BHT-206A/B-SERIES-MM-1
5-00-00
Page 38 Rev. 14 30 APR 2013
Export Classification C, ECCN EAR99
5. Replace removed, damaged, or worn anti-chafing adhesive
tape (C-460) as required.
6. Examine driveshaft cover retaining clips for condition and
security.
Chapter 53 7. Examine horizontal stabilizer for condition and security of
attachment. Verify security of all attachment bolts. Make sure
the vertical through bolts can be rotated. Inspect the inboard rib
for cracks.
8. Inspect the vertical fin attachment support for condition and
damage. Pay particular attention to the vertical fin attachment
points.
9. Examine vertical fin assembly for condition and security.
10. Torque check vertical fin attachment hardware 75 to
95 inch-pounds (8.47 to 10.75 Nm).
Chapter 32 11. Examine vertical fin tail skid for condition, security, and
signs of ground contact.
12. Examine for open drains on lower skin of tailboom and
clear any obstructions.
13. Examine antennas for damage and security.
TAIL ROTOR DRIVESHAFTS
Chapter 65 1. Examine tail rotor driveshaft hanger bearings for excessive
grease leakage and evidence of overheating.
2. Examine hanger bearing support brackets for condition
and security.
3. Examine long tail rotor driveshaft or segmented driveshafts
and aft splined adapter for condition and security. Check aft
splined adapter for adequate lubrication and freedom of
movement.
4. Torque check disc pack coupling fasteners 50 to
70 inch-pounds (5.7 to 7.9 Nm). Apply torque seal after
torquing.
5-18. 100-HOUR AIRFRAME PROGRESSIVE INSPECTION — EVENT NO. 3 (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
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