What it approves
Installation of Extended Squitter Mode S Transponders and GPS Position Source
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:
ST09861AC Aircraft Systems and Manufacturing, Inc.
1717 Universal City Blvd.
Universal City, TX 78148 25 Code of Federal Regulations A6WE Boeing ATC Transponder System Upgrade to Support ADS-B Out Equipage (with an option for GPS Position Source Installation) in accordance with Aircraft Systems and Manufacturing, Inc. Master Data List 5711-0000-00 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.
07/16/2014 07/14/2016 08/18/2020 3 Robert H. Wilcox ODA administrator ODA-834704-SW
FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___
ST09861AC 3
FAA Form 8110-2 (4/20) Page ___ of ___
ST09861AC Description of Type Design Change (cont'd):
AFMS Document No. 5711-2160-00, Rev IR, December 21, 2016 or later FAA approved revision, or 5711-2160-03, Rev IR dated August 10, 2020 or later FAA approved revision is a required part of this modification. Instructions for Continued Airworthiness Document No. 5711-2170-00, Rev B dated August 26, 2016 or later FAA approved revision, or 5711-2170-03, Rev D dated July 1, 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); 25.561(a,b); 25.601; 25.603(a); 25.605(a);
25.607; 25.609(a); 25.611(a)(b); 25.625(a)(b)(c); 25.899(a)(b); 25.1301(a); 25.1307(c); 25.1309(a)(b)(c)(d)
(e); 25.1310; 25.1316(b); 25.1321(e); 25.1322(b)(d)(e)(1)(f); 25.1351(a); 25.1353(a)(c); 25.1357(a)(c)(e);
25.1431; 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 26.11(c).
Regulations at an intermediate amendment:
14 CFR 25.571(a)(b1-5) Amdt 25-86; 25.613(a)(b)(c) Amdt 25-72; 25.869(a1,4) Amdt 25-72; 25.981(a3) Amdt 25-102.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 5
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| August 18, 2020 | Amended, current | Certificate |
| July 14, 2016 | Issued, earlier issue | Certificate |