What was found
(CAN) FUSELAGE PRESSURE SKINS PN 50-120156-81 AND 82 CRACKED AT LOWER SPAR CAP PENETRATIONS. (TC 20100218012)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) FUSELAGE PRESSURE SKINS PN 50-120156-81 AND 82 CRACKED AT LOWER SPAR CAP PENETRATIONS. (TC 20100218012)