CSP−900RMM−2MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 219
Revision 28
05-20-50
INSPECTION 4 − LANDING GEAR
Table 205. Inspection 4 − Landing Gear
Registration No. Serial No. Helicopter Total Hours
Model Requirement RMM Section Initial
900 Make sure you comply with applicable Special Inspections (Calendar)
for landing gear area and make entries in the Rotorcraft Log Book.
05−20−10
General
900 Fully clean helicopter as necessary before you start inspection. CSP−SPM
20−00−00
900 Refer to related manufacturers’ publications for detailed necessary
inspection of engines, starter/generators, battery and all installed STC
and optional equipment.
01−00−00
900 Examine the aircraft maintenance records for aircraft discrepancies
and correct as necessary.
N/A
900 Examine Integrated Instrument Display System (IIDS) Exceedance
Log Menu and Fault Log Menu. Record and correct discrepancies as
necessary. (NOTE: Logs may be viewed on the IIDS or refer to
GBMC User Guide for complete download and save of IIDS data).
95−30−00
900 Make sure you comply with component mandatory retirement, refer to
Airworthiness Limitation Schedule and make entries in Rotorcraft Log
Book.
04−00−00
900 Make sure you comply with component overhaul, refer to Overhaul
Schedule and make entries in Log Book.
05−10−00
900 Make sure you comply with all applicable Airworthiness Directives
and service bulletins and make entries in Log Book.
N/A
900 Make sure all placards and markings are installed. 11−00−00
900 Remove trim panels, covers, and access panels as necessary. 06−00−00
Landing Gear
900 Inspect forward and aft cross tubes, fuselage attach fittings, and
saddle clamps for damage, indication of failure and condition:
inspect saddle clamp pads for too much extrusion and attach
hardware for security.
32−00−00
900 Inspect side stops for damage and condition. Visually inspect:
attach hardware, adjust bolts, and stop pads for condition and
security
bonding jumpers for condition and correct mechanical connection.
32−00−00
900 Inspect forward spacer fittings for condition, indication of failure, and
security of attach hardware.
32−00−00