BELL HELICOPTER 430 - 5-28. EVERY 100 HOURS OF COMPONENT OPERATION; SWASHPLATE CONTROLS; NOTE; MAIN ROTOR YOKES

BHT-430-MM-2
5-00-00
1 NOV 2012 Rev. 19 Page 79
ECCN EAR99
SCHEDULED INSPECTIONS
5-28. EVERY 100 HOURS OF COMPONENT OPERATION
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
DATE: __________________W.O. _____________________
FACILITY: __________________________________________
HELICOPTER S/N: ___________________________________
REGISTRY NO.: _____________________________________
TOTAL TIME:_______________________________________
SIGNATURE:________________________________________
SWASHPLATE CONTROLS
1. Examine the swashplate assembly.
Chapter 62 a. Remove the pitch change links and disconnect the drive
link from the rotating ring. (R1)
NOTE
Examine the duplex bearing before you lubricate the
swashplate.
b. Rotate the swashplate outer ring and make sure the
duplex bearing operates smoothly. Replace the bearing if it feels
rough.
Chapter 12 c. Lubricate swashplate duplex bearing.
MAIN ROTOR YOKES
Chapter 4
NOTE
Step 1 is an airworthiness inspection limitation. This
inspection only applies to main rotor yokes with
cracks greater than 3.0 inches (76.19 mm) located
between station 23.0 and station 31.0.