What was found
DURING ROUTINE INSPECTION, THE EXTERIOR ANGLE AT STA 867 FUSELAGE TO VERTICAL STABILIZER ATTACH POINT WAS FOUND CRACKED 1.5 IN LENGTH. MAINTENANCE FABRICATED NEW ANGLE AND INSTALLED IAW SRM 53-09 FIG 23. RETURNED A/C TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSPECTION, THE EXTERIOR ANGLE AT STA 867 FUSELAGE TO VERTICAL STABILIZER ATTACH POINT WAS FOUND CRACKED 1.5 IN LENGTH. MAINTENANCE FABRICATED NEW ANGLE AND INSTALLED IAW SRM 53-09 FIG 23. RETURNED A/C TO SERVICE.