CSP−900RMM−2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 262
Revision 34
05-50-00
Table 214. Main Rotor Overspeed, 111 to 114% N
R
, Power On, Conditional Inspection (Cont.)
Registration No. Serial No. Helicopter Total Hours
Model Initial
Ref. RMM
Section
Requirement
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 have signs of contact with felt seal
900 Do a conditional inspection (ref. Table 204). 05−50−00
Flight Controls
900 Examine hydraulic servo actuators:
Examine for too much leakage
Examine piston rods for damage or deformation
Examine for loose fasteners
67−10−00
Powerplant
900 Ref. the applicable manufacturer 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
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
Touch−up all damaged paint and exterior markings, as necessary.
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.
Post Inspection Run−Up (If Applicable)
Ref. the latest revision of the applicable RFM for cockpit check and engine start procedures.
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