What it approves
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.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may 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 ProductType 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)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 3
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| March 7, 2012 | Reissued, current | Certificate |
| January 21, 2010 | Reissued, current | CertificateST00065SE |