What was found
L/H WING FWD BOOST POMP AREA UPPER ANGLE CRACK<[01] REMOVED AND REPLACED DAMAGE ANGLE UPPER OF BOOST POMP ;PER REF. SRM 51-40-02-0G-0 AND DRAWING # 112A2004;[02] VERIFIED REMOVAL AND REPLACEMENT OF UPPER ANGLE OF BOOST PUMP
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
L/H WING FWD BOOST POMP AREA UPPER ANGLE CRACK<[01] REMOVED AND REPLACED DAMAGE ANGLE UPPER OF BOOST POMP ;PER REF. SRM 51-40-02-0G-0 AND DRAWING # 112A2004;[02] VERIFIED REMOVAL AND REPLACEMENT OF UPPER ANGLE OF BOOST PUMP