What was found
GSO - INSPECTION FOUND SKIN CRACKED AT SEVERAL FASTENER HOLES BETWEEN BS 188 AND BS 251.6 ON THE LT SIDE OF FUSELAGE. ALL CRACKS WERE APPROXIMTELY .25 INCH LONG. THE CRACKS WERE REPAIRED IAW EA 5310-01188, PART 3. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
GSO - INSPECTION FOUND SKIN CRACKED AT SEVERAL FASTENER HOLES BETWEEN BS 188 AND BS 251.6 ON THE LT SIDE OF FUSELAGE. ALL CRACKS WERE APPROXIMTELY .25 INCH LONG. THE CRACKS WERE REPAIRED IAW EA 5310-01188, PART 3. (X)