CSP−900RMM−2MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 229
Revision 28
05-20-50
INSPECTION 7 − TAIL
Table 208. Inspection 7 − Tail (Area 7)
Registration No. Serial No. Helicopter Total Hours
Model Requirement RMM Section Initial
900 Make sure you comply with applicable Special Inspections (Calendar)
for Area 7 and make entries in Log Book.
05−20−10
General
900 Fully clean helicopter as necessary before you start inspection. CSP−SPM
20−20−00
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 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
Empennage
900 Inspect empennage attach frames for damage, condition, and
security of attach hardware.
53−40−00
900 Inspect horizontal stabilizer:
attach frames for damage, condition, and security of attach
hardware
elastomeric damping spring for damage, condition, and security of
attach hardware.
53−55−00
900 Inspect upper and lower endplates:
attach hardware for security
for incorrect movement (wiggle).
53−55−00
900 Inspect tailboom bumper for deformity, condition, and security. 53−40−00
If horizontal damping spring component time is 2000 hours or greater:
900 Do the “Elastomeric Damping Spring Condition − Verification Test”. 53−55−00
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