PHASE NO. _____
Area Name and No.
Aircraft Serial No.
FORWARD ROTOR, CROWN, AND
TUNNEL, AREA #7
Faults and/or Remarks
7.19 First stage mixing bellcranks
and links for damage, corrosion,
security, and evidence of interference.
Control stops for damage and security.
Adjacent area for damage and foreign
7.20 First stage mixing complex
supports and adjacent structure for
buckling and cracks.
7.21 Longitudinal cyclic trim link for
security. Longitudinal cyclic trim
actuator and connector for security.
Actuator, link wire bundles, and rod
ends for evidence of chafing. Access
7.22 Longitudinal cyclic trim yoke for
damage and corrosion. Inspect forward
yoke and inside diameter of the forward
yoke shaft for corrosion. Yoke attaching
hardware for security and evidence of
looseness or wear. Access 30, 72
Check work area for tools and parts after completion of maintenance and inspection.