Dynon Avionics SkyView HDX User manual

SkyView HDX System
Autopilot Servo Installation Manual
Beechcraft Bonanza P35 –V35BTC
Applicable to serial numbers D-6842 through D-10403
103662-000
Revision B
5/8/2019
Copyright © 2019 by Dynon Avionics, Inc.
Dynon grants third parties’ permission to print this document

Contact Information
Dynon Avionics, Inc.
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Woodinville, WA 98072
Phone: [phone]
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Technical Support Operations: 7:00 AM - 4:00 PM (Pacific Time) Monday - Friday
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Email Support: [email protected]
Fax: [phone]
Web: www.dynoncertified.com
Copyright
©2019 Dynon Avionics, Inc. All rights reserved. No part of this manual may be reproduced, copied, transmitted, disseminated or stored in any
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provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Information in this document is subject to change without notice. Dynon Avionics reserves the right to change or improve its products and to
make changes in the content without obligation to notify any person or organization of such changes. Visit the Dynon Avionics website
(www.dynonavionics.com) for current updates and supplemental information concerning the use and operation of this and other Dynon Avionics
products.

SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
Page | i
Revision History
REV
CHANGE
DATE
APPROVAL
A
Initial Release
5/8/2019
ECO# 323983
B
•Added PN 503560-000 SALES ASSY PMA KIT CLAMP
SERVO CAPSTAN 1/8IN to Section 2 Part callout
tables,
•Revised cascaded Section 2 Part Callout numbers.
•Added Step #6 on Page 12 to detail different (5/32” and
1/8” bridle clamps) installations of roll servo.
Subsequent steps renumbered.
•Revised Figure 8 and added Figure 9 to illustrate
different (5/32” and 1/8” bridle clamps) installations of
roll servo. Subsequent figures renumbered.
•Updated all figures with revised part callout numbers.
•Standardized nomenclature and formatting throughout
doc, added page # callouts to figure # callouts for
installers who prefer using a printed version of
document.
5/8/2019
ECO# 327879

Page | ii
SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
References
DOCUMENT
103272-000 SkyView HDX Aircraft Flight Manual Supplement for STC
102949-003 SkyView HDX Pilot’s User Guide Dynon Document
103261-000 SkyView HDX Installation Manual for AML STC SA02594SE
43.13-1B Acceptable Methods, Techniques, and Practices - Aircraft Inspection and Repair
43.13-2B Acceptable Methods, Techniques, and Practices - Aircraft Alterations
Beechcraft Bonanza V35B Illustrated Parts Catalog D-4866 through D-9068
Beechcraft Bonanza H35 through V35A-TC Illustrated Parts Catalog D-9069 & AFTER
Beechcraft Bonanza 35 Series Shop Manual D-1 through D-10119

SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
Page | iii
Table of Contents
1Introduction.............................................................................................. 1
2Materials ................................................................................................... 2
2.1 Roll Servo Materials ..................................................................................................... 2
2.2 Pitch and Yaw Servo Materials..................................................................................... 3
3Autopilot Servo Mounting Bracket Installation...................................... 5
3.1 Roll Servo Mounting Bracket Installation...................................................................... 5
3.2 Pitch / Yaw Servo Mounting Bracket Installation .......................................................... 6
4Servo Electrical Wiring .......................................................................... 10
5Continued Airworthiness....................................................................... 11
5.1 Roll Servo Removal and Installation........................................................................... 11
5.2 Pitch Servo Removal and Installation......................................................................... 13
5.3 Yaw Servo Removal and Installation.......................................................................... 15
5.4 Servo Calibration Procedure ...................................................................................... 16
5.5 Servo Test Procedure................................................................................................. 17
6Figures.................................................................................................... 18
6.1 Roll Servo Parts and Assemblies............................................................................... 18
6.2 Roll Servo Installation................................................................................................. 21
6.3 Pitch / Yaw Servo Parts and Assemblies.................................................................... 27
6.4 Pitch / Yaw Servo Installation..................................................................................... 31

Page | 1
SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
1 Introduction
This document provides guidance to retrofit the Dynon SkyView HDX System three-axis
autopilot servos into an unmodified Beechcraft Bonanza 35 Series aircraft. Any airplane
configurations that include modifications to the areas where these servos are installed are not
addressed by this document.
Reference Section 5, Continued Airworthiness for autopilot servo removal, installation,
calibration, and test procedures.
The SkyView autopilot servo settings are available for download as a configuration file that is
loaded into the SkyView HDX System. This file configures the autopilot servo performance
settings to meet the applicable certification regulations.

Page | 2
SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
2 Materials
The materials listed below assume installation of the roll, pitch, and yaw servos in an unmodified
aircraft.
2.1 Roll Servo Materials
The materials identified in Table 1 are required to install the roll servo into a Beechcraft Bonanza
35 Series aircraft. The item numbers refer to the Figures in Sections 6.1 and 6.2.
Table 1:Roll Servo Installation Materials
ITEM
DYNON P/N
DESCRIPTION
QTY
1
503406-000
SALES ASSY PMA SV42C
1
2
503672-000
ASSY KIT PMA ACCESSORY SERVO CAPSTAN 5/32IN CONTROL CABLE
1
2-1
→100976-011
AN365-1032A NUT LOCK STL #10-32
6
2-2
→100978-003
AN960-10 WASHER FLAT STL #10
6
2-3
→100981-003
AN3H-6A BOLT HEX #10-32 3/4IN DRILLED HEAD
6
2-4
→103694-000
CLAMP CABLE BRIDLE CAPSTAN 5/32 IN
4
2-5
→101113-000
ASSY BRIDLE CABLE SERVO CAPSTAN
1
2-6
→101670-000
ST2-2 SWAGE STOP FOR 1/16IN CABLE
2
3
503540-000
BRACKET ALUM ROLL SERVO BASE BONANZA V35
1
4
503541-000
BRACKET ALUM ROLL SERVO MOUNT BONANZA V35
1
5
101880-000
AN525-832R8 SCREW PHIL WASHER-HEAD STL CAD PLT #8-32 1/2IN
3
6
101867-004
AN525-10R8 SCREW WASHER HEAD STL CAD PLT #10-32
1
7
100981-000
AN3H-3A BOLT HEX #10-32 DRILLED HEAD
3
8
100979-002
MS35333-39 WASHER LOCK STAR INT STL #10
3
9
100978-003
AN960-10 WASHER FLAT STL #10
4
10
100976-011
AN365-1032A NUT LOCK STL #10-32
1
11
101877-000
RIVETS CHERRY N CCP-42
3
12
503560-000
SALES ASSY PMA SERVO CAPSTAN CLAMP KIT 1/8IN CONTROL CABLE
1
12-1
→103693-000
CLAMP CABLE BRIDLE CAPSTAN 1/8 IN
2
12-2
→100976-011
AN365-1032A NUT LOCK STL #10-32
2

SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
Page | 3
ITEM
DYNON P/N
DESCRIPTION
QTY
12-3
→100978-003
AN960-10 WASHER FLAT STL #10
2
12-4
→100981-003
AN3H-6A BOLT HEX #10-32 3/4IN DRILLED HEAD
2
NOTE: ARROW (→) INDICATES ITEMS PACKAGED WITHIN A SALES ASSEMBLY
2.2 Pitch and Yaw Servo Materials
The materials identified in Table 2 are required to install the pitch servo into a Beechcraft
Bonanza 35 Series aircraft. The item numbers refer to the Figures in Section 6.3 and 6.4.
Table 2:Pitch and Yaw Servo Installation Materials
ITEM
DYNON P/N
DESCRIPTION
QTY
13
503406-000
SALES ASSY PMA SV42C (YAW SERVO)
1
14
503672-000
ASSY KIT PMA ACCESSORY SERVO CAPSTAN 5/32IN CONTROL CABLE
1
14-1
→100976-011
AN365-1032A NUT LOCK STL #10-32
6
14-2
→100978-003
AN960-10 WASHER FLAT STL #10
6
14-3
→100981-003
AN3H-6A BOLT HEX #10-32 3/4IN DRILLED HEAD
6
14-4
→103694-000
CLAMP CABLE BRIDLE CAPSTAN 5/32IN
4
14-5
→101113-000
ASSY BRIDLE CABLE SERVO CAPSTAN
1
14-6
→101670-000
ST2-2 SWAGE STOP FOR 1/16IN CABLE
2
15
503679-000
SALES ASSY PMA SV32C-150 (PITCH SERVO)
1
16
503674-000
ASSY KIT PMA ACCESSORY SERVO CAPSTAN 1/8IN CONTROL CABLE
1
16-1
→100976-011
AN365-1032A NUT LOCK STL #10-32
4
16-2
→100978-003
AN960-10 WASHER FLAT STL #10
4
16-3
→100981-003
AN3H-6A BOLT HEX #10-32 3/4IN DRILLED HEAD
4
16-4
→103693-000
CLAMP CABLE BRIDLE CAPSTAN 1/8 IN
4
16-5
→101113-000
ASSY BRIDLE CABLE SERVO CAPSTAN
1
16-6
→101670-000
ST2-2 SWAGE STOP FOR 1/16IN CABLE
2
17
503542-000
MOUNT PLATE ALUM PITCH SERVO BONANZA V35
1
18
503544-000
BRACKET ALUM MOUNT PITCH SERVO BONANZA V35
1

Page | 4
SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
ITEM
DYNON P/N
DESCRIPTION
QTY
19
503546-000
BRACKET ALUM MOUNT YAW SERVO BONANZA V35
1
20
503550-000
BRACE ALUM ANGLE AFT PITCH/YAW SERVO BONANZA V35B
1
21
503549-000
BRACE ALUM ANGLE FORWARD PITCH/YAW SERVO BONANZA V35B
1
22
503547-000
BRACKET ALUM MOUNT TOP PITCH YAW SERVO BONANZA V35B
1
23
101880-006
AN525-832R10 SCREW WASHER HEAD #8-32
10
24
100978-002
AN960-08 WASHER FLAT STL #8
14
25
100976-007
AN365-832A NUT LOCK STL #8-32
10
26
100981-000
AN3H-4A BOLT HEX #10-32 DRILLED HEAD
8
27
100979-002
MS35333-39 WASHER LOCK STAR INT STL #10
8
28
100978-003
AN960-10 WASHER FLAT STL #10
14
29
103673-006
MS24694-S52 SCREW PHIL 100DEG STL CAD PLT #10-32 21/32IN L
6
30
100976-011
AN365-1032A NUT LOCK STL #10-32
6
31
103676-003
MS35206-244 SCREW PHIL PAN STL CAD PLT #8-32 7/16IN L
4
NOTE: ARROW (→) INDICATES ITEMS PACKAGED WITHIN A SALES ASSEMBLY

SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
Page | 5
3 Autopilot Servo Mounting Bracket Installation
The instructions that follow detail how to permanently install the brackets that mount the roll,
pitch, and yaw servo mounting bracketry into the airplane.
3.1 Roll Servo Mounting Bracket Installation
This section details how to assemble and install the roll servo mounting brackets.
The roll servo base bracket mounts directly to the airplane. The roll servo mount bracket has the
roll servo fastened to it, and it is then is fastened to the base bracket. The roll servo is connected
to the aileron control cables by a bridle cable and bridal cable clamps.
Refer to Section 4 Servo Electrical Wiring for servo wiring information.
Refer to Section 5 Continued Airworthiness to remove or install a roll servo after the bracket
installation is complete.
NOTE: Before installing the roll servo, verify that the aileron flight control cables are
rigged and tensioned according to the manufacturer’s specifications.
3.1.1 Location and Access
The roll servo is located on the left cabin sidewall just forward of the rear spar, approximately
STA187 as indicated in Figure 4 (Page 21).
This location is accessed by removing the front and rear seats, the rear spar cover assembly,
and the left-hand upholstery sidewall. Additionally, it may be necessary to open the left main
landing gear inner gear door to access the wheel well. Refer to the Beechcraft Bonanza 35
Series Shop Manual to accomplish the removal of interior parts and components, as well as the
opening of the inner gear door.
3.1.2 Roll Servo Base Bracket Installation
Complete the following steps to install the roll servo mounting brackets:
1) Remove the 4 fasteners mounting the forward end of the left outboard seat rail to the
forward seat support structure.
2) Remove the 2 fasteners mounting the middle of the left outboard seat rail to the rear
spar carry-through structure.
3) Place the roll servo base bracket as shown in Figure 4 (Page 21) and Figure 5
(Page 22) so that:
a) The aft edge rests on the rear spar carry-through structure,
b) The inboard edge slides between the left outboard seat attach rail and the rail
support structure below,
c) The vertical outboard attach flange contacts the forward side of the sidewall
structure it will attach to,

Page | 6
SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
d) The holes in the roll servo base bracket align with the mounting holes already
located in the structure.
When satisfied with the fit, refer to Figure 5 (Page 22) and Figure 6 (Page 23), and do the
following steps:
1) Install the base bracket using the fasteners removed earlier.
2) Drill three #40 size holes in the structure using the existing pilot holes on the forward
vertical flange as a guide, and temporarily fasten.
3) Drill the #40 holes up to #30 size.
4) Install three 1/8-inch blind rivets into the holes.
3.1.3 Roll Servo Mount Bracket Installation
Refer to Section 5 Continued Airworthiness for instructions on how to:
1) Install the roll servo into the roll servo mount bracket,
2) Install the roll servo mount assembly into the roll servo base bracket (after the roll servo
base bracket installation is complete).
3.2 Pitch / Yaw Servo Mounting Bracket Installation
This section assembles and installs the combined pitch and yaw servo mounting brackets.
The pitch servo and yawservo mounting brackets are fastened together bythe installer to create
the pitch/yaw servo mount bracket assembly. This assembly is then fit and fastened into the
airplane. Then the bracket assembly receives its top bracket and two stabilizing angle braces.
The pitch servo is then fastened to the right-hand pitch servo bracket, and the yaw servo is
fastened to left-hand yaw servo bracket.
Both the pitch and yaw servos are connected to the elevator and rudder control cables by bridle
cables and bridle cable clamps.
Refer to Section 4 Servo Electrical Wiring for servo wiring information.
Refer to Section 5 Continued Airworthiness to remove or install a pitch or yaw servo after the
bracket installation is complete.
3.2.1 Location and Access
The Beechcraft Bonanza 35 pitch and yaw servos are accessed from the baggage area and are
located behind the STA170 access panel, between frames STA179 and STA207, as shown in
Figure 14 (Page 31).
Remove the STA170 access panel according to the Beechcraft Bonanza 35 Series Shop
Manual, to access the pitch/yaw servo installation location.
3.2.2 Pitch/Yaw Servo Mount Bracket Assembly
Reference Figure 15 (Page 32), and accomplish the following steps to create the servo mount
assembly:

SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
Page | 7
1) Fasten the pitch servo mount to the base plate.
2) Fasten the yaw servo mount to the base plate.
3) DO NOT attach the top bracket to the assembly.
3.2.3 Pitch/Yaw Servo Mount Bracket Installation
Accomplish the following steps to locate the servo bracket assembly in the airplane:
1) Holding the assembly sideways so that the base plate is approximately vertical
(Figure 16, Page 33, Step #1), pass the assembly from one side of the control cables
so that the cables enter the space between the two servo mount brackets (Figure 16,
Step #2).
2) Rotate the assembly about the control cables so that the base plate becomes
approximately horizontal (Figure 16, Step #3).
3) Place the assembly on the rivet shop heads mounting the attach flanges of the two
inboard stringers mounted to the belly skin (Figure 16, Step #4).
4) Reference Figure 17 (Page 34) and Figure 18 (Page 35) to locate the assembly,
adjusting it forward or aft as required to meet the following requirements:
a) The assembly shall rest on the lower flanges of the inboard stringers between
approximately 12 and 12.5 inches behind the STA179 frame. Movement within
this range may be necessary to meet all requirements.
b) The base plate shall cover a minimum of three skin to stringer attach fastener
locations on both the left and right side.
c) The base plate shall maintain a minimum edge margin of 0.25 inches from both
the forward and aft edges to the center of the last fastener hole in the row, unless
more than three fasteners are captured by the base plate.
d) If more than three fasteners are captured by the base plate, then the base plate
should maintain a minimum edge margin of 0.25 inches to the center of the
fastener hole in the row from one of the forward or aft edges, but not necessarily
both.
NOTE: It is acceptable to trim material from the forward and aft edge of the base
plate to avoid partial contact with skin/stringer fasteners, providing all the
above requirements have been met.
e) The base plate shall avoid the radius of stringers vertical flange on both the left
and right sides by maintaining a gap of 0.125 inches.
NOTE: It is acceptable to trim material from the left and or right edges of the base
plate in order to meet all the above requirements.
5) When satisfied with the positioning, identify the rivets to be removed from the skin and
stringers to attach the pitch/yaw servo mount assembly to the skin and stringers.
6) Move the assembly clear of the rivet removal area.

Page | 8
SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
7) Drill out the rivets affected by the mount bracket installation.
8) Replace the assembly into its intended position,
9) Using a #30 drill, back drill the base plate using the skin/stringer holes as a guide,
temporarily fastening as you go.
10) Drill the skin/stringer/base plate holes up to the final hole size of #21.
11) Disassemble and deburr the newly drilled holes in all parts.
12) Reassemble the parts, and permanently fasten the assembly to the skins and stringers
as shown in Figure 19 (Page 36).
3.2.4 Pitch/Yaw Servo Mount Stabilization Angle Bracket Installation
Referencing Figure 23 (Page 40), complete the following steps to install the forward angle
bracket:
1) Temporarily fasten the forward angle brace to the pitch servo mount
2) Allow the forward/lower end of the angle to rest on the right-hand inboard stringer
attach flange.
3) Identify the best fastener to remove that will attach the bracket maintaining minimum
hole edge margin of 0.25 inches from the center of the fastener hole.
4) Drill out the rivet.
5) Using a #30 drill, back drill the base plate using the skin/stringer holes as a guide.
6) Drill the skin/stringer/angle bracket holes up to the final hole size of #21.
7) Fasten the forward end of the angle to the skins and stringers as shown.
Referencing Figure 23 (Page 40), complete the following steps to install the aft angle bracket:
1) Temporarily fasten the aft angle brace to the pitch servo mount
2) Allow the aft/lower end of the angle to rest on the right-hand inboard stringer attach
flange.
3) Identify the best stringer attaching rivet to remove that will attach the bracket while
maintaining minimum hole edge margins of 0.25 inches.
4) Drill out the rivet.
5) Using a #30 drill, back drill the base plate using the skin/stringer holes as a guide.
6) Drill the skin/stringer/angle bracket holes up to the final hole size of #21.
7) Fasten the forward end of the angle to the skins and stringers as shown.
Refer to Section 5.2 Pitch Servo Removal and Installation for instructions on how to install the
pitch servo into the pitch servo mount bracket (after the pitch servo mount bracket installation is
complete).

SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
Page | 9
Refer to Section 5.3 Yaw Servo Removal and Installation for instructions on how to install the
yaw servo into the yaw servo mount bracket (after the yaw servo pitch servo mount bracket
installation is complete).

Page | 10
SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
4 Servo Electrical Wiring
For the complete wiring and network configuration instructions, refer to the following documents:
•Dynon SkyView HDX System Installation Manual for AML STC SA02594SE; Document
103261-000, Section 11 Autopilot Servo Installation, Configuration, and Calibration.
•Wiring Diagram Typical, HDX Dual Display; Document 103488-000
Route the servo electrical harnesses through the airframe structure as appropriate. Take
precautions to prevent the servo harnesses from chafing or interfering with the aircrafts flight
controls or other moving components.
NOTE: Servo power and the autopilot disconnect circuits are required to be separate
from the signal and power circuits provided over the SkyView network. The servos should
receive power from a common power source with circuit protection sized for the loads
associated with all servos.
Terminate the servo network electrical harnesses with a D9 connector shell with female pins.
Terminate the servo electrical harness pigtails with the mating D9 connector.
Dynon provides the SV-NET-SERVO Network Autopilot Servo Cable Kit (p/n 101342-020) to aid
in wiring the servos. Contact Dynon Sales for more information.
NOTE: Power for all servos must be controlled by a switch prominently mounted on the
instrument panel. This provides the pilot the ability to quickly turn off power to the servos
should it be needed.

SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
Page | 11
5 Continued Airworthiness
5.1 Roll Servo Removal and Installation
5.1.1 Location and Access
The roll servo is located on the left cabin sidewall just forward of the rear spar approximately
STA187 as indicated in Figure 4 (Page 21).
This location is accessed by removing the front and rear seats, the rear spar cover assembly,
and the left-hand upholstery sidewall. Additionally, it may be necessary to open the left main
landing gear inner gear door to access the wheel well. Refer to the Beechcraft Bonanza 35
Series Shop Manual to accomplish the removal of interior parts and components, as well as the
opening of the inner gear door.
5.1.2 Roll Servo Removal
The roll servo attaches to the servo mounting bracket. The servo mounting bracket in turn
attaches to the servo base bracket which is permanently attached to the airframe. Follow these
steps to remove the roll servo mounting bracket from the roll servo base bracket:
1) Remove the bridal cable clamps from the aileron control cables. It is recommended
that you mark the location of the cable clamps for ease of re-installation.
2) Disconnect the D9 harness connector from the servo.
3) Remove the fasteners securing the roll servo mounting bracket assembly to the base
bracket (Figure 7, Page 24) and retain for re-installation.
4) Remove the roll servo mounting bracket assembly from the airplane.
To remove the roll servo from the roll servo mount bracket assembly:
1) Remove the safety wire and unfasten the hardware securing the servo to the roll servo
mounting bracket (Figure 3, Page 20),
2) Remove the servo from the mount bracket.
5.1.3 Roll Servo Installation
Prepare the airplane for the servo installation by:
1) Securing the ailerons and/or yoke in the neutral position.
2) Ensuring that the aileron control cables in the areas that the bridal cable clamps will
attach are clean and free of dirt and grease before installing cable clamps.
To install the SV42C Servo into the roll servo mount bracket (Figure 3, Page 20), complete the
steps that follow:
1) Place the servo into the mount bracket.
2) Install the hardware.
3) Torque the servo bolts to between 15 to 20-inch pounds.

Page | 12
SkyView HDX System Autopilot Servo Installation Manual - Beechcraft Bonanza P35 –V35BTC, Revision B
4) Safety wire the servo bolts.
Complete the following steps to load the bridal cable onto the servo capstan:
1) Rotate the servo capstan so that the swage hole is facing directly aft.
2) Pass one end of the bridal cable underneath one of the cable guard flanges so that
the cable will sit in the center groove.
3) Set the cable swage into its accompanying hole in the pulley and pass the other end
of the bridle cable under the opposite flange.
4) Feed both cable ends around the pulley and underneath the next set of cable guard
flanges following the grooves. When complete, the cable will have wrapped the
capstan one complete turn.
To install the roll servo mount bracket assembly, as shown in Figure 3 (Page 20) and Figure 7
(Page 24), complete the steps that follow:
1) Holding the capstan so that the hole for the swage cable remains facing aft, insert the
roll servo mount bracket assembly up and into the roll servo base bracket from below.
2) Align the base and mount bracket mounting holes, and then fasten with hardware.
3) Assemble clamps onto the cables and position, as shown in Figure 8 (Page 25). The
grooves in the cable clamps are designed to work with the provided bridle cable
diameter (small groove) and aircraft control cable (large grooves).
4) The outboard bridal clamp installation area is in the left main gear wheel well, accessed
via the left main gear inner door.
5) The inboard bridal clamp installation area is near the turnbuckle connecting the left
aileron balance cable with the center aileron balance cable.
6) If this is a new installation, consider the following:
a. If the bridal cable can be clamped to the aileron balance cable inboard of the
balance cable turnbuckle, install the bridal cable to the center balance cable using
the 1/8” bridal cable clamp, as shown in Figure 8 (Page 25).
b. If the bridal cable can be clamped to the aileron balance cable outboard of the
balance cable turnbuckle, install the bridal cable to the center balance cable using
the 5/32” bridal cable clamp, as shown in Figure 9 (Page 26).
7) If this is a reinstallation, locate the clamps at the locations marked during removal.
8) The capstan cables should be tensioned to 15 ± 2 pounds.
9) Secure the cable clamp bolts and torque to 35 ± 5-inch pounds.
10) Verify full travel of the aileron using the control yoke. The bridle clamps must not
contact cable pulleys or structure during the entire travel.
11) The capstan should never rotate more than 150 degrees in either direction from
neutral.