# STC ST04413AT

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Quiet Technology Aerospace
- Description: Replacement of the inner aluminum barrel of the engine inlet cowl, with an inlet barrel of carbon graphite sandwich construction, to provide a solution for in-service corrosion
- Status date: November 27, 2017
- Data sheets: A50NM
- Certificate PDF: https://openairdocs.org/files/sha256/92/5b/925bf91ad97ef5641d089f92a4a6a3155e2b13f47b862804c2965eff316abff5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D5D0D6BC1F62F30A862581E7004E8F0C.0001
- Page: https://openairdocs.org/stc/ST04413AT

## ADs that name it

None.

## Approved models (1)

- Dassault Aviation FALCON 2000EX (TCDS A50NM)

## 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 Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.

FAA Form 8110-2 (5/14) Page 1 of 2

Number: ST04413AT

This certificate issued to: Quiet Technology Aerospace 4100 N 29th Terrace Hollywood, FL 33020

Part 25 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A50NM Make: Dassault AViation Model: Falcon 2000EX

Description of Type Design Change: Replacement of the inner aluminum barrel of the engine inlet cowl, with an inlet barrel of carbon graphite sandwich construction, to provide a solution for in-service corrosion, in accordance with QTA Nose Cowl Assy - Falcon F2000, Drawing F20-NC-2000, Rev. NC, dated September 29, 2017; Assemble Procedure, Report # QTA-2005, Rev. IR, dated August 16, 2017; Instructions for Continued Airworthiness, Report # QTA-2006, Rev. IR. dated September 31, 2017; and Structural Repair Manual, Report # QTA-2007, Rev. IR, dated October 02, 2017, or later FAA approved revisions. This modification has been determined by the FAA to be a no acoustic change per 14 CFR §21.93(b).

1) Compatibility of this design change with previously approved modifications must be determined by the installer.

2) A copy of this certificate must be maintained as part of the permanent records for the modified aircraft.

3) 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: April 14, 2016 Date Reissued:

Date of Issuance: November 27, 2017 Date Amended:

Signature Title (for) Christina M. Underwood Manager, Atlanta ACO Branch

FAA Form 8110-2 (5/14) Page 2 of 2

Transfer the ownership of Supplemental Type Certificate Number: ST04413AT

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (1)

- November 27, 2017: Issued, Current. [certificate](https://openairdocs.org/files/sha256/92/5b/925bf91ad97ef5641d089f92a4a6a3155e2b13f47b862804c2965eff316abff5)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.