What was found
FOUND UPPER VERTICAL STAB PANEL CHAFING ON FORWARD STRUCTURE. BLENDED CHAFED AREAS, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR SECTIONS AND INSTALLED IAW DC9 SRM 55-01 FIGURE 2 AND 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND UPPER VERTICAL STAB PANEL CHAFING ON FORWARD STRUCTURE. BLENDED CHAFED AREAS, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR SECTIONS AND INSTALLED IAW DC9 SRM 55-01 FIGURE 2 AND 51-10-2.