Textron Bell 212 - 5-51. AFTER BLADE STRIKE OR OTHER ROTATING SYSTEM TORQUE SPIKE

BHT-212-MM-1
5-00-00
26 JUN 2013 Rev. 14 Page 197
Export Classification C, ECCN EAR99
CONDITIONAL INSPECTIONS
5-51. AFTER BLADE STRIKE OR OTHER ROTATING SYSTEM TORQUE SPIKE
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
DATE: __________________W.O. _____________________
FACILITY: __________________________________________
HELICOPTER S/N: ___________________________________
REGISTRY NO.: _____________________________________
TOTAL TIME:_______________________________________
SIGNATURE:________________________________________
NOTE
To be accomplished after a main rotor blade or tail
rotor blade strike or any drive system failure that
inhibits free rotation of drive system.
AFTER BLADE STRIKE OR OTHER ROTATING SYSTEM
TORQUE SPIKE
NOTE
If the blade strike or rotating system torque spike is
the result of crash damage or results in crash
damage, all rotating system components shall be
considered unserviceable and non-repairable.
Crash damage is any damage sustained beyond the
scope of that identified in the After Hard Landing
conditional inspection (paragraph 5-50).