# STC ST00324SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Rockwell Collins Aerospace & Electronics Inc.
Flight Dynmics Division, United States
- Description: Installation of HUD Guidance System (HGS), Model 2700. (DO 328-100 MOD 10CONFIGURATION)
- Applied: September 26, 1991
- Status date: March 7, 2012
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A45NM](https://openairdocs.org/tcds/A45NM)
- Certificate PDF: https://openairdocs.org/files/sha256/a2/99/a2996d24d488d921f7a30bb7492a6fc21de3123b44167fa1081ca1e758d6402d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/689EFA56311D9FB1862579C2007AA7FB.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/ST00324SE

## ADs that name it (0)

None.

## Approved models (1)

- Dornier-Werke G.m.b.H. Do 328-100 ([TCDS A45NM](https://openairdocs.org/tcds/A45NM))

## 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.

Number ST00324SE

This certificate, issued to Rockwell Collins, Inc.

27300 SW Parkway Ave Wilsonville, OR 97070

Part 25 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A45NM Make: Dornier Model: DO-328-100MOD.10 configuration

Description of the Type Design Change: Installation of Head-Up Display (HUD) Guidance System (HGS) Model 2700 in accordance with Flight Dynamics Master Drawing List 9701-0964, Revision D, dated January 9, 1996, or later Federal Aviation Administration (FAA) approved revisions.

Limitations and Conditions: Approval of this change in type design applies to above model aircraft only. This change has only been demonstrated to be acceptable for use in operations associated with Category I and II Landing Minima as defined in FAA Advisory Circular 120-29. 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 relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft. This installation is limited to aircraft where autopilot does not have Category II option as specified in Appendix 004 of the Airplane Flight Manual (AFM).

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.

Date of application: September 26, 1991 Date reissued: 5/2/96; 4/16/03; 7/ 8/04; 1/21/10; 3/7/12 Date of issuance: February 29, 1996 Date amended: 4/16/03; 7/8/04

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (3)

- March 7, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a2/99/a2996d24d488d921f7a30bb7492a6fc21de3123b44167fa1081ca1e758d6402d)
- January 21, 2010: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/fb/e8/fbe87f828fc7ceb01535d1a299ffd40c96a1cdfdd41186997312f2360cce6097)
- July 8, 2004: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/2c/2d/2c2d88d0600976a65567be94a58c0402f5d7ad1e9e0d14185f6fd128f61b199c)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.