What was found
(AUS) FUSELAGE FRAME PN 65B01754-24 AND FRAME DOUBLER PN 65B26275-34 CRACKED. INVESTIGATION FOUND CRACKING WAS DUE TO THE USE OF A SPLICE PLATE OF THE INCORRECT MATERIAL AS STATED IN BSB 747-53-2483.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) FUSELAGE FRAME PN 65B01754-24 AND FRAME DOUBLER PN 65B26275-34 CRACKED. INVESTIGATION FOUND CRACKING WAS DUE TO THE USE OF A SPLICE PLATE OF THE INCORRECT MATERIAL AS STATED IN BSB 747-53-2483.