What was found
(RIGHT WING) UPPER T/E SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED UPPER T/E SUPPORT ANGLE AT THE TRANSVERSE WEB ABOVE #2 PYLON IAW SOPM 20-50-01 84036 24JUN17
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(RIGHT WING) UPPER T/E SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED UPPER T/E SUPPORT ANGLE AT THE TRANSVERSE WEB ABOVE #2 PYLON IAW SOPM 20-50-01 84036 24JUN17