What was found
FRAME BS 236.00 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 29P AND 30P. REMOVED CORROSION IAW SRM 51-21-00-00-02. REMAINING THICKNESS .038", CONFIRMED CRACK FREE. MATERIAL LOSS WITHIN LIMITS. RESTORED SURFACE PROTECTION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FRAME BS 236.00 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 29P AND 30P. REMOVED CORROSION IAW SRM 51-21-00-00-02. REMAINING THICKNESS .038", CONFIRMED CRACK FREE. MATERIAL LOSS WITHIN LIMITS. RESTORED SURFACE PROTECTION.