What was found
WHILE ACCOMPLISHING A VISUAL INSPECTION OF THE LOWER FUSELAGE SKIN IAW AD 85-03-08, A 1.5 INCH CRACK WAS FOUND AT STA 465 AND LONGERON 30. INSTALLED TEMPORARY REPAIR IAW SB A53-188 AND DAC DRAWING SB 09530188.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE ACCOMPLISHING A VISUAL INSPECTION OF THE LOWER FUSELAGE SKIN IAW AD 85-03-08, A 1.5 INCH CRACK WAS FOUND AT STA 465 AND LONGERON 30. INSTALLED TEMPORARY REPAIR IAW SB A53-188 AND DAC DRAWING SB 09530188.