# STC ST09580SC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aircraft Systems and Manufacturing Inc
- Description: Installation of Digital Flight Data Recorder (DFDR) Expanded Paramater Upgrade.
- Status date: May 6, 2021
- Data sheets: A1NM, A1NM, A1NM
- Certificate PDF: https://openairdocs.org/files/sha256/fb/ab/fbaba40b97cc53b414642b02ade036cc42840cdff88f95d47273ea4986966c08
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/718D2C7A8A4F7AB386258712004B61BA.0001
- Page: https://openairdocs.org/stc/ST09580SC

## ADs that name it

None.

## Approved models (3)

- The Boeing Company 767-200 Series (TCDS A1NM)
- The Boeing Company 767-300 Series (TCDS A1NM)
- The Boeing Company 767-400ER Series (TCDS A1NM)

## 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.

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:

ST09580SC Aircraft Systems and Manufacturing, Inc.

1717 Universal City Blvd.

Universal City, TX 78148 25 Code of Federal Regulations A1NM Boeing 767-200/-300/-400ER Installation of a Digital Flight Data Recording (DFDR) System with Expanded Parameter Upgrade using a Teledyne ARINC 717 Digital Flight Data Acquisition Unit (DFDAU) in accordance with the Aircraft Systems and Manufacturing, Inc. Master Data List 5532-0000-00, Revision IR, dated May xx, 2021, or later ODA approved revision.

Compatibility of this design change with previously approved modifications must be determined by the installer. 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. See continuation Page 3 of 3.

April 26, 1999 May 06, 2021 November 8, 1999 June 14, 2003 March 3, 2019 3 Charles E. Williams ODA administrator ODA-834704-SW

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:

ST09580SC 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:

ST09580SC Limitations and Conditions (cont'd):

Instructions for Continued Airworthiness Document No. 5532-2170-00, Revision E, dated January 12, 2021, or 5532-2170-05, Revision IR, dated February 11, 2018, or later FAA accepted revisions, must be made available to the operator at the time of installation.

Airworthiness Limitations inspections per 14 CFR Part 25, Appendix H are contained in Chapter 7 of the Instructions for Continued Airworthiness.

Note: 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:

Based on 14 CFR Sections 21.115 and 21.101, and FAA policy for significant changes in FAA Order 8110.48, the certification basis for the 767-200/-300/-400ER series is follows:

a. The type certification basis for Boeing Model 767 series airplanes is shown on TCDS A1NM 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 this application is based upon Part 25 as amended by Amendment 25-125 and 14 CFR Part 26

Regulations at the amendment level in TCDS A1NM 14 CFR § 25.29 (b); 25.1301 (a)(b)(c)(d); 25.1309 (a)(b)(c)(d); 25.1351 (a); 25.1353 (a);

25.1431(a)(b)(c); 25.1529; 25.1541(a1)(b).

4 CFR Part 26 regulations Based on 14 CFR § 21.101(g), applicable provisions of 14 CFR part 26 are included in the certification basis. For any future 14 CFR part 26 amendments, the holder of the STC must demonstrate compliance with the applicable sections. As of the issuance date of this STC, compliance has been found for the following regulations 14 CFR § 26.11 - amendment 26-0.

**END 3 3**

## Every issue (2)

- May 6, 2021: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/fb/ab/fbaba40b97cc53b414642b02ade036cc42840cdff88f95d47273ea4986966c08)
- March 5, 2019: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/69/54/695412f210ca5478ca7e7cf6c4905ead2387677d559d49168163fd55624e5b5b)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.
