What was found
RT FUSELAGE EXTERIOR SKIN BETWEEN STA 1139-1119 LT 25 CRACKED. CRACKED AREA BLENDED AS PER SRM 51-21-01 VOL2 WITH NO FURTHER CRACK AND FOUND WITHIN LIMIT AS PER SRM 53-20-00 FIG 6 VOL 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT FUSELAGE EXTERIOR SKIN BETWEEN STA 1139-1119 LT 25 CRACKED. CRACKED AREA BLENDED AS PER SRM 51-21-01 VOL2 WITH NO FURTHER CRACK AND FOUND WITHIN LIMIT AS PER SRM 53-20-00 FIG 6 VOL 1.