What was found
CRACK WAS FOUND ON THE FRAME HOLES WHICH ATTACH THE BRACKET BETWEEN S8L - S9L. STA787 L=0.15" FABRICATED ANGLES PER EA5310-04716 REVF STEP9 FIG3. REMOVED CRACK PER EA5310-04716 REVF STEP9 FIG3. INSTALLED REPAIR PARTS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK WAS FOUND ON THE FRAME HOLES WHICH ATTACH THE BRACKET BETWEEN S8L - S9L. STA787 L=0.15" FABRICATED ANGLES PER EA5310-04716 REVF STEP9 FIG3. REMOVED CRACK PER EA5310-04716 REVF STEP9 FIG3. INSTALLED REPAIR PARTS.