# STC SA01782SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Reliable Equipment & Engineering Inc., United States - Description: Replace existing incandescent wing leading edge landing and taxi lights with XeVision High Intensity Discharge (HID) lights. - Applied: March 3, 2006 - Status date: April 15, 2008 - Product: Aircraft, Single-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A47CE](https://openairdocs.org/tcds/A47CE) - Certificate PDF: https://openairdocs.org/files/sha256/77/84/778488bf17b1e3549e9272679dd32a42ffc573046fdb5c0af15c28e00d41ec56 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B2511A03EF2A1A8286257449004DA44F.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA01782SE ## ADs that name it (0) None. ## Approved models (1) - Diamond Aircraft Industries GmbH DA 40 ([TCDS A47CE](https://openairdocs.org/tcds/A47CE)) ## 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. United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SA01782SE This certificate, issued to: Reliable Equipment & Engineering, Inc. 4245 Airport Road Ogden, UT 84405 Part 23 of the Code of Federal Regulations. Original Product ⎯Type Certificate Number: A47CE Make: Diamond Aircraft Industries GmbH Model: DA 40 Description of the Type Design Change: Replace existing incandescent wing leading edge landing and taxi lights with XeVision High Intensity Discharge (HID) lights. Installation in accordance with FAA-approved Master Drawing List FastCap, LLC document FC-MDL, Revision B, dated August 22, 2007, or later FAA-approved revision. This modification must be inspected and maintained in accordance with the FAA-approved Instructions for Continued Airworthiness (ICA), FastCap, LLC document FC102, Revision IR, dated August 16, 2007, or later FAA-approved revision. Limitations and Conditions: Approval of this change in type design applies to only the Diamond DA 40 model aircraft. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer 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. Aircraft modified in accordance with this STC must be operated in accordance with a copy of the FAA-approved FastCap, LLC Airplane Flight Manual Supplement , Document FC112, Revision IR, dated August 23, 2007, or later FAA-approved revision. A copy of this certificate, FAA-approved AFMS and ICA must be maintained as part of the permanent records of 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 3, 2006 Date reissued: April 15, 2008 Date of issuance: August 24, 2007 Date amended: April 15, 2008 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (1) - April 15, 2008: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/77/84/778488bf17b1e3549e9272679dd32a42ffc573046fdb5c0af15c28e00d41ec56) --- 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.