BELL HELICOPTER 430 - 5-32. EVERY 600 HOURS OF COMPONENT OPERATION; MAIN ROTOR YOKES; NOTE

BHT-430-MM-2
5-00-00
Page 88 Rev. 19 1 NOV 2012
ECCN EAR99
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
Chapter 4
NOTE
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.
NOTE
This inspection is limited to yoke arm(s) that has
crack(s) less than 3.0 inches (76.19 mm).
NOTE
Main rotor blade must be removed to perform this
inspection.
BHT-430-CR&O-2,
Chapter 62
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.
SCHEDULED INSPECTIONS
5-32. EVERY 600 HOURS OF COMPONENT OPERATION
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER