What was found
INSPECTION TYPE-D, BODY FRAME HAS EXFOLIATED CORROSION AT STA 1380 BETWEEN LONGERONS 3R AND 4R. REMOVED CORROSION, TREATED AND PRIMED PER SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-2-0 FIG 7, 51-1-21 AND 51-1-20D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE-D, BODY FRAME HAS EXFOLIATED CORROSION AT STA 1380 BETWEEN LONGERONS 3R AND 4R. REMOVED CORROSION, TREATED AND PRIMED PER SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-2-0 FIG 7, 51-1-21 AND 51-1-20D.