A319/A320/A321
ovilm.i.
EMERGENCY PROCEDURES
REV 36
1 . ii
SEQ 138
HYD G + B SYS LO PR Summary
SPD BRK DO NOT USE
MAX SPD 320/.77
MANEUVER WITH CARE
ALTN LAW : PROT LOST
LANDING CONF
APPROACH SPEED
LANDING DIST
Use FLAP 3
VAPP = VREF + 25 KT
multiply by 1.6SLATS JAMMED / FLAPS SLOW CAT 1 ONLY
ATHR OFF
GPWS LDG FLAP 3 ON
For Flaps extension : SPD SEL VFE NEXT — 5KT
When in landing CONF : DECELERATE TO CALCULATED VAPP
L/G GRAVITY EXTENSION
* WHEN L/G down : USE MAN PITCH TRIM
FLARE : Only one ELEV and two spoilers per wing. No ailerons. A/C slightly sluggish — Direct law
SPOILERS : Only 2 per wing BRAKING : ALTERNATE
NO NOSEWHEEL STEERING
REVERSER : Only N°2
NO GEAR RETRACTION. Increased fuel consumption
* For circuit : MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed : MAX SPD — 10 KT
* For diversion : SELECT CLEAN CONFIGURATION
If Slats at zero : Normal operating speeds
If Slats not at zero : Recommended speed MAX SPD — 10 KT
ACTUAL LANDING DISTANCES (m (for contaminated runways, refer to 4.03)
WEIGHT (1000 KG)
46
50
54
58
62
66
70
74
78
DRY runway
655
690
740
795
855
925
1000
1085
1170
WET runway
940
1000
1060
1120
1180
1245
1315
1385
1460CORRECTIONS
+ 1000 ft above SL
+ 10 kt tailwind
DRY runway
+ 4 %
+ 14 °A
WET runway
+ 4 %
+ 20 °AThe method for approach speed computation is given in the QRH 2.31.
A319/A320/A321
ovilm.i.
EMERGENCY PROCEDURES
REV 36
„
1 . 12
SEQ 130
HYD G + Y SYS LO PR Summary
ACTUAL LANDING DISTANCES (m (for contaminated runways, refer to 4.03)
WEIGHT (1000 KG)
46
50
54
58
62
66
70
74
78
DRY runway
655
690
740
795
855
925
1000
1085
1170
WET runway
940
1000
1060
1120
1180
1245
1315
1385
1460CORRECTIONS
+ 1000 ft above SL
+ 10 kt tailwind
DRY runway
+ 4 %
+ 14 °A
WET runway
+ 4 %
+ 20 °AThe method for approach speed computation is given in the QRH 2.31.
A319/A320/A321
ovilavril.,,
EMERGENCY PROCEDURES
REV 36
1 . ii
SEQ 146
HYD G + B SYS LO PR Summary
SPD BRK DO NOT USE
MAX SPD 320/.77
MANEUVER WITH CARE
ALTN LAW : PROT LOST
LANDING CONF
APPROACH SPEED
LANDING DIST
Use FLAP 3
VAPP = VREF + 25 KT
multiply by 1.5SLATS JAMMED / FLAPS SLOW CAT 1 ONLY
ATHR OFF
GPWS LDG FLAP 3 ON
For Flaps extension : SPD SEL VFE NEXT — 5KT
When in landing CONF : DECELERATE TO CALCULATED VAPP
L/G GRAVITY EXTENSION
* WHEN L/G down : USE MAN PITCH TRIM
FLARE : Only one ELEV and two spoilers per wing. No ailerons. A/C slightly sluggish — Direct law
SPOILERS : Only 2 per wing BRAKING : ALTERNATE
NO NOSEWHEEL STEERING
REVERSER : Only N°2
NO GEAR RETRACTION. Increased fuel consumption
* For circuit : MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed : MAX SPD — 10 KT
* For diversion : SELECT CLEAN CONFIGURATION
If Slats at zero : Normal operating speeds
If Slats not at zero : Recommended speed MAX SPD — 10 KT
ACTUAL LANDING DISTANCES (m) (for contaminated runways, refer to 4.03)
WEIGHT (1000 KG)
40
44
48
52
56
60
64
68
72
76
DRY runway
750
740
750
800
830
860
900
960
1040
1130
WET runway
900
900
920
990
1050
1110
1170
1240
1320
1400CORRECTIONS
+ 1000 ft above SL
+ 10 kt tailwind
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