What was found
KUL - SEVERAL PREVIOUS CORROSION BELNDOUTS ON FUSELAGE SKIN FORWARD OF BS 1166 AND BETWEEN STRINGER 23L AND 25L FOUND BEYOND SRM ALLOWABLE LIMITS. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
KUL - SEVERAL PREVIOUS CORROSION BELNDOUTS ON FUSELAGE SKIN FORWARD OF BS 1166 AND BETWEEN STRINGER 23L AND 25L FOUND BEYOND SRM ALLOWABLE LIMITS. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3. (M)