22-30 Flight Control Computer (continued)
B. Installation
1. Turn battery & avionics switches off and pull out AUTOPILOT (5 amp) circuit breaker
at panel.
2. Position 01311-03-11 flight control computer under pilot's seat and install screws
securing computer to D358-1 support assemblies. Tighten screws. Verify security.
3. Remove plugs and connect pitot and static tubes to computer. Perform pitot and
static system leak checks per § 95-10.
4. Connect D323 and D354-4 harness assemblies to computer's J1 PITCH, J2, J3 ROLL,
and J4 receptacles. Install ty-raps securing harnesses as required. Cinch ty-raps until
snug without over-tightening, and trim tips flush with heads. Verify harness security.
5. Verify freedom of flight controls through full travel with and without friction applied.
6. Push in AUTOPILOT circuit breaker (5 amp) at panel. Perform ground checks as
appropriate per § 22-61.
7. Install G702-7 cover assembly under pilot's seat.
22-40 Control Panel
Refer to R66 Illustrated Parts Catalog (IPC) Figure 22-1.
A. Removal
1. Turn battery & avionics switches off and pull out AUTOPILOT (5 amp) circuit breaker
at panel.
2. Loosen radio keys securing 01309-01-01 control panel from avionics tray.
3. Carefully unplug/remove control panel from tray.
B. Installation
1. Turn battery & avionics switches off and pull out AUTOPILOT (5 amp) circuit breaker
at panel.
2. Carefully plug-in/install 01309-01-01 control panel in avionics tray.
3. Tighten radio keys securing control panel to tray. Verify security.
4. Push in AUTOPILOT circuit breaker (5 amp) at panel. Perform ground checks as
appropriate per § 22-61.
Page 22.6 Chapter 22 Autopilot MAY 2015