What was found
INSPECTION FOUND A 10 INCH CRACK IN VERTICAL STABILIZER L/H FRONT SPAR AT LOWER END AT CANTED BULKHEAD STA 1388. INSTALLED DOUBLERS IAW SRM 55-02, FIGURE 26.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 10 INCH CRACK IN VERTICAL STABILIZER L/H FRONT SPAR AT LOWER END AT CANTED BULKHEAD STA 1388. INSTALLED DOUBLERS IAW SRM 55-02, FIGURE 26.