What was found
CRACK ON FUSELAGE SKIN AT BS 1406 NEAR LONGERON 2R BESIDE DORSAL FIN ATTACH ANGLE. REPAIRED IAW ETI-88-17-016 REVISION 3 AND ER/A 541702-14AD SECTION II.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FUSELAGE SKIN AT BS 1406 NEAR LONGERON 2R BESIDE DORSAL FIN ATTACH ANGLE. REPAIRED IAW ETI-88-17-016 REVISION 3 AND ER/A 541702-14AD SECTION II.