What was found
TWO CRACKS WERE FOUND ON FUSELAGE SKIN AND DOUBLER AT THE AFT LOWER CORNER OF: 0.250", FUSELAGE SKIN AND 1.593", DOUBLER AT BS 423.750 AND BETWEEN LONGERON 26 AND 27 RT. CRACKS ON FUSELAGE SKIN WERE REPAIRED IAW SRM 53-05, FIG 105.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TWO CRACKS WERE FOUND ON FUSELAGE SKIN AND DOUBLER AT THE AFT LOWER CORNER OF: 0.250", FUSELAGE SKIN AND 1.593", DOUBLER AT BS 423.750 AND BETWEEN LONGERON 26 AND 27 RT. CRACKS ON FUSELAGE SKIN WERE REPAIRED IAW SRM 53-05, FIG 105.