BHT-430-MM-2
5-00-00
26 JAN 2007 Rev. 15 Page 25
Chapter 53 9. Inspect horizontal stabilizer center area as follows:
a. Remove upper support assembly. Save attaching
hardware.
b. Clean upper surface of stabilizer.
NOTE
Surface must be free of all dirt and residue.
c. With bright light, inspect upper surface for any cracks,
corrosion or working rivets.
d. If no cracks, corrosion or working rivets are located,
install support assembly.
e. Remove lower support assembly. Save attaching
hardware.
f. Clean lower surface of stabilizer.
g. With bright light, inspect lower surface for any cracks,
corrosion or working rivets.
h. If no cracks, corrosion or working rivets are located,
install support assembly.
Chapter 67 10. Remove the aft fuselage access panel. Examine the
control tube, bellcrank and support assembly for corrosion,
mechanical damage and worn bearings and clevises. Make
sure they are correctly attached. (F4)
Chapter 67 and
BHT-430-CR&O-4
11. Remove the tail rotor control tube. Examine the control
tube, nylatron sleeves at the four areas where the tube contacts
the tailboom fairleads and the heat shrink at the two ends of the
control tube. (T1/T2)
Chapter 65 12. Disconnect the tail rotor driveshaft from the transmission
and tail rotor gearbox. Examine each tail rotor driveshaft hanger
assembly as follows: (T1/T2)
a. Rotate the driveshaft by hand and feel for roughness in
the bearing.
SCHEDULED INSPECTIONS
5-15. 600 HOUR/ANNUAL INSPECTION (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
To Next Page
Loading...
