CSP−900RMM−2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 246
Revision 34
05-50-00
Table 209. Transmission and Drive System Overtorque (902 CONFIG), Conditional Inspection.
Both Engines Operative, 8% Maximum Engine Torque Differential (Cont.)
Registration No. Serial No. Helicopter Total Hours
Model Initial
Ref. RMM
Section
Requirement
Averaged Input 146% and Above (Cont.)
900 If not replaced by single engine torque value, examine input drive
shaft assemblies and fasteners for condition and installation. Make
sure the torque is correct.
63−10−00
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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