What was found
NR 2 ENGINE 1ST STAGE ROTO DISK FAN SHAFT HAS OIL LEAKS. REMOVED AND REPLACED NR 2 ENGINE FAN HUB MANIFOLD SEAL, PER MM 72-31-03-404-005-H00. OPERATED ENGINE PER MM 71-00-00-862-053-H03. NO LEAKS NOTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 ENGINE 1ST STAGE ROTO DISK FAN SHAFT HAS OIL LEAKS. REMOVED AND REPLACED NR 2 ENGINE FAN HUB MANIFOLD SEAL, PER MM 72-31-03-404-005-H00. OPERATED ENGINE PER MM 71-00-00-862-053-H03. NO LEAKS NOTED.