What was found
RIGHT WING L/E I/B ON TOP OF FUEL BOOST PUMP FOUND ANGLE CRACKED. P/N 116A3939-2 / REMOVED AND REPLACED CRACK ANGLE ON R/H WING L/E I/B ON BOOST PUMP AREA PER REF SRM 57-20-10-1A-3; ANGLE P/N 116A3939-2
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING L/E I/B ON TOP OF FUEL BOOST PUMP FOUND ANGLE CRACKED. P/N 116A3939-2 / REMOVED AND REPLACED CRACK ANGLE ON R/H WING L/E I/B ON BOOST PUMP AREA PER REF SRM 57-20-10-1A-3; ANGLE P/N 116A3939-2