CSP−900RMM−2MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 247
Revision 34
05-50-00
Table 210. Transmission and Drive System Overtorque, Conditional Inspection. Both Engines
Operative, Greater Than 8% Engine Torque Differential
Registration No. Serial No. Helicopter Total Hours
Model Requirement
Ref. RMM
Section
Initial
For each single input fault, do the requirements of Table 207, Transmission and Drive System
Overtorque, Conditional Inspection Single Engine Operation.
Do the averaged input portion of the applicable “Both Engines Operative Overtorque
Inspection” (ref. Table 208 900 CONFIG and Table 209 902 CONFIG).
CAUTION
Single Input 136% or Above
900 Replace transmission, all acoustic isolators, and related fasteners. 63−20−00
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.
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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