What was found
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH LONG CRACK AFT OF REAR SPAR, 18 INCH BELOW NR 4 RUDDER HINGE VERTICAL STABILIZER PANEL. INSTALLED DOUBLER, REPAIRED PER EA 42154. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH LONG CRACK AFT OF REAR SPAR, 18 INCH BELOW NR 4 RUDDER HINGE VERTICAL STABILIZER PANEL. INSTALLED DOUBLER, REPAIRED PER EA 42154. (M)