CSP−900RMM−2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 226
Revision 34
05-50-00
Table 204. Anti−Torque Fan Sudden Stoppage, Conditional Inspection (Cont.)
Registration No. Serial No. Helicopter Total Hours
Model Initial
Ref. RMM
Section
Requirement
Flight Controls
900 Examine diverter plate assembly for FOD damage. 67−20−00
900 Do an operational test of directional flight controls:
Do a test with lower access panels removed and fan assembly not
installed
Make sure the movement of diverter plate assembly is correct
67−10−10
900 Examine thruster:
Examine interior for FOD damage
Examine airfoils of thruster cascade for FOD damage
Examine opening and interior of rotating cone for FOD damage
67−20−10
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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