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case of failure of the critical engine, the other
engine remaining attake-off power (take-off flaps
setting and gear retracted).
: Equal to 1.25 Vs Slats 15.Flaps 0 . It is the
minimum speed at which the flaps may be
retracted to 0".
Represented by u F B on airspeed scale when
the SLATELAP handle is in the 15/15 or 15/20
the aircraft can be controlle B by use of the
. . - S c: oEnqfiugaulr atotio 1n..2 5 Vs Slats 0 Flaps 0 , It is the
minimum speed at which the slats may be
. ...:. . . . .
. . . . . . . . ' .. :..
retracted to '0".
Represented by u.S D on airspeed scale when the
- 0 (a GRSELEANT FDLOATP D )h a:n EdNleG IIsN IEn OthUeT 1 O5P/0E cRoAnTfiIgNuGr asptioene.d
(BEST LIFT TO DRAG RATIO speed or DRIFT
DOWN speed) in clean configuration. It
corresponds also to the FINAL TAKE OFF speed.
It is equal to205 k a t 120 t f 1 kt perton + 3 kt
per 1 000 ft above 20 000 pt.
Represented by uOm (green dot) on airspeed
scale when the SLATFLAP handle is in the 0/0
configuration.
N S : 0, FandS speeddisplayedare only valid,
8s manoeuvring speeds, when the
SLATS/FLAPS 8~ in the commanded
position. -- VVFREE F :: MReafxeirmenucmes pse eedef odr euascehd s lafotsrf lapas ncoornmfigaul rfaintioanl
approach, it E equal to 1.3 Vs Slats 30 /Flaps
- VLS : 4L0o wceosntf i# eulreactitoanb.l e speed. It is represented by
an amber strip along the airspeed scale which
appears 5 seconds after lift-off.
In the T10 schedule VLS = 1.2 Vs of the actual
. .
. ... ..'
R
R T/O configuration.
..
' In the LANDING Schedule VW = 1.3 Vs of the
-a cCtuhaaln lgaen dinfrgo mco nfTig/Our attioon . landin schedule
is triggered by SLATS/FLAk handle
displacement (either retraction or extention, - CFange from landing to T/O schedule s
triggered by LDG GEAR SHOCK absorber
compression (NC on QTound).
Above 25 000 ft VLS is calculated so that %ere
is 0.3 g margin with respect to BUFFETING.
In case of SLATS orland :LAPS JAMMING, 4 3
represents 1.3 Vs of the actual (ABNOPMALI
configuration.
: Stick shaker speed : Pe speed at Nhich the
stick shaker is activated. t is represented by d
red and black strip along the airspeed scale. It
is equal to 1.128 Vs ia clean configuratiop,
1.11 Vs in other configurations.
- Vss
- VAPP : Final approach speed,
+ VAPPc an be computed based on VREFo r ~ L S:
VAPP = VREF + VREF INCREMENT + WIND CORR,
V-A IPnP =S L VALTSS + = V/FLLSA IPNSC RE40M EcNoTnf +ig uWraINtioDn C, OLRLRS. =
- VREF incrementsareconsidered in case offailures
- aVfLfSe citnincgre tmhee mntas naeruev ceoranbsiilditeyr oerd th web s t?anlle mvierrg tihne,
failure is not accounted in the VLS cp rmpmtion
1i.e. kruger retracted or rod spoilers inoperative).
VREF,
2. WIND CORRECTION
I -7
I (1/3 AVERAWGEIN WD INCDO)R ORRE C(GTIUOSNT = I F, HIGHER) I
N B : 1. The average wind is the wind speed due
reportedb y the ATlS or tnwer, irrespective 3f its
direction.
2. Thegustis the differencedetween themaxmum
wind speed and the average wind pees e.g.
for a wind of 20.kVgustmg 25 kz the average
wind speed is 20 &and tPe gust is (25-20) I 5 kt.
+ Apply WIND CORR only ifthere is notail-wind component
+ If MHR is used or when significant ice accretion is
suspected :
if WIND CORR < 5 kt, take WI JD CORR = 5 kt,
+ Maximum WIND CORR = 15 kt,
+ If LDG SPD INCREMENT ON VR :F c 20 kt ;
maximum LDG SPD INCREME NT ON VREF + WIND
' CORR = 20 kt,
+ If LDG SPD INCREMENT ON VR IF > 20 kt ,
do not apply any WIND CORF
FMS VAPP (on APPROACH page IS defined as :
VAPP = VREF + (11 kt, if bndir 3 in 20/20) t 5 kt + WIND CORR.
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t I 2.03.1 0 I
STANDARD OPERATING PROCEDURES
PAGE 1
@A300-600
WGW CREW OPERATING MANUAL I TAXI
NOSE Light ........................ TAXI
Select NOSE Light to TAXI day and night
TAXI CLEARANCE ................ Obtained
PARKING BRAKE ...................... OFF - Release the parking brake and check brake pressure
ELAPSED TIME ...................... Start
To record block time
EXTERIOR LTS ..................... As req
THRUST LEVERS .................... As req . In order to get the aircraft moving, little if an wer
above idle thrust will be required (max 40% Nlr. grust
should normally be used symmetrically. Once aircraft is
　
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