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Size Determination and Adjustment 
Refer to Sizing Guide (C) to determine wing positioning. Detach 

Pull Tab, lift Velcro Connnector, slide wing in or out to adjust. 

Press down Velcro Connector. Repeat on opposite wing panel.

Adjust Height
With brace donned (1) Separate base of ThoraCare 

Support (2) Adjust upward or downward so that top 

center of ThoraCare support aligns at T3/scapular spine 

level

Customize for waist to hip disparities: Follow procedures from 

section 2.1-2 to release wing. Angle wings to up or down to 

address disparities and pendulous abdomen.

2.0 SIZING

2.1

2.2

2.3

PULL

TAB

VELCRO

CONNECTOR

WING

(1)

(2)

(3.1) When removing the brace, always replace Pull Tabs  

B

  to ready position

(3.2) Lay brace on a flat surface then pull both Wings   

A

  outward to reset the tightening mechanism. 

Pull downward on straps to 

tighten shoulder harness.

1

2

L

R

Detach pull tabs and adjust 

compression by pulling forward and 

re-attaching the pull tabs to the front 

of the brace.

Removing Brace:

Loosen shoulder straps, detach pull tabs from front of brace and re-attach laterally. Separate wings and slide brace off over 

the shoulders. Reset brace.

3.0 Reset

3.1

3.2

3.3

3.4

3.5

3.7

3.6

3.0 Donning/Doffing

First loosen the shoulder straps, don brace over the 

shoulders.

Adjust “ThoraCare” strap up or down to accommodate larger 

patients. Position brace to desired height (T-3 / scapular spine level).

(1) Wrap left wing to align with 

medial  line of abdomen. 

(2) Wrap right wing and attach at 

mid-line.

B

B

A

A

4.0 Customizations

  (Customizations are to be carried out by a medical professional with expertise)

              

Wing Panel Customization:

(1) Open wing pocket. (2) Remove and customize the felt wing panels and Rigid Interior shells (3)

            Interior Rigid Shell Customization:

Posterior shells can be heat modified, trimmed and /or custom contoured to create the appropriate support and 

height for the patient, Utilize and modify both shells or 1 shell.

4.1

4.1

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