BHT-430-MM-2
5-00-00
Page 74 Rev. 15 26 JAN 2007
Chapter 67 and
BHT-ALL-SPM
19. Examine the cyclic and collective shaft assemblies and
control tubes installed on the roof for loose bearings, wear,
corrosion or mechanical damage. Make sure they are correctly
attached. (F5/F6)
NOTE
Examine inspection window(s) and sight glass(es)
for cracking and discoloration. If either of these
conditions are present the part must be removed and
replaced prior to returning helicopter to service.
Chapter 29 20. Examine the hydraulic lines for leaks. Examine the color
and level of the fluid in the PC-1 system and PC-2 system
reservoirs. Examine the module pressure and return filters for
impending bypass indication. Make sure that the flexible hoses
are in good condition and do not show signs of chafing. (F5/F6)
BHT-430-CR&O-2 21. Inspect hydraulic actuator support attaching nuts for proper
torque. (R1)
Chapter 53 22. Remove the fairing cover plate(s) and examine the wing(s)
to fuselage attachment points for corrosion, looseness and
damage. Check torque of attaching bolts/nuts.
SCHEDULED INSPECTIONS
5-26. PROGRESSIVE INSPECTION — EVENT 11 (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
To Next Page
Loading...
