BHT-206A/B-SERIES-MM-1
5-00-00
30 APR 2013 Rev. 14
Page 53
Export Classification C, ECCN EAR99
d.
Ensure no sealant voids are visible around shields (up
to and including hub assembly 206-011-100-021) or wear
sleeve, strap fittings, and grip closure. Recoat with sealant
(C-308) as required.
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-206A/B/L-Series-
CR&O,
Chapter 64
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.
PROGRESSIVE INSPECTIONS
5-21.
300-HOUR AIRFRAME PROGRESSIVE INSPECTION — EVENT NO. 1 (CONT)
DATA REFERENCE
INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
Summary of Contents for Bell 206A Series
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