AIRCRAFT MAINTENANCE MANUALINTRODUCTION - DESCRIPTION AND OPERATIONGENERALFleet No./MSN Cross-reference tableSERVICE BULLETIN LIST

ChapterSectionSubjectGENERAL
TASK 32-10-02-000-801Procedure
Torque Links RemovalSUBTASK 32-10-02-210-001
  1. Procedures for the right and left components are the same. Only the procedures for the left are given.

SUBTASK 32-10-02-020-002
  1. Remove the wheel assy.

SUBTASK 32-10-02-010-003
    1. Remove the screw (13), clamp (14) and nut (21) from the torque link standoff bracket (18).

    2. Remove the cotter pins (16), nuts (15), washers (17), bolts (20), standoff bracket (18) and switch bracket (19) from the upper torque link (2).

    3. Remove the nuts (12), washers (11), bolts (8) and the switch terminal bracket (9) from the lower torque link (7).

    4. Remove the cotter pin (5), nut (4), washer (6) and bolt (10) from the torque links (2 and 7).

    5. Remove the safety wires from the upper and lower slotted spring pins (3). Remove the spring pins (3).

    6. Remove link pins (1) from the upper (2) and lower (7) torque links.

    7. Remove the upper torque link (2) and lower torque link (7) from the strut and axle.

SUBTASK 32-10-02-220-004
  1. Inspect the strut, pins and torque link bushings.

Torque Links Removal