pitch (°)/Thrust (% N1)
3 F 4.0/70.2 4.0/65.5 4.0/60.5
2 F 6.5/68.2 6.5/63.6 6.5/58.8
1 + F S 3.0/66.6 3.0/62.4 3.0/57.5
1 S 7.0/65.2 7.0/61.2 7.0/56.0
CLEAN
FL Speed Pitch (°)/Thrust (% N1)
Below FL 200 265 kt 2.0/73.0 1.5/71.2 1.0/69.8
FL 200 -FL 280 300 kt 2.0/83.4 1.5/81.6 1.0/80.2
Above FL 280 M 0.76 2.5/86.9 2.0/85.2 1.5/83.2
PITCH/THRUST FOR INITIAL LEVEL OFF
Flying technique to stabilize speed:
Adjust pitch in order to ‐ fly the required flight path.
‐ When target pitch is reached, flying intended flight path, adjust thrust to target:
• If the aircraft pitch tends to increase, aircraft is slow, then increase thrust;
• If the aircraft pitch tends to decrease, aircraft is fast, then decrease thrust.
To be continued on next page
ABN-34
6/8
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.R ‐ efer 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.........................................................................................................................
.... CLB
FLAPS.........................................................................................................................RE
TRACT
Retract from 3 or 2 to 1, once CLB thrust is set.
Retract from 1 to 0, when the aircraft pitch is lower than the pitch for S speed (Refer
to
ABN-34-C UNRELIABLE SPEED INDICATION/ADR CHECK PROC - Level-Off
　
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