BHT-206L4-MM-1
5-00-00
7 NOV 2014 Rev. 20 Page 83
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.
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.
TAILBOOM
ANY CRACK, CORROSION, OR LOOSE OR
SHEARED RIVET IS CAUSE FOR IMMEDIATE
GROUNDING OF THE HELICOPTER UNTIL THE
PROBLEM IS CORRECTED.
Chapter 53
Chapter 4
2. Remove access panel on right side of aft fuselage.
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