What was found
FUSELAGE SKIN CRACKED AT AFT UPPER DOOR STOP AT PASSENGER ENTRANCE. CRACK WAS LESS THAN .5 INCH LONG. REPAIRED AREA IAW EA 53100126-001 AND DC9 SRM 53-05, FIGURE 114.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACKED AT AFT UPPER DOOR STOP AT PASSENGER ENTRANCE. CRACK WAS LESS THAN .5 INCH LONG. REPAIRED AREA IAW EA 53100126-001 AND DC9 SRM 53-05, FIGURE 114.