What was found
During "H" check found corrosion on upper surface of fuselage frame at BS 1240 from LBL 16 to LBL 28 and BS 1260 from LBL 18 to LBL 21 and BS 1260 from RBL 19 to RBL 25. Repaired per EA 55-187411.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
During "H" check found corrosion on upper surface of fuselage frame at BS 1240 from LBL 16 to LBL 28 and BS 1260 from LBL 18 to LBL 21 and BS 1260 from RBL 19 to RBL 25. Repaired per EA 55-187411.