What was found
EXTERIOR FUSELAGE AT BS 727A PLUS 10, STR 10 LT LAP JOINT AREA, LOWER SKIN WITH HOLE CRACKED. POSSIBLE CAUSE OF CRACK WAS SKIN FATIGUE. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXTERIOR FUSELAGE AT BS 727A PLUS 10, STR 10 LT LAP JOINT AREA, LOWER SKIN WITH HOLE CRACKED. POSSIBLE CAUSE OF CRACK WAS SKIN FATIGUE. (X)