BELL HELICOPTER 222, Maintenance Manual

Page: 44 / 198

BHT-222/222B-MM-1
5-00-00
Page 26
Rev. 7 9 SEP 2011 ECCN EAR99
Chapter 27 4. Check cyclic stick, collective stick, and tail rotor pedal
minimum friction. Adjust if necessary. F2
Chapter 12 5. Remove access panels along bottom centerline of fuselage
to FS 356.00. F3/F4
Chapter 27 a. lnspect directional control tubes, rod end bearings,
bellcranks, supports, and attachment bolts for corrosion,
evidence of wear, and security of attachments. F3/F4
b. Check wiring bundles for security and evidence of
chafing. Visually inspect all exposed structure for corrosion,
distortion, or cracks. F3/F4
Chapter 29 c. lnspect directional control actuator for leaks and
security of attachment, and FS 340.00 bulkhead structure for
distortion or cracks. F3/F4
Chapter 27
BHT-ALL-SPM 6. Open control tunnel access in the canted bulkhead behind
the pilot station. lnspect the lower and upper cyclic and
collective pitch control bellcranks for bearing security of
attachment, corrosion or mechanical damage to clevises, and
security of attachment to supports and control tube bearings.
F5/F6
Chapter 25 7. On helicopters equipped with emergency exit windows in
the passenger doors and/or aft window position, inspect as
follows after removing interior trim from around windows: F3/F4
a. On passenger door only, visually inspect window
retainer to door frame bond. Replace the retainer if it is not
securely bonded to the frame at all points except at the two
lower corners. F3/F4
b. Visually inspect the inboard side of all rubber retainers.
Any nicks or cracks in the retainer is cause for replacement of
the retainer. F3/F4
c. Check that all filler strips and pull tab are firmly seated
in their retainer grooves. F3/F4
Chapter 25 d. Install interior trim. F3/F4
SCHEDULED INSPECTIONS
5-15. 600-HOUR INSPECTION (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER