TruTrak Vizion C182E Manuel utilisateur

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Appendix F
Vizion PMA Autopilot C182E-C182T Installation
RESTRICTION ON USE, DUPLICATION, OR DISCLOSURE OF
PROPRIETARY INFORMATION
THIS DOCUMENT CONTAINS PROPRIETARY INFORMATION OF
TRUTRAK FLIGHT SYSTEMS, INC. AND MAY NOT BE REPRODUCED, COPIED,
DISCLOSED OR UTILIZED IN ANY WAY, IN WHOLE OR IN PART, WITHOUT THE
PRIOR WRITTEN CONSENT OF TRUTRAK FLIGHT SYSTEMS, INC.
Prepared by
TruTrak Flight Systems, Inc.
Function/Title
Name
Prepared by
Engineering
Zach Williamson
Prepared by
President
Andrew Barker
Checked by
GM
Moss Foster
Approved by
President
Andrew Barker
Make
TCDS
Models
Cessna Aircraft Company
A42EU
F182P, F182Q, FR182
Textron Aviation, Inc.
3A13
182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N,
182P, 182Q, 182R, 182S, 182T, R182,T182, TR182,
T182T

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Table of Contents
1. Document Revision History ................................................................................ 3
2. Cessna 182E-182T Controller / Wiring Harness Installation.................................. 4
2.1. Wiring Harness Materials List................................................................................................................ 4
2.2. Wiring Harness / Controller Mounting Instructions................................................................... 5
3. Cessna 182E-182T Servo Installation..................................................................11
3.1. Roll Servo Materials List..........................................................................................................................11
3.2. Cessna 182E-182T Roll Servo Mounting Instructions..............................................................12
3.3. Pitch Servo Materials List.......................................................................................................................21
3.4. Cessna 182E-182T Pitch Servo Mounting Instructions............................................................22
3.5. Cessna 182E-182T Vizion Roll IPC.....................................................................................................28
3.6. Cessna 182E-182T Vizion Pitch IPC...................................................................................................29
4. Cessna 182E-182T Autopilot Settings.................................................................30
4.1. Lateral Autopilot Settings.......................................................................................................................30
4.2. Vertical Autopilot Settings......................................................................................................................31

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1. Document Revision History
Rev
Description
Pages
Date
IR
Initial Release
30
8-16-18
A
Added BK part numbers, made changes for PV.40
software, made revisions to roll install for P model
on.
33
6-5-19

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2. Cessna 182E-182T Controller / Wiring Harness Installation
2.1. Wiring Harness Materials List
Qty
Description
Part Number
1
Vizion Wiring Harness 30’
8220-033
1
Vizion 2” Controller
OR
Vizion 3” Controller
OR
Vizion Flat Pack Controller
8000-174 or 8000-183
OR
8000-176 or 8000-184
OR
8000-175 or 8000-185
100
MS3367-1-0 Cable Tie
2
Connector D-sub Female 9 Pin Crimp
2100-044
16
Female Socket Crimp Connector D-sub
2100-045
2
Connector Backshell 9 Pin
2100-010
1
Vizion Emergency Level Button Kit
8100-113
1
Vizion Limitations Placard
8300-092
1
5A AP circuit breaker (not supplied)
1
Control Wheel Steering Switch
(not supplied, but MUST be RED in color)
1
AP Master Switch (not supplied)
4
6-32 X 3/8” Instrument mounting screw
(not supplied)
N/A
Various terminals and pins for connection of
power and GPS
N/A
1/8”-27 NPT male fittings and tees for
connecting the A/P pitot and static to the
aircraft systems

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2.2. Wiring Harness / Controller Mounting Instructions
1. Begin by disconnecting the aircraft battery.
2. Select a mounting location for the autopilot controller.
2.1. Consider the overall mounting depth of the controller with pitot, static, and
electrical connections and allow clearance where necessary, especially
surrounding the moving yoke assembly.
2.2. Ensure that mounting location does not require autopilot servo lines to run
near com antenna coax.
2.3. Ensure that there is sufficient space near the autopilot controller to install the
Vizion Limitations Placard (Trutrak P/N 8300-092)
3. Remove the instrument panel and panel overlays as necessary.
4. Remove the seats.
5. Remove the left A-pillar and kick panel trim.
6. Remove carpeting.
7. Wiring harness routing.
7.1. Route the pitch (white) and roll (black) servo harnesses from the controller
to the left side of the panel.
7.2.Route the roll (black) servo harness up the left A pillar and out the leading
edge of the left wing as shown in Figure 2-1, Figure 2-2, and Figure 2-3.
Extend the excess harness out the inspection hole just forward of the

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inboard end of the left aileron. The excess length will be trimmed and the
harness terminated when the roll servo is installed.
Figure 2-1

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Figure 2-2
Figure 2-3
7.3. Route the pitch (white) servo harness down the left kick panel and under the
floor. Continue running the harness to the pitch servo mounting location as
shown in Figure 2-4 and Figure 2-5. The excess length will be trimmed and
the harness terminated when the pitch servo is in place.

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Figure 2-4
Figure 2-5
8. Select appropriate mounting locations for the AP Master, AP Circuit Breaker,
Emergency Level and control wheel steering switches. Connect these items per
the Vizion wiring diagram in the Vizion PMA Installation Guide (TruTrak Doc.
166).
8.1. All items in this step are required to be installed. The AP Master Switch,
AP Circuit Breaker, and Control Wheel Steering switches must be
labeled. The Control Wheel Steering Switch must be RED.

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9. Connect GPS inputs per the Vizion wiring diagram in Vizion PMA Installation
Guide (TruTrak Doc. 166)
10.Conduct pitot / static check of aircraft system before opening any pitot/
static connections!
11. Mount autopilot controller in panel using 4 6-32 X 3/8” screws. Connect wiring
harness and connect pitot and static per Vizion PMA Installation Guide (TruTrak
Doc. 166).

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12. Install Vizion Limitations Placard (Trutrak P/N 8300-092) near the Vizion
autopilot. A sample panel with potential placard location is shown below:
13. Reinstall the instrument panel and panel overlays.
14. Reinstall interior trim.
15. Reinstall carpeting.
16. Reinstall seats.
17. Reconnect battery.
18. Once autopilot settings are confirmed, perform autopilot system test per the
Vizion PMA Installation Guide (TruTrak Doc. 166).
Potential location of
Limitations Placard
Ce manuel convient aux modèles suivants
1
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