BHT-206A/B-SERIES-MM-1
5-00-00
30 APR 2013 Rev. 14 Page 19
Export Classification C, ECCN EAR99
5-16. 100-HOUR AIRFRAME PROGRESSIVE INSPECTION — EVENT NO. 1
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
DATE: __________________W.O. _____________________
FACILITY: __________________________________________
HELICOPTER S/N: ___________________________________
REGISTRY NO.: _____________________________________
TOTAL TIME:_______________________________________
SIGNATURE:________________________________________
ZONE 1 — MAIN ROTOR SYSTEM
Chapter 11 PLACARDS AND MARKINGS
1. Examine the placards, decals, and markings. Make sure
they are readable, correctly applied, and in agreement with the
applicable configuration of your helicopter.
Chapter 62 MAIN ROTOR SYSTEM
1. Verify main rotor flap restraint for freedom of movement,
and for condition and security.
2. Examine static stops and mast for evidence of mast
bumping.
3. Examine main rotor blades for cleanliness and overall
condition. Examine for cracks, corrosion, and de-bonding of
doublers.
4. Examine the tip weight cap for corrosion, cracks, erosion,
and deformation.
5. Examine the following main rotor hub assembly
components for condition and security:
a. Mast nut
b. Trunnion
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