# STC SR01067SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Honeywell International Inc, United States
- Description: Installation of the Enhanced Ground Proximity Warning System in accordance with Honeywell, Master Drawing List 960-0524-001, Revision -, dated February 5, 2002, or later Federal Aviation Administration (FAA) approved revisions.
- Applied: December 3, 2001
- Status date: January 4, 2022
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 27
- Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU)
- Certificate PDF: https://openairdocs.org/files/sha256/82/bf/82bf5662464e7ec15e49518d988b0b75153d61c8db7a895702522db316feb02f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181865659720221208165057.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01067SE

## ADs that name it (0)

None.

## Approved models (1)

- Airbus Helicopters AS350BA ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))

## 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:

SR01067SE Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 27 Federal Aviation Regulations H9EU Airbus Helicopters AS350BA series Installation of the Enhanced Ground Proximity Warning System in accordance with Honeywell, Master Drawing List 960-0524-001, Revision -, dated February 5, 2002, or later Federal Aviation Administration (FAA) approved revisions.

This approval of this change in type design applies to the above model of rotorcraft only. This approval should not be extended to other rotorcraft of this model on which other previously approved modifications are incorporated unless it Is determined that the relationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of the aircraft. A copy of this Certificate and FAA approved Rotorcraft Flight Manual Supplement (RFMS) drawings 060-4314-104, Rev. "new", 060-4314-110, Rev. "new", 060-4314-111, Rev. "new", FAA approved March 26, 2002, or later FAA approved revisions must be maintained as part of the permanent records for the modified aircraft. A system self-test as specified in section 4.3 of the RFMS shall be performed at a minimum before the first flight of each flight day.

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.

December 3, 2001 January 4, 2022 March 26, 2002 July 12, 2004 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:

SR01067SE 2

## Every issue (3)

- January 4, 2022: Issued, Current. [certificate](https://openairdocs.org/files/sha256/82/bf/82bf5662464e7ec15e49518d988b0b75153d61c8db7a895702522db316feb02f)
- January 4, 2022: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/f2/ba/f2ba4da3fb3d3802f8c3e91cc7e9ee7f19d8fd9e705ce5b1d1875c511029355a)
- July 12, 2004: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/33/9e/339eca4687dab89cef1661df9bfda059a2dd919f98b702053690a47093b41580)

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