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To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A330/A340 FLEET PRO-ABN-80 P 55/140
FCOM 19 AUG 10
Continued from previous page
UNRELIABLE SPEED INDICATION/ADR
CHECK PROC 3 15 1.25* 1.20*
TRIPLE ADR FAULT 3 15 1.25* 1.20*
DOUBLE ADR/IR FAULT 3 5 1.15* 1.10*
(15) In case of dispatch with one or more reverser(s) inoperative, use the LDG DIST factors ″WITHOUT REV.″, whatever
the actual thrust reversers selection at landing.
FULL 10 1.20 1.15
BLEED
WING LEAK/ENG BLEED LEAK/ABNORM
BLEED CONFIG/BLEED LO TEMP (1)with
ice accretion 3 15 1.20 1.15
(16) Flaps FULL and Flaps 3 are both acceptable positions. Flaps FULL is recommended, but the flight crew may use
Flaps 3, if necessary, for operational reasons.
(17) In case of dispatch with one or more reverser(s) inoperative, use the LDG DIST factors ″WITHOUT REV.″, whatever
the actual thrust reversers selection at landing.
SHUTDOWN (if no damage) 3 5 1.25 1.20
SHUTDOWN (if damage without ice
accretion) 3 5 1.25 1.20
SHUTDOWN (if damage with ice accretion) 3 15 1.70 1.60
THR LEVER FAULT/DISAGREE 3 5 1.25* 1.20*
ENG
REV UNLOCKED (with buffet) 2 25 1.50* 1.50*
(18) In case of dispatch with one or more reverser(s) inoperative, use the LDG DIST factors ″WITHOUT REV.″, whatever
the actual thrust reversers selection at landing.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A330/A340 FLEET PRO-ABN-80 P 56/140
FCOM 19 AUG 10
LDG CONF/APPR SPD/LDG DIST ON DRY RUNWAYS FOLLOWING FAILURES
Applicable to:
DRY RUNWAYS
LDG DIST Factors
SYS FAILURE
FLAPS
LEVER
POSITION
FOR LDG
Δ VREF
APPR SPD
INCREMENT
DRY
WITHOUT
REV. (2)
DRY
WITH REV.
EMER CONFIG 3 5 1.25 N/A
DC BUS 1+2 FAULT (1)FULL - 1.20 N/A 3 5 1.25 N/A
DC BUS 2 FAULT (1)FULL - 1.20 1.20 3 5 1.25 1.25
DC ESS BUS FAULT (1) if ice accretion FU3LL 1105 11..2355 11..2305
FULL 10 1.25 1.25
ELEC
DC ESS SHED (1) if ice accretion 3 15 1.35 1.30
(1) Flaps FULL and Flaps 3 are both acceptable positions. Flaps FULL is recommended, but the flight crew may use
Flaps 3, if necessary, for operational reasons.
(2) In case of dispatch with one or more reverser(s) inoperative, use the LDG DIST factors “WITHOUT REV.” whatever
the actual thrust reversers selection at landing.
0 ≤ Flaps < 1+F 2 30 1.65* 1.55*
1+F ≤ Flaps < 2 2 15 1.40* 1.35*
2 ≤ Flaps < 3 2 10 1.30* 1.25*
Flaps = 3 3 5 1.25* 1.20*
FLAPS FAULT
Flaps > 3 FULL 5 1.20* 1.20*
0 ≤ Slats < 1 2 30 1.60* 1.50*
SLATS FAULT 1 ≤ Slats < 2 2 15 1.35* 1.30*
Slats ≥ 2 3 5 1.25* 1.20*
0 ≤ Flaps < 1+F 1 50 1.90* 1.85*
1+F ≤ Flaps < 2 2 40 1.75* 1.70*
2 ≤ Flaps < 3 2 30 1.60* 1.50*
Flaps = 3 3 25 1.50 1.45
0 ≤ Slats < 1
Flaps > 3 FULL 25 1.50* 1.45*
0 ≤ Flaps < 1+F 2 30 1.65* 1.55*
1+F ≤ Flaps < 2 2 20 1.45* 1.40*
2 ≤ Flaps < 3 2 15 1.35* 1.30*
Flaps = 3 3 10 1.30* 1.25*
1 ≤ Slats < 2
Flaps > 3 FULL 10 1.25* 1.25*
0 ≤ Flaps < 1+F 2 30 1.65* 1.55*
S/F
Slats ≥ 2 1+F ≤ Flaps < 2 2 15 1.40* 1.35*
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A330/A340 FLEET PRO-ABN-80 P 57/140
FCOM 19 AUG 10
Continued from previous page
2 ≤ Flaps < 3 2 10 1.30* 1.25*
Flaps = 3 3 5 1.25 1.20*
Flaps > 3 FULL - 1.15* 1.15*
NO FLAPS/NO SLATS 1 50 1.90* 1.85*
(3) In case of dispatch with one or more reverser(s) inoperative, use the LDG DIST factors ″WITHOUT REV.″, whatever
the actual thrust reversers selection at landing.
STAB CTL FAULT (MAN trim not available) 2 20 1.45* 1.40*
STAB CTL FAULT (MAN trim available) 3 5 1.25* 1.20*
L/R/L+R ELEV FAULT 2 20 1.45* 1.40*
RUDDER JAM/RUDDER FAULT 2 10 1.75* 1.60*
RUDDER JAM/RUDDER FAULT
(Engine-out) 2 170 kt
(APPR SPD) 2.55* 2.55*
ALTN/DIRECT LAW 3 5 1.25* 1.20*
YAW DAMPER FAULT 3 5 1.25* 1.20*
PRIM 1(2)(3)/1+2 FAULT (1)FULL - 1.20 1.15 3 5 1.25 1.20
PRIM 1+3/2+3 FAULT (1)FULL - 1.20 N/A 3 5 1.25 N/A
PRIM 1+2+3 FAULT 3 5 1.35 N/A
SEC 1(2)/1+2 FAULT (1)FULL - 1.20 1.15 3 5 1.25 1.20
ONE/TWO pairs of spoilers (1)FULL - 1.20 1.15 3 5 1.25 1.20
THREE/FOUR pairs of spoilers (1)FULL - 1.25 1.20 3 5 1.25 1.25
　
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