# STC SA00306BO

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aerodyme Corp, United States
- Description: Change the horizontal stabilizer angle of incidence in accordance with Aerodyme Installation Instructions AD1225-01, Revision 1, dated December 15, 2010, or later FAA approved revision.
- Applied: December 30, 2008
- Status date: January 3, 2011
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A12SO](https://openairdocs.org/tcds/A12SO)
- Certificate PDF: https://openairdocs.org/files/sha256/cd/76/cd76b9b05ea728fd77c097768f8317663831d567c8bc60700945e0029c3bda3f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4D4386974282659E8625783F007BCBE7.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00306BO

## ADs that name it (0)

None.

## Approved models (8)

- CPAC Inc. 112 ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- CPAC Inc. 112B ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- CPAC Inc. 112TC ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- CPAC Inc. 112TCA ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- CPAC Inc. 114 ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- CPAC Inc. 114A ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- CPAC Inc. 114B ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- CPAC Inc. 114TC ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Part 23 of the Federal Aviation Regulations. (See Type Certificate Data Sheet No. A12SO for complete certification basis)

Change the horizontal stabilizer angle of incidence in accordance with Aerodyme Installation Instructions AD1225-01, Revision 1, dated December 15, 2010, or later FAA approved revision.

1. FAA Accepted Instructions for Continued Airworthiness, AD1226-01, Revision 2, dated December 15, 2010, or later FAA accepted revision is required for this modification.

2. The installer must determine whether this design change is compatible with previously approved modifications.

3. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

Aerodyme Corporation 274 Valley Road South Burlington, VT 05403 A12SO Make : CPAC, Inc.

Model : 112, 112B, 112TC, 112TCA, 114, 114A, 114B, 114TC Date of application : December 30, 2008

Date of issuance : January 03, 2011

Original Signed By:

Mary Ellen A. Schutt ( Signature) Mary Ellen A. Schutt, Manager, Airframe and Administrative Branch Chicago Aircraft Certification Office

( Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES Number

## Every issue (1)

- January 3, 2011: Issued, Current. [certificate](https://openairdocs.org/files/sha256/cd/76/cd76b9b05ea728fd77c097768f8317663831d567c8bc60700945e0029c3bda3f)

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