What was found
CORROSION ON UPPER FLANGE OF FRAME AT BS 1148 BETWEEN STRINGER 27L AND 26L. REMOVED CORROSION. ORIGINAL MATERIAL THICKNESS .063, MATERIAL LOSS .003. FOUND WITHIN LIMITS IAW SRM 53-10-1 AND 53-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON UPPER FLANGE OF FRAME AT BS 1148 BETWEEN STRINGER 27L AND 26L. REMOVED CORROSION. ORIGINAL MATERIAL THICKNESS .063, MATERIAL LOSS .003. FOUND WITHIN LIMITS IAW SRM 53-10-1 AND 53-10-2.