BELL HELICOPTER 430 Maintenance Manual page 122

BHT-430-MM-2
5-34. EVERY 2500 HOURS OF COMPONENT OPERATION (CONT)
DATA REFERENCE
BHT-430-CR&O-2
Chapter 4
Chapter 63
5-00-00
Page 92 Rev. 15 26 JAN 2007
SCHEDULED INSPECTIONS
INSPECTION TASK DESCRIPTION
b. Do a visual inspection of the yokes for cracks,
delamination, and impact damage.
c. If any defect is found, refer to BHT-430-CR&O-2
(Chapter 62) for damage criteria.
PYLON SYSTEM
Step 1 is an airworthiness inspection limitation.
1. Remove and replace, one at a time, torque shear pad
attaching bolts (qty 16).
NOTE
INITIAL
MECH OTHER