97-50 Avionics for R66 S/N 293, 520, 522, & Subsequent
97-51 Cyclic Grip Assembly
Refer to R66 Illustrated Parts Catalog (IPC) Figures 67-1 & 67-9.
A. Description of New Features
The angle of the pilot’s cyclic grip can be adjusted fore and aft relative to the cross
tube. The most forward position provides the most control clearance at aft cyclic.
B. Grip Angle Adjustment
1. Loosen cap screws securing pilot's cyclic grip, block assembly, and bar to grip
weldment.
2. Rotate grip about weldment to desired angle. Special torque cap screws to 40 in.-lb.
C. Removal and Installation
Refer to § 67-12 for cyclic grip assembly removal and installation procedures.
D. Schematic
Refer to Figure 98-1 for F024 electrical system schematic.
97-52 Aspen EFD Electronic Flight Instrument System (EFIS) Installations
Refer to § 95-80 for Aspen EFD EFIS Installations.
A. Schematic
Refer to Figure 98-16 for Aspen EFD500H Display Installation electrical schematic.
Refer to Figure 98-17 for Aspen EFD1000H Display Installation electrical schematic.
MAY 2015 Chapter 97 Avionics Page 97.17
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