no such file or directory: fort.80

Dear all,
I try to run my first tutorial with Salome+Code Aster.
Unfortunatly the simulation does not start and I get following error:

<A> COPYFILE: No such file or directory fort.80

Where can lie the error?

Here the .comm file

U4.11.02
DEBUT();

#U4.21.01
mesh=LIRE_MAILLAGE(UNITE=20,
FORMAT='MED',
INFO=1,);

#U4.22.01
mesh=DEFI_GROUP(reuse =mesh,
MAILLAGE=mesh,
CREA_GROUP_MA=_F(NOM='TOUT',
TOUT='OUI',),
CREA_GROUP_NO=_F(TOUT_GROUP_MA='OUI',),);

IMPR_RESU(FORMAT='MED',
UNITE=71,
RESU=_F(MAILLAGE=mesh,),);

#U4.41.01
model=AFFE_MODELE(MAILLAGE=mesh,
AFFE=(_F(GROUP_MA=('topbeam','mast',),
PHENOMENE='MECANIQUE',
MODELISATION='POU_D_T',),
_F(GROUP_MA='massN',
PHENOMENE='MECANIQUE',
MODELISATION='DIS_T',),),);

#F MATERIALI ##########################################################################################

#U4.43.01
steel=DEFI_MATERIAU(ELAS=_F(E=210000.0,
NU=0.3,
RHO=8e-09,),);

#U4.43.03
material=AFFE_MATERIAU(MAILLAGE=mesh,
AFFE=_F(GROUP_MA=('topbeam','mast',),
MATER=steel,),);

#U4.42.01
elemcar=AFFE_CARA_ELEM (
MODELE=model ,
POUTRE = (
#the vertical members are rectangular section
#(40x20 mm) with a thickness of 1.5 mm
_F (
GROUP_MA = ( 'mast' , ) ,
SECTION='RECTANGLE' ,
CARA = ( 'HY' , 'HZ' , 'EPY' , 'EPZ', ) ,
VALE = ( 40 , 20 , 1.5 , 1.5, ) ,
),
#same with the horizontal bar
_F (
GROUP_MA = ( 'topbeam' , ) , SECTION='RECTANGLE' ,
CARA = ( 'HY' , 'HZ' , 'EPY' , 'EPZ', ) , VALE = ( 40 , 20 , 1.5 , 1.5, ) ,
),
),
DISCRET = (
_F ( GROUP_MA='massN' , CARA='M_T_D_N' , VALE = ( .01 ) , ) ,
#following block set stiffness of point element 'massN'
#to null stiffness
#although this is not necessary,
#commenting this block would raise a warning,
#unimportant in this case
_F (
GROUP_MA = ( 'massN' , ) ,
CARA='K_T_D_N' ,
VALE = ( 0 , 0 , 0 , ) ,
REPERE='GLOBAL' ,
),
),
);


#F BOUNDARY CONDITIONS ################################################################################

#F incastro ai nodi di terra
#U4.44.01
ground=AFFE_CHAR_MECA(MODELE=model,
DDL_IMPO=_F(GROUP_NO=('groundS','groundN',),
DX=0.0,
DY=0.0,
DZ=0.0,
DRX=0.0,
DRY=0.0,
DRZ=0.0,),);

#F LOADS ##############################################################################################

#F gravità (PESANTEUR)
selfwght=AFFE_CHAR_MECA(MODELE=model,
PESANTEUR=_F(GROUP_MA=('topbeam','mast','massN',),
GRAVITE=10000.0,
DIRECTION=(0.0,0.0,-1.0,),),);

#F forza in un punto della struttura ('loadS')
cc=AFFE_CHAR_MECA(MODELE=model,
FORCE_NODALE=_F(GROUP_NO='loadS',
FZ=-135.0,),);

#F forza distribuita ('topbeam') (ASTER non accetta due forze distribuite (gravità più questa)
# quindi la azssegno nodo per nodo)
cr=AFFE_CHAR_MECA(MODELE=model,
FORCE_NODALE=_F(GROUP_NO='topbeam',
FZ=-11.7647058824,),);

#F stepping di applicazione delle forze
selfw_m=DEFI_FONCTION(
NOM_PARA='INST',
VALE=(2.0 ,0.0 ,
3.0 ,1.35 ,
5.0 ,1.35 ,
6.0 ,0.0 ,),
PROL_DROITE='CONSTANT',
PROL_GAUCHE='CONSTANT',);

cc_m=DEFI_FONCTION(
NOM_PARA='INST',
VALE=(3.0 ,0.0 ,
4.0 ,1.0 ,
5.0 ,1.0 ,
6.0 ,0.0 ,),
PROL_DROITE='CONSTANT',
PROL_GAUCHE='CONSTANT',);

cr_m=DEFI_FONCTION(
NOM_PARA='INST',
VALE=(4.0 ,0.0 ,
5.0 ,1.5 ,
6.0 ,1.0 ,),
PROL_DROITE='CONSTANT',
PROL_GAUCHE='CONSTANT',);

# SOLUZIONE ###########################################################################################

#F stepping the soluzione
liste=DEFI_LIST_REEL(DEBUT=2.0,
INTERVALLE=_F(JUSQU_A=6.0,
PAS=1.0,),);

#U4.51.01

stat=MECA_STATIQUE(MODELE=model,
CHAM_MATER=material,
CARA_ELEM=elemcar,
EXCIT=(_F(CHARGE=ground,),
_F(CHARGE=selfwght,
FONC_MULT=selfw_m,),
_F(CHARGE=cc,
FONC_MULT=cc_m,
TYPE_CHARGE='FIXE',),
_F(CHARGE=cr,
FONC_MULT=cr_m,
TYPE_CHARGE='FIXE',),),
LIST_INST=liste,);

# RISULTATI ###########################################################################################
#U4.80.01

stat=CALC_CHAMP(reuse =stat,
RESULTAT=stat,
CONTRAINTE=('SIEF_ELNO','SIPO_ELNO','SIPM_ELNO',),
FORCE='REAC_NODA',);

#F calcola le masse e le restituisce in una tabella

masse=POST_ELEM(MASS_INER=_F(GROUP_MA=('topbeam','mast','massN',),),
MODELE=model,
RESULTAT=stat,
TITRE='masse',);

#U4.91.03

IMPR_TABLE(TABLE=masse,
FORMAT_R='1PE12.3',);

#F calcola le reazioni vincolari e le restituisce in una tabella
#U4.81.21

sum_reac=POST_RELEVE_T(ACTION=_F(OPERATION='EXTRACTION',
INTITULE='sum reactions',
RESULTAT=stat,
NOM_CHAM='REAC_NODA',
TOUT_ORDRE='OUI',
GROUP_NO=('groundS','groundN',),
RESULTANTE=('DX','DY','DZ',),
MOMENT=('DRX','DRY','DRZ',),
POINT=(0.0,0.0,0.0,),),);

IMPR_TABLE(TABLE=sum_reac,
FORMAT_R='1PE12.3',);

#F calcola le reazioni vincolari e le restituisce in una tabella
#then in tabular format per group of node

reac1=POST_RELEVE_T(ACTION=_F(OPERATION='EXTRACTION',
INTITULE='reactionsS',
RESULTAT=stat,
NOM_CHAM='REAC_NODA',
TOUT_ORDRE='OUI',
GROUP_NO='groundS',
RESULTANTE=('DX','DY','DZ',),),);

#very simple form
#IMPR_TABLE (TABLE=reac1,)
#or more detailed with field separator

IMPR_TABLE(TABLE=reac1,
FORMAT='TABLEAU',
UNITE=8,
FORMAT_R='1PE12.3',
SEPARATEUR=' * ',
TITRE='reaction_1',
INFO=2,);

reac2=POST_RELEVE_T(ACTION=_F(OPERATION='EXTRACTION',
INTITULE='reactionsN',
RESULTAT=stat,
NOM_CHAM='REAC_NODA',
TOUT_ORDRE='OUI',
GROUP_NO='groundN',
RESULTANTE=('DX','DY','DZ',),),);

IMPR_TABLE(TABLE=reac2,
FORMAT_R='1PE12.3',);

#now we print the individual reactions
#in the .resu file in RESULTAT format
#U4.91.01

IMPR_RESU(FORMAT='RESULTAT',
MODELE=model,
RESU=_F(RESULTAT=stat,
NOM_CHAM='REAC_NODA',
GROUP_NO=('groundS','groundN',),
FORMAT_R='1PE12.3',),);

IMPR_RESU(FORMAT='RESULTAT',
MODELE=model,
RESU=(_F(RESULTAT=stat,
NOM_CHAM='DEPL',
NOM_CMP='DZ',
GROUP_MA='topbeam',
VALE_MAX='OUI',
VALE_MIN='OUI',
FORMAT_R='1PE12.3',),
_F(RESULTAT=stat,
NOM_CHAM='SIEF_ELNO',
NOM_CMP='N',
GROUP_MA='mast',
VALE_MAX='OUI',
VALE_MIN='OUI',
FORMAT_R='1PE12.3',),
_F(RESULTAT=stat,
NOM_CHAM='SIEF_ELNO',
NOM_CMP=('MFY','MFZ',),
GROUP_MA='topbeam',
VALE_MAX='OUI',
VALE_MIN='OUI',
FORMAT_R='1PE12.3',),),);

IMPR_RESU(FORMAT='RESULTAT',
MODELE=model,
RESU=_F(RESULTAT=stat,
NOM_CHAM='SIPO_ELNO',
GROUP_MA=('topbeam','mast',),
FORMAT_R='1PE12.3',),);

# stampa risultati per via grafica
#U7.05.21
IMPR_RESU(FORMAT='MED',
UNITE=80,
RESU=_F(RESULTAT=stat,
NOM_CHAM=('DEPL','SIEF_ELNO','SIPO_ELNO','SIPM_ELNO','REAC_NODA',),
GROUP_MA=('topbeam','mast',),),);

#U4.11.02
FIN();
#CHECKSUM:6dd3acf7402fc55ad65faab30775c6fd -:FIN CHECKSUM[/color]