BHT-206A/B-SERIES-MM-1
5-00-00
30 APR 2013 Rev. 14 Page 95
Export Classification C, ECCN EAR99
5-28. 100-HOUR INSPECTION
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
DATE: __________________W.O. _____________________
FACILITY: __________________________________________
HELICOPTER S/N: ___________________________________
REGISTRY NO.: _____________________________________
TOTAL TIME:_______________________________________
SIGNATURE:________________________________________
100-hour inspection must be accomplished when
using the 300-hour airframe progressive inspection
program or the 300-hour airframe periodic inspection
program.
Chapter 62 MAIN ROTOR
1. Torque check pillow block retention hardware 84 to
107 inch-pounds (9.4 to 12 Nm). Examine for misalignment of
anti-slippage marks (ASB 206-97-90).
Chapter 67 FLIGHT CONTROLS
ASB 206-76-1 2. Examine servo actuator support for condition.
a. If installed, inspect hydraulic actuator support
206-001-520-005 as follows:
• Visually inspect the two forward webs of the support
assembly for cracks with a 5X magnifying glass. All
cracks reported in the support assembly have
originated in the top edge of the forward web.
• If a crack is found, remove and replace the support
assembly. Notify Product Support Engineering
concerning any assembly found cracked.
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