What was found
HEAVY CORROSION FOUND ON THE T-SECTION AT FRAME 92, BETWEEN STRG 19-23 LT (TAILCONE). REPAIR PERFORMED BY CUT OUT THE T-SECTION AND INSTALLING NEW PORTION AND REPAIR ANGLES IAW EA 6-5319-92229 AND RAS/DAHAM/4020157/2005 ISSUE B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HEAVY CORROSION FOUND ON THE T-SECTION AT FRAME 92, BETWEEN STRG 19-23 LT (TAILCONE). REPAIR PERFORMED BY CUT OUT THE T-SECTION AND INSTALLING NEW PORTION AND REPAIR ANGLES IAW EA 6-5319-92229 AND RAS/DAHAM/4020157/2005 ISSUE B.