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ABN-24
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AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET ,
ELEC EMER CONFIG SUMMARY
CRUISE
MAX
SPD..................................................................................................................................
......... 320 KT
ALTN
LAW
: PROT LOST
ONLY CAPT PITOT AND AOA HEATED
FUEL: CTR TK UNUSABLE.
COM: VHF1, ATC1, RMP1, only
NAV: ILS1, VOR1, GPS1 (if MMR is installed) only
LANDING CONF APPROACH SPEED
Use FLAP 3 VAPP = VREF + 10 kt + APPR COR/140 kt
W (1000 KG) 40 44 48 52 56 60 64 68 72 76 78
VREF = VLS CONF FULL 106 111 116 121 125 130 134 138 142 146 148
APPROACH
MINIMUM RAT SPEED 140 KT CAT 2 INOP
SLATS FLAPS SLOW
�� AT FT AGL:
L/G..................................................................................................................................
.............. DOWN
�� When L/G down: BATTERIES ONLY, USE MAN PITCH TRIM
LANDING
FLARE: Only 2 spoilers per wing. Direct law
SPOILERS: Only 2 per wing
NO?REVERSER
BRAKING: ALTERNATE without antiskid
MAX BRK PR 1000 PSI
NO?NOSEWHEEL?STEERING
GO-AROUND
�� When L/G uplocked:
EMER ELEC
PWR......................................................................................................................MAN
ON
ACTUAL LANDING DISTANCES (m) WITH FAILURE WITHOUT REV
WEIGHT (1000 KG) 46 50 54 58 62 66 70 74 78
DRY runway 2 210 2 300 2 430 2 520 2 650 2 870 3 120 3 410 3 690
WET runway Refer to FPE-IFL Landing Distance Without AUTOBRAKE
- CONF FULL and apply LDG DIST Factor = 2.40
CONTA runway Refer to FPE-IFL Landing Distance Without AUTOBRAKE
- CONF FULL and apply LDG DIST Factor = 2.15
CORRECTIONS +1 000 ft above SL +10 kt tailwind
DRY Runway +3 % +18 %
Refer to ABN-80 VAPP CALCULATION for the approach speed computation method.
ABN-24
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AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET ,
ABN-24
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AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , ,
ELEC EMER CONFIG SYS REMAINING
ELEC EMER CONFIG SYS REMAINING EMER GEN RUNNING IN
FLIGHT BAT ONLOYN THE GROUND
PRESS AUTO SYS 1 Norm Norm Norm
MAN PRESS CTL Inop Inop Inop (1)
RAM AIR Norm Norm Norm
PACK VALVE 1 Norm Closure Inop Closure Inop
PACK VALVE 2 Closure Inop Closure Inop Closure Inop (1)
AVIONIC VENT Norm Norm Partial
AFT CRG ISOL VALVE Norm Inop Inop
AIR COND
PRESS
AFT CRG HEAT Norm Inop Inop
(1) Restored, when speed is below 100 kt.
FMGC (NAV FUNCTION) N° 1 only Inop Inop
MCDU N° 1 only Inop Inop
FMGS FAC N° 1 only Inop Inop
FCU ch 1 only ch 1 only ch 1 only
VHF 1 Norm Norm Norm
HF1 Norm Inop Inop
RMP 1 Norm Norm Norm
ACP (Capt, F/O) Norm Norm Norm
CIDS Norm Norm Norm
INTERPHONE Norm Norm Norm
CVR Norm Inop Inop
COM
LOUDSPEAKER 1 Norm Norm Norm
CREW OXY Norm Norm (1) Norm (1)
PAX OXY mask release (auto
EMER EQPT + man) Norm Inop Inop
SLIDES ARM/WARN Norm Norm Norm
(1) Crew oxygen valve inoperative.
ENG 1 LOOP A only A only A only
ENG 2 LOOP B only B only B only
APU LOOP Inop Inop Inop (1)
CARGO SMOKE DET Channel 1 Inop Inop
ENG FIRE EXT. Bottle 1 only Bottle 1 only Bottle 1 only
APU FIRE EXT. Squib A only Squib A only Squib A only
CARGO FIRE EXT. Inop Inop Inop (1)
FIRE
APU AUTO EXT. Inop Inop Inop (1)
(2) Restored, when speed is below 100 kt.
ELAC N° 1 only N° 1+ N° 2 N°1+ N°2 (2)
SEC N° 1 only N° 1 N° 1 (2)
FCDC N° 1 only Inop Inop
SFCC N° 1 only N° 1 only N° 1 only
FLT CTL
Flaps POS ind Norm Norm Norm (1)
(1) Lost 30 s after last engine shutdown.
(3) Lost, when speed is below 50 kt.
LP VALVE Norm Norm Norm
FQI channel 1 Norm Inop Inop
FUEL X FEED VALVE Norm Inop Inop
TRANSFER VALVE Norm Inop Inop
HYD FIRE VALVES Norm Norm Norm
WING A.ICE Norm Inop Inop
ENG A. ICE VALVE Open Open Open
CAPT PITOT Norm Norm Norm (1)
CAPT AOA Norm Inop Inop
ICE - RAIN
RAIN REPELLANT (CAPT) Norm Norm Norm
(4) Lost, when speed is below 50 kt
PFD 1 Norm Norm Norm(1)
EIS ND 1 Norm Inop Inop
ECAM upper disp. Norm Norm Norm (1)
To be continued on next page
ABN-24
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AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
　
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