BHT-206L4-MM-1
5-00-00
25 FEB 2011 Rev. 13 Page 49
ECCN EAR99
d. Ensure no sealant voids are visible around shields or
wear sleeve, strap fittings, and grip closure. Recoat with sealant
(C-308) as required. On main rotor hub assemblies up to and
including P/N 206-011-100-025, coat the remaining exposed
fillet radius and repaired surfaces with a film of corrosion
preventive compound (C-101).
ZONE 2 — TAIL ROTOR ASSEMBLY
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 64 TAIL ROTOR ASSEMBLY
1. Clean tail rotor blades to maintain visibility of warning
stripes.
BHT-206L-CR&O 2. Examine the following tail rotor hub assembly components
for condition and security of attachment:
a. Yoke
b. Pitch horns
c. Trunnion and trunnion caps
d. Counterweight hardware
Chapter 64 3. Examine tail rotor blades as follows:
a. Tip block rivets for damage, corrosion, erosion, and
looseness.
b. Skin for bulges, nicks, dents, scratches, or other
damage.
c. Deformed or cracked skin in the area of the chordwise
weights.
d. Leading edge for erosion, nicks, dents or scratches.
5-21. 300-HOUR AIRFRAME PROGRESSIVE INSPECTION — EVENT NO. 1 (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
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