What was found
DURING ROUTINE C CHECK INSPECTION, FOUND LEFT MAIN LANDING GEAR WHEEL WELL PRESSURE WALL SKIN CORRODED AT STATION 902.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS AS NEEDED. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-21, DC8 SRM 51-1--20D, DC8 SRM 51-3-1, FAA FORM 8110-3 NUMBER 06551 DATED 11-09-06, SEMAN DRAWING NUMBERED-4360 DATED 11-07-06, AND SEMAN ENGINEERING ORDER NUMBER 2006800 DATED 11-07-06.