BHT-430-MM-2
5-00-00
26 JAN 2007 Rev. 15 Page 87
5-32. EVERY 600 HOURS OF COMPONENT OPERATION
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
DATE: __________________W.O. _____________________
FACILITY: __________________________________________
HELICOPTER S/N: ___________________________________
REGISTRY NO.: _____________________________________
TOTAL TIME:_______________________________________
SIGNATURE:________________________________________
ENGINE STARTER-GENERATOR
BHT-430-CR&O-V.2
The component manufacturer's recommended
inspection intervals can be followed as an alternate
means of compliance.
Chapter 96 1. Examine the right engine starter-generator brushes for
wear down to the diagonal groove wear indicator. (E2)
Chapter 96 2. Examine the left engine starter-generator brushes for wear
down to the diagonal groove wear indicator. (E1)
PYLON FLUID MOUNTS
Chapter 4
Step 1 and step 2 are airworthiness inspection
limitations.
This inspection applies to part numbers
430-310-200-103 and 430-310-200-105.
This inspection does not apply to part number
430-310-200-107.
1. Examine the left pylon fluid mount as follows: (F5)
a. Remove the left pylon fluid mount.