CSP−HMI−2
MD Helicopters, Inc
.
MAINTENANCE MANUAL
05−20−00
Page 1
Revision 39
Form HOE005 (Rev 5/04)
CONTINUED AIRWORTHINESS
100
−
HOUR OR ANNUAL INSPECTION CHECKLIST
1. 100
−
Hour or Annual Inspection
This check sheet is designed to be used when
performing 100−Hour or Annual inspections as
defined under FAR, Part 43, Appendix D. This
checklist, when completed, should be kept as a
permanent part of the helicopter’s records.
Adherence to Maintenance Manual informa-
tion is required, and the manual should be
consulted when using the checklist.
NOTE:
D
The Chap/Sect column of the following
table is for reference unless a specific in-
spection requirement is called out. If
there is only two numbers in the column,
it refers to the Chapter. If there is three
numbers, it refers to the Section the in-
spection is found.
D
Refer to applicable Rolls−Royce engine in-
spection check list for required engine
maintenance.
Table 1. 100
−
Hour or Annual Inspection
Registration No.
Serial No.
Helicopter Hours
Torque Events
Model
Requirement
Chap/Sect Initial
GENERAL
ALL
Thoroughly clean helicopter and engine prior to start of inspection.
20
ALL
Remove trim panels, covers and access panels as necessary.
52
−
50
−
00
ALL
Ensure all placards and markings are installed.
11
−
00
−
00
ALL
Ensure compliance with component mandatory retirement schedule.
04
−
00
−
00
ALL
Calculate and record TE’s or RIN’s, of all affected components, in Table 2.
04
−
00
−
00
ALL
Ensure compliance with component overhaul schedule.
05
−
10
−
00
ALL
Ensure compliance with all applicable airworthiness directives, service
bulletins and special inspections.
N/A
ALL
Review aircraft maintenance records for recorded discrepancies and correct
discrepancies as applicable.
N/A
ALL
Refer to related manufacturer’s publications for detailed requirements on
inspection of engine, starter/generator, battery and all installed STC
equipment.
01
−
00
−
00
EXTERIOR
ALL
*
Air intake for cleanliness and foreign matter.
*
Visible portion of engine compressor inlet for foreign object damage.
71
CAUTION:
Ensure that compressor cover is installed to prevent FOD.
ALL
Engine air plenum chamber for:
*
Damage and cleanliness.
*
Wear and security of internal components.
*
Particle separator mounting structure for cracks or damage.
71
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