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BELL HELICOPTER 430 - 5-13. 50 HOUR INSPECTION (CONT)

BELL HELICOPTER 430
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BHT-430-MM-2
5-00-00
Page 12 Rev. 16 9 JAN 2008
16. Examine the main rotor adapter assemblies for evidence of
contact between the adapter pads and the yoke assembly. (R1)
17. If evidence of contact is found in step 15 and step 16, do
the steps that follow: (R1)
Chapter 62 a. Remove the main rotor blades and examine damage.
Chapter 62 b. Examine the yoke assembly for cracks and
delamination.
Chapter 62 c. Examine the adapters and upper stop assemblies for
damage and deformations.
Chapter 62 d. Examine the lead lag dampers for delamination and
general condition.
e. Prior to main rotor blade installation, remove contact
evidence from up-stop end plug and replace adapter lead lag
pads as required.
SCHEDULED INSPECTIONS
5-13. 50 HOUR INSPECTION (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER

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