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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 kt
WINDSHIELD HEAT (L or R windshield) 1 for PF
WINDSHIELD WIPERS OR RAIN
REPELLENT (if activated)
1 for PF
ND 1 2 2
AUTO CALLOUT FUNCTION one is required
for autoland
1 1
ATTITUDE INDICATION (STBY ) 1 1 1
NOT FMGS
MONITORED
FOR FMA LDG
CAPABILITY
DH INDICATION 1 for PNF
(1) For automatic rollout, one is required. For autoland without automatic rollout,
none is required.
Note: ‐ Flight crews are not expected to check the equipment list before approach.
When an ECAM or
local caution occurs, the crew should use the list to confirm the landing capability.
‐ On ground, the equipment list determines which approach category the aircraft will
be able to
perform at the next landing.
‐ Electrical power supply split : This ensures that each FMGC 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.
OPS
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OPERATIONAL DATA
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OPERATIONAL DATA
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OPERATIONAL DATA
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OPS-PLP PRELIMINARY PAGES
TABLE OF
CONTENTS.....................................................................................................................
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Required Equipment for CAT2 and
CAT3..........................................................................................................................3/4
OPS
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OPS
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OPERATIONAL DATA
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A318/A319/A320/A321 FLEET MSN 4617
SEVERE TURBULENCE
SPEED AND THRUST SETTING FOR RECOMMENDED TURBULENCE SPEED
GROSS WEIGHT (1000 kg)
FL 54 58 62 66 70 74 78 82 86 90 94
SPD
or
Mach N1 %
390 0.76 79.4 80.6 - - - - - - - - -
370 0.76 77.9 78.9 80.0 81.2 - - - - - - -
350 0.76 77.2 77.9 78.8 79.7 80.7 - - - - - -
330 0.76 76.9 77.6 78.2 79.0 79.8 80.7 81.6 - - - -
310 0.76 76.7 77.3 77.9 78.5 79.2 79.9 80.6 81.5 82.4 - -
290 0.76 76.7 77.2 77.7 78.2 78.8 79.4 80.0 80.6 81.4 82.1 83.0
270 300 76.2 76.6 77.0 77.5 78.0 78.5 79.1 79.6 80.3 80.9 81.6
250 300 75.0 75.4 75.8 76.2 76.7 77.1 77.7 78.2 78.9 79.5 80.2
200 300 72.2 72.5 72.9 73.3 73.7 74.2 74.7 75.2 75.8 76.4 77.0
150 270 65.5 65.9 66.5 67.0 67.7 68.4 69.2 70.3 71.0 71.8 72.6
100 270 62.5 62.9 63.5 64.0 64.6 65.3 66.0 66.8 67.6 68.4 69.2
50 270 59.1 59.5 60.0 60.5 61.1 61.8 62.6 63.4 64.2 65.0 65.7
SIGNS.............................................................................................................................
.......................... ON
AUTO
PILOT..............................................................................................................................
....KEEP ON
A/THR (when thrust changes become
excessive).................................................................. DISCONNECT
�� FOR APPROACH:
A/THR in managed
speed..................................................................................................................USE
OPS
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HYDRAULIC ARCHITECTURE
OPS
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FLIGHT CONTROLS ARCHITECTURE
→ Arrows indicate the control reconfiguration priorities
G B Y indicates the hydraulic power source for each servo control
REQUIRED EQUIPMENT FOR CAT2 AND CAT3
FMA CAPABILITY →
EQUIPMENT ↓ CAT 2 CAT 3 SINGLE CAT 3 DUAL
AP 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
　
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