Maximum Take-Off Weight
Eng. Bruno Moreira
MTOW
Maximum Take Off Weight
Calculating the MTOW
Take Off limitations
Optimization : Airbus philosophy
Eng. Bruno Moreira
Maximum Take Off Weight
limitations
Structural :
Aircrafts features
Companys needs
Ground installations :
Runways characteristics
Obstacles
MTOW
Performance :
T.O. Parameters
Mother Natures influence
3
T/O optimization
Eng. Bruno Moreira
MTOW
Maximum Take Off Weight
Calculating the MTOW
Take Off limitations
Optimization : Airbus philosophy
Eng. Bruno Moreira
Calculating the MTOW
Operating speeds :
V1
1
VR
T/O chosen parameters :
V
1.13 2 1.35, 1.4, 1.5
VS
Flap setting, V1, V2. They influence performance.
0.84
Range :
according to the type of aircraft.
flaps : Conf 1+F, Conf 2, Conf 3
V1 : position around VR (ground phase)
V2 : position around VS (in-flight phase)
Remember:
V1 Vr
1.13 Vs1g V2
according to the regulation.
Eng. Bruno Moreira
Calculating the MTOW
T/O chosen parameters :
Flap setting, V1, V2. They influence performance.
Range :
flaps : Conf 1+F, Conf 2, Conf 3
V1 : position around VR (ground phase)
V2 : position around VS (in-flight phase)
Principle :
At given Conf (and all sustained parameters), Take Off Weight
limitations are set as a function of V1/VR and V2/VS.
Eng. Bruno Moreira
Calculating the MTOW
T/O chosen parameters :
Flap setting, V1, V2. They influence performance.
Range :
flaps : Conf 1+F, Conf 2, Conf 3
V1 : position around VR (ground phase)
V2 : position around VS (in-flight phase)
Principle :
At given Conf (and all sustained parameters), Take Off Weight
limitations are set as a function of V1/VR and V2/VS.
MTOW is calculated for a fixed V2 and a full range of V1 ,
( or fixed V1 and full range of V2 ).
Eng. Bruno Moreira
Calculating the MTOW
T/O chosen parameters :
Airport :
Flap setting, V1,
Sea level
Temperature
Range : = 20 C
no wind
Aircraft :
:
Obstacle :
V2.Runway
They influence
performance.
TORA = 2300 m
TODA = 2300 m
ASDA = 2400 m
1+F,
Conf 2, Conf
no slope
Distance = 6450 m
Height = 260 ft
flaps : Conf
3
V1 : position around VR (ground phase)
Conf 1+F, V2/VS = 1.21,
0.84 <
VA320-211,
phase)
2 : position around VS (in-flight
V1
<1
VR
Principle :
At given Conf (and all sustained parameters), Take Off Weight
limitations are set as a function of V1/VR and V2/VS.
MTOW is calculated for a fixed V2 and a full range of V1 ,
( or fixed V1 and full range of V2 ).
Eng. Bruno Moreira
Calculating the MTOW
Graphic MTOW calculation
T/O chosen parameters :
Airport :
Flap setting, V1,
Sea level
Temperature
Range : = 20 C
no wind
Aircraft :
:
Obstacle :
V2.Runway
They influence
performance.
TORA = 2300 m
TODA = 2300 m
ASDA = 2400 m
1+F,
Conf 2, Conf
no slope
Distance = 6450 m
Height = 260 ft
flaps : Conf
3
V1 : position around VR (ground phase)
0.84 <
Conf 1+F, V2/VS = 1.21,
VA320-211,
phase)
2 : position around VS (in-flight
V1
<1
VR
Principle :
At given Conf (and all sustained parameters), Take Off Weight
limitations are set as a function of V1/VR and V2/VS.
MTOW is calculated for a fixed V2 and a full range of V1 ,
( or fixed V1 and full range of V2 ).
Eng. Bruno Moreira
Calculating the MTOW
Graphic MTOW calculation
some limitations
10
Eng. Bruno Moreira
Calculating the MTOW
Graphic MTOW calculation
some limitations
11
Eng. Bruno Moreira
Calculating the MTOW
Graphic MTOW calculation
some limitations
Optimum V1 / VR
12
Eng. Bruno Moreira
Calculating the MTOW
Graphic MTOW calculation
some limitations
MTOW
Optimum V1 / VR
13
Eng. Bruno Moreira
MTOW
Maximum Take Off Weight
Calculating the MTOW
Take Off limitations
Optimization : Airbus philosophy
14
Eng. Bruno Moreira
Take off limitations
Limitation code
Reminder :
Runway,
with One Engine Inoperative (3) :
Runway,
with All Engines Operating (7) :
TOD AEO
TOD OEI
TOR AEO
TOR OEI
These limits are set to their maximum value
ASD
( e.g. TOD = TODA, FTO at 400 ft, ... )
to increase the TOW.
In flight :
Rolling :
15
1st segment
2nd segment
Final Take Off
(acceleration segment)
Obstacles
(2)
(2)
Tire speed (5)
Brake energy (6)
(8)
(4)
Eng. Bruno Moreira
Take off limitations
Runway limitations
Take Off Distance
16
remember :
Increasing
V 1 / VR
TODOEI :
with the same weight.
Eng. Bruno Moreira
Take off limitations
Runway limitations
MTOW
Take Off Distance
80 t
remember :
Increasing
V 1 / VR
TODOEI :
with the same weight.
TOW :
with the same TODOEI .
TOD OEI
60 t
17
Operational
point of view :
V1 / VR
Eng. Bruno Moreira
Take off limitations
Runway limitations
MTOW
Take Off Distance
All Engines
Operating...
Increasing
80 t
TOD AEO
V 1 / VR
TODAEO :
=
with the same weight.
TOW :
=
with the same TODAEO.
TOD OEI
60 t
V1 / VR
18
Eng. Bruno Moreira
Take off limitations
Runway limitations
Take Off Run
Its variations are similar
to those of the TOD.
MTOW
TOR AEO 80 t
TOD AEO
TOR OEI
TOD OEI
60 t
V1 / VR
19
Eng. Bruno Moreira
Take off limitations
Runway limitations
MTOW
Take Off Run
TOR AEO 80 t
Its variations are similar
to those of the TOD.
TOD AEO
ASD
Accelerate Stop Distance
Increasing
V 1 / VR
ASD :
with the same weight.
TOR OEI
TOD OEI
60 t
TOW :
with the same ASD.
20
V1 / VR
Eng. Bruno Moreira
Take off limitations
Runway limitations
MTOW
Take Off Run
TOR AEO 80 t
Its variations are similar
to those of the TOD.
TOD AEO
ASD
Accelerate Stop Distance
Increasing
V 1 / VR
ASD :
with the same weight.
MTOW
TOR OEI
TOD OEI
60 t
TOW :
with the same ASD.
21
optimum V1 V/ 1V/ RVR
Eng. Bruno Moreira
Take off limitations
Runway limitations
Effect of a stopway ?
MTOW
TOR AEO 80 t
TOD AEO
ASD
TOR OEI
TOD OEI
60 t
V1 / VR
22
Eng. Bruno Moreira
Take off limitations
Runway limitations
Effect of a stopway :
- It increases the ASDA
MTOW
TOR AEO 80 t
TOD AEO
ASD
TOR OEI
TOD OEI
60 t
V1 / VR
23
Eng. Bruno Moreira
Take off limitations
Runway limitations
Effect of a stopway :
- It increases the ASDA
MTOW
TOR AEO 80 t
TOD AEO
ASD
- The MTOW is higher :
MTOW with stopway
MTOW without stopway
TOR OEI
TOD OEI
60 t
V1 / VR
24
Eng. Bruno Moreira
Take off limitations
Runway limitations
Effect of a clearway ?
MTOW
TOR AEO 80 t
TOD AEO
ASD
TOR OEI
TOD OEI
60 t
V1 / VR
25
Eng. Bruno Moreira
Take off limitations
Runway limitations
Effect of a clearway :
- It increases TODA
MTOW
TOR AEO 80 t
TOD AEO
ASD
TOR OEI
TOD OEI
60 t
V1 / VR
26
Eng. Bruno Moreira
Take off limitations
Runway limitations
Effect of a clearway :
- It increases TODA
MTOW
TOR AEO 80 t
TOD AEO
ASD
- The MTOW is higher :
MTOW with clearway
MTOW without clearway
TOR OEI
TOD OEI
60 t
V1 / VR
27
Eng. Bruno Moreira
Take off limitations
Runway limitations
Effect of a clearway :
- It increases TODA
MTOW
TOR AEO 80 t
TOD AEO
ASD
- The MTOW is higher :
MTOW with clearway
TOR OEI
TOD OEI
Note : When TORA limitation is reached,
lengthening the clearway isnt useful anymore.
28
60 t
V1 / VR
Eng. Bruno Moreira
Take off limitations
Reminder :
Runway,
with One Engine Inoperative (3) :
29
Runway,
with All Engines Operating (7) :
TOD AEO
TOR AEO
Rolling :
TOD OEI
TOR OEI
ASD
In flight :
1st segment
2nd segment
Final Take Off
(acceleration segment)
Obstacles
(2)
(2)
Tire speed (5)
Brake energy (6)
(8)
(4)
Eng. Bruno Moreira
Take off limitations
In flight limitations
MTOW
1st, 2nd segment, and FTO :
Variations with V1 / VR :
At fixed V2 ( VR ), its
independent from V1 / VR .
100 t
FTO
1st seg.
2nd seg.
Obstacles
70 t
V1 / VR
30
Eng. Bruno Moreira
Take off limitations
In flight limitations
MTOW
1st, 2nd segment, and FTO :
Variations with V1 / VR :
100 t
FTO
At fixed V2 ( VR ), its
independent from V1 / VR .
Variations with V2 / VS :
1st seg.
2nd seg.
At fixed V1 , limitations
depend on V2.
Obstacles
70 t
V2 / VS
31
Eng. Bruno Moreira
Take off limitations
Example of the 2nd segment limitation :
MTOW
In flight limitations
Increasing V2 gives :
gradient
at fixed
st, 2nd climb
a1better
segment,
and FTO
: TOW,
a better TOW at fixed gradient.
Variations with V1 / VR :
100 t
MTOW
V2 / VS
FTO
At fixed V2 ( VR ), its
independent from V1 / VR .
Variations with V2 / VS :
1st seg.
2nd seg.
At fixed V1 , limitations
depend on V2.
Obstacles
70 t
V2 / VS
32
Eng. Bruno Moreira
Take off limitations
Example of the 2nd segment limitation :
MTOW
In flight limitations
Increasing V2 gives :
gradient
at fixed
st, 2nd climb
a1better
segment,
and FTO
: TOW,
a better TOW at fixed gradient.
Variations with V1 / VR :
100 t
MTOW
V2 / VS
FTO
... but when thrust limit is reached,
), its
Atbe
fixed
V2 ( VRby
increased
reducing gradient :
V2 can just
independent
from V1 / VVR . becomes more limiting.
From a certain
point, increasing
2
Variations with V2 / VS :
1st seg.
2nd seg.
At fixed V1 , limitations
depend on V2.
Obstacles
70 t
V2 / VS
33
Eng. Bruno Moreira
Take off limitations
In flight limitations
MTOW
Obstacles :
Variation with V1 / VR :
At fixed V2 ( VR ),
increasing V1 shortens TOD
and improves performance.
100 t
FTO
1st seg.
2nd seg.
Obstacles
70 t
V1 / VR
34
Eng. Bruno Moreira
Take off limitations
In flight limitations
MTOW
Obstacles :
Variations with V2 / VS :
100 t
FTO
Performance increases
as climb gradient
becomes higher.
1st seg.
2nd seg.
Obstacles
70 t
V2 / VS
35
Eng. Bruno Moreira
Take off limitations
In flight limitations
MTOW
Obstacles :
Variations with V2 / VS :
100 t
FTO
Performance increases
as climb gradient
becomes higher.
1st seg.
... but TOD increases too :
it shortens the distance to
the obstacle.
From a certain point,
increasing V2 becomes
more limiting.
36
2nd seg.
Obstacles
70 t
V2 / VS
Eng. Bruno Moreira
Take off limitations
Reminder :
Runway,
with One Engine Inoperative (3) :
37
Runway,
with All Engines Operating (7) :
TOD AEO
TOR AEO
Rolling :
TOD OEI
TOR OEI
ASD
In flight :
1st segment
2nd segment
Final Take Off
(acceleration segment)
Obstacles
(2)
(2)
Tire speed (5)
Brake energy (6)
(8)
(4)
Eng. Bruno Moreira
Take off limitations
Rolling limitations
MTOW
Tire speed
VLOF < VTYRE
A320 : VTYRE = 195.5 kts
110 t
Brake
Energy
Tire
Speed
Brake Energy : VMBE
V1 < VMBE
90 t
V1 / VR
38
Eng. Bruno Moreira
Take off limitations
Flaps configuration effect :
MTOW
From Conf 1+F to Conf 3
TOR AEO 80 t
TOD AEO
More flaps improves
runway performance.
ASD
TOR OEI
TOD OEI
60 t
V1 / VR
39
Eng. Bruno Moreira
Take off limitations
Flaps configuration effect :
MTOW
From Conf 1+F to Conf 3
100 t
FTO
More flaps improves
runway performance.
1st seg.
More flaps decreases
in flight perfo.
2nd seg.
Obstacles
70 t
V2 / VS
40
Eng. Bruno Moreira
MTOW
Maximum Take Off Weight
Calculating the MTOW
Take Off limitations
Optimization : Airbus philosophy
41
Eng. Bruno Moreira
Optimization : Airbus philosophy
MTOW calculation :
Airport :
Sea level
Temperature = 20 C
no wind
Aircraft :
42
A320-211,
Runway :
TORA = 2300 m
TODA = 2300 m
ASDA = 2400 m
no slope
Conf 1+F,
Obstacle :
Distance = 6450 m
Height = 260 ft
V2/VS = 1.21,
Inputs :
Sustained parameters
+ chosen conf
+ chosen V2 / Vs ratio
0.84 < V1 < 1
VR
Eng. Bruno Moreira
Optimization : Airbus philosophy
MTOW calculation :
Airport :
Sea level
Temperature = 20 C
no wind
Aircraft :
A320-211,
Runway :
TORA = 2300 m
TODA = 2300 m
ASDA = 2400 m
no slope
Conf 1+F,
Obstacle :
Distance = 6450 m
Height = 260 ft
V2/VS = 1.21,
Inputs :
Sustained parameters
+ chosen conf
+ chosen V2 / Vs ratio
0.84 < V1 < 1
VR
Outputs :
MTOW
Optimum V1 / VR
43
Eng. Bruno Moreira
Optimization : Airbus philosophy
MTOW calculation :
Airport :
Sea level
Temperature = 20 C
no wind
Aircraft :
A320-211,
Runway :
TORA = 2300 m
TODA = 2300 m
ASDA = 2400 m
no slope
Conf 1+F,
Obstacle :
Distance = 6450 m
Height = 260 ft
V2/VS = 1.21,
Inputs :
Sustained parameters
+ chosen conf
+ chosen V2 / Vs ratio
0.84 < V1 < 1
VR
Note : Too many MTOWS !
There are as many MTOWs
as V2 / Vs values.
Changing configuration
increases this number as well.
44
Outputs :
MTOW
Optimum V1 / VR
Eng. Bruno Moreira
Optimization : Airbus philosophy
Optimization consists in calculating the highest MTOW
Inputs : of all.
Sustained parameters
MTOW calculation :
+ chosen conf
+ chosen V2 / Vs ratio
Runway :
Obstacle :
Airport :
Sea level
Temperature = 20 C
no wind
Aircraft :
A320-211,
TORA = 2300 m
TODA = 2300 m
ASDA = 2400 m
no slope
Conf 1+F,
Distance = 6450 m
Height = 260 ft
V2/VS = 1.21,
0.84 < V1 < 1
VR
Note : Too many MTOWS !
There are as many MTOWs
as V2 / Vs values.
Changing configuration
increases this number as well.
45
Outputs :
MTOW
Optimum V1 / VR
Eng. Bruno Moreira
Optimization : Airbus philosophy
Principle :
Airport :
Sea level
Temperature = 20 C
no wind
Aircraft :
46
A320-211,
Runway :
TORA = 2300 m
TODA = 2300 m
ASDA = 2400 m
no slope
Conf 1+F,
2
3
Obstacle :
Distance = 6450 m
Height = 260 ft
1.13 < V2 < 1.35,
VS
Inputs :
Sustained parameters
+ each conf
+ every V2 / Vs ratio
0.84 < V1 < 1
VR
Eng. Bruno Moreira
Optimization : Airbus philosophy
Principle :
Airport :
Sea level
Temperature = 20 C
no wind
Aircraft :
A320-211,
Runway :
TORA = 2300 m
TODA = 2300 m
ASDA = 2400 m
no slope
Conf 1+F,
2
3
Obstacle :
Distance = 6450 m
Height = 260 ft
1.13 < V2 < 1.35,
VS
Inputs :
Sustained parameters
+ each conf
+ every V2 / Vs ratio
0.84 < V1 < 1
VR
Outputs :
many MTOWs
and associated V1 / VR
47
Eng. Bruno Moreira
Optimization : Airbus philosophy
Principle :
Airport :
Sea level
Temperature = 20 C
no wind
Aircraft :
MTOW
of the day
A320-211,
Runway :
TORA = 2300 m
TODA = 2300 m
ASDA = 2400 m
no slope
Conf 1+F,
2
3
Obstacle :
Distance = 6450 m
Height = 260 ft
1.13 < V2 < 1.35,
VS
Inputs :
Sustained parameters
+ each conf
+ every V2 / Vs ratio
0.84 < V1 < 1
VR
Winner :
The highest MTOW,
with the corresponding
V1 / VR ,
V2 / Vs ,
and configuration.
48
Outputs :
many MTOWs
and associated V1 / VR
Eng. Bruno Moreira
Optimization : Airbus philosophy
RTOW chart : ( Runway Take Off Weight )
Optimized MTOWs table, with associated V1 / VR + V2 / Vs ,
depending on :
49
Flaps Configuration
Temperature
Wind
... for a given runway.
Eng. Bruno Moreira
Optimization : Airbus philosophy
RTOW chart : ( Runway Take Off Weight )
Optimized MTOWs table, with associated V1 / VR + V2 / Vs ,
depending on :
Flaps Configuration
Temperature
Wind
meteo
obstacles
runway
50
... for a given runway.
------------------------------------------------------------------------*******
:HECA CAIRO
RWY 23R
JARA 11-10-96 ELEV.
196.FT*CONF.*
:FOR TRAINING ONLY
MC69
TORA
3300.M * 1+F*
:
ASDA
3300.M *CG25%*
:A320-2XX/AB/ENG.TYPE DRY RUNWAY
AIR COND. ON
TODA
3300.M *******
:-------TREF= 29/TMAX= 49 GRAD1= 50/GRAD2= 200
*****
SLOPE -.10 % : TGA :
:WEIGHT:----------------------------------------------------------------: 2 :
:1000KG:
-10
:
-5
:
0
:
10
:
20
: 3 :
:-----------------------------------------------------------------------------:
:
: 19
4-4 : 32
4-4 : 35
4-4 : 37
4-4 : 38
2-4 :33
:
: 73.5 : .0
: .2
: .4
: .1
: .1
:
:
:
:147-150-150 :151-152-152 :159-159-159 :159-159-159 :161-161-161 :
34:
:------:------------:------------:------------:------------:------------:-----:
:
: 29
4-4 : 36
4-4 : 38
4-4 : 40
2-4 : 41
2-4 :35
:
: 72.0 : .8
: .2
: .4
: .0
: .1
:
:
:
:145-149-149 :153-153-153 :157-157-157 :158-158-158 :160-160-160 :
36:
:------:------------:------------:------------:------------:------------:-----:
:
: 37
4-4 : 40
4-4 : 42
4-4 : 43
2-4 : 44
2-4 :39
:
: 70.0 : .2
: .4
: .4
: .5
: .5
:
:
:
:148-148-148 :155-155-155 :156-156-156 :157-157-157 :159-159-159 :
39:
:------:------------:------------:------------:------------:------------:-----:
:
: 42
4-4 : 44
4-4 : 46
4-4 : 47
4-4 : 48
2-2 :42
:
: 68.0 : .4
: .4
: .3
: .4
: .2
:
:
:
:150-150-150 :153-153-153 :155-155-155 :156-156-156 :159-159-159 :
43:
:------:------------:------------:------------:------------:------------:-----:
:
: 46
4-4 : 48
4-4 : 50
4-4 : 51
2-4 : 52
2-4 :45
:
: 66.0 : .5
: .4
: .3
: .4
: .1
:
:
:
:151-151-151 :151-151-151 :154-154-154 :155-155-155 :157-157-157 :
46:
:------:------------:------------:------------:------------:------------:-----:
:
: 51
4-4 : 53
4-4 : 54
4-4 : 55
2-4 : 55
2-2 :49
:
: 64.0 : .1
: .0
: .4
: .4
: .5
:
:
:
:148-148-148 :150-150-150 :152-152-152 :153-153-153 :154-155-155 :
49:
:------:------------:------------:------------:------------:------------:-----:
:
: 55
4-4 : 57
4-4 : 59
4-4 : 59
2-4 : 59
2-2 :49
:
: 62.0 : .2
: .2
: .0
: .4
: .4
:
:
:
:147-147-147 :149-149-149 :149-149-149 :153-153-153 :152-153-153 :
49:
:------:------------:------------:------------:------------:------------:-----:
:
: 59
4-4 : 60
4-4 : 60
2-4 : 60
2-2 : 60
2-2 :49
:
: 60.0 : .4
: .8
: 1.6
: 1.9
: 1.9
:
:
:
:145-145-145 :148-148-148 :149-149-149 :152-152-152 :151-152-152 :
49:
:------:------------:------------:------------:------------:------------:-----:
:
: 60
4-4 : 60
2
: 60
2
: 60
2
: 60
2
:49
:
: 58.0 : 2.0
: .0
: .0
: .0
: .0
:
:
:
:145-145-145 :128-134-134 :125-134-134 :124-134-134 :124-134-134 :
49:
:------:------------:------------:------------:------------:------------:-----:
:
: 60
: 60
: 60
: 60
: 60
:49
:
: 56.0 : .0
: .0
: .0
: .0
: .0
:
:
:
:122-131-131 :122-131-131 :122-131-131 :122-131-131 :122-131-131 :
49:
:------:------------:------------:------------:------------:------------:-----:
:
: 60
: 60
: 60
: 60
: 60
:49
:
: 54.0 : .0
: .0
: .0
: .0
: .0
:
:
:
:121-128-128 :121-128-128 :121-128-128 :121-128-128 :121-128-128 :
49:
:------:------------:------------:------------:------------:------------:-----:
:
: 60
: 60
: 60
: 60
: 60
:49
:
: 52.0 : .0
: .0
: .0
: .0
: .0
:
:
:
:120-126-126 :120-126-126 :120-126-126 :120-126-126 :120-126-126 :
49:
:------:------------:------------:------------:------------:------------:-----:
:
: 60
: 60
: 60
: 60
: 60
:49
:
: 50.0 : .0
: .0
: .0
: .0
: .0
:
:
:
:118-123-123 :118-123-123 :118-123-123 :118-123-123 :118-123-123 :
49:
:------:------------:------------:------------:------------:------------:-----:
:
: 60
: 60
: 60
: 60
: 60
:49
:
: 48.0 : .0
: .0
: .0
: .0
: .0
:
:
:
:117-120-121 :117-120-121 :117-120-121 :117-120-121 :117-120-121 :
49:
:------:------------:------------:------------:------------:------------:-----:
/MINI. ACCELERATION HEIGHT :
800.(FT) QNH ALT. :
996.(FT)
/MAXI. ACCELERATION HEIGHT : 2047.(FT) QNH ALT. : 2243.(FT)
Eng. Bruno Moreira
Optimization : Airbus philosophy
RTOW chart : ( Runway Take Off Weight )
Optimized MTOWs table, with associated V1 / VR + V2 / Vs ,
depending on :
51
... for a given runway.
RTOW chart are computed through the low speeds performance
programs :
Flaps Configuration
Temperature
Wind
TLC
OCTOPUS
for the A300-600, A310, A320
for A319, A321, A330, A340.
Correction can be made afterwards by the charts users (QNH, ...).
Eng. Bruno Moreira
TAP: RTOW
Regulatory
Take
Off
Weight
52
J16415 VH4.1
MADRID (BARAJAS) 36L
A320-214 CFM56-5-B4 MC69
CG25%
T.O. SHIFT
0M TORA
4350M CONF 2
OBST: 28'/ 740M 134'/ 2800M
ELEV 2000' ASDA
4350M
A/C OFF
TREF 40~C TODA
4610M
DRY RWY
==== ANTI-ICING OFF QNH = 1013.25 HPA
TMAX 51~C SLOPE 0.12%
=====
OAT=======================================================================OAT
~C TAILWIND -10 KT TAILWIND -5 KT
0 KT
HEADWIND 10 KT ~C
==========================================================================
479.3 4-4 39/57/6080.7 4-4 45/59/6182.3 2-4 50/61/6383.2 2-4 55/65/67 4
3277.4 4-4 34/53/5578.9 4-4 39/54/5680.3 4-4 45/58/6081.4 2-4 49/59/61 32
3677.2 4-4 33/52/5478.7 4-4 38/54/5680.1 4-4 44/57/5981.2 2-4 48/59/61 36
--------------------------------------------------------------------------
4077.0 4-4 32/51/5378.5 4-4 38/53/5579.3 2-8 38/52/5479.3 2-8 33/52/54 40
--------------------------------------------------------------------------
4275.7 4-4 33/52/5377.2 4-4 39/53/5577.8 2-8 36/51/5277.8 2-8 31/51/52 42
5070.8 4-4 38/50/5172.2 4-4 44/51/5373.6 2-4 49/56/5774.4 2-4 53/59/61 50
#5269.6 4-4 40/50/5171.0 4-4 45/51/5372.3 2-4 50/56/5773.1 2-4 55/60/61#52
--------------------------------------------------------------------------
#6263.9 4-4 47/47/4865.2 4-4 53/53/5365.5 2-2 50/53/5465.5 2-2 47/53/54#62
#6462.8 4-4 49/49/4963.8 4-4 53/53/5363.9 2-2 47/52/5263.9 2-2 44/52/52#64
--------------------------------------------------------------------------
#6459.8
46/46/4660.8
50/50/5060.9
44/49/4960.9
41/49/49#64
#6456.8
43/43/4357.8
47/47/4757.9
41/46/4657.9
38/46/46#64
#64****
***/**/**54.8
44/44/4454.9
38/43/4354.9
35/43/43#64
#64****
***/**/******
***/**/******
***/**/******
***/**/**#64
===============================================================================
WET RWY
INFLUENCE OF RUNWAY CONDITION
-------------------------------------------------------------------------------
WET
*** SEE WET TABLE OVERLEAF ***
===============================================================================
D QNH HPA
INFLUENCE OF DELTA PRESSURE
-------------------------------------------------------------------------------
-20-0.9 -1/-1/-1
-1.0 -1/-1/-1
-1.0 -1/-1/-1
-1.0 -1/-1/-1
-20
(+36)
(+36)
(+36)
(+36)
-1.5
0/-1/-1 -3-1.6 -2/-1/-1 -3-1.9 -3/-1/-1 -4-1.9 -3/-1/-1 -4
===============================================================================
LABEL FOR INFLUENCE:
MTOW (1000 KG) CODES
V1MIN/VR/V2 (KT)
DW(1000KG) DV1/DVR/DV2(KT)
---------------------------------------------
(TVMC DEG C)
1=1ST SEG. 2=2ND SEG. 3=RWY LENGTH 4=OBSTACLE
DW(1000KG) DV1/DVR/DV2(KT) DTFLEX5=T.SP 6=BRK ENERGY 7=MAX WEIGHT 8=FINAL T.O.
-------------------------------------------------------------------------------
MINIMUM SPEEDS: V1/VR/V2=110/113/116KT CORRECTIONS TO V1/VR/V2= 1.0KT/1000KG
=================================================================================
EOSID: LT TO "BRA" VORDME THEN PRCD VIA R-145 TO "PDT" VORDME AND
HOLD (073 INBD, RT, 5000').
ACC. ALT.- MIN/MAX = 3500'/4142'QNH
01 JUN 06
Eng. Bruno Moreira
Anti-Icing
Aircraft Engine -DataBase
CG position
Airpot Elevation
TakeOff Position Shift
J16415 VH4.1
MADRID (BARAJAS) 36L
A320-214 CFM56-5-B4 MC69
CG25%
T.O. SHIFT
0M TORA
4350M CONF 2
OBST: 28'/ 740M 134'/ 2800M
ELEV 2000' ASDA
4350M
A/C OFF
TREF 40~C TODA
4610M
DRY RWY
==== ANTI-ICING OFF QNH = 1013.25 HPA
TMAX 51~C SLOPE 0.12%
=====
OAT=======================================================================OAT
~C TAILWIND -10 KT TAILWIND -5 KT
0 KT
HEADWIND 10 KT ~C
==========================================================================
479.3 4-4 39/57/6080.7 4-4 45/59/6182.3 2-4 50/61/6383.2 2-4 55/65/67 4
3277.4 4-4 34/53/5578.9 4-4 39/54/5680.3 4-4 45/58/6081.4 2-4 49/59/61 32
3677.2 4-4 33/52/5478.7 4-4 38/54/5680.1 4-4 44/57/5981.2 2-4 48/59/61 36
--------------------------------------------------------------------------
4077.0 4-4 32/51/5378.5 4-4 38/53/5579.3 2-8 38/52/5479.3 2-8 33/52/54 40
--------------------------------------------------------------------------
4275.7 4-4 33/52/5377.2 4-4 39/53/5577.8 2-8 36/51/5277.8 2-8 31/51/52 42
5070.8 4-4 38/50/5172.2 4-4 44/51/5373.6 2-4 49/56/5774.4 2-4 53/59/61 50
#5269.6 4-4 40/50/5171.0 4-4 45/51/5372.3 2-4 50/56/5773.1 2-4 55/60/61#52
--------------------------------------------------------------------------
#6263.9 4-4 47/47/4865.2 4-4 53/53/5365.5 2-2 50/53/5465.5 2-2 47/53/54#62
#6462.8 4-4 49/49/4963.8 4-4 53/53/5363.9 2-2 47/52/5263.9 2-2 44/52/52#64
--------------------------------------------------------------------------
#6459.8
46/46/4660.8
50/50/5060.9
44/49/4960.9
41/49/49#64
#6456.8
43/43/4357.8
47/47/4757.9
41/46/4657.9
38/46/46#64
#64****
***/**/**54.8
44/44/4454.9
38/43/4354.9
35/43/43#64
#64****
***/**/******
***/**/******
***/**/******
***/**/**#64
===============================================================================
WET RWY
INFLUENCE OF RUNWAY CONDITION
-------------------------------------------------------------------------------
WET
*** SEE WET TABLE OVERLEAF ***
===============================================================================
D QNH HPA
INFLUENCE OF DELTA PRESSURE
-------------------------------------------------------------------------------
-20-0.9 -1/-1/-1
-1.0 -1/-1/-1
-1.0 -1/-1/-1
-1.0 -1/-1/-1
-20
(+36)
(+36)
(+36)
(+36)
-1.5
0/-1/-1 -3-1.6 -2/-1/-1 -3-1.9 -3/-1/-1 -4-1.9 -3/-1/-1 -4
===============================================================================
LABEL FOR INFLUENCE:
MTOW (1000 KG) CODES
V1MIN/VR/V2 (KT)
DW(1000KG) DV1/DVR/DV2(KT)
---------------------------------------------
(TVMC DEG C)
1=1ST SEG. 2=2ND SEG. 3=RWY LENGTH 4=OBSTACLE
DW(1000KG) DV1/DVR/DV2(KT) DTFLEX5=T.SP 6=BRK ENERGY 7=MAX WEIGHT 8=FINAL T.O.
-------------------------------------------------------------------------------
MINIMUM SPEEDS: V1/VR/V2=110/113/116KT CORRECTIONS TO V1/VR/V2= 1.0KT/1000KG
=================================================================================
EOSID: LT TO "BRA" VORDME THEN PRCD VIA R-145 TO "PDT" VORDME AND
HOLD (073 INBD, RT, 5000').
ACC. ALT.- MIN/MAX = 3500'/4142'QNH
01 JUN 06
TAP: RTOW
QNH Standard
MTOW
Limitation Code
78.5 4-4 38/53/55
V1-100/V2-100/V3-100
EOSID Procedure
Acceleration Altitude
53
Airport Runway Ident
T. O. Conf Flaps / Slats
A/C
Runway Condition
Declared Dsitances
Runway Slope
TREF & TMAX
OAT
HEAD/TAIL WIND
QNH CORRECTION
Eng. Bruno Moreira
