What was found
A CRACK WAS FOUND ON FUSELAGE SKIN AT BS 371.5 BETWEEN LONGERONS 20 - 21R . THE SKIN WAS REPAIRED IAW SRM 53-05, FIG 105, 51-10-3, P. 21-14, AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A CRACK WAS FOUND ON FUSELAGE SKIN AT BS 371.5 BETWEEN LONGERONS 20 - 21R . THE SKIN WAS REPAIRED IAW SRM 53-05, FIG 105, 51-10-3, P. 21-14, AND 51-30-5.