What was found
LT HORIZONTAL STAB TE LOWER SKIN APPROX 64 INCHES FROM FUSELAGE AND 2 INCHES FWD OF REAR SPAR CRACKED. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER SHIM AND ACCESS PLATES. REFERENCE SRM 5-10-01 REPAIR 6 FIGURE 803.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT HORIZONTAL STAB TE LOWER SKIN APPROX 64 INCHES FROM FUSELAGE AND 2 INCHES FWD OF REAR SPAR CRACKED. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER SHIM AND ACCESS PLATES. REFERENCE SRM 5-10-01 REPAIR 6 FIGURE 803.