What was found
FOUND PITTING CORROSION ON STRINGER 44 RT, BETWEEN FRAME 54-55/58. REPAIR PERFORMED BY REPLACEMENT OF STRINGER PORTION AS LONG AS POSSIBLE BY USING ADDITIONAL COUPLINGS AS PER SRM 53-10-14/FIG 201 AND IAW SRM 51-72-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND PITTING CORROSION ON STRINGER 44 RT, BETWEEN FRAME 54-55/58. REPAIR PERFORMED BY REPLACEMENT OF STRINGER PORTION AS LONG AS POSSIBLE BY USING ADDITIONAL COUPLINGS AS PER SRM 53-10-14/FIG 201 AND IAW SRM 51-72-10.