Eagle ICA-D212-725, Instructions Manual

Page: 43 / 729

ICA-D212-725 (05)
Page 22 of 25
CHAPTER 05 – INSPECTION AND COMPONENT OVERHAUL SCHEDULE (05-00-00)
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COPYRIGHT

2007 BY DART AEROSPACE LTD.
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THIS DOCUMENT IS PRIVATE AND CONFIDENTIAL AND IS SUPPLIED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED FOR ANY PURPOSE OR COPIED OR COMMUNICATED TO
ANY OTHER PERSON WITHOUT WRITTEN PERMISSION FROM DART AEROSPACE LTD.
Revision: 4
Date: 11.06.01
5.13 AFTER OVER-TORQUE
Mech Other
NOTE
Refer to the Bell 212 Maintenance Manual for the After Over-
Torque Inspection requirements. Those requirements must
be supplemented to include the following items
AFTER OVER-TORQUE
Honeywell
Maintenance
Manual T5313B
and T5317
Series 5.13.1 Refer to Honeywell Maintenance Manual T531
3B and T5317 Series for engine overtorque inspection
requirements.
5.13.2 Overtorque inspections in the Bell 212
Maintenance Manual that are required when overtorque
“does not exceed 104%” must be accomplished on the Eagle
Single when overtorque has not exceeded 58 psi.
5.13.3 Overtorque inspections in the Bell 212
Maintenance Manual that are required when overtorque
“exceeds 104% but does not exceed 112%” must be
accomplished on the Eagle Single when overtorque exceeds
58 psi, but does not exceed 62.4 psi:
5.13.4 Overtorque inspections in the Bell 212
Maintenance Manual that are required when overtorque
“exceeds 112%” must be accomplished on the Eagle Single
when overtorque has exceeded 62.4 psi:
When determining the required inspection criteria after an overtorque event use the following information:
100% = 55.7 psi
104% = 58 psi
112% = 62.4 psi