What was found
1EA THROUGH THICKNESS CRACK WAS FOUND ON THE MARKED HOLE AT THE AFT CHANNEL LAYER ( 2ND LAYER COUNTED FROM FWD ) ON 5 O'CLOCK POSITION ON RH STA 840 TENSION TIE.(<P>REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 FIG 201.</P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
1EA THROUGH THICKNESS CRACK WAS FOUND ON THE MARKED HOLE AT THE AFT CHANNEL LAYER ( 2ND LAYER COUNTED FROM FWD ) ON 5 O'CLOCK POSITION ON RH STA 840 TENSION TIE.(<P>REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 FIG 201.</P>)