DYNON AVIONICS
1. Servo Arm
2. Flat washer
3. Wave washer
4. Castle nut
5. Cotter pin
6. Shear screw
Required Tools
1. Needle nose
Pliers
2. Torque Wrench
(must be able to read
4.5 in-lb)
3. 1/2IN SAE
Socket
Dynon Servo Arm/Capstan Removal and Replacement
Instructions
If it is necessary to change the arm or capstan on a Dynon autopilot servo, these instructions,
when followed properly, enable the customer to perform this task in the field. If the
customer does not feel comfortable performing these actions, Dynon will be happy to inspect
and/or repair servos as necessary.
Removing Arm/Capstan
Remove the cotter pin from the castellated nut. Note that cotter pins should never be reused;
replace with a new pin. Unthread the castellated nut, remove wave and nylon washers, and
finally remove the arm or capstan. Put all these pieces aside – they will be reused. DO NOT
REMOVE the socket head safety shear screw.
101156-001 – Rev A 1
Fig 1
DYNON AVIONICS
1. Servo Arm
2. Flat washer
3. Wave washer
4. Castle nut
5. Cotter pin
The autopilot safety shear screw should NEVER be removed or adjusted during this
procedure. If the shear screw has broken/damaged and needs replacement, there is
specific documentation available for this purpose at http://docs.dynonavionics.com.
Fig 2
Reassembling the Arm/Capstan Stack
Reverse the disassembly steps to install the remaining hardware. See Figure 2. Assembly order
is:
1. Servo Arm/Capstan
2. Nylon Washer
3. Wave Washer
4. Castle Nut (AN310-5)
5. Cotter Pin (MS24665-210)
Tighten the castellated nut finger tight, and then using a Torque Wrench, tighten until a slot
in the nut lines up with the hole in the shaft for the cotter pin. DO NOT EXCEED 4.5 in-lb (72
in-oz) torque on castle nut. Exceeding this torque specification will affect the yield torque
of the safety shear screw, compromising the safety-enhancing intent of its design.
Install a new cotter pin, MS24665-210, following the standard method of trimming and
bending the pin legs.
Servo arm/capstan rotation should be smooth. No movement should be observed between the
arm/capstan and the attachment disc as described earlier.
101156-001 – Rev A 2