PHASE NO. _____
Area Name and No.
Aircraft Serial No.
AFT ROTOR AND PYLON, AREA #6
Faults and/or Remarks
6.22 Flight control bellcranks,
connecting links, and idlers in
pylon area for cracks and security.
Connecting link swaged inserts for
evidence of looseness. Access 5, 47
6.23 Bellcrank supports in pylon area
(STA 553.00 LH and STA 562.00 RH)
and adjacent structure for security,
excessive wear, and cracks. Access 5,
6.24 Utility and flight boost cooling fans
for security, corrosion, damage, and
paint for chipping or peeling. Safety
screens for dents, breaks, and security.
Adjacent structure for damage, cracks,
and corrosion. Access 43
6.25 Power transfer unit for leakage and
security. Access 7
6.26 Flight boost power control module
housing for cracks and damage. Mount
structure for cracks and buckling.
2, 4, C
6.27 Replace No. 2 boost pressure and
return filter elements.
Check work area for tools and parts after completion of maintenance and inspection.