TM 1-1520-238-23 Change 8 2-268.1 2.76. MAIN LANDING GEAR LEFT SHOCK STRUT STRUCTURAL SUPPORT REMOVAL/INSTALLATION – continued 2.76.6. Installation NOTE It may be necessary to add additional washers to bolts after MWO 1-1520-238-50-46 has been applied. Use shock strut support wrench set (figure D-484, App D) to hold nuts as necessary. Inspect replacement shock strut sup- port for guide pins prior to installation. If support does not have pins installed, install new pins or reuse pins form old support. a. Install support (5) on airframe (2). Torque three nuts (34), two nuts (31), nut (27), two nuts (24), nine nuts (17), and nut (14) to 90 INCH-POUNDS. (1) If required install pins in new support (5) (para 2.77A). (2) Install bolt (6) and (11) and two bolts (12) on support (5). Do not tighten. (3) Install bolt (7), two washers (10), washer (9), and nut (8) on support (5). Do not tighten. (4) Install bolts (19) and (20), two washers (22), and nuts (21) on support (5). Do not tighten. Use torque wrench adapter. (5) Install three bolts (33), washers (35), and nuts (34) on support (5). Torque nuts (34) to 90 INCH-POUNDS. Use torque wrench. (6) Install angle (29) on support (5). (a) Position angle (29) on support (5). (b) Install two bolts (30), washers (32), nuts (31), and angle (29) on support (5). Torque nuts (31) to 90 INCH-POUNDS. Use torque wrench. (7) Install bolt (26), washer (28), and nut (27) on support (5). Torque nut (27) to 90 INCH- POUNDS. Use torque wrench. (8) Install two bolts (23), washers (25), and nuts (24) on support (5). Torque nuts (24) to 90 INCH-POUNDS. Use torque wrench. GO TO NEXT PAGE 5 2 6 12 11 7 8 ⁹10 33 35 34 20 ²¹22 19 M04-3744-5A M04-3744-6A 26 23 16 16 16 24 25 28 27 5 30 13 14 15 18 17 32 31 29