What was found
CRACK WAS FOUND 0.250" OF LENGTH ON FUSELAGE SKIN STA Y=160 BTW LONGS 3L & 4L. FUSELAGE SKIN WAS REPAIRED PER SRM 53-04-3 FIG 8 (SHEET 5).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK WAS FOUND 0.250" OF LENGTH ON FUSELAGE SKIN STA Y=160 BTW LONGS 3L & 4L. FUSELAGE SKIN WAS REPAIRED PER SRM 53-04-3 FIG 8 (SHEET 5).