STC SA01782SE

Supplemental type certificate · Reliable Equipment & Engineering Inc.

Holder
Reliable Equipment & Engineering Inc. · United States
Status
Current · Reissued
Status date
April 15, 2008
Applied
March 3, 2006
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23
Data sheet
TCDSA47CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Replace existing incandescent wing leading edge landing and taxi lights with XeVision High Intensity Discharge (HID) lights.

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.

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)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
Diamond Aircraft Industries GmbHDA 40A47CE