MD Helicopters CSP-900RMM-2, Servicing And Maintenance

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CSP − 900RMM − 2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 209
Revision 35
05-20-10
Table 202. Special Inspection − Calender (Cont.)
Registration No. Serial No. Helicopter Total Hours
Model Initial RMM Section Requirement
1 YEAR (Do a the 1 YEAR requirements in conjunction with the Area Inspections in the ASIP)
Fuel System: Functional Check of Low Fuel Light
900
900 CONFIG −
Do the “Low Fuel Light Functional Test”.
902 CONFIG −
Do the “Fuel Transfer System Functional Test”.
28 − 00 − 00
Fuel System: Fuel Vent System Inspection
900 Do the “Fuel Vent System Inspection”. Examine fuel vent system
components and interconnecting lines for condition and proper
installation.
28 − 00 − 00
Fuel System: Vapor Shroud System Inspection
900 Do the “Vapor Shroud Box, Cover Assembly and Vapor Shroud Hose
Inspection”. Examine vapor shroud boxes, cover assemblies, and
interconnecting hoses for condition and proper installation.
28 − 00 − 00
Landing Gear: Landing Gear Cross Tube Inspection
900 Do the “Forward Crosstube Inspection” and “Aft Crosstube
Inspection”. Make sure that forward and aft cross tube spread is
within allowable maximum limits.
32 − 00 − 00
Fuselage: Cabin Door Latch Mechanism Rigging Verification
900 Do the “Cabin Door Latch Mechanism Rigging Verification” 52 − 00 − 00
Fuselage: Fuselage Internal Structure Inspection
900 Examine cockpit floor substructure and installation for distortion,
corrosion, apparent defects, and security of attachment hardware:
Examine plough beams and attachment components.
Examine FS 106.00 bulkhead assembly and attachment
components.
Examine FS 130.00 bulkhead assembly and attachment
components.
Examine crew seat fittings and attachment components.
53 − 20 − 00
900 Examine FS 155.50 frame assembly and installation for distortion,
corrosion, apparent defects, and security of attachment hardware.
53 − 20 − 00
900 Examine A − Frame assembly and installation for distortion, corrosion,
apparent defects, and security of attachment hardware:
Examine vertical leg and center beam components.
Examine forward mast fitting assemblies.
53 − 30 − 00