Page 75 - Demo

2.10/59
REV 26
A330
CHINA AIRLINES
REV 26
PAGE 59
OVERWEIGHT LANDING
Under crew responsibility, an automatic landing may be performed up to 504 853 lb.
– LDG CONF.....................................................AS REQUIRED Use ECAM flap setting, if required for abnormal operation. In all other cases :
– FULL is preferred for optimized landing performance.
–If the aircraft weight is above the maximum weight for go-around (given in the table below), use FLAP 3 for landing.
In all cases, if landing configuration is different from FLAP FULL, use 1 + F for go-around.
– LDG DIST...................................................................CHECK
– PACK 1 and 2 ................................OFF or supplied by APU Selecting packs off (or supplied from APU) will increase the
maximum thrust available from the engines, in the event of a go-around.
! Infinalstagesofapproach:
– TARGET SPEED ..........................................................VLS
Reduce speed to reach VLS at runway threshold.
Touch down as smoothly as possible (Maximum V/S at touchdown 360 ft/min).
! Atmainlandinggeartouchdown
– REVERSE THRUST ...................... USE MAX AVAILABLE
! Afternosewheeltouchdown:
– BRAKES .................................... APPLY AS NECESSARY
Maximum braking may be used after nosewheel touchdown. But, if landing distance permits, delay or reduce braking to take full benefit of the available runway length.
! Landingcomplete
– BRAKE FANS ..........................................ON (if available)
Be prepared for tire deflation, if temp. exceed 800°C.
MAX WT FOR GO AROUND IN CONF 3 (1000 LB) CLB GRADIENT2.1%
OAT ()
AIRPORT ELEVATION (feet)
0
2000
4000
6000
8000
10000
12000
14000
10
523
498
470
440
410
381
350
322
15
522
498
470
439
406
372
340
313
20
522
497
469
434
396
360
327
305
25
521
496
460
421
383
345
318
298
30
517
480
445
405
367
331
310
35
498
461
427
389
351
40
480
445
411
373
45
459
424
393
50
435
401
55