TM 1-1520-238-T-7
11–144
11–20. LONGITUDINAL (CYCLIC) FLIGHT CONTROLS – RIGGING OPERATIONAL
11–20
CHECK (cont)
LONG AFT POINTER
MIN MARK
MAX MARK
ALIGNMENT TOOL
CENTER POINT
MAIN ROTOR
RIGGING FIXTURE
MAIN ROTOR
RIGGING PLATE
LONG AFT
POINTER
LONGITUDINAL
BELLCRANK
AFT BOLTHEAD
MAST BASE
LATERAL
BELLCRANK
ALIGNMENT
TOOL
M70-154
Figure 11–80.
Cyclic AFT Limit Check
2. Remove rig pins, warning flags and cover installed in steps a and b.
3. Remove rigging fixture and plate (TM 1-1520-238-23) and alignment tool.
4. Perform flight control system maintenance operational check (para 11–12).
5. Disconnect maintenance headset (TM 1-1520-238-T-4).
6. Remove external power – electrical and hydraulic (primary) (TM 1-1520-238-23).
7. Install pilot and CPG collective stick covers (TM 1-1520-238-23).
8. Secure access panels L200 and R200 (TM 1-1520-238-23).
9. Perform maintenance test flight (TM 1-1520-238-MTF).
END OF TASK
