Kjadam98

Hello, would someone mind helping me figure out why my ac3d model won't generate? This text works for the datcom outputs? I recently added flaps and ailerons...Any help would be greatly appreciated! $FLTCON NMACH = 1.0, MACH(1) = 0.13,NALPHA=10.0, ALSCHD(1)=-4.0,-2.0,0.0,2.0,4.0,6.0,8.0,10.0,12.0,14.0,ALT=3000.0,WT=583.0,LOOP=1.,$$SYNTHS XCG=1.66872, ZCG=0.0,XW=1.668, ZW=0.5222885, ALIW=8.5,XH=5.137, ZH=0.0, ALIH=0.0,XV=5.137, ZV=0.0,$$BODY NX=8.0,X(1)=0.0,0.298,1.396,3.084,3.681,4.128,4.725,5.372,S(1)=0.0001,0.0486,0.856,0.856,0.497,0.278,0.095,0.031,$NACA-W-4-2412NACA-H-6-66-009NACA-V-6-66-009$WGPLNF CHRDTP=1.31,SSPNE=4.5, SSPN=4.725,CHRDR=1.435,SAVSO=0.0,CHSTAT=0.25,TWISTA=0.0,DHDADI=1.0,TYPE=1.0,$$SYMFLP FTYPE=1.0, NTYPE=1.0,NDELTA=9.0, DELTA(1)=-20.0,-15.0,-10.0,-5.0,0.0,5.0,10.0,13.0,16.0,CHRDFI=0.298, CHRDFO=0.249, SPANFI=0.298, SPANFO=2.09,$$ASYFLP STYPE=4.0,NDELTA=9.0,DELTAL(1)=-32.0,-20.0,-10.0,-5.0,0.0, 5.0, 10.0, 20.0, 32.0,DELTAR(1)= 32.0, 20.0, 10.0, 5.0,0.0,-5.0,-10.0,-20.0,-32.0,SPANFI=2.08895, SPANFO=4.72501, CHRDFI=0.2487, CHRDFO=0.1492,$$HTPLNF CHRDTP=0.72,SSPNE=1.17, SSPN=1.27,CHRDR=0.65,SAVSI=0.06,CHSTAT=0.25,TYPE=1.0,$$SYMFLP FTYPE=1.0, NTYPE=1.0,NDELTA=9.0, DELTA(1)=-20.0,-15.0,-10.0,-5.0,0.0,5.0,10.0,13.0,16.0,CHRDFI=0.4476, CHRDFO=0.2489, SPANFI=0.09947, SPANFO=1.2434,$$VTPLNF CHRDTP=0.62,SSPNE=1.08, SSPN=1.08,CHRDR=0.982,SAVSI=25.0,CHSTAT=0.25,TYPE=1.0,$DIM MBUILDPLOTCASEID IKARUS C42SAVENEXT CASEAlso, how can I get all the coefficients needed for the AIR file?