What was found
ON REMOVAL OF FUSELAGE SKIN, FOUND LONGERON 49 LT CRACKED AT BS 808. CARRIED OUT REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON REMOVAL OF FUSELAGE SKIN, FOUND LONGERON 49 LT CRACKED AT BS 808. CARRIED OUT REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115