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‐ 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.
OPERATIONAL DATA
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TABLE OF
CONTENTS.....................................................................................................................
................................1/2
Required Equipment for CAT2 and
CAT3..........................................................................................................................4/6
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SEVERE TURBULENCE
SPEED AND THRUST SETTING FOR RECOMMENDED TURBULENCE SPEED
GROSS WEIGHT (1000 kg)
FL 40 44 48 52 56 60 64 68 72 76
SPD
or
Mach N1 %
390 0.76 78.9 79.7 80.6 81.7 82.8 - - - - -
370 0.76 78.2 78.8 79.5 80.3 81.3 82.3 83.4 - - -
350 0.76 77.8 78.4 79.0 79.6 80.3 81.2 82.1 83.1 84.1 -
330 0.76 77.8 78.3 78.9 79.5 80.0 80.7 81.4 82.2 83.1 84.0
310 275 77.1 77.6 78.1 78.7 79.3 80.0 80.6 81.2 81.9 82.8
290 275 75.6 76.1 76.6 77.1 77.7 78.4 79.2 80.0 80.6 81.4
270 275 74.1 74.5 75.1 75.7 76.2 76.9 77.6 78.3 79.2 80.1
250 275 72.6 73.0 73.5 74.1 74.7 75.3 76.1 76.8 77.6 78.4
200 275 69.2 69.5 69.9 70.3 70.8 71.4 72.0 72.7 73.4 74.1
150 250 61.4 61.9 62.5 63.2 64.0 64.8 65.7 66.8 67.9 68.8
100 250 58.0 58.5 59.1 59.7 60.3 61.0 61.7 62.6 63.5 64.5
50 250 54.1 54.5 55.1 55.7 56.4 57.2 58.0 58.9 59.9 60.8
SIGNS.............................................................................................................................
.......................... ON
AUTO
PILOT..............................................................................................................................
....KEEP ON
A/THR (when thrust changes become
excessive).................................................................. DISCONNECT
�� FOR APPROACH:
A/THR in managed
speed..................................................................................................................USE
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HYDRAULIC ARCHITECTURE
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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
FAC 1 1 2
ELAC 1 1 2
YAW DAMPER/RUDDER TRIM 1/1 1/1 2/2
HYDRAULIC CIRCUIT 2 2 3
PFD 2 2 2
FLIGHT WARNING COMPUTER 1 1 2
BSCU CHANNEL 1(1) 1(1) 1
FMGS
MONITORED
FOR FMA LDG
CAPABILITY
ANTISKID 1(1) 1(1) 1
To be continued on next page
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Continued from previous page
NOSEWHEEL STEERING 1(1) 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
AP DISCONNECT PB 2 2 2
”AP OFF” ECAM WARNING 1 1 2
　
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