What was found
CORROSION WAS FOUND DURING AIRCRAFT INSPECTION OF THE FUSELAGE SKINS, STRINGERS AND FRAMES AT THE FOLLOWING LOCATIONS: 1. LEFT SIDE FUSELAGE AT FRAME 22 TO FRAME 25, TO INCLUDE STRINGERS 10L, 11L, 12L, 13L, 13AL AND 14L. 2. LEFT SIDE FUSELAGE AT FRAME 22 BETWEEN STRINGERS 9L AND 10L. 3. RIGHT SIDE OF FUSELAGE AT STRINGER 17R, BETWEEN FRAMES 14 AND 15 TO INCLUDE STRINGERS 15R, 16R, 18R, AND 19R. REPAIRS ARE BEING PERFORMED AT THIS TIME.