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Only combine PRIMARY or SINGLE failures
Determine the Flaps lever position for landing to be selected:
Use the lowest Flaps Lever Position for landing ‐ (i.e. if FULL and 3, use 3)
Computd􀀃sgd􀀃U􀀤OO9􀀃U􀀤OO􀀃<􀀃UQDE􀀃􀀎􀀃Δ􀀃UQDE􀀃􀀎􀀃􀀤OOQ􀀃BNQ
‐􀀃Trd􀀃sgd􀀃ghfgdrs􀀃Δ􀀃UQDE􀀃sn􀀃bnlotsd􀀃U􀀤OO
‐ Determine the APPRoach CORrection (Refer to QRH/ABN-80 VAPP CALCULATION)
Compute the LDG DIST:
‐ Determine the applicable LDG DIST factors in the same column (“WITH REV.” or “WITHOUT
REV.”)
‐ Multiply the applicable LDG DIST factors together, unless all values are marked with an asterisk
(*). If all values are marked with an asterisk, use the highest LDG DIST factor. Multiply it by the
additional factor, if any (Refer to QRH/ABN-80 VAPP CALCULATION)
‐ Multiply the obtained LDG DIST factor by the ACTUAL LANDING DISTANCE WITHOUT
AUTOBRAKE – CONFIGURATION FULL – without reversers correction (Refer to QRH/FPE-IFL
Landing Distance Without AUTOBRAKE - CONF FULL)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A318/A319/A320/A321 FLEET PRO-ABN-80 P 85/182
FCOM 19 AUG 10
FAILURES
Flaps Lever
Position
For Landing
Δ VREF APPR
COR
Additional
Factor LDG DIST Factor
FLAPS FAULT
(F < 3, S ≥ 1) 3 10 1.40*
BRK ANTI SKID FULL
3
-6
1.60
1.75
RESULT 3 10
5 1.1
1.40 × 1.75 × 1.1 = 2.70
Examples applicable to Dry runways / A/THR ON / No wind / WITHOUT REV./Without ice accretion:
VREF = 131 kt. Therefore VAPP = 131 +10 + 5= 146 kt.
HYPOTHESIS OF COMPUTATION : Δ VREF/LDG DIST FACTORS
Sgd􀀃Δ􀀃UQDE􀀃u􀁄ktdr􀀃s􀁄􀁎d􀀃hmsn􀀃􀁄bbntms􀀃sgd􀀃mdbdrr􀁄qx􀀃bnqqdbshnmr􀀃ctd􀀃sn9
The failure, including SECONDARY(s) ‐ failures (as per ECAM definition)
‐ The required Flaps Lever Position for landing
The LDG DIST factors take into account:
‐􀀃􀀤m􀀃􀁄ooqn􀁄bg􀀃roddc􀀃􀁄s􀀃UQDE􀀃􀀎􀀃Δ􀀃UQDE
‐ The SECONDARY(s) failures, including inoperative reverser(s) if any
‐ No wind conditions
Applicable to:
LDG CONF / APPR SPD / LDG DIST COMPUTATION FOR MULTIPLE FAILURES
Only combine PRIMARY or SINGLE failures
Determine the Flaps lever position for landing to be selected:
‐ Use the lowest Flaps Lever Position for landing (i.e. if FULL and 3, use 3)
Bnlotsd􀀃sgd􀀃U􀀤OO9􀀃U􀀤OO􀀃<􀀃UQDE􀀃􀀎􀀃Δ􀀃UQDE􀀃􀀎􀀃􀀤OOQ􀀃BNQ
‐􀀃Trd􀀃sgd􀀃ghfgdrs􀀃Δ VREF to compute VAPP
‐ Determine the APPRoach CORrection (Refer to QRH/ABN-80 VAPP CALCULATION)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A318/A319/A320/A321 FLEET PRO-ABN-80 P 86/182
FCOM 19 AUG 10
Compute the LDG DIST:
‐ Determine the applicable LDG DIST factors in the same column (“WITH REV.” or “WITHOUT
REV.”)
‐ Multiply the applicable LDG DIST factors together, unless all values are marked with an asterisk
(*). If all values are marked with an asterisk, use the highest LDG DIST factor. Multiply it by the
additional factor, if any (Refer to QRH/ABN-80 VAPP CALCULATION)
‐ Multiply the obtained LDG DIST factor by the ACTUAL LANDING DISTANCE WITHOUT
AUTOBRAKE – CONFIGURATION FULL – without reversers correction (Refer to QRH/FPE-IFL
Landing Distance Without AUTOBRAKE - CONF FULL)
FAILURES
Flaps Lever
Position
For Landing
Δ VREF APPR
COR
Additional
Factor LDG DIST Factor
FLAPS FAULT
(F < 3, S ≥ 1) 3 10 1.35*
BRK ANTI SKID FULL
3
-
10
1.75
2.00
RESULT 3 10
5 1.1
1.35 × 2.00 × 1.1 = 3.00
Examples applicable to Dry runways / A/THR ON / No wind / WITHOUT REV./Without ice accretion:
VREF = 131 kt. Therefore VAPP = 131 +10 + 5 =146 kt.
HYPOTHESIS OF COMPUTATION : Δ VREF/LDG DIST FACTORS
Sgd􀀃Δ􀀃UQDE􀀃u􀁄kues take into account the necessary corrections due to:
The failure, including SECONDARY(s) ‐ failures (as per ECAM definition)
　
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