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BELL HELICOPTER 430 - Page 182

BELL HELICOPTER 430
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BHT-430-MM-2
5-00-00
Page 152 Rev. 15 26 JAN 2007
b. Visually examine the complete tail boom structure for
distortion, buckles, cracks in the skin and sheared or loose
rivets.
c. Visually examine the pylon support and engine mount
structures for distortion, buckles, cracks, sheared or loose
rivets.
d. If the damage found during step a through step c
cannot be repaired with standard repair procedures, replace the
parts as necessary.
CONDITIONAL INSPECTIONS
5-52. COMPRESSOR STALL OR SURGE (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER

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