What was found
FUSELAGE SKIN, STA 540 UNDER DRAG LINK ASSEMBLY AT STR S-21R + 7.250 IN, FASTENER HOLE WITH CRACK INDICATION. REPAIRED FUSELAGE SKIN BTWN STA 520 AND STA 540, STR 21R - 23R.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN, STA 540 UNDER DRAG LINK ASSEMBLY AT STR S-21R + 7.250 IN, FASTENER HOLE WITH CRACK INDICATION. REPAIRED FUSELAGE SKIN BTWN STA 520 AND STA 540, STR 21R - 23R.