5-45 100-Hour / Annual Maintenance and Inspection [3 of 25 Pages]
CONSOLE (continued)
Tail Rotor Pedal Bearing Block Supports:
Examine accessible portion with inspection light and mirror. Inspect both vertical sheet
metal supports inside lower console and verify no cracks. Pay particular attention to area
near NAS6603-13 bolts. Replace any cracked support prior to flight.
Tail Rotor Controls:
Examine accessible portion with inspection light and mirror. Inspect tail rotor control
components for obvious defects. Verify operating clearance.
Cabin Heater Hose:
Inspect condition. Verify no collapsed areas or chafing. Verify hose clamp and hose
security.
Copper Bus Bars:
Inspect condition. Verify no corrosion or bends in bus bar. Verify bus bar security and
isolation from surrounding structure.
Wiring:
Inspect condition. Verify no loose, chafed, or broken wires or terminals. Verify
neatness, proper routing and installation, and security.
Fasteners & Torque Stripes:
Inspect condition. Verify proper installation and security of fasteners. Renew
deteriorated torque stripes per Figure 5-1.
Close & Secure:
Verify foreign objects are removed. Verify equipment security and cleanliness of
interior. Close console and verify security.
PILOT-SIDE CONSOLE (Optional equipment)
Pilot Avionics Support Weldment:
Inspect condition. Verify no significant nicks, scratches, or dents on console shell.
Verify no cracks in welds. Verify weldment mounting security.
CIRCUIT BREAKER PANEL
CAUTION
Ensure BATTERY switch is turned off while circuit breaker panel
is open.
Panel Cover:
Inspect condition. Verify no damage to nutplates and rails in panel interior. Verify
marking legibility.
Fuses and Fuse Holders:
Inspect condition. Verify security and no corrosion. Verify correct fuse installation.
Circuit Breakers:
Inspect condition. Check airworthiness directive applicability. Verify proper installation
and security.
SEP 2012 R66 Maintenance Manual Chapter 5 Inspection Schedule Page 5.15
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