What was found
MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED ON RH GEARWELL AFT SPAR, FWD FACE, LOWER CLIP, INBD OF WS 37.00 IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND LIMITS IAW C680 SRM 51-70-02 LIMITATIONS EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSION BLEND IAW TEXTRON ENGINEERING FIELD REPAIR FR-680-0134-14777 REV- TITLE: FIELD REPAIR-CORROSION,RH WING, AFT SPAR, LOWER CAP WS 18.50-23, DATE: 21FEB2025. PERFORMED INITIAL HI-LOK BOLT HOLE INSPECTION, HOLES #118-120 USING NDT EDDY CURRENT AS INSTRUCTED IN ORIGINAL REPAIR TABLE 2 SPECIAL INSPECTION REQUIREMENTS. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: (SPECIAL INSPECTION REQUIREMENTS) COMPONENT 6922435-4 RH FWD ANGLE, WS 18.50-23, FIGURE 4, TECHNIQUE BHET2, INITIAL HOURS 14,736.1, RECURRING HOURS 6,000.