What was found
FUSELAGE EXTERIOR .25 INCH LONG CRACK 9 O''CLOCK POSITION AT NR 2 AFT DOOR STOP ADJUST HOLE. TRIMMED OUTER SKIN, CRACK REMOVED. FABRICATED DOUBLER AND FILLER. REPAIRED PER EA 96-179114 AND SRM 53-05 FIG 114. LOGPAGE 1491024.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERIOR .25 INCH LONG CRACK 9 O''CLOCK POSITION AT NR 2 AFT DOOR STOP ADJUST HOLE. TRIMMED OUTER SKIN, CRACK REMOVED. FABRICATED DOUBLER AND FILLER. REPAIRED PER EA 96-179114 AND SRM 53-05 FIG 114. LOGPAGE 1491024.