STC ST09596SC

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:

ST09596SC Aircraft Systems and Manufacturing, Inc.

1717 Universal City Blvd.

Universal City, TX 78148 25 Code of Federal Regulations A2NM Boeing 757-200 Series Installation of a Digital Flight Data Recording System with Expanded Parameter Upgrade using a Teledyne ARINC 717 Digital Flight Data Acquisition Unit in accordance with ASM Master Data List 5528-0000-00 Rev IR dated January 22, 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 4.

April 26, 1999 November 15, 1999 June 24, 2011 January 22, 2021 Robert H. Wilcox ODA administrator ODA-834704-SW 4

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:

ST09596SC 4

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:

ST09596SC

Limitations and Conditions (cont'd):

Instructions for Continued Airworthiness (ICA) document no. 5528-2170-00, Rev B dated March 16, 2009 or later FAA approved revision, or 5528-2170-01 Rev B dated November 30, 2020 or later FAA approved revision, must be made available to the operator at the time of installation.

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 757-200 series aircraft is as follows:

The type certification basis for the airplane for parts not changed is shown on TCDS A2NM, Revision 32, dated February 16, 2016.

The certification basis for parts changed or affected by this change since the reference date of this application, 14-August-2020, is based upon Part 25 as amended through Amendment 25-146 and Part 26 as amended through Amendment 26-6.

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; 305 (a)(b); 307 (a); 25.561 (a)(b)(c); 25.601;

25.603; 25.605 (a); 25.607; 25.611 (a)(b); 25.613(a)(b)(c); 25.789 (a); 25.899 (a)(b1);

25.1301 (a); 25.1309 (a)(b)(c)(d)(e); 25.1310; 25.1316 (b); 25.1351 (a); 25.1353 (a)(c);

25.1355 (a)(c); 25.1357 (a)(c)(e); 25.1431; 25.1529; 25.1541.

See continuation Page 4 of 4.

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:

ST09596SC

Limitations and Conditions (cont'd):

Regulations at the latest amendment 26-0 through 26-6 14 CFR § 26.11 (c).

*Regulations at an intermediate amendment:

14 CFR § 25.981(a3) Amdt 25-102; 25.1459 Amdt 65.

END 4 4