What was found
FOUND FUSELAGE EXTERIOR FASTENER SHEARED AT LONGERON 39 LEFT AND SKIN BULGED AT FS -32.00. REPAIRED FUSELAGE EXTERIOR SKIN AT FS 32.00, LONGERON 30 LEFT IAW DC8 SRM 53-2-1, 51-1-8, AND DWG K04888.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND FUSELAGE EXTERIOR FASTENER SHEARED AT LONGERON 39 LEFT AND SKIN BULGED AT FS -32.00. REPAIRED FUSELAGE EXTERIOR SKIN AT FS 32.00, LONGERON 30 LEFT IAW DC8 SRM 53-2-1, 51-1-8, AND DWG K04888.