BELL HELICOPTER 430 Maintenance Manual page 118

BHT-430-MM-2
5-32. EVERY 600 HOURS OF COMPONENT OPERATION
DATA REFERENCE
Chapter 4
BHT-430-CR&O-2,
Chapter 62
5-00-00
Page 88 Rev. 19 1 NOV 2012
SCHEDULED INSPECTIONS
INSPECTION TASK DESCRIPTION
b. Return the pylon fluid mount to manufacturer for
disassembly and dye penetrant inspection of the inner metal
member.
2. Examine the right pylon fluid mount as follows: (F6)
a. Remove the right pylon fluid mount.
b. Return the pylon fluid mount to manufacturer for
disassembly and dye penetrant inspection of the inner metal
member.
MAIN ROTOR YOKES
Step 1 is an airworthiness inspection limitation. This
inspection only applies to main rotor yokes with
cracks less than 3.0 inches (76.19 mm) located
between station 23.0 and station 31.0.
This inspection is limited to yoke arm(s) that has
crack(s) less than 3.0 inches (76.19 mm).
Main rotor blade must be removed to perform this
inspection.
1. Examine the main rotor yokes as follows: (R1)
a. Clean the yoke(s).
b. Do a visual inspection of the yokes for cracks.
c. Refer to BHT-430-CR&O-2, Chapter 62 for damage
criteria.
NOTE
NOTE
NOTE
INITIAL
MECH OTHER
ECCN EAR99