# STC SA2741SO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of CAS-81 TCAS II system and compatible Mode S transponders.
- Applied: March 29, 1990
- Status date: January 19, 2022
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 25
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE)
- Certificate PDF: https://openairdocs.org/files/sha256/29/7e/297e48c8de56aec8e6c5e093bc85ba5beeef53e01b856ff4adedf6c738305e09
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126183016620221130125511.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2741SO

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company 737-400 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))

## 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:

SA2741SO Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 25 the Federal Aviation Regulations A16WE Boeing 737-400 Series Installation of a CAS-81 TCAS II system and compatible Mode "S" transponders in accordance with Page Avjet Master Drawing List MDL-90-09, Revision A, dated April 9, 1990 and Bendix/King Drawing No. 699-62501, Inital Release, dated October 14, 1991; or AlliedSignal Master Drawing List No. 699-50012, Revision H, dated October 8, 1999; or later FAA approved revision.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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. FAA approved Airplane Flight Manual Supplement No. 699-56004, Revision C, dated October 19, 1999, or later FAA approved revision, is a required part of this STC.

March 29, 1990 February 24, 2000; January 19, 2022 April 17, 1990 December 26, 1991; February 24, 2000 For Acting Manager, Seattle ACO Branch 2

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:

SA2741SO 2

## Every issue (2)

- January 19, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/29/7e/297e48c8de56aec8e6c5e093bc85ba5beeef53e01b856ff4adedf6c738305e09)
- January 19, 2022: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/da/d2/dad2ef9602f243f9a17ddec48ec728d268fdf3d48f61f3d085c2163b29f25d71)

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