What was found
BLEND OUT ON FUSELAGE SKIN, BS 309 BETWEEN LONGERONS 29 RT AND 30. DAMAGE WAS DRILLED IAW SRM 53-04-2, PARAGRAPH 3. 2, A, 1, A. PLUG OF REPAIR WAS INSTALLED IAW SRM 53-04-2, 3C, 2, A, 1, A, 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
BLEND OUT ON FUSELAGE SKIN, BS 309 BETWEEN LONGERONS 29 RT AND 30. DAMAGE WAS DRILLED IAW SRM 53-04-2, PARAGRAPH 3. 2, A, 1, A. PLUG OF REPAIR WAS INSTALLED IAW SRM 53-04-2, 3C, 2, A, 1, A, 3.