1.2
SEC 1 + 2 or 2 + 3 FAULT
NORM (1)
1.1
SEC 1 + 2 + 3 FAULT
3
10
1.4
FLAPS/
SLAPS
FLAPS and SLATS at zero
1
60 (APPR)
50 (THRESHOLD)
1.7 *
0 < FLAPS < 1 : Slats < 1
Slats _. 1
3
45
1.6
3
25
1.35
1 .-, FLAPS < 2 : Slats < 1
Slats _. 1
3
30
1.4
3
15
1.2
2 .-, FLAPS < 3 : Slats < 1
Slats _. 1
3
25
1.35
3
10
1.15
FLAPS = 3 : Slats < 1
1 .-, Slats .-, 3
Slats > 3
3
25
1.35
3
10
1.15*
3
5
1.1
FLAPS > 3 : Slats < 1
1 .-, Slats .-, 3
Slats > 3
Not allowed
FULL
10
1.15
FULL
5
1.1
HYD
BLUE or YELLOW or GREEN
NORM (1)
1.1
GREEN +BLUE
3
25
1.5
GREEN +YELLOW
3
25
2.3
YELLOW +BLUE
NORM (1)
1.1
BRK
ANTI SKID
NORM (1)
1.4
AUTO BRK FAULT
NORM (1)
1.2
NAV
IR 1+2+3 FAULT
3
10
2.1
DUAL IR FAULT
DUAL ADR FAULT
ADR 1 + 2 + 3 FAULT
3
10
1.2
ENG
REV UNLOCK with buffet
1 **
55 (APPR)
40 (THRESHOLD)
1.75
REV UNLOCK with buffet
3 **
10
1.2Refer to 2.33 - MULTIPLE FAILURES.
R ** Landing configuration as recommended by the ECAM.
(1) If CONF 3 is used when "NORM" is indicated in the table, multiply the resulting landing distance by an additional factor of 1.1.
A319/A320/A321
occilml.+7
ABNORMAL PROCEDURES
REV 36
2.31
SEQ 210
VAPP DETERMINATION
R • NORMAL CONFIGURATION (OR NO AVREF)
R The FMGS performs the following VAPP computation for landing in
R normal configuration (CONF 3 or CONF FULL). These VAPP also
R apply for failure cases without AVREF.
Note : For CG < 25 %, add 2 knots to VLS CONE FULL and VLS CONE 3.
W(1000KG)
40
44
48
52
56
60
64
68
72
76
78
VLS CONF FULL (KT)
106
111
116
121
125
130
134
138
142
146
148
VLS CONF 3 (KT)
110
115
120
125
130
135
139
143
147
151
153-VAPP
VAPP= MAX(VLS + 5Kt*; VLS + WIND CORK)I
The 5 knot increment is required when the A/THR is used, or when an autoland is performed.
NOTE: * — In case of ice accretion, Vapp must not be lower than VLS + 5 knots.
— In case of gusty crosswind greater than 20 knots, Vapp should be at least VLS + 5 knots.
R • ABNORMAL/EMERGENCY CONFIGURATION (WITH AVREF)
Note : For CG < 25 %, add 2 knots to VREF.
W(1000Kg)
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
148AVREF
WIND CORRECTION
AVREF> 20KT
LVREF < 20KT
NO WIND
CORRECTION
1/3 HEADWIND
(AVREF + WIND CORR
LIMITED TO 20KT)V APP = VREF +A VREF WIND CORR
TO BE INSERTED ON MCDU PERF APPR PAGE
A319/A320/A321
ocAlmls,
ABNORMAL PROCEDURES
REV 36
2.32
SEQ 100
LDG CONF - APPR SPD
LDG DIST
CORRECTIONS FOR FAILURES
FLAPS LEVER
POSITION
FOR LDG
APPR SPD:
INCREMENT
TO VREF
(A VREF)
LDG DIST
CONF FULL
MULTIPLY BY
ELEC
EMER ELEC CONFIG
3
10
2.0
DC EMER CONFIG
NORM (1)
1.7
DC BUS 1 + 2
NORM (1)
1.75
DC BUS 2
NORM (1)
1.15
DC ESS BUS
NORM (1)
Negl.
AC BUS 1
NORM (1)
1.1
FLT
CTL
ALTN LAW/DIRECT LAW
ELAC 1 + 2/L(R) ELEV FAULT STAB JAM/L + R ELEV FAULT
3
10
1.2
One SPLR FAULT (except n°3 or 5)
NORM (1)
1.1
Two SPLR FAULT
NORM (1)
1.1
Three or more SPLR FAULT
NORM (1)
1.35
SEC 1 or 3 FAULT
NORM (1)
1.1
SEC 2 FAULT
NORM (1)
Negl.
SEC 1 + 2 or 2 + 3 FAULT
NORM (1)
1.2
SEC 1 + 3 FAULT
NORM (1)
