Page 178 - Demo

2.40/64
REV 18
A330
CHINA AIRLINES
REV 18
PAGE 64
REQUIRED EQUIPMENT FOR CAT II / CAT III APPROACH
CAT III a
1 AP ENGAGED
1
2
0
1
1
1
2
2
2
1
1*
1*
1*
2
2
No. 1 + No. 2
2/2
2
2
1
1
1
CAPABILITY → EQUIPMENT ↓
CAT II
AP/FD 1 AP ENGAGED 2 AP ENGAGED
CAT III b
1 FMA1 2
AUTOTHRUST 0
ELEC POWER SUPPLY SPLIT
01
PRIM 1
(No. 1 + No. 2) or (No. 1 + No. 3)
SEC1 2 RUDDER TRIM 1 2
HYDRAULIC CIRCUIT
23
PFD2 2 DMC2 2
FLIGHT WARNING COMPUTER
12
BSCU CHANNEL 1* 1 ANTISKID 1* 1
NOSEWHEEL STEERING
RADIO ALTIMETER
ILS RECEIVER ATTITUDE INDICATION (PFD1/PFD2) ADR / IR BEAM EXCESSIVE DEVIATION
AP DISCONNECT PB “AP OFF” ECAM WARNING “A/THR OFF” ECAM CAUTION “AUTOLAND” LIGHT
WINDSHIELD HEAT
(L or R windshield)
WINDSHIELD WIPERS OR RAIN REPELLENT
(if activated)
ND
AUTO CALLOUT FUNCTION ATTITUDE INDICATION (STBY) DH INDICATION
1*
1 (displayed on both sides)
1
2 2 2
No. 1 + No. 2
2/2
1 for CM2
No. 1
+ No. 2
1 for CM2
* Required only for automatic roll out, if functions not available,
3/3 2
22 12
01 11 1 for CM1
1 for CM1
1 2 11
11
2
1
1
perform manual roll out.
Note:
– Flightcrewsarenotexpectedtochecktheequipmentlist before approach. When an ECAM or local caution occurs, the crew should use the list to confirm the landing capability.
– Onground,theequipmentlistdetermineswhichapproach category the aircraft will be able to perform at the next landing.
– Electrical power supply split : This ensures that each FMGEC is powered by an independent electrical source (AC and DC)
– Failure of antiskid and / or nosewheel steering mechanical
parts are not monitored for landing capability.
– The DH will be displayed on the FMA, and the "Hundred
Above" and "Minimum " auto callouts will be announced, provided that the DH value has been entered on the MCDU.
NOT FMGS MONITORED FOR FMGS MONITORED FOR FMA FMA LDG CAPABILITY LDG CAPABILITY