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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
(Pitch &
Thrust Table) )
Once in clean configuration, Refer to ABN-34-C UNRELIABLE SPEED
INDICATION/ADR
CHECK PROC - Climb/Cruise/Descent (Pitch & Thrust Tables) for flight
continuation.
To be continued on next page
ABN-34
9/10
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)
�� Other cases:
Refer to ABN-34-C UNRELIABLE SPEED INDICATION/ADR CHECK PROC -
Climb/Cruise/Descent (Pitch & Thrust Tables) for flight continuation.
CLIMB
Set the thrust to CL.
CLEAN
Above 78 t 78 t-66 t Below 66 t
FL Speed Pitch (°)/Thrust (% N1)
Below FL 50 9.0/CLB 9.5/CLB 10.5/CLB
FL 50 - FL 100 8.0/CLB 8.5/CLB 9.0/CLB
FL 100 - FL 150 7.0/CLB 7.0/CLB 8.0/CLB
FL 150 - FL 200
265 kt
6.0/CLB 6.0/CLB 6.5/CLB
FL 200 - FL 250 5.0/CLB 5.0/CLB 5.5/CLB
FL 250 - FL 280 300 kt 3.0/CLB 3.0/CLB 3.0/CLB
Above FL 280 M 0.76 3.0/CLB 3.0/CLB 3.5/CLB
CRUISE
Adjust N1 to maintain approximate level flight with pitch attitude held constant.
When time permits,
(Refer to OPS SEVERE TURBULENCE) and adjust pitch to maintain level flight.
CLEAN
Above 78 t 78 t-66 t Below 66 t
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
DESCENT
Set the thrust to IDLE.
CLEAN
Above 78 t 78 t-66 t Below 66 t
FL Speed Pitch (°)/Thrust (% N1)
Above FL 280 M 0.76 -1.5/IDLE -1.5/IDLE -2.5/IDLE
FL 280-FL 200 300 kt -0.5/IDLE -1.0/IDLE -2.5/IDLE
FL 200 - FL 100 265 kt 0.5/IDLE -0.5/IDLE -2.0/IDLE
Below FL 100 265 kt 0.0/IDLE -1.0/IDLE -2.5/IDLE
Below FL 100 G-DOT 1.5/IDLE 1.5/IDLE 1.5/IDLE
To be continued on next page
ABN-34
10/10
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)
INITIAL AND INTERMEDIATE APPROACH IN LEVEL FLIGHT
The approach phase between Green Dot speed (clean configuration) and the landing
configuration
(CONF 3), is flown in level flight.
LANDING GEAR UP IN LEVEL FLIGHT
Above 78 t 78 t - 66 t Below 66 t
CONF Speed (kts) Pitch (°)/Thrust (% N1)
0 G-DOT 5.0/63.2 5.0/59.4 5.0/54.3
1 S 7.0/65.0 7.0/61.3 7.0/56.2
1+F (1) S 3.0/66.5 3.0/62.4 3.0/57.5
2 F 6.5/68.0 6.5/63.7 6.5/58.8
LANDING GEAR DOWN IN LEVEL FLIGHT (EXPECT GRVTY
EXTENSION)
3 F 4.0/74.8 4.0/70.6 4.0/65.0
(1) Due to the fact that the speed is unreliable, the SFCC may select the 1+F
configuration in approach, instead of 1.
FINAL APPROACH AT STANDARD -3 ° DESCENT FLIGHT PATH
LANDING GEAR DOWN
Above 78 t 78 t - 66 t Below 66 t
CONF Speed (kts) Pitch (°)/Thrust (% N1)
3 VLS +10 1.5/59.2 1.5/54.5 1.0/49.8
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.
AFFECTED ADR(S) IDENTIFICATION
Crosscheck all speeds and altitudes indications.
Alternates sources may be used to evaluate the air data:
‐ GPS altitude
‐ GPS and IRS Group Speeds, taking into account altitude and wind effect.
�� If affected ADR(s) identified:
Affected ADR(s)
P/B.......................................................................................................................OFF
REMAINING AIR
DATA........................................................................................................ CONFIRM
�� If affected ADR(s) cannot be identified or all ADRs are affected:
ALL ADRs
P/B..............................................................................................................................OF
F
All ADRs must be switched off to replace the PFD's normal speed scale and altitude
　
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