100-Hour Inspection - Bell 206L4 Maintenance Manual

5-28.

100-HOUR INSPECTION

DATA REFERENCE
Chapter 53
Chapter 4
Export Classification C, ECCN EAR99
SCHEDULED INSPECTIONS
INSPECTION TASK DESCRIPTION
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
AN Y CRA CK , CORROS ION, OR LOOS E OR
SHEARED RIVET IS CAUSE FOR IMMEDIATE
GROUNDING OF THE HELICOPTER UNTIL THE
PROBLEM IS CORRECTED.
2. Remove access panel on right side of aft fuselage.
NOTE
CAUTION
7 NOV 2014 Rev. 20
BHT-206L4-MM-1
INITIAL
MECH OTHER
5-00-00
Page 83