What was found
DURING INSPECTION OF THE R/H #5 MED CUT-OUT AFT UPPER CORNER, INTERNAL BEAR STRAP FOUND CRACKED. ACCOMPLISHED REPAIR AS REQUIRED BY BOEING SB 747-53A2839 PART 5, TO INCLUDE DEVIATION (DAMAGE REMOVAL TRIM OUT RADIUS REDUCED TO 1.0” INSTEAD OF 1.5” AS REQ. BY SB) APPROVED BY BAC SR #4-5508991981 AND FORM 8100-9 ISSUED BY BOEING; DATED 05/29/2022. THIS IS AN APPROVED AMOC TO AD 2013-19-15 PARA (G)(2).