STC ST11379DS

Supplemental type certificate · Aircraft Systems and Manufacturing Inc

Holder
Aircraft Systems and Manufacturing Inc · United States
Status
Current · Issued
Status date
August 18, 2020
Applied
December 13, 2018
Product
Aircraft · Large Airplane
Certification basis
Part 21, Part 25, Part 26
Data sheet
TCDSA6WE

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

What it approves

Installation of Flight Deck Universal Serial Bus (USB) Power Ports

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 (4/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___

Part of the .

Model: DC-9-81(MD-81), DC-9-82(MD-82), DC-9-83(MD-83), DC-9-87(MD-87), MD-88 Description of Type Design Change:

ST11379DS Aircraft Systems and Manufacturing, Inc.

1717 Universal City Blvd.

Universal City, TX 78148 25 Code of Federal Regulations A6WE Boeing Installation of Flight Deck Universal Serial Bus (USB) Power Ports in accordance with Aircraft Systems and Manufacturing, Inc. Master Data List 5743-0000-00 Rev IR dated August 18, 2020 or later ODA approved revision.

See continuation Page 3 of 3.

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 must give the other person written evidence of that permission.

See continuation Page 3 of 3.

12/13/2018 08/18/2020 3 Robert H. Wilcox ODA administrator ODA-834704-SW

FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___

ST11379DS 3

FAA Form 8110-2 (4/20) Page ___ of ___

ST11379DS Description of Type Design Change (cont'd):

AFMS Document No. 5743-2160-00, Rev IR dated August 11, 2020, or later FAA approved revision, is a required part of this modification. Instructions for Continued Airworthiness Document No. 5743-2170-00, Rev G dated July 6, 2020, or later FAA approved revision is a required part of this modification.

Limitations and Conditions (cont'd):

The FAA has reviewed the applicant's assessment showing that this modification does not impact the existing electrical wiring interconnection system instructions for continued airworthiness (EWIS ICA) and found that no additional EWIS ICA tasks are required.

The type certification basis for the airplanes is shown on TCDS A6WE, Revision 30, dated March 25, 2014, for parts not changed or not affected by this change is 14 CFR Part 25 Amendments 25-1 through 25-40, including 14 CFR § 25.1309 (Amdt. No. 25-41), § 25.1351 (Amdt. No. 25-41), and § 26.11 (Amdt. No. 26-0), § 26.33 (Amdt. No 26-3), and § 26.43 and 26.45 (Amdt. No. 26-1).

The certification basis for parts changed or affected by this change is based upon Part 25 as amended through Amendment 25-145.

Regulations at the latest amendment 25-0 through 25-145 14 CFR § 25.29(b); 25.301(a,b); 25.303; 25.305(a,b); 25.307(a); 25.601; 25.603(a); 25.605(a); 25.607; 25.609

(a); 25.611(a)(b); 25.619; 25.625(a)(b)(c); 25.853(a); 25.899; 25.1301(a); 25.1302; 25.1307(c); 25.1309(a)(b)(c)

(d)(e); 25.1310; 25.1316(b); 25.1321(e); 25.1322(b)(d)(e1)(f); 25.1351(a); 25.1353(a); 25.1355(a); 25.1357(a)(c)

(e); 25-1360(a)(b); 25.1431(a)(b)(c)(d); 25.1529; 25.1541; 25.1581(a)(b)(c); 25.1583(e); 25.1585(a).

Regulations at the latest amendment 26-0 through 26-6 14 CFR § 26.1, 26.11(c), 26.47 and 26.49.

Regulations at an intermediate amendment:

14 CFR § 25.571 (a)(b1-5) Amdt 25-86; 25.613 (a)(b)(c), Amdt 25-72;16 Amdt 25-121; 25.869 (a1,4), Amdt 25-72; 25.981 (a3), Amdt 25-102.

END 3 3

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 · 5

MakeModelData sheet
The Boeing CompanyDC-9-81 (MD-81)A6WE
The Boeing CompanyDC-9-82 (MD-82)A6WE
The Boeing CompanyDC-9-83 (MD-83)A6WE
The Boeing CompanyDC-9-87 (MD-87)A6WE
The Boeing CompanyMD-88A6WE