What was found
INSPECTION FOUND A 1.125" CRACK IN WHEEL WELL CENTER KEEL EXTERIOR SKIN PANEL. THE CRACK WAS LOCATED ALONG R/H SIDE BETWEEN STA 685 AND 706. A DOUBLER WAS INSTALLED AND PAINTED IAW SRM 53-60-12, FIGURE 202.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.125" CRACK IN WHEEL WELL CENTER KEEL EXTERIOR SKIN PANEL. THE CRACK WAS LOCATED ALONG R/H SIDE BETWEEN STA 685 AND 706. A DOUBLER WAS INSTALLED AND PAINTED IAW SRM 53-60-12, FIGURE 202.