BHT-212-MM-1
5-00-00
26 JUN 2013 Rev. 14 Page 45
Export Classification C, ECCN EAR99
TAIL ROTOR FLIGHT CONTROL ACTUATOR
1. Tail rotor hydraulic actuator for leaks and security of
attachment, mechanical damage, corrosion, and bearings and
linkages for looseness.
Chapter 71 POWER PLANT
Every third 100 hour inspection (300 hours) or 12 months:
If applicable, refer to BHT-212-SI-96 for installation of
adjustable seals or refer to Chapter 71 for seal
adjustment.
ASB 212-10-137 1. Inspect the left-hand and right-hand engine air inlet
cowlings for gaps between the lower surface of the cowling
firewall and the mating horizontal engine firewall.
Chapter 71 LEFT POWER SECTION
Refer to Pratt & Whitney Canada PT6T-3/-3B
Maintenance Manual for engine inspection
requirements.
Every third 100 hour inspection (300 hours) or 12 months:
— Detailed Visual Inspection
1. Ignition leads for corrosion, chafing and security.
2. Chip detectors for debris.
— Restoration
1. Clean chip detectors.
— Functional Check
1. Test chip detectors electrical circuits.
5-9. 100 HOURS/12 CALENDAR MONTHS — PART A (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
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