What was found
LT O/B AILERON UPPER SKIN HAS .5" BPT CRACK 4" FWD T/E, 11' IB OF OB END. APPLIED SPEED TAPE PER SRM 51-40-09 FIG 1 TABLE 1 AND TABLE II. REINSPECT EVERY "A" CHECK. PERMANENT REPAIR AT NEXT "C" CHECK. TRANSFERRED TO D368106.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT O/B AILERON UPPER SKIN HAS .5" BPT CRACK 4" FWD T/E, 11' IB OF OB END. APPLIED SPEED TAPE PER SRM 51-40-09 FIG 1 TABLE 1 AND TABLE II. REINSPECT EVERY "A" CHECK. PERMANENT REPAIR AT NEXT "C" CHECK. TRANSFERRED TO D368106.