CSP−900RMM−2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 202
Revision 35
05-20-10
Table 201. Special Inspection − Hourly (Cont.)
Registration No. Serial No. Helicopter Total Hours
Model InitialRMM SectionRequirement
100 Hour
Transmission and Drive System:
900 Do a check of the main rotor drive plate nut torque at the initial
helicopter 100−hour inspection. Refer to Main Rotor Drive Plate Nut
Torque Check.
63−10−00
900 Deleted. Moved to 1000 Hour Special Inspection.
900 Do the transmission Chip Detector Test. 63−20−00
Anti−Torque Assembly:
900 Deleted.
900 Examine the anti−torque fan blades for damage and defects (ref.
Figure 602 and Table 602, Fan Blade Damage Limits).
64−30−01
900 Examine the counterweights on the pitch horns for correct
installation (ref. Inspection, NOTAR® Fan Blade Assembly).
64−30−01
900 Examine fan hub sleeves for damage (ref. Figure 603, Inspection
Areas for Fan Hub, and Table 603, Fan Hub Damage Limits).
64−30−01
Landing Gear:
900 Examine skid tube abrasion strips for wear and correct installation.
Refer to Skid Tube Assembly Inspection.
32−00−00
900 If ground handling wheels have been attached to Station 203
forward ground handling attachment pins:
Examine skid tube upper surface between the aft ground handling
wheel attach pins. Refer to Skid Tube Assembly Inspection and do
a Fluorescent Penetrant Inspection.
32−00−00
and
CSP−SPM
20−90−00
VSCS:
900 Do the “VSCS Operational Test” or VSCS Check. 67−20−00
or
Rotorcraft
Flight Manual
Hydraulic System:
900 Do the Hydraulic System Operational Test (Aircraft Ground Run) or
Hydraulic System Check (ref. the appropriate Rotorcraft Flight
Manual).
29−00−00
and
Rotorcraft
Flight Manual
Fuel:
900 Do the Fuel Cell Longitudinal Baffle Integrity Test (902 CONFIG).
Do the Fuel Transfer System Functional Test (902 CONFIG).
28−00−00
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