What was found
DURING C CHECK INSPECTION, FOUND ATTACH ANGLE CRACKED F/S 640 BETWEEN LONGERON 26 AND 27 RT. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE, DRILLED, PRIMED AND INSTALLED NEW ANGLE IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C CHECK INSPECTION, FOUND ATTACH ANGLE CRACKED F/S 640 BETWEEN LONGERON 26 AND 27 RT. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE, DRILLED, PRIMED AND INSTALLED NEW ANGLE IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21