What was found
EMPENNAGE 76 RT ACCESS PANEL SKIN CRACKED 1 INCH. REMOVED DAMAGED AREA PER SRM 55-2-0 FIG 2. FABRICATED REINFORCEMENT AND PLATE PER SRM 56-2-0 FIG 2. INSTALLED REINFORCEMENT AND PLATE PER SRM 55-2-0 FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EMPENNAGE 76 RT ACCESS PANEL SKIN CRACKED 1 INCH. REMOVED DAMAGED AREA PER SRM 55-2-0 FIG 2. FABRICATED REINFORCEMENT AND PLATE PER SRM 56-2-0 FIG 2. INSTALLED REINFORCEMENT AND PLATE PER SRM 55-2-0 FIG 2.