# STC ST10819SC

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Aircraft Systems & Mfg, United States
- Description: Installation of a Teledyne Controls Airborne Wireless LAN Unit (AWLU) and an Enhanced Airborne Data Loader (eADL).
- Applied: January 24, 2007
- Status date: May 5, 2010
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25, Part 26
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE)
- Certificate PDF: https://openairdocs.org/files/sha256/47/47/4747eff739b3d8a4a3993526e10a6707b5380c7a36d345051a467a49351543db
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E889FF886BF11B038625775A004CB4EC.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST10819SC

## ADs that name it (0)

None.

## Approved models (4)

- The Boeing Company 737-300 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-800 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-900 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-900ER Series ([TCDS A16WE](https://openairdocs.org/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.

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Project No. SA9196SC-T KSC/TP

Part 25 of the Federal Aviation Regulations.

Description of Type Design Change: Installation of a Teledyne Controls Airborne Wireless LAN Unit (AWLU) and an Enhanced Airborne Data Loader (eADL) in accordance with Aircraft Systems and Manufacturing Top Drawing List No. 5683-0001-00, Rev Q, dated April 27, 2010, or later FAA approved revisions.

Limitations and Conditions: This STC is approved for ON GROUND USE ONLY and is not approved for use in flight. The installer must determine whether this design change is compatible with previously approved modifications. 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.

Aircraft Systems & Manufacturing 302 Toledo Trail Georgetown, TX 78628 A16WE Make : Boeing Model : 737-700 Series; 737-800 Series; 737-900 Series;

737-900ER Date of application : January 24, 2007

Date of issuance : March 04, 2008

Date amended : May 5, 2010

( Signature) S. Frances Cox Manager, Special Certification Office Southwest Region

( Title)

FAA Form 8110-2-1(10-69) Page 2 of 3

FAA Form 8110-2-1(10-69) Page 3 of 3

Number ST10819SC Date of Issuance: March 04, 2008 Date Amended: May 5, 2010

This modification may not be installed after August 30, 2010 unless (1) previously approved electrical wiring interconnection system (EWIS) instructions for continued airworthiness (ICA) have been evaluated and determined to be adequate for this installation by the FAA, or (2) revised EWIS ICA have been approved by the FAA Oversite Office.

(Refer to 14 CFR 26.11)

Certification Basis: Based on 14 CFR §§ 21.115 and 21.101(b)(1), and FAA Order 8110.48, the certification basis for Boeing 737-700 Series, 737-800 Series, 737-900 Series, and 737-900ER modified by the installation of a Teledyne Controls Airborne Wireless LAN Unit (AWLU) and an Enhanced Airborne Data Loader (eADL) is as follows:

a. The type certification basis for Boeing 737- 700 Series, 737-800 Series, 737-900 Series, and 737-900ER airplanes is shown on TCDS A16WE Revision 44 for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of applications, December 11, 2009, is based upon part 25 as amended by Amendment 25-123.

Based on 14 CFR § 21.115 and 21.101(b)(1), and FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 25-0 through 25-123 14 CFR § 25.1, 25.2, 25.301, 25.303, 25.305, 25.307, 25.561 (a)(b)(c)(d), 25.571(a), 25.581, 25.603 (a), 25.605

(a), 25.607, 25.613, 25.625, 25.789, 25.1301 (a), 25.1307 (c), 25.1309 (b)(d)(e)(1), 25.1316, 25.1321 (a)(d)(e),

25.1322 (a)(b)(d), 25.1351 (a), 25.1353 (a), 25.1357 (a)(b )(e), 25.1431 (a)(b)(c), 25.1525, 25.1529, 25.1541 (b),

25.1581, 25.1583, 26.11, 26.47, and 26.49.

Regulations at an intermediate amendment 14 CFR § 25.869 (a)(1) Amendment 25-113 14 CFR § 25.981 (a)(1)(2)(3) Amendment 25-102 14 CFR § 25.1585 Amendment 25-0

-End-

## Every issue (1)

- May 5, 2010: Amended, Current. [certificate](https://openairdocs.org/files/sha256/47/47/4747eff739b3d8a4a3993526e10a6707b5380c7a36d345051a467a49351543db)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
