What was found
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK NOSE WHEEL WELL 5 INCHES AFT OF 227 BULKHEAD 1 INCH BELOW W/W CEILING WEB. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK NOSE WHEEL WELL 5 INCHES AFT OF 227 BULKHEAD 1 INCH BELOW W/W CEILING WEB. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)