What it approves
Installation of an ANR Headset 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 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:
ST11385DS Aircraft Systems and Manufacturing, Inc.
1717 Universal City Boulevard Universal City, Texas 78148 Part 25 Title14 of the Code of Federal Regulations A16WE Boeing 737-600/-700/-700C/-800/-900/-900ER Installation of an ANR Headset System in accordance with JANA Engineering Master Data List, Doc. No.
5773-0000-00, Rev IR, dated August 16, 2023, or later approved revision. The FAA Approved Airplane Flight Manual Supplement, Doc. No. 5773-2160-00, Rev IR, dated August 16, 2023, or later approved revision, must be attached to the Airplane Flight Manual when this STC is incorporated.
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 on Page 3 of 3.
November 18, 2022 August 16, 2023 Robert H. Wilcox ODA Administrator, ODA-834704-SW 3
FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:
ST11385DS 3
FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:
ST11385DS Limitations and Conditions continued:
In addition to the basic aircraft maintenance manuals, the aircraft must be maintained in accordance with the Instructions for Continued Airworthiness (ICA) Document No. 5773-2170-00, Rev A, dated August 4, 2023, or later FAA accepted revision. Airworthiness Limitations inspections per 14 CFR Part 25, Appendix H are contained in Chapter 7 of the ICA.
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.
Certification Basis:
The type certification basis for the airplanes is shown in TCDS A16WE, Revision 73, dated March 15, 2023 for parts not changed or not affected by this change.
The certification basis for parts changed or affected by this change is based upon Part 25 as amended through Amendment 25‐146 and Part 26 as amended through Amendment 26‐7.
Regulations at the latest amendment 25‐0 through 25-146 used for this modification:
14 CFR § 25.29(b), 25.301(a)(b), 25.303, 25.305(a,b), 25.307(a), 25.561(a,b3,c), 25.601, 25.603, 25.605
(a), 25.607, 25.609, 25.611(a), 25.613(a,b,c), 25.771(a,e), 25.777(a), 25.789, 25.853(a), 25.899(a,b1),
25.1301(a), 25.1307(c), 25.1309(a,b,c,d), 25.1310, 25.1322(a,e), 25.1351(a), 25.1353(a), 25.1355(a,c),
25.1357(a,c,e), 25.1360, 25.1431(a,b,c,d), 25.1529, 25.1541, 25.1581(a,b,d), 25.1583(e,c1), 25.1585(a)
Regulations at an intermediate amendment:
25.869(a1,4), Amdt. 25-113
Regulations at the latest amendment 26‐0 through 26-7:
26.11(c), Amdt. 26-7
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ADs that name this STC · 0
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