CSP−900RMM−2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 256
Revision 34
05-50-00
Table 213. Main Rotor Overspeed, 111 to 114% N
R
, Power Off, 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 damage, deformation, 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 damage and deformation
Examine fasteners for damage or deformation
Make sure there is correct freedom of movement and installation of
bearings
62−20−00
900 Examine mixer assembly:
Examine drive link lugs for damage or deformation
Make sure there is correct freedom of movement
Examine mixer pivot support assemblies for damage, deformation,
and installation of hardware
62−20−00
Transmission and Drive System
900 Examine anti−torque fan drive shaft assembly:
Examine surface along entire length of center section for removal
of black anodize, scratches, and signs of contact with surrounding
components.
Examine flanges for damage, deformation, and installation of
fasteners
Examine flexible couplings for scratches, cracks, and deformation
of diaphragms
Examine transmission output flange for damage or deformation
63−10−00
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 show 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