WO: 144 MOS INSP (212012) FAA 2011-27-03 PARA DETAILED INSPECTION TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY LOAD PATH FOR THE (G)(1)(I)(1) BALLSCREW IN THE DRIVE MECHANISM OF THE HSTA AND SUBSEQUENT WEAR AND FAILURE OF THE SECONDARY LOAD PATH IN ACCORDANCE WITH SERVICE BULETIN 737-27A1277 R2 MAN

LUBRICATION OPEN 9.0 FM 2011.27-03 PAM (6)(1)(1)(1) DETAILED INSPECTION TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY LOAD PATH FOR THE OPEN BALLSCREW IN THE DRIVE MECHANISM OF THE HSTA AND SUBSEQUENT WEAR AND FAILURE OF THE SECONDARY LOAD PATH IN ACCORDANCE WITH SERVICE BUITIN 737-27A1277 R2 10.0