CSP−HMI−2
MD Helicopters, Inc
.
MAINTENANCE MANUAL
05−20−00
Page 11
Revision 39
Form HOE005 (Rev 5/04)
Hour or Annual Inspection (Cont.)
Registration No.
Serial No.
Helicopter Hours
Torque Events
Model
Initial
Chap/Sect
Requirement
ALL
Install or close all stressed panels, covers and trim panels removed or
opened for inspection. Check closure, fit and security. All loose equipment for
proper stowage.
52
−
50
−
00
CAUTION:
Helicopter must not be flown unless controls access panel and fuel cell access panels in cargo
compartment are securely installed. These are stressed panels.
POST INSPECTION RUN UP
See applicable Pilot’s Flight Manual for cockpit check and engine starting procedures. For troubleshooting
procedures, refer to applicable section of this manual.
100
−
HOUR OR ANNUAL INSPECTION CERTIFICATION
It is certified that this helicopter has been thoroughly inspected as required by FAR, found to be airworthy, and
appropriate entries made in the helicopter log book. It is further certified that the helicopter conforms to FAA
specifications, that all FAA Airworthiness Directives and Manufacturer’s Service Notices and Maintenance
Manual data have been complied with, and the helicopter records are in proper order
Signature
Rating Type or Certificate No.
Date
2. Retirement Index Numbers Attachment
Table 2 is to be used for calculating and
recording the Retirement Index Number (RIN)
or Torque Events (TE) of components that are
affected by Torque Events (TE).
This record of RINs/TE’s should be kept as a
permanent record.
Refer to Section 04−00−00 for components
requiring calculation of RIN’s/TE’s and
information pertaining to calculation of
RIN’s/TE’s.
Component must be scrapped when it reaches
1,000,000 RIN’s or maximum TE’s (Ref. Sec.
04−00−00).
Table 2. Permanent Record of Retirement Index Numbers/Torque Events
Component
Part No.
Serial No.
Hours
TE’s
RIN’s
Signature
