ICA-D212-725 (05)
Page 20 of 25
CHAPTER 05 – INSPECTION AND COMPONENT OVERHAUL SCHEDULE (05-00-00)
COPYRIGHT
2007 BY DART AEROSPACE LTD.
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
5.11
AFTER BLADE STRIKE OR OTHER ROTATING SYSTEM TORQUE SPIKE
Data Reference
Inspection Task Description
Initial
Mech Other
NOTE
Refer to the Bell 212 Maintenance Manual for the After Blade
Strike or other rotating torque spike Inspection requirements.
Those requirements must be supplemented to include the
following items
AFTER SUDDEN STOPPAGE – POWER ON OR OFF
BHT-205A1-
CR&O
TB 205-82-45
5.11.1
Remove and inspect main driveshaft visually. If
evidence of yielding or deformation is noted, scrap driveshaft
assembly and attaching bolts. If no visual evidence of
damage is detected, perform an overhaul evaluation. Make
an entry in component record to show reason for removal
was sudden stoppage.
Honeywell
Maintenance
Manual T5313B
and T5317
Series
5.11.2
Inspect engine in accordance with Honeywell
Maintenance Manual T5313B and T5317 Series.
Содержание ICA-D212-725
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