# STC SE01291LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Global United Capital LLC, United States
- Description: Installation of a Really Quiet LLC Internal Mixer Part Number RQ720100T, Revision B, dated January 25, 2000, or later FAA approved revisions, in accordance with Installation Instructions RQ73-3000-401/-402, Revision C, dated January 9, 2002, or later FAA approved revisions.  This installation must be done concurrently with STC No. ST01292LA which modifies the airplane engine installation.
- Applied: June 20, 1998
- Status date: March 15, 2004
- Product: Engine
- Certification basis: Part 13, Part 21
- Data sheets: [TCDS E2EU](https://openairdocs.org/tcds/E2EU)
- Certificate PDF: https://openairdocs.org/files/sha256/8d/8b/8d8b344d3c7567dd708a966e38bc41ebc07518ba4bfae7c61d262a95c33170e7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BA13D554ACFA282E86256E980062A108.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SE01291LA

## ADs that name it (0)

None.

## Approved models (1)

- Rolls-Royce Corporation Spey 511-8 ([TCDS E2EU](https://openairdocs.org/tcds/E2EU))

## 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 SE01291LA RE-ISSUED ON MARCH 15, 2004 TO SUPERSEDE THE ORIGINAL STC WHICH HAS BEEN LOST OR MISPLACED.

This certificate issued to: Global United Capital, LLC 527 Third Avenue, Suite 145 New York, NY 10016

Part 13* of the Civil Aviation Regulations. *Certification basis is set forth in Type Certificate Data Sheet E2EU.

Original Product - Type Certificate Number: E2EU Make: Rolls-Roy ce Model: Spey 511-8 Description of Type Design Change:

Installation of a Really Quiet LLC Internal Mixer Part Number RQ720100T, Revision B, dated January 25, 2000, or later FAA approved revisions, in accordance with Installation Instructions RQ73-3000-401/-402, Revision C, dated January 9, 2002, or later FAA approved revisions. This installation must be done concurrently with STC No.

ST01292LA which modifies the airplane engine installation.

Approval of this change in type design applies to the above engine model(s) only. This approval should not be extended to an engine model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of that engine. The instructions for continued airworthiness are included in STC ST01292LA limitations and conditions. A copy of this STC must be included in the permanent records of the modified engine. 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 20, 1998 Date of issuance: January 25, 2002 Date reissued: May 7, 2003; May 20, 2003;

March 15, 2004 Date amended:

Original signed by Eual M. Conditt, Jr.

(Signature) Eual M. Conditt, Jr.

Associate ACO Manager, Airframe, Propulsion & Services Wichita Aircraft Certification Office (Title)

## Every issue (1)

- March 15, 2004: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/8d/8b/8d8b344d3c7567dd708a966e38bc41ebc07518ba4bfae7c61d262a95c33170e7)

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