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Textron Bell 206L3 - 300-Hour Airframe Progressive Inspection - Event No. 2

Textron Bell 206L3
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BHT-206L3-MM-1
5-00-00
Page 56 Rev. 16 25 FEB 2011
ECCN EAR99
8. Examine particle separator (if applicable) vortex tubes,
ejector tubes, and ejector nozzles for cleanliness, condition, and
security.
9. Examine forward deck drain(s) to ensure absence of
obstruction.
10. Examine antennas for condition and security.
Chapter 67 CONTROLS
1. Examine the following flight control components for signs
of interference, corrosion, wear, mechanical damage and
security:
a. Control tubes.
b. Links.
c. Rod and bearings.
d. Bellcranks.
e. Bellcrank supports.
f. Attaching bolts and nuts.
2. Inspect main rotor pitch links with a 3X magnifying glass for
damage, corrosion and cracks. Give particular attention to
swaged ends at jam nut or inserts.
Chapter 76 3. Examine N
2
control linkages on forward deck for condition
and security. Pay particular attention to the jackshaft assembly
for damage or evidence or twisting.
4. Verify all control tubes and bellcranks for freedom of travel
throughout range.
Chapter 62 SWASHPLATE ASSEMBLY AND MAST
1. Clean swashplate assembly and mast.
2. Disconnect main rotor pitch links from outer ring.
PROGRESSIVE INSPECTIONS
5-22. 300-HOUR AIRFRAME PROGRESSIVE INSPECTION — EVENT NO. 2 (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER

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