# STC ST00065SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Rockwell Collins Aerospace & Electronics Inc. Flight Dynmics Division, United States - Description: Installation of Head Up Display (HUD) Guidance System (HGS), Model 2800, in accordance with Flight Dynamics Installation Drawing List 9701-0868, Revision T, dated March 29, 2000, or later Federal Aviation Administration approved revision. - Applied: March 26, 1993 - Status date: March 7, 2012 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM) - Certificate PDF: https://openairdocs.org/files/sha256/7e/55/7e55caa8dc3059c02b7bb9831994d1b4cab1b4519593fb2b63fe455372b93e08 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D92274CBE863E6ED862579C2007AA940.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST00065SE ## ADs that name it (0) None. ## Approved models (3) - Bombardier-Rotax GmbH DHC-8-100 Series ([TCDS A13NM](https://openairdocs.org/tcds/A13NM)) - Bombardier-Rotax GmbH DHC-8-200 Series ([TCDS A13NM](https://openairdocs.org/tcds/A13NM)) - Bombardier-Rotax GmbH DHC-8-300 Series ([TCDS A13NM](https://openairdocs.org/tcds/A13NM)) ## 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 ST00065SE 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: A13NM Make: deHavilland Model: DH-8-100/-200/-300 Description of the Type Design Change: Installation of Head Up Display (HUD) Guidance System (HGS), Model 2800, in accordance with Flight Dynamics Installation Drawing List 9701-0868, Revision T, dated March 29, 2000, or later Federal Aviation Administration approved revision. Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. 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. The HGS circuit breakers must be collared and the wires connected to these circuit breakers must be capped and stowed. Line Replaceable Units (LRU) for the Overhead Unit, HGS Control Panel, HGS Computer Remote Airspeed Select Unit, Drive Electronics Unit, Combiner, Annunciator Panel, Radio Altitude Power Supply (if required by configuration), Air Data Adapter Unit (if required by configuration), Inertial Reference Unit and its Mode Select Unit must be removed from the aircraft as part of this Supplemental Type Certificate (STC). An Electromagnetic Interference and CAT II Functional Test must be performed after removal of the above LRUs for any systems which were affected by installation of this HGS “partial provisions only” STC. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft. 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: March 26, 1993 Date reissued: 4/16/03; 1/21/10; 3/7/12 Date of issuance: March 11, 1994 Date amended: 3/27/97; 4/10/00; 4/16/03 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (2) - March 7, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/7e/55/7e55caa8dc3059c02b7bb9831994d1b4cab1b4519593fb2b63fe455372b93e08) - January 21, 2010: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a6/76/a6768914fd49e4abb04b0f3b235968113683692ece9222305c114a501627972a), [ST00065SE.pdf](https://openairdocs.org/files/sha256/90/b6/90b6ba4ddad345b3b5bc86b31c9d137e63c3dde405058e9be29bab105ef635d0) --- 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.