曝光台 注意防骗
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moving little thrust is required. . The wing mounted engines are close to the ground.
Avoid placing engines over unconsolidated or unprepared
ground e.g over the edge of taxyways.
Avoid high thrust settings at low ground speeds due to
the risk of ingestion (FOD).
BRAKES ........................... Check . Brakes can be checked once the aircraft is moving or
while stopped.
To check the brakes while sto ped, depress brake
pedals with parking brake ON, sepect the parking brake
OFF and check that the yellow hyd pressure is zero on
the brake pressure triple indicator.
The main purpose of the brake check is to check that
green pressure has taken over and that yellow pressure
is at zero on the brake pressure triple indicator.
Note : Anypressure below 13Opsion the brake pressure
. Thereafter the normal maximum taxi speed should be
30 kt in a straight line, 15 kt for a sharp turn. The ground
speed is difficult to assess so monitor ground speed on
ND. Do not "ride" the brakes, as 30 kt is exceeded, apply
brakes smoothly and decelerate to 10 kt, release the
brakes and allow the aircraft to accelerate again. . Below - 40" C, small braking inputs are required during
Taxi.= will beindicatedin placeofthe braketemperatures
while the temperatures are below 0".
CAUTION
If the brakes fail during ground o rations,
immediately select the BRWAISKID sw to ETN-OFF
and modulate the brakes with pedals.
Brake pedals should be released when the #ISKID is
switched OFF. Otherwise the pedal braking orders
will be taken into account and the aircraft will react
strongly.
In an extreme emergency and only if pedals are
ineffective with the antiskid OFF the aircraft may be
stopped with the parking brake (full pressure
application will occur).
zero.
.
- trble indicator can be considered as zero.
- If aircraft has beenC pAaUrkTeIdO iNn wet conditions for a
long period, efficiency of first brakes application at
low speed will be reduced.
ECAM .................. Select WCTL page
Mod: 5670
FLIGHT CONTROLS ................. Check
At a convenient stage during taxi :
1. The PNF checl$ full travel and feel of the elevators and
ailerons/spoilers, whilst monitoring on the ECAM F/CTL
page.
: If PlTCH FEEL pushbptron is selected OFFIR then
ON, full traveland feel force ofthe elevators must
be checked.
2. The PF holds the nose wheel steering handle to
maintain theaircraft direction and checks fulltraveland
feel of the rudder, whitst the PNF monitors the €CAM
F/CTL page.
Check all indications return to zero position with
R
R
R
respective controls at neutral, except the ailerons
where droop position is indicated.
3. If the OAT is below - 40" C, the PNF should check full
extension ofthespeedbrakes by setting the speedbrake
lever notch bv notch up to the FULL position whilst
monitoring EdAM F/CTL page.
Note 1 : HYD SYS LO PR waming may occur it test is
pehmed on more than one axis at a time.
Note 2 : FUGHT CONTROL check should be done with
CWS OFF ff CWS is selected full travel will not
be available
Note 3 : &tin aileron check, rudderdeflectsleftorright
coordking wh?h ailemnmovement hawdamper
ATC clearance .............. obtain/confirm
TAKE OFF DATA/CONDITIONS ... Check/Revise - lftake off data have become more limiting such as wind
change or Tower temperature increase, or in case of
runway change, prepare updated take off data and as
appropriate :
SlA- TS/eFlLeActP T aWke EofRf p .o.si.ti.on. ........ takeoff position
V 2 , . ......................... resetonFCU
Initial cfimb speed .............. preset on FCU
F U TO temperature ............ Reinsert in TRP
PITCH TRIM ................... ChecWAdjust
If flap setting is changed, pitch trim setting should be
adjusted.
FMS
V1,VR ........................... Reinsert
F-PLN (Runway) ..................... Revise
Particular care should be taken to confirm the ATC
clearance agrees with the FMS if NAV is to be used.
-
ECAM . !??q.. ............d eselect WCTL page
-
. F-PLN (SID, TRANS) ........... Revise or :heck
FCU ............................. Asreq
m h o u l d not be selected in CMD for Take off.
CLEARED ALT ................... Set on FCU
IF PROFILE NAV mode is used
PROF1 L E . . . . . . . . . . . . . . . . . . . . . . , . . . , . . A r m
NAV ...............................A m
INITIAL AFTER T.O. HDG ....... Set on FCU/As req
If an ATC HDG is required after ta ke off set the heading on
the FCU, NAV will be disarmed
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