STC ST11107SC

Supplemental type certificate · Associated Air Center, Inc. - c/o CT Corporation System

Holder
Associated Air Center, Inc. - c/o CT Corporation System · USA
Status
Current · Reissued
Status date
December 11, 2017
Applied
July 25, 2014
Product
Aircraft · Large Airplane
Certification basis
Part 25
Data sheet
TCDSA16WE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of a Controller - Pilot Link Communication System

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may 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

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
The Boeing Company737-300 SeriesA16WE