What was found
DURING HMV-2, CORROSION WAS FOUND ALONG FUSELAGE SKIN BETWEEN L-28L TO L-29L AND STA 692-718. CORROSION WAS BLENDED AND PERMANENT REPAIR MADE PER SRM 53-04 FIGURE 12B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV-2, CORROSION WAS FOUND ALONG FUSELAGE SKIN BETWEEN L-28L TO L-29L AND STA 692-718. CORROSION WAS BLENDED AND PERMANENT REPAIR MADE PER SRM 53-04 FIGURE 12B.