# STC ST11107SC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Associated Air Center, Inc. - c/o CT Corporation System
- Description: Installation of a Controller - Pilot Link Communication System
- Status date: December 11, 2017
- Data sheets: A16WE
- Certificate PDF: https://openairdocs.org/files/sha256/d4/38/d43801b1ef944828968caa980607616231b76713f658a694b973ec11d995afa5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163633978920230414140814.0001
- Page: https://openairdocs.org/stc/ST11107SC

## ADs that name it

None.

## Approved models (1)

- The Boeing Company 737-300 Series (TCDS A16WE)

## 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.

FAA Form 8110-2 (8/13) Page 1

Part of the Federal A viation Regulations.

Original Product – Type Certificate Number: MDNH:

MRGHO:

Signature

Title

ST11107SC Associated Air Center, Inc. - c/o CT Corporation System 1999 Bryan Street, Suite 900 Dallas, TX 75201 25 A16WE Boeing 737-300 Installation of a Controller - Pilot Link Communication System in accordance with Associated Air Center (AAC) "Master Document List" Document Number 3242000000, Revision IR, dated December 30, 2014, or later FAA/ODA approved revision. Airplane Flight Manual Supplement (AFMS), Document Number 3242021090, Revision IR, dated December 30, 2014, or later FAA/ODA approved revision is required.

Descriptive data about this design change cannot be used to duplicate other products. This approval is limited to only the installation made in Boeing 737-300, S/N 24095. This STC does not permit manufacturing of parts for multiple installations.

7/25/2014 12/30/2014 12/11/2017 Jose Mora-Vargas ODA Administrator ODA-710437-SW

FAA Form 8110-2 (8/13) Page 2

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

ST11107SC

FAA Form 8110-2 (8/13) Page 3

ST11107SC Limitations and Conditions (Continued):

Airworthiness limitation inspections per 14 CFR Part 25, Appendix H are contained in Chapter 3 of AAC Document Number 3242050090, Revision IR, dated November 14, 2014, titled "Instructions for Continued Airworthiness" or later FAA/ODA approved revision.

Certification Basis: The same as that identified on Type Certificate Data Sheet A16WE, except for the election of later amendments as listed:

DT and fatigue eval of structure: 25.571 (a)(b) Amdt. 25-86 Fasteners: 25.607 Amdt. 25-23 Cockpit controls: 25.777 (a)(b)(c) Amdt. 25-46 Fire protection systems: 25.869 (a)(4) Amdt. 25-72 Fuel tank ignition prevention: 25.981 (a)(3)(b) Amdt. 25-102 System lightning protection: 25.1316 (b)(c)(6) Amdt. 25-80 Warning, caution, and advisory lights: 25.1322 Amdt. 25-131 Instrument lights: 25.1381 Amdt. 25-72 Cockpit voice recorders: 25.1457 Amdt. 25-124

END

## Every issue (1)

- December 11, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d4/38/d43801b1ef944828968caa980607616231b76713f658a694b973ec11d995afa5)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.