What was found
INSPECTION FOUND A 1.25 INCH CRACK IN PLATE INSIDE LT I/B MIDFLAP AT I/B CARRIAGE SPINDLE CUTOUT ACCESS THROUGH PANEL 8443. THE PLATE WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 57-50-4 FIGURE 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.25 INCH CRACK IN PLATE INSIDE LT I/B MIDFLAP AT I/B CARRIAGE SPINDLE CUTOUT ACCESS THROUGH PANEL 8443. THE PLATE WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 57-50-4 FIGURE 4.