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and thereby cool IDG oil.
2. High Speed- Reduce generator load, or turn off generator.
If the oil temperature continues to increase, mechanically
disconnect IDG.
OIL QTY
< 5 qt
If the quantity of oil is low at a high power setting, expect
level increase after power reduction
NAC TEMP ≥ 320 °C Monitor engine parameters and crosscheck with other
engine.
VIBRATION
N1 ≥ 5 units
N2 ≥ 5 units
Refer to PRO-ABN-70 HIGH ENGINE VIBRATION.
USE OF THE FOLLOWING TABLES
Applicable to: ALL
USE OF THE LDG DIST FACTORS
Use the LDG DIST factors “WITHOUT REV” when:
All ‐ reversers are inoperative, or
‐ Maximum reverse thrust on available reverser(s) is not selected, or
‐ The aircraft has been dispatched with one or more reverser(s) inoperative.
Use the LDG DIST factors “WITH REV” when at least one reverser is operative and maximum
reverse thrust is selected at landing.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A318/A319/A320/A321 FLEET PRO-ABN-80 P 83/182
FCOM 19 AUG 10
Applicable to: ALL
LDG CONF/APPR SPD/ LDG DIST COMPUTATION FOR A SINGLE FAILURE
Determine the Flaps Lever Position for landing to be selected
Compute the VAPP: VAPP = VREF + ΔUQDE􀀃􀀎􀀃􀀤OOQ􀀃BNQ
‐􀀃Cdsdqlhmd􀀃sgd􀀃ΔUQDE
‐ Determine the APPRoach CORrection (Refer to QRH/ABN-80 VAPP CALCULATION)
Compute the LDG DIST:
‐ Determine le 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)
Applicable to: MSN,
4473
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􀀃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 84/182
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
1.75
1.90
RESULT 3 10
5 1.1
1.40 × 1.90 × 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􀁄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: ,
, MSN,,
LDG CONF / APPR SPD / LDG DIST COMPUTATION FOR MULTIPLE FAILURES
　
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