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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.
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TABLE OF
CONTENTS.....................................................................................................................
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SEVERE
TURBULENCE...............................................................................................................
.................................... 1/4
Required Equipment for CAT2 and
CAT3..........................................................................................................................3/4
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SEVERE TURBULENCE
SPEED AND THRUST SETTING FOR RECOMMENDED TURBULENCE SPEED
GROSS WEIGHT (1000 kg)
FL 54 58 62 66 70 74 78 82 86
SPD
or
Mach N1 %
390 0.76 83.7 84.7 - - - - - - -
370 0.76 82.6 83.4 84.2 85.2 - - - - -
350 0.76 82.0 82.7 83.3 84.1 84.8 - - - -
330 0.76 81.8 82.4 83.1 83.7 84.3 85.0 85.7 - -
310 0.76 81.8 82.3 82.8 83.4 83.9 84.5 85.1 85.7 86.4
290 0.76 82.0 82.3 82.7 83.2 83.7 84.2 84.7 85.3 85.8
270 300 81.5 81.8 82.1 82.5 82.9 83.4 83.9 84.4 85.0
250 300 80.1 80.5 80.9 81.4 81.8 82.2 82.7 83.2 83.7
200 265 71.2 71.8 72.5 73.2 74.0 74.9 75.8 76.8 77.7
150 265 67.5 68.1 68.7 69.3 70.0 70.7 71.5 72.3 73.2
100 265 63.5 64.1 64.7 65.3 66.1 66.8 67.6 68.5 69.4
50 265 60.2 60.7 61.2 61.7 62.3 62.9 63.6 64.3 65.1
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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