What was found
CLT - Q6 - SKIN, 1.50 INCH CRACK. 1.25 INCH FWD OF REAR SPAR, SPAR STA 124 TO 55-123.6. HORIZONTAL STABILIZER. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW EA. (K)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q6 - SKIN, 1.50 INCH CRACK. 1.25 INCH FWD OF REAR SPAR, SPAR STA 124 TO 55-123.6. HORIZONTAL STABILIZER. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW EA. (K)