SEQ 001
REQUIRED EQUIPMENT FOR CATII AND CATIII
FMA CAPABILITY —>
CAT 2
CAT 3 SINGLE
CAT 3 DUAL
EQUIPMENT 1
FMGS MONITORED FOR FMA
LDG CAPABILITY
AP/FD
1 AP ENGAGED
1 AP ENGAGED
2 AP ENGAGED
AUTOTHRUST
0
1
1
FMA
1
2
2
A/THR CAUTION
0
1
1
ELECTRICAL SUPPLY SPLIT
0
0
1
FAC
1
1
2
ELAC
1
1
2
YAW DAMPER/RUDDER TRIM
1/1
1/1
2/2
PFD DUs
2
2
2
FLIGHT WARNING COMPUTER
1
1
2
BSCU CHANNEL
1*
1*
1
ANTISKID
1*
1*
1
NOSEWHEEL STEERING
1*
1*
1
RADIO ALTIMETER
1
(displayed on
both sides)
2
2
ILS RECEIVER
2
2
2
BEAM EXCESSIVE DEVIATION WARNING
1 for PNF
2
2
ATTITUDE INDICATION (PFD1/PFD2)
N° 1 + N° 2
N° 1 + N° 2
N° 1 + N° 2
ADR/IR
2/2
2/2
3/3
NOT FMGS MONITORED FOR
FMA LDG CAPABILITY
AP DISCONNECT PB
2
2
2
"AP OFF" ECAM WARNING
1
1
2
"AUTOLAND" LIGHT
1
1
1
RUDDER TRAVEL LIMIT SYSTEM
1 required for autoland with crosswind
higher than 12 Id
WINDOW HEAT (L or R windshield)
1 for PF
WINDSHIELD WIPERS OR RAIN REPELLENT (if activated)
1 for PF
ND DUs
1
2
2
AUTO CALLOUT FUNCTION
required one is req
for autoland
1
1
ATTITUDE INDICATION (STBY)
1
1
1
DH INDICATION
1 for PNF* For automatic rollout, one is required. For autoland without automatic rollout, none is required.
Note : . Failure of ant/skid or nosewheel steering mechanical parts are not monitored for LDG capability.
. Electrical power supply split : device ensuring that both FMGCs
are powered by independent electrical sources (AC and DC).
. DH indication and auto callout "hundred above" and "minimum" are only announced if a manual entry is performed on MCDU
. Flight crews are not expected to check the listed equipment before approach. When an ECAM or local caution occurs, the crew should use the list to confirm the landing capability.
. On the ground, the list of equipment determines what category of approach the aircraft is able to perform at next landing.
A319/A320/A321
Occ'Et1ri°,2!
NORMAL CHECK LIST
REV 35
7.01
SEQ 002
NCL5-00-0007-001-A002AA
CES MSN 1028-1070 1312-1361 1532 1542 1639 1906-2068
A319/A320/A321
0 cci2IMISO
NORMAL CHECK LIST
REV 35
7.01
SEQ 130
NCL5-00-0007-001-A130AA
CES MSN 1285-1303 1377-1386 1541 1551-1603 1778-1786
THIS TABLE GIVES, FOR EACH AIRCRAFT INCLUDED IN THE MANUAL, THE CROSS REFERENCE BETWEEN
* THE MANUFACTURING SERIAL NUMBER (MSN1 WHICH APPEARS IN THE LIST OF EFFECTIVE PAGES
* THE REGISTRATION NUMBER OF THE AIRCRAFT AS KNOWN IV AIRBUS INDUSTRIE.
MSN
REGISTRATION
1028
1.2207
1030
1.2209
1070
1.2208
1285
1.2331
1303
1.2332
1312
1.2335
1330
1.2336
1357
1.2337
1361
1.2338
1377
1.2333
1386
1.2334
1532
1.2219
1541
1.2215
1542
1.2220
1551
1.2216
1601
1.2217
1603
1.2222
1639
1.2221
1778
1.2227
1786
1.2226
1906
1.2228
1911
1.2229
1964
1.2230
1981
1.6001
2022
1.6002
2034
1.6003
2036
1.6005
2049
1.6008
2056
1.6007
2068
1.6006
0.04
318/319/320/321 QUICK REFERENCE HANDBOOK REV036A
M
M
11
---PAGE---
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0 .00
0 .01
0 .02
0 .02A
0 .026
0 .02C
0 .03-
0 .04-
0 .06-
0 .07-
1 .00
1 .01
1 .02
1 .03
1 .04
1 .05
1 .06
1 .05
1 .06
1 .05
1 .06
1 .07
1 .08
1 .07
1 .08
1 .09
1 .10
1 .09
1 .10
1 .09
1 .10
1 .09
1 .10
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