(1)Takeoff Speed Tables Instructions
1. Use only Optimum V
2
takeoff speeds from the specific
airport runway analysis page when utilizing Optimum
V
2
performance.
2. Use actual takeoff weight rounded DOWN to the
nearest 1,000 kg. increment for takeoff speed
deter-mination.
3. Make speed adjustments as instructed on the Takeoff
Speed Adjustments page.
Takeoff Speed Adjustments
"3 1. Make V1A/R density altitude adjustments from the
0 graph located on each page using the temperature
-j at which thrust will be set. Use the assumed
tem-.-, perature if making a reduced thrust takeoff (Flex
f Thrust).
D 2. Add 1 knot to all speeds when operating with
Ex--j tended Forward C.G..
3. V1 for takeoff is the lesser of the Speed Book V1 or
t the Performance Handbook MAX V1 for the
(2)MINIMUM SPEEDS
A320-200 V2500-AI
V1
VR
V2
FLAPS 1
114
119
FLAPS 2
112
117
FLAPS 3
112
117
120
VMCG
VMCA
VMCA
5
•5
! ' Maneuvering and Landing Speeds
f ' 3 1. Use estimated landing weight rounded to the nearest
j,! 5 1,000 kg. increment for V
|s
/V
ref
determination.
2. Add 2 knots to all speeds for Extended Fwd C.G..
(forward of 25% MAC)
3. Minimum maneuvering speeds are based on a bank
") angle of 30° plus a 15° overshoot before cc
max
at an
5 altitude of 10,000 feet and are equivalent to V
ls
as
~ displayed on the PFD. They may be applied up to
FL200, but must be increased by 1 knot/2,000 feet
5 above 10,000. In smooth air at the appropriate
5 minimum maneuvering speed, a
max
will occur at
(3)Holding Speeds
The Holding Speeds table provides the green dot
speeds, which are between minimum fuel speed and
minimum drag speed. These speeds are protected by
at
least a 1.3g
buffet
margin.
High Altitude Buffet Boundaries
The Buffet Boundaries tables provide the speeds at
which the
aircraft will experience high and low speed
buffet at
a 1,3
G-load. A
1.3
G-load is equivalent to a 39"
bank angle in
still
air
or
straight and
level
flight in
moder-ate turbulence.
HOLDING SPEEDS
ALL ENGINES
OPERATING
A320-200
ALTITUDE
FL390
FL370
FL350
FL300
FL250
FL200
15,000 FT
10,000 FT
5,000 FT
1,500 FT
HOLDING SP
Gross Wei
50
199
197
195
190
1«S
180
180
180
180
180
EEDS
52
203
201
199
194
189
184
184
184
184
184
AREB
54
208
206
204
199
194
189
189
189
189
189
ASED
57
212
210
208
203
198
193
193
193
193
193
ONTH
59
217
215
213
208
203
198
198
198
198
198
EGRE
ght (1,000 kg.)
61
222
220
218
213
208
203
203
203
203
203
EN DO
63
226
224
222
217
212
207
207
207
207
207
TSPE
66
229
227
222
217
212
212
212
212
212
;D.
68
233
231
226
221
216
216
216
216
216
/O
238
236
231
226
221
221
221
221
221
73
240
235
230
225
225
225
225
225
(4)HIGH ALTITUDE
LOW AND HIGH SPEED BUFFET BOUNDARIES
1.3 G-LOAD (39 degree BANK ANGLE)
A320-200
D
WEIGHT
FL390
FL370
FL350
FL330
FL310
52,000
.660 - .820
201 -255
.624 - .820
198-267
.589 - .820
195 - 280
.556 - .820
192-292
.524 -.820
189-306
54,000
.676 - .820
206 - 255
.640 - .820
203 - 267
.605 - .820
201-280
.571 - .820
198 - 292
.538 - .820
195 - 306
57,000
.692 - .820
211 -255
.655 - .820
209 - 267
.620 - .820
206 - 280
.585 - .820
203-292
.553 - .820
200 - 306
59,000
.707 - .820
216-255
.670 - .820
214 - 267
.634 - .820
211 -280
.600 - .820
209-292
.567 - .820
205 - 306
61,000
.720 - .818
221 -254
.685 - .820
219-287
.648 -.820
216-280
.61 3 -.820
213-292
.580 - .820
210-306
MACH
KIAS
•
.
3
HIGH
ALTITUDE
LOW AND
HIGH SPEED BUFFET BOUNDARIES
1.3 G-LOAD (39 degree
BANK
ANGLE)
A320-200
WEIGHT
FU390
FL.370
FL350
FL330
FU10
63,000
.735 -.811
226 - 252
.699 - .820
224 - 267
.662 - .820
221 - 280
.626 - .820
218 - 292
.593 - .820
215-306
66,000
.751 - .803
231 - 249
.711 -.820
228 - 267
.675 - .820
226-2BO
.639 - .820
223 - 292
.606 - .820
220 - 306
68,000
.776 - .783
240 - 242
.724 - .816
233-266
.688 - .820
231 - 280
.652 - .820
228 - 292
.61 8 -.820
225-306
70,000
.737 - .810
237-263
.701 - .820
235 - 280
.665 - .820
233 - 292
.630 - .820
230 - 306
73,000
.752 - .803
243 - 261
.712 - .820
239 - 280
.677 - .820
237 - 292
.641 - .820
234 - 306
MACH I
KIAS |
(5)HIGH
ALTITUDE
LOW AND HIGH SPEED BUFFET
BOUNDARIES
1.3 Q-LOAD (39 degree BANK ANGLE)
A320-200
WEIGHT
FL290
FL280
FL270
FL260
FL250
52,000
.495
-
.820
186-319
.481
-
.820
185-326
.467
-
.820
183-333
.454
-
.820
182-340
.441
-
.820
180-347
54,000
.508
-
.820
191 - 319
.494
-
.820
190-326
.480
-
.820
189 - 333
.466
-
.820
187-340
.453
-
.820
186-347
57,000
.522
-
.820
197-319
.507
-
.820
195-326
.493
-
.820
194 - 333
.479
-
.820
192-340
.465
-
.820
191 - 347
59,000
.535
-
.820
202-319
.520
-
.820
200 - 326
.505
-
.820
199 - 333
.491
-
.820
197-340
.478
-
.820
196-347
61,000
.548
-
.820
207-319
.532
-
.820
205 - 326
.51 7 -.820
204 - 333
.503
-
.820
202 - 340
.489
-
.820
201 - 347
MACH
KIAS
HIGH ALTITUDE
LOW AND
HIGH
SPEED BUFFET BOUNDARIES
1.3 G-LOAD (39 degree BANK ANGLE)
A320-200
WEIGHT
FL290
FL280
FL270
FU60
FL250~
63.000
561
-.820
212-319
,545
-
.820
210 - 326
529 -
.820
J09 • 333
.515-.820
207 • 340
.501 -.820
206-347
,573
-
.820
217 • 319
.557
-
.820
215 - 326
.541
-
.820
214 - 333
526 -
.820
212 - 340
.512
-
.820
210-347
68,000
SBS -
.820
222-319
,569
-
.820
J20-326
.553
-
.820
219 - 333
,538
-
.820
217-340
.523
-
.820
215-347
70.000
.597
-
.820
227 - 319
.581
-
.820
225 - 326
.565
-
.820
223 - 333
[.549
-
.820
222 - 340
.534-.820
220 - 347
73,OQ9I
.609
-
.820
231-319
.592
-
.820
230 - 326
.576
-
.820
228-333
[.561
-
.820
226-340
J.54S-.820
225 - 347
MACH
KIAS
(6)Maneuvering and Landing Speeds - continued
Before slowing to a maneuvering speed, determine if
1.4 g will provide sufficient margin. Moderate turbu-,
lence will produce aircraft loading of 1.3 g, therefore,
the maneuvering speeds would only be appropriate
in turbulent conditions if little or no turning
is
re-quired. Adding 15 knots to the maneuvering speeds
will increase the buffet margin to approximately 1.6 g
(52° bank).
4. Maneuvering speeds
are
equivalent to
V
ls
for each
flap setting. Therefore, maneuvering speeds can be
used as V,
8
for non-normal
landing flap
settings in
emergency
situations.
:i
)
J
3
3
3
3
I
48,000
F P S 1+F
TAKEOFF
FLAPS 3
119 VI/VR 117
124
V2
122
V1&VR
Additives
PRESS
ALHFQ
10,000
8,000
6.000
4,000
2,000
0
OAT°C
-SO
3
2
1
1
0
0
10
3
2
1
1
0
0
20
3
2
1
1
1
0
30
3
3
2
1
1
0
40
3
3
2
2
1
1
50
3
2
2
1
60
2
MANEUVERING / LANDING
0 168
1 135
1+F129
2 121
3 119
FULL'-HS
(7)FLAPS 1+F
119
124
V1 &VR
Additives
49^000
TAKEOFF
V1/VR
V2
PRESS
ALT (FT)
10,000
8,000
6,000
4.OOO
2,000
FLAPS
3
117
122
OAT°
-50
3
2
1
1
0
10
3
2
1
1
0
20
3
2
1
1
1
30
3
3
2
1
1
C
40
3
3
2
2
1
SO
3
J
2
60
MANEUVERING /LANDING ^>< J
0
17fl 4J 3
1 f V Ti • }
FLAPS 1+F TAKEOFF
50,000
1
136 *'|
119 VWR
1+F 130 2j ' 124
V2
2 122 $1
3
<4 fl<4 j\ •-} V I & V R
T V | ^n v
Additives
1 «. I /I ^
PRESS
ALT (FT)
10,000
8,000
6,000
4,000
2,000
FLAPS 3
117
122
OAT'
-50
3
2
1
1
0
10
3
2
1
1
0
20
3
2
1
1
1
30
3
3
2
1
1
C
40
3
3
2
2
1
50
3
2
2
60
MANEUVERING / LANDING
0 172
1 138
1+F132
2 123
3 122
FULL-119
(8)51,000
FLAPS 1+F
TAKEOFF
FLAPS 3
120 VI/VR 117
124
V2 122
V1 &VR
Additives
PRESS
ALT (FT)
10,000
8,000
6,000
4,000
2,000
0
OAT'C
-50
3
2
1
1
0
0
10
3
2
1
1
0
0
20
a
•i
1
1
1
0
i
3
3
2
1
1
0
•
,
3
2
2
1
1
|
3
2
2
1
•'"'.
2
MANEUVERING / LANDING
-0 173 I
1 139 I
1+F133 I
2 124 *
3 123 «
FuLL-120 I;
> 52,000
^ PLAINS 1+F TAKEOFF
^ 122 Vl/VR
>
126
v:
f
*m
A V1 & VR
t? Additives
^
PRESS
ALT (FT)
10,000
8,000
6JJOO
4,000
2,000
FLAPS 3
117
2 122
OAT'
-50
3
2
1
1
0
10
3
2
1
1
0
20
3
2
1
1
1
30
3
3
2
1
1
c
40
3
3
2
2
1
50
3
2
?
60
MAN
0
1
1
2
••«
UANKUVEBINQ / LANDING
MANEUVERING / LANDING
175
141
1+F135
126
125
FULL~121
(9)53.000
FLAPS 1+F TAKEOFF FLAPS 3
123 VI/VR 117
127 V2 122
V 1 & V R
Additives
PRESS
ALT (FT}
10JXK)
4,000
0
-50
3
g
1
0
OAT'C
10
3
2
1
0
20
3
2
1
0
30
3
3
1
0
40
3
3
2
i
2
1
fin
2
MANEUVERING/ LANDING
0 177
1 142
1+F136
2 127
3 126
FULL 123
i "AMBiix/ERINO / LANDING
*
4
1
4
*! 3
54,000
FLAPS 1+F TAKEOFF
124
128
V1 &VR
Additives
V1/VR
ALT (FT)
'i'o'iwo
6,000
, ZjpOP...
V
-•iO
3
ii
1
1
0
2
10
3
2
1
1
0
C
3
2
1
1
1
FLAPS 3
117
122
AT
3
3
2
1
1
C
3
3
?
?
1
3
?
2
MANEUVERING / LANDING
0
179
1 143
1+F 137
2
129
3
127
•M • A
(10)-55,000
126
130
V1 &VR
Additives
V
PRESS
ALTJFT)
10,000
8,000
6,000
•yroo
2,000
0
1/VR
V2
OAT
-50 10 20 30
3 3 3 3
2 2 2 3
1
1
0
0
1
)
c
1
1
i
0
2
1
1
0
FLAPS
117
122
c
40 50 60
3
2
2
1
1
3
2
2
?
3
f
>
MANEUVERING / LANDING £ •£
0
<4
Of\ if*
3 ~ — -j
56.000
• Oil -| PLAP81+F TAKEOFF FLAPS 3
1 145 * I 127 V1/VR 117
1+F138**131 V2 122
2
4
<%fi
4 3 •
.HI -k
pnESS OAT
",
c
' %^%r <g?
ALT
ff
T
) "
50 10
"*°
30 4fl 50 60
3
4 <rtrt -%
V 1 & V R la
°°°
28 ^ Additives
.
. **>
FULL 1 25 *
8,000
6,000
4,000
2,000
0
2
1
1
0
0
2
1
t
0
0
2
1
1
1
0
3
2
1
1
0
3
2
2
1
1
3
2
2
1 2
MANF
MAN
0
1
1
2
3
Fi
I UANPIIVERING/ LANDING
MANEUVERING / LANDING
182
146
1+F139
131
130
FuLL-126
(11)57,000
FLAPS 1 + F T A K E O F F FLAPS 3
129 VI/VR 118
132
124
V 1 & V R
Additives
PRESS
ALTJFTl
10.000
8,000
6,000
4,000
2,000
0
-bU
3
2
1
1
0
0
10
a
2
1
1
0
0
OAT'C
20
3
2
1
1
1
0
30
s
3
2
1
1
o
40
3
3
2
2
1
1
50
3
2
h 2
1
60
?
MANEUVERING/LANDING J*!
0 184 !
FLAPS 1+F58,000
TAKEOFF FLAPS 3
1 148 «j I 130 VI/VR 120
1+F 140 « j ? 133 va 125
2 132:
3 131 ;
FULL 127
» vi & vn
J Additives
PRESS
ALT (FT)
10,000
8,000
6,000
4,000
2,000
0
OAT°C
-50
3
2
1
1
0
0
10
3
2
1
1
0
0
20
a
2
1
1
1
0
30
3
3
2
1
1
0
40
3
3
2
2
1
1
50
3
2
2
1
60
2
MANEUVERING / LANDING
0 185
1 149
1+F141
2 134
3
132
FuLL-128
(12)59,000
FLAPS 1+F TAKEOFF
FLAPS 3
132 VWR 121
135
va
126
V1 & V R
Additives
PRESS
ALT (FT)
10,000
8,000
6,000
4,000
2,000
0
OAT'C
-50
3
2
1
i
0
0
Jjj
3
2
1
1
0
0
20
::
2
1
i
1
0
30
§
3
2
1
1
0
^0
3
3
2
2
1
1
SO) 60
3
2
2
1 2
MANEUVERING/LANDING f
0 187*
1
151
c
1+F143
I
2 135 £
3 133 f
FULL-! 29
60,
000
3J FLAPS 1+F TAKEOFF "
| 133 VI/VR
1
136
V2
*>
«i V1 4 VR
» Additives
) I
PRESS
ALT fFTl
8,000
6,000
4.000
2,000
0
OAT
-50
2
1
1
0
0
10
V
1
1
o
0
m
1
1
1
0
HO
ft
1
II
FLAPS 3
122
127
c
ft
ri
1
3
2
1 •>
MAN
0
1
1
2
3
F,
MANEUVERING / LANDING
188
152
1+F144
136
135
FULL 130
(13)61
,000
FLAPS 1+F TAKEOFF
134
V1/VR
137
V1 & VR
Additives
PRESS
ALT (FT)
10.000
8.000
6,000
4,000
2,000
v:
I
FLAPS 3
123
•
OAT°
-50
3
Z
1
1
0
10
3
2
1
1
0
20
3
2
1
1
1
30
3
3
2
1
1
128
c
40
3
3
2
2
1
50
3
2
2
60
MANEUVERING / LANDING JM
0 190 «
1 153 c
1+F145 |
2 137 «
3 136 i
FuLL-131 n
62,000
FLAPS 1+F
TAKEOFF
FLAPS 3
>
>
3
,.,«*l
If
j
136 VWR 125
138
V2 129
V1S.VR
Additives
PRESS
ALT (FT)
10.000
8,000
9,000
4.000
2.000
0
OAT'C
-50
3
2
1
1
0
0
1U
3
2
1
1
0
0
20
3
2
1
1
1
0
30
3
3
2
1
1
0
40| 50
3
3
2
2
1
1
3
2
2
1
60
2
MANEUVERING / LANDING
0 192
1
155
1+F147
2
139
3 137
FuLL-133
(14)63,000
FLAPS 1+F
TAKEOFF
FLAPS 3
137 VI/VR 126
139 V2 130
V 1 & V R
Additives
PRESS
ALT (FTJ
10,000
8,000
6,000
4,000
2,000
0
OAT°C
-50
a
2
1
1
0
0
10
3
2
1
1
0
0
20
3
2
1
1
1
0
301 40
3
3
2
1
1
0
3
3
2
2
1
1
50 | SO
3
2
2
1 2
MANEUVERING / LANDING
0 194
1
157
1+F148
2 140
3 138
FULL 134
64,000
FLAPS 1+F
TAKEOFF
FLAPS 3
-•
>
138 VI/VR 127
140 va 131
V1 & VR
Additives
PRESS
ALT (FT)
10,000
B.OOO
6,000
4,000
2,000
0
OAT'C
-60
3
2
1
1
0
0
10
3
2
1
1
0
0
20
3
2
1
1
1
0
,
|
3
2
1
1
0
w
:
3
2
2
1
1
50
3
2
2
1
|
2
MANEUVERING / LANDING
0 195
1 158
1+F149
2
141
3 139
FuLL-135
(15)65,000
FLAPS 1+F
TAKEOFF
FLAPS 3
140 VI/VR 128
141 va 132
V1 &VR
Additives
PRESS
ALT (FT)
10,000
8,000
6.000
4.000
2,000
0
OAT'C
-50
3
2
1
1
0
0
10
3
2
1
1
0
0
20
!
2
1
1
1
0
3
3
2
1
1
0
40
3
2
2
1
1
50
3
2
2
1
' '
.?
MANEUVERING / LANDING
0 196
1 159
1+F150
2 142
3 140
FULL 136
a
n
66,000
PCJIPI 't+F TAKEOFF
;ii4i
:
: 1 43
V1 & VR
Additives
^1
V1/VR
V2
PRESS
ALT (FTf
10,006
3,000
6,000
4,000
2,000
FLAPS 3
130
133
OAT°
-50
3
2
1
1
0
10
3
2
1
1
0
20
3
2
1
1
1
30
3
3
a
1
1
c
40
3
3
2
2
1
50
3
2
2
60
.,.-... «-«-M n 0_* ! A M n 1 Kin
MANEUVERING / LANDING
0 198
1 161
1+F151
2 143
3 142
FULL 137
(16)67,000
FLAPS 1+F TAKEOFF FLAPS 3
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