What was found
CRACKED PREVIOUS REPAIR DOUBLER ON FUSELAGE SKIN BETWEEN BS 101 TO BS 110 AND PROJECTION LONGERON 27LT. DOUBLER WAS REPLACED IAW SRM 53-05, FIG 158, 51-30-2, 51-30-5, 51-30-11 AND 51-10-3 PAR 14 AND 21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED PREVIOUS REPAIR DOUBLER ON FUSELAGE SKIN BETWEEN BS 101 TO BS 110 AND PROJECTION LONGERON 27LT. DOUBLER WAS REPLACED IAW SRM 53-05, FIG 158, 51-30-2, 51-30-5, 51-30-11 AND 51-10-3 PAR 14 AND 21.