CSP−900RMM−2MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 253
Revision 34
05-50-00
Table 212. Main Rotor Overspeed, 106 to 110% N
R
, Power On, Conditional Inspection (Cont.)
Registration No. Serial No. Helicopter Total Hours
Model Initial
Ref. RMM
Section
Requirement
Main Rotor (Cont.)
900 Examine swashplate assembly:
Examine pitch link lugs for obvious damage, deformation, and
installation of bushings
Make sure there is correct freedom of movement of rotating and
stationary swashplate subassemblies
Make sure there is correct freedom of movement of swashplate
assembly on static mast
62−20−00
900 Examine link assemblies:
Examine for obvious damage and deformation
Examine fasteners for correct installation and looseness
Make sure there is correct freedom of movement
62−20−00
Anti−Torque Assembly
900 Examine fan assembly blades for damage and/or signs of contact
with felt seal.
64−00−00
If fan assembly blades exhibit signs of contact with felt seal
900 Do a conditional inspection in accordance with ”Unscheduled,
Conditional Inspection, Sudden Stoppage, Anti−Torque Fan”.
05−50−00
Powerplant
900 Refer to related manufacturers’ publications for engine inspection
requirements
01−00−00
900 Examine LH and RH engine mounts:
Examine for damage and deformation
Examine fasteners for installation
71−20−00
900 Make sure the engine to transmission alignment is correct 71−20−00
After Inspection
Touch−up all damaged paint and exterior markings, as necessary.
Rotorcraft must not be moved or flown unless cockpit floor, cabin floor, and bag-
gage floor panels are correctly installed. These are stressed panels.
CAUTION
Install all floor and access panels, covers, and trim panels removed or opened for inspection. Do a
check for closure, fit, and tightness. Make sure all loose equipment has been correctly put in
storage.
Do a check of all fluid levels. Fill fluid levels that are low. Make sure the filler caps are correctly
installed and are not loose.
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