# STC SR00112BO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Outerlink Corporation, United States
- Description: Installation of  either the OuterLink Corporation CP-2 or  CP-3i SATCOM System in accordance with OuterLink Corporation Master Document List No. D000-0042, Revision N, dated August 19, 2009, or later FAA-approved revision.
- Applied: August 11, 1999
- Status date: March 29, 2023
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H1NE](https://openairdocs.org/tcds/H1NE)
- Certificate PDF: https://openairdocs.org/files/sha256/4f/9f/4f9f8aeac8a943bbd7e1cec59e3bd5b89adf268ffc6e123f601077823afc4452
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110351678420230406133202.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00112BO

## ADs that name it (0)

None.

## Approved models (3)

- Sikorsky Aircraft Corporation S-76A ([TCDS H1NE](https://openairdocs.org/tcds/H1NE))
- Sikorsky Aircraft Corporation S-76B ([TCDS H1NE](https://openairdocs.org/tcds/H1NE))
- Sikorsky Aircraft Corporation S-76C ([TCDS H1NE](https://openairdocs.org/tcds/H1NE))

## 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.

Number SR00112BO

FAA Form 8110-2 (03/21) SUPERSEDES PREVIOUS EDITION Page 1 of 3 This certificate issued to:

Outerlink Corporation 150 Baker Avenue Ext., Suite 302 Concord, MA 01742-2199 Part 29 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: H1NE Make: Sikorsky Aircraft Corporation Model: S-76A, S-76B, S-76C

Installation of either the OuterLink Corporation CP-2 or CP-3i SATCOM System in accordance with OuterLink Corporation Master Document List No. D000-0042, Revision N, dated August 19, 2009, or later FAA-approved revision.

1. OuterLink Corporation, Rotorcraft Flight Manual Supplement No. D000-0048 for Sikorsky Aircraft Corporation Models S-76A, S-76B, S-76C Helicopter, Revision E, dated October 1, 2009, or later FAA-approved revision, is required with this modification.

2. Instructions for Continued Airworthiness (ICA), OuterLink Document No. D000-0050, Revision 5, dated March 12, 2009, or later FAA-accepted revision shall be made available to the operator at the time of installation. (continued on Page 3 of 3)

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

Date of Application: August 11, 1999 Date reissued: April 12, 2000; August 18, 2004;

August 5, 2011; March 29, 2023

Date of Issuance: January 19, 2000 Date amended: February 8, 2002; July 22, 2003;

October 1, 2009

Signature Nicholas Faust

Manager, Boston Aircraft Certification Office Title

Number SR00112BO

FAA Form 8110-2 (03/21) SUPERSEDES PREVIOUS EDITION Page 2 of 3

To (Name and address of transferee) Name:

Address (Number and Street, City, State, and ZIP Code):

From (Name and address of grantor) Name:

Address (Number and Street, City, State, and ZIP Code):

(Continuation Sheet) Number SR00112BO

FAA Form 8110-2 (03/21) SUPERSEDES PREVIOUS EDITION Page 3 of 3 Effective Date: August 5, 2011

Limitations and Conditions: (continued from Page 1 of 3)

3. Compatibility of this design with previously approved modifications must be determined by the installer.

4. This is a non-interference STC. The modification has not been evaluated to check its proper operations for its intended function.

5. The installation described by this STC data illustrates provisions (connection stubs) to allow the OuterLink Voice Panel (OVP) and the OuterLink Voice and Video Recorder (OVVR) to connect to external devices such as the vehicle’s Inter-Communications System (ICS). These stub connections are not approved as part of this STC. Information on the potential connections is contained in drawing N008-0080 (see Flag Note 11 of N008-0080).

6. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.

------------------------------------------------------------END-------------------------------------------------------

## Every issue (3)

- March 29, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/4f/9f/4f9f8aeac8a943bbd7e1cec59e3bd5b89adf268ffc6e123f601077823afc4452)
- August 5, 2011: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b4/3c/b43c09539469ef451336eea8e729f960ec38602124ebeb77f2cfb4f8c0e2dd29)
- August 18, 2004: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/fd/c1/fdc1c8e3f7daf39c8bc7ca0cb786f413424b7654d5fd988291ee404259eb5ea0)

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