BHT-212-MM-1
5-00-00
Page 154 Rev. 16 15 NOV 2018 Export Classification C, ECCN 9E991
ASB 212-02-116
ASB 212-14-150
MAIN ROTOR GRIPS P/N 204-011-121-009 AND P/N
204-011-121-121
Chapter 62 1. Carry out ultrasonic inspection.
2. Any indication of a crack detected in accordance with the
instructions will require the grip to be removed from service and
a serviceable grip installed. If the grip was inspected by a level I
special, the unserviceable grip is to be sent to a facility that has
level II or III ultrasonic capability for further investigation. All
grips that have a crack indication and have been inspected by a
level II or III are to be sent to Bell Helicopter Textron. Refer to
Information Letter IL GEN-04-98 for shipping instructions.
5-36. MAIN ROTOR GRIP ULTRASONIC INSPECTION (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
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