What was found
INSPECTION FOUND A HOLE MEASURING APPROXIMATELY 4 INCHES X 5 INCHES IN FUSELAGE SKIN BETWEEN STA 986.5 AND 1006 BETWEEN S3L AND S4L. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 210.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A HOLE MEASURING APPROXIMATELY 4 INCHES X 5 INCHES IN FUSELAGE SKIN BETWEEN STA 986.5 AND 1006 BETWEEN S3L AND S4L. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 210.