# STC ST00018LB-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of the Honeywell Enhanced Ground Proximity Warning
System
- Applied: June 10, 1996
- Status date: January 4, 2022
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 25, Part 121
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM)
- Certificate PDF: https://openairdocs.org/files/sha256/b5/85/b585cb2a25694847bf824a4e079eba81d65676b5a1451ff4c9ab0ffea516664f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110906455920221208134824.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00018LB-D

## ADs that name it (0)

None.

## Approved models (6)

- Airbus A320-211 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus A320-212 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus A320-214 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus A320-231 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus A320-232 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus A320-233 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))

## 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:

ST00018LB-D Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 25 Federal Aviation Regulations A28NM Airbus Industrie A320-200 Series Installation of the Honeywell Enhanced Ground Proximity Warning System per Master Drawing 960-2227-007, Revision New, dated June 27,1997, or later FAA-approved revisions.

Approval of this change in type design applies to the above model aircraft equipped with a flight management computer (FMC), which meets AC 90-45A. U.S.

registered aircraft that operate under FAR part 121 may not incorporate the Honeywell "alternate" glideslope cancel feature and any aircraft imported into the U.S with the intent to operate under FAR part 121 must remove this feature prior to operation. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship 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 the FAA Approved Airplane Flight Manual Supplement (AFMS) must be maintained as part of the permanent records for the modified aircraft. A system self test as specified in Document No. 060-4167-004, production ground test procedures, shall be performed at intervals not to exceed 6,000 flight hours or 15 months, which ever comes first.

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.

June 10, 1996 March 21, 1997; January 4, 2022 June 21, 1996 October 9, 1996; January 29, 1998; November 9, 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:

ST00018LB-D 2

## Every issue (3)

- January 4, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/b5/85/b585cb2a25694847bf824a4e079eba81d65676b5a1451ff4c9ab0ffea516664f)
- January 4, 2022: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/17/b1/17b18000ae80c7a5add35b7758cc2ec25d4235476418e5a6d5da8618d285f551)
- November 9, 2000: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/af/18/af18e7075b56b3ab823ca27c35843c8d9845622b2dbd51b64734807c15c0b92e)

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