What was found
TURBINE EXHAUST STRUT AT 11 O'CLOCK POSITION HAS 1.5 INCH CRACK AT BASE. STRUT REPAIRED PER GMM 72-54-01 PG 801 PROCEDURE 'A' AND 'B' ITEM 1-5, PERFORMED BY WELDER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TURBINE EXHAUST STRUT AT 11 O'CLOCK POSITION HAS 1.5 INCH CRACK AT BASE. STRUT REPAIRED PER GMM 72-54-01 PG 801 PROCEDURE 'A' AND 'B' ITEM 1-5, PERFORMED BY WELDER.