Different movings of the ailerons - the outer one only moves up!

My sailplane Nimbus 8m has 3 ailerons at each wing. They all have different movings (the outer one only goes up!).
It is not possible to change these parameters using the model editor, you have to change the tmd-file!
Notice:
If you try to do the changes via the model editor nevertheless, it will cause the loss of the changes you did in the tmd-file

Append tmdservo01 ServoLeftaileron
Append tmdservo01 ServoRightaileron
Append tmdservo01 ServoLeftaileron1
Append tmdservo01 ServoRightaileron1
Append tmdservo01 ServoLeftaileron2
Append tmdservo01 ServoRightaileron2

cd ServoLeftaileron/
SignalIn = ~Aircraft/Receiver/Out(10)
ValueNumber = 3
ValueIn(0) = -1
ValueOut(0) = -0.2
ValueIn(1) = 0
ValueOut(1) = 0
ValueIn(2) = 1
ValueOut(2) = 0.1
PositionFirst = -1
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
cd ../

cd ServoRightaileron/
SignalIn = ~Aircraft/Receiver/Out(11)
ValueNumber = 3
ValueIn(0) = -1
ValueOut(0) = 0.1
ValueIn(1) = 0
ValueOut(1) = 0
ValueIn(2) = 1
ValueOut(2) = -0.2
PositionFirst = 1
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Mass =
RangeMassMax = 0
RangeMassMin = 0
Inertia = {  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
cd ../

cd ServoLeftaileron1/
SignalIn = ~Aircraft/Receiver/Out(10)
ValueNumber = 3
ValueIn(0) = -1
ValueOut(0) = -0.4
ValueIn(1) = 0
ValueOut(1) = 0
ValueIn(2) = 1
ValueOut(2) = 0.2
PositionFirst = -1
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
cd ../

cd ServoRightaileron1/
SignalIn = ~Aircraft/Receiver/Out(11)
ValueNumber = 3
ValueIn(0) = -1
ValueOut(0) = 0.2
ValueIn(1) = 0
ValueOut(1) = 0
ValueIn(2) = 1
ValueOut(2) = -0.4
PositionFirst = 1
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
cd ../

cd ServoLeftaileron2/
SignalIn = ~Aircraft/Receiver/Out(10)
ValueNumber = 3
ValueIn(0) = -1
ValueOut(0) = -0.6
ValueIn(1) = 0
ValueOut(1) = 0
ValueIn(2) = 1
ValueOut(2) = 0
PositionFirst = -1
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
cd ../

cd ServoRightaileron2/
SignalIn = ~Aircraft/Receiver/Out(11)
ValueNumber = 3
ValueIn(0) = -1
ValueOut(0) = 0
ValueIn(1) = 0
ValueOut(1) = 0
ValueIn(2) = 1
ValueOut(2) = -0.6
PositionFirst = 1
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,  0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
cd ../