What was found
DURING H-CHECK, FOUND A 1.50 INCH CRACK IN THE LEFT WHEELWELL KEEL TO SLANTED PRESSURE PANEL SUPPORT FITTING. REPLACED FITTING PER SRM 53-01, PAGE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING H-CHECK, FOUND A 1.50 INCH CRACK IN THE LEFT WHEELWELL KEEL TO SLANTED PRESSURE PANEL SUPPORT FITTING. REPLACED FITTING PER SRM 53-01, PAGE 1.