CSP−900RMM−2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 212
Revision 34
05-20-20
Table 205. Airframe Periodic Inspection — Area 5, Powerplant (Cont.)
Registration No. Serial No. Helicopter Total Hours
Model Requirement RMM Section Initial
Fuselage
900 Examine fuselage exterior panels, exterior surfaces of upper deck
fairings and cowls, and structure that is in view for damage,
deterioration, and distortion.
53−30−00
Powerplant
900 Examine left and right inlet panels for condition and security of attach
hardware.
71−60−00
900 Examine left and right engine tubes for fluid leaks, condition, and
security of connections and supports.
71−70−00
79−00−00
900 Examine left and right, aft engine firewall to plenum seals for
condition and security of fire seal clamp.
71−00−00
900 Examine left and right aft engine mounts for condition, indication of
failure, and security of attach hardware.
71−20−00
900 Do the “Engine N
P
Overspeed Test Procedure” in the applicable
Rotorcraft Flight Manual.
Rotorcraft
Flight Manual
If optional inlet particle separator system is installed:
900 Examine left and right engine inlet air particle separator panels for
impact damage, condition, and security of attach hardware.
71−60−00
900 Examine left and right bypass doors and installations for condition
and security of attach hardware.
71−60−00
900 Do the “Inlet Plenum Inspection” and “Inlet Particle Separator
Functional Test”.
71−60−00
Engine Bleed Air
900 Examine bleed air closure plates on engines for correct installation
and security of attach hardware.
75−00−00
If optional heat/defog or inlet particle separator system is installed:
900 Examine bleed air fittings on engines for correct installation and
security of attach hardware.
75−00−00
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